N213TS STATUS REPORT BOMBARDIER with relations - ASO · 4/6/2016 · Eng 2 CF34-3A 350107 10-Feb-2016 12020.4 Hrs 6728 Enc Eng 1 CF34-3A 350101 10-Feb-2016 12137.4 Hrs 6769 Enc Airframe

BOMBARDIERN213TS STATUS REPORT

with relations

General Categories: RVSM,FAR 91,FAA,Standard Cost:

740.5+Man Hrs:

3,315+

Owner:

Operator:

DuPage Aerospace Corporation

DuPage Aerospace Corporation

7859 APUS7859 Hrs15-Dec-2015P-107CGTCP36-100APU 1

6728 Enc12020.4 Hrs10-Feb-2016350107CF34-3AEng 2

6769 Enc12137.4 Hrs10-Feb-2016350101CF34-3AEng 1

6326 Ldg12041.2 Hrs10-Feb-20163013Challenger 601Airframe

Analyst: Jeffrey Ivy [email protected]

RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN

TimeCategoriesDescriptionTask No

▼ 5 - TIME LIMITS/MAINTENANCE CHECKS

Unscheduled Maintenance CheckRE (A/R)05-50-01 Hard/Overweight Landing Checks

Mos

Hrs

Ldg

5 A/F

Unscheduled Maintenance CheckRE (A/R)05-50-02 Extreme Turbulence Or Maneuver Checks

Mos

Hrs

Ldg

5 A/F

Unscheduled Maintenance CheckRE (A/R)05-50-03 Lightning Strike Check

Mos

Hrs

Ldg

5 A/F

Unscheduled Maintenance CheckRE (A/R)05-50-04 Engine Checks

Mos

Hrs

Enc

5 ENG1

Unscheduled Maintenance CheckRE (A/R)05-50-04 Engine Checks

Mos

Hrs

Enc

5 ENG2

Unscheduled Maintenance CheckRE (A/R)05-50-05 Main Wheel Fusible Plug Release

Mos

Hrs

Ldg

5 A/F

Unscheduled Maintenance CheckRE (A/R)05-50-06 APU Enclosure Fire

Mos

Hrs

Ldg

5 A/F

Unscheduled Maintenance CheckRE (A/R)05-50-07 Hydraulic System Overheat

Mos

Hrs

Ldg

5 A/F

[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance

Generated: 6-Apr-2016 1:15 PM1/429

BOMBARDIERChallenger 601 N213TS,SN 3013

N213TS STATUS REPORT (with relations)

Owner/Operator: DuPage Aerospace Corporation DuPage

Aerospace Corporation



Unscheduled Maintenance CheckRE (A/R)05-50-08 Wing Leading Edge Overheat

Mos

Hrs

Ldg

5 A/F

Unscheduled Maintenance CheckRE (A/R)05-50-09 Air Driven Generator In - Flight Deployment - Inspection/Check

Mos

Hrs

Ldg

5 A/F

Unscheduled Maintenance CheckRE (A/R)05-50-10 Hydraulic Pump Shock Mount Contamination

Mos

Hrs

Ldg

5 A/F

Unscheduled Maintenance CheckRE (A/R)05-50-11 Cabin Overpressurization

Mos

Hrs

Ldg

5 A/F

Unscheduled Maintenance CheckRE (A/R)05-50-12 Landing Gear Overspeed Check

Mos

Hrs

Ldg

5 A/F

Unscheduled Maintenance CheckRE (A/R)05-50-13 Wing Flap System Overspeed Check

Mos

Hrs

Ldg

5 A/F

Unscheduled Maintenance CheckRE (A/R)05-50-14 Hydraulic Harrison “H” Fittings

Mos

Hrs

Ldg

5 A/F

Unscheduled Maintenance CheckRE (A/R)05-50-15 Aircraft Tire Limitations

Mos

Hrs

Ldg

5 A/F

Unscheduled Maintenance CheckRE (A/R)05-50-16 CF 34 - Compressor Cleaning

Mos

Hrs

Enc

5 ENG1

Unscheduled Maintenance CheckRE (A/R)05-50-16 CF 34 - Compressor Cleaning

Mos

Hrs

Enc

5 ENG2

Unscheduled Maintenance CheckRE (A/R)05-50-17 Inspection Of Engine Driven Pump (EDP) After Dry Operation Due To Hydraulic Fluid Loss

Mos

Hrs

Enc

5 ENG1









Unscheduled Maintenance CheckRE (A/R)05-50-17 Inspection Of Engine Driven Pump (EDP) After Dry Operation Due To Hydraulic Fluid Loss

Mos

Hrs

Enc

5 ENG2

Unscheduled Maintenance CheckRE (A/R)05-50-18 High Energy Stop/Rejected Takeoff (RTO) Damage

Mos

Hrs

Ldg

5 A/F

Unscheduled Maintenance CheckRE (A/R)05-50-19 Inspection After The Aircraft Is Parked In Strong Winds Or Windgusts

Mos

Hrs

Ldg

5 A/F

Unscheduled Maintenance CheckRE (A/R)05-50-20 Inspection After A Bird Strike

Mos

Hrs

Ldg

5 A/F

Unscheduled Maintenance CheckRE (A/R)05-50-21 Inspection After A Tire Burst

Mos

Hrs

Ldg

5 A/F

MandatoryRE (-)2006-25-16 Corrosion Prevention and Control Program (CPCP)

12-Sep-2008Mos

11,455.7Hrs

5,898Ldg

5 A/FINSPECTEDEff: 19-Jan-2007 Complied

With

MandatoryRE (-)2013-03-08 Periodic Inspections

10-May-2013Mos

11,786Hrs

6,141Ldg

5 A/FREVISED MAINT DOCSEff: 19-Mar-2013 Complied

With

Nextdue Share EarliestDUE:1. T 60 Days | 2. RE -Periodic Inspections - Time Limits/Maintenance Checks (TLMC)...2013-03-08 Paragraph (g)A/F5

Nextdue Share EarliestDUE:1. T 12 Mos, 7800 Ldg (later) | 2. RE -Periodic Inspections - Initial Compliance Times for Inspect...2013-03-08 Paragraph (h)A/F5

MandatoryRE (-)2013-03-08 Paragraph (g) Periodic Inspections - Time Limits/Maintenance Checks (TLMC) Manual Revision

10-May-2013Days

11,786Hrs

6,141Ldg


With

MandatoryRE (-)2013-03-08 Paragraph (h) Periodic Inspections - Initial Compliance Times for Inspections

10-May-2013Mos

11,786Hrs

6,141Ldg


With

OptionalT (A/R)601-0590 Scheduled Maintenance Instructions (MSG-3 Derived) – Qualification

Mos

Hrs

Ldg

5 A/FEff: 17-Dec-2007









FAA, FAAREFAA 14 CFR Part 47 FAA - Aircraft Registration

4.9 Months (+181

Days)01-Sep-2016+63628-Feb-2014Mos

Hrs

Ldg

5 A/FExpiration Date 28-Feb-2017

FAA, FAA ≈20-May-2017REFAA RVSM FAA - RVSM Height Monitoring

-1.6 Year27-Aug-20142427-Aug-2012Mos

612.3 Hrs12,653.51,00011,653.5Hrs

Ldg

5 A/F

REPKG 12 Month 12 Monthly Tasks

6.6 Months (+31

Days)21-Oct-2016-/+11221-Oct-2015Mos

Hrs

Ldg

5 A/F

In PackageDUE: 21-Oct-20161. RE 12 MosScheduled Servicing - Lubricate throttle control inner eleme...12-20-00-309A/F12

In PackageDUE: 21-Oct-20161. RE 12 MosScheduled Servicing - Lubricate air driven generator (ADG)12-20-00-312A/F12

In PackageDUE: 21-Oct-20161. RE 12 MosScheduled Servicing - Lubricate flap actuator12-20-00-313A/F12

In PackageDUE: 21-Oct-20161. RE 12 MosWire Cables - Flight Controls Visual Check (using a borescop...20-40-00-203A/F20

In PackageDUE: 21-Oct-20161. RE 12 MosBattery System - Operational Test (Cycling) of the Thermal C...24-00-00-301A/F24

In PackageDUE: 21-Oct-20161. RE 12 MosADG Auto-Deploy Control Unit Operational Test - ADG Auto-De...24-23-46-210A/F24

In PackageDUE: 21-Oct-20161. RE 12 MosBattery System Functional Test - Main Battery Charger Therm...24-33-00-213A/F24

In PackageDUE: 21-Oct-20161. RE 12 MosAuxiliary Power Unit Firex Container - Check APU Firex Conta...26-21-11-206A/F26

In PackageDUE: 21-Oct-20161. RE 12 MosAuxiliary Power Unit Firex Discharge Line Visual Check26-21-21-205A/F26

In PackageDUE: 21-Oct-20161. RE 12 MosPower Plant Firex Container - Check Power Plant Firex Contai...26-23-11-210A/F26

In PackageDUE: 21-Oct-20161. RE 12 MosPower Plant Firex Container - Check Power Plant Firex Contai...26-23-11-210A/F26

In PackageDUE: 21-Oct-20161. RE 12 MosPortable Fire Extinguisher - Check weight26-25-00-213A/F26

In PackageDUE: 21-Oct-20161. RE 12 MosPortable Fire Extinguisher - Check weight26-25-00-213A/F26

In PackageDUE: 21-Oct-20161. RE 12 MosMain Gear Trailing Arm Check transverse shear bolt32-10-36-204A/F32

In PackageDUE: 21-Oct-20161. RE 12 MosEmergency Lighting Inspect Power Supplies per Check section ...33-50-00-203A/F33

In PackageDUE: 21-Oct-20161. RE 12 MosEmergency Lighting Inspect Power Supplies per Check section ...33-50-00-203A/F33

In PackageDUE: 21-Oct-20161. RE 12 MosPitot Static System and Temperature Sensing System Pitot sta...34-11-00-202A/F34

In PackageDUE: 21-Oct-20161. RE 12 MosStandby Magnetic Compass - Compass Swing34-27-00-206A/F34

In PackageDUE: 21-Oct-20161. RE 12 MosAPU Starting and Ignition (Post SB 601-0099 and A/C 3045 to ...49-40-00-211A/F49

In PackageDUE: 21-Oct-20161. RE 12 MosFloor Structure Under Toilet and Galley (without removal) ca...53-10-11-228A/F53

In PackageDUE: 21-Oct-20161. RE 12 MosAttachment Fittings (Nose Gear Trunnion Assembly) Visual Che...53-40-00-225A/F53

In PackageDUE: 21-Oct-20161. RE 12 MosWing Structure Visual Check of the following areas: (1) Wing...57-00-00-203A/F57

In PackageDUE: 21-Oct-20161. RE 12 MosPlates/Skins (Wing Box Lower Skin BL0.00 to WS148.00) Visual...57-30-00-213A/F57

≈20-Oct-2017REPKG 1200 Eng Hour 1200 Engine Hourly Task

29-Oct-2012Mos

812.3 Hrs (+40)12,949.7-/+401,20011,749.7Hrs

Enc

5 ENG1

In PackageDUE: 12,949.7 Hrs1. RE 1200 HrsEngine - General - Borescope inspection of combustion liner ...72-00-00-210ENG172

In PackageDUE: 12,949.7 Hrs1. RE 1200 HrsEngine - General - Borescope inspection of turbine section, ...72-00-00-211ENG172

In PackageDUE: 12,949.7 Hrs1. RE 1200 HrsEngine - General (Pre G.E. SB (CF34) 72-11) - Borescope insp...72-00-00-212ENG172

In PackageDUE: 12,949.7 Hrs1. RE 1200 HrsEngine - General (Pre SB 75-2) - B-Sump pressure measurement...72-00-00-220ENG172

In PackageDUE: 12,949.7 Hrs1. RE 1200 HrsOil/Fuel Heat Exchanger Assembly - Visual Check, paying part...79-20-26-208ENG179









≈20-Oct-2017REPKG 1200 Eng Hour 1200 Engine Hourly Task

29-Oct-2012Mos

812.3 Hrs (+40)12,832.7-/+401,20011,632.7Hrs

Enc

5 ENG2

In PackageDUE: 12,832.7 Hrs1. RE 1200 HrsEngine - General - Borescope inspection of combustion liner ...72-00-00-210ENG272

In PackageDUE: 12,832.7 Hrs1. RE 1200 HrsEngine - General - Borescope inspection of turbine section, ...72-00-00-211ENG272

In PackageDUE: 12,832.7 Hrs1. RE 1200 HrsEngine - General (Pre G.E. SB (CF34) 72-11) - Borescope insp...72-00-00-212ENG272

In PackageDUE: 12,832.7 Hrs1. RE 1200 HrsEngine - General (Pre SB 75-2) - B-Sump pressure measurement...72-00-00-220ENG272

In PackageDUE: 12,832.7 Hrs1. RE 1200 HrsOil/Fuel Heat Exchanger Assembly - Visual Check, paying part...79-20-26-208ENG279

≈20-Oct-2017REPKG 1200 Hour 1200 Hourly Tasks

29-Oct-2012Mos

812.3 Hrs (+40)12,853.5-/+401,20011,653.5Hrs

Ldg

5 A/F

Also ConsiderDUE: 12,632 Hrs1. RE 600 Hrs600 Hourly TasksPKG 600 HourA/F5

In PackageDUE: 12,853.5 Hrs1. RE 1200 HrsScheduled Servicing - Lubricate wing-fuselage pick-up link12-20-00-311A/F12

In PackageDUE: 12,853.5 Hrs1. RE 1200 HrsOutflow Valves Outflow valve Functional Test (Using Pressure...21-30-11-208A/F21

In PackageDUE: 12,853.5 Hrs1. RE 1200 HrsStatic Dischargers Visual Check - Static Dischargers Functio...23-60-00-201A/F23

In PackageDUE: 12,853.5 Hrs1. RE 1200 HrsMain Landing Gear Bay Overheat Detection System Functional T...26-10-21-203A/F26

In PackageDUE: 12,853.5 Hrs1. RE 1200 HrsAnti-Float Mechanism Operational Test - Anti-Float Mechanis...27-13-11-204A/F27

In PackageDUE: 12,853.5 Hrs1. RE 1200 HrsElevator Control (Pre SB 601-0304) Visual Check of elevator ...27-31-00-214A/F27

In PackageDUE: 12,853.5 Hrs1. RE 1200 HrsPitch Trim Actuator - Lubricate horizontal stabilizer pitch ...27-40-00-238A/F27

In PackageDUE: 12,853.5 Hrs1. RE 1200 HrsMain Systems Functional Test of Reservoir-Mounted Return Lin...29-10-00-204A/F29

In PackageDUE: 12,853.5 Hrs1. RE 1200 HrsCase Drain Filter Check Filter Elements in No. 1, No. 2 and ...29-11-31-208A/F29

In PackageDUE: 12,853.5 Hrs1. RE 1200 HrsPressure Manifold Check Filter Elements in No. 1, No. 2 and ...29-11-36-209A/F29

In PackageDUE: 12,853.5 Hrs1. RE 1200 HrsReturn Manifold Check Filter Elements in No. 1, No. 2 and No...29-11-41-210A/F29

In PackageDUE: 12,853.5 Hrs1. RE 1200 HrsElectrical Anti-Icing Functional Test of Heating Element - F...30-41-00-210A/F30

In PackageDUE: 12,853.5 Hrs1. RE 1200 HrsVaristor Suppressor Nominal varistor voltage test - DC stand...30-41-16-211A/F30

In PackageDUE: 12,853.5 Hrs1. RE 1200 HrsExtension and Retraction Landing gear control unit - check f...32-30-00-208A/F32

In PackageDUE: 12,853.5 Hrs1. RE N/ADownward Opening Door (Pre SB 601-0451) Internally Lubricate...52-12-00-204A/F52

In PackageDUE: 12,853.5 Hrs1. RE 1200 HrsDownward Opening Passenger/Crew Entrance Door Visual Check o...52-12-00-205A/F52

In PackageDUE: 12,853.5 Hrs1. RE 1200 HrsDownward Opening Passenger/Crew Entrance Door Functional Tes...52-12-00-206A/F52

In PackageDUE: 12,853.5 Hrs1. RE 1200 HrsDoor Warning Functional Test - Baggage Door Switches- Funct...52-70-00-211A/F52

In PackageDUE: 12,853.5 Hrs1. RE 1200 HrsFuselage Visual Check of the external skin, paying particula...53-00-00-202A/F53

In PackageDUE: 12,853.5 Hrs1. RE 1200 HrsExhaust Nozzle Assembly Remove exhaust nozzle fairing and ca...78-10-00-211 (Left)A/F78

In PackageDUE: 12,853.5 Hrs1. RE 1200 HrsExhaust Nozzle Assembly Remove exhaust nozzle fairing and ca...78-10-00-211 (Right)A/F78

In PackageDUE: 12,853.5 Hrs1. RE 1200 HrsThrust Reverser Functional Test of auto stow system78-30-00-202 (Left)A/F78

In PackageDUE: 12,853.5 Hrs1. RE 1200 HrsThrust Reverser Functional Test of auto stow system78-30-00-202 (Right)A/F78

In PackageDUE: 12,853.5 Hrs1. RE 1200 HrsThrust Reverser Thrust Reverser Unlocked Light Functional Te...78-30-00-216 (Left)A/F78

In PackageDUE: 12,853.5 Hrs1. RE 1200 HrsThrust Reverser Thrust Reverser Unlocked Light Functional Te...78-30-00-216 (Right)A/F78

In PackageDUE: 12,853.5 Hrs1. RE 1200 HrsMain and Pylon Track Slider Blocks Detailed Inspection of sl...78-30-41-201 (Left)A/F78

In PackageDUE: 12,853.5 Hrs1. RE 1200 HrsMain and Pylon Track Slider Blocks Detailed Inspection of sl...78-30-41-201 (Right)A/F78

In PackageDUE: 12,853.5 Hrs1. RE 1200 HrsAuto-Throttle Retarder Control Functional Test of Auto-Throt...78-30-61-213 (Left)A/F78

In PackageDUE: 12,853.5 Hrs1. RE 1200 HrsAuto-Throttle Retarder Control Functional Test of Auto-Throt...78-30-61-213 (Right)A/F78










10 Months (+29

Days)30-Jan-2017-/+12430-Jan-2015Mos

Hrs

Ldg

5 A/F

Also ConsiderDUE: 21-Oct-20161. RE 12 Mos12 Monthly TasksPKG 12 MonthA/F5

In PackageDUE: 30-Jan-20171. RE 24 MosAir Driven Generator System Operational Test - ADG24-23-00-209A/F24

In PackageDUE: 30-Jan-20171. RE 24 MosHydraulic Power - Hydraulic fluid acidity check29-00-00-301A/F29

In PackageDUE: 30-Jan-20171. RE 24 MosAural Warning System Functional Test of: (1) Overspeed warni...31-51-00-202A/F31

In PackageDUE: 30-Jan-20171. RE 24 MosPitot Static System and Temperature Sensing System Pressure ...34-11-00-203A/F34

In PackageDUE: 30-Jan-20171. RE 24 MosPitot Static System and Temperature Sensing System Altimeter...34-11-00-205A/F34



In PackageDUE: 30-Jan-20171. RE 24 MosATC Transponder System - Functional Test34-54-00-207A/F34

In PackageDUE: 30-Jan-20171. RE 24 MosATC Transponder System - Functional Test34-54-00-207A/F34

In PackageDUE: 30-Jan-20171. RE 24 MosDigital Clocks - Remove and install new batteries34-62-00-303A/F34

In PackageDUE: 30-Jan-20171. RE 24 MosDigital Clocks - Remove and install new batteries34-62-00-303A/F34

In PackageDUE: 30-Jan-20171. RE 24 MosOverwing Emergency Exit Operational Test52-20-00-207A/F52

In PackageDUE: 30-Jan-20171. RE 24 MosOverwing Emergency Exit Betalight brightness check52-20-00-208A/F52

In PackageDUE: 30-Jan-20171. RE 24 MosOverwing Emergency Exit Lubricate the Overwing Emergency Exi...52-20-00-216A/F52

In PackageDUE: 30-Jan-20171. RE 24 MosNacelles/Pylons, External - CPCP CheckC54-00-801A/F54

In PackageDUE: 30-Jan-20171. RE 24 MosHorizontal Stabilizer Visual Check of the following items pa...55-10-00-202A/F55

In PackageDUE: 30-Jan-20171. RE 24 MosHorizontal Stabilizer Visual Check (Upon removal of the inne...55-10-11-206A/F55

In PackageDUE: 30-Jan-20171. RE 24 MosVertical Stabilizer Visual Check of the Canted Top Rib for c...55-30-00-209A/F55

In PackageDUE: 30-Jan-20171. RE 24 MosAttachment Fittings Visual Check of Horizontal Stabilizer Pi...55-50-00-211A/F55

In PackageDUE: 30-Jan-20171. RE 24 MosAttachment Fittings Visual Check of the vertical stabilizer ...55-50-00-212A/F55

In PackageDUE: 30-Jan-20171. RE 24 MosAttachment Fittings Visual Check of Horizontal Stabilizer - ...55-50-00-213A/F55

In PackageDUE: 30-Jan-20171. RE 24 MosWing Lower External Surface, BL0.00 to WS353.00 - CPCP Check...C57-00-802A/F57









≈13-Jul-2017REPKG 2400 Hour 2400 Hourly Tasks

04-May-2004Mos

684 Hrs (+30)12,725.2-/+302,40010,325.2Hrs

Ldg

5 A/F

Also ConsiderDUE: 12,853.5 Hrs1. RE 1200 Hrs1200 Hourly TasksPKG 1200 HourA/F5

In PackageDUE: 12,725.2 Hrs1. RE 2400 HrsCheck Valves Check Valve inspection21-20-11-202A/F21

In PackageDUE: 12,725.2 Hrs1. RE 2400 HrsPressurization Control Cabin Low Pressure Warning System Ope...21-30-00-206A/F21

In PackageDUE: 12,725.2 Hrs1. RE 2400 HrsPressurization Control Operational Test of Manual Pressuriza...21-30-00-207A/F21

In PackageDUE: 12,725.2 Hrs1. RE 2400 HrsIDG Oil-in Filter Assembly Remove, inspect and install new f...24-21-16-204A/F24

In PackageDUE: 12,725.2 Hrs1. RE 2400 HrsIDG Oil-out Filter Assembly Remove, inspect and install new ...24-21-21-205A/F24

In PackageDUE: 12,725.2 Hrs1. RE 2400 HrsRudder Control Rudder Anti-Jam Mechanism Functional Test27-21-00-211A/F27

In PackageDUE: 12,725.2 Hrs1. RE 2400 HrsPitch Control System Pitch Trim Suppressor Unit - Bench Chec...27-30-00-235A/F27

In PackageDUE: 12,859 Hrs1. RE 2400 HrsElevator Control Elevator load limiters test27-31-00-215A/F27

In PackageDUE: 12,725.2 Hrs1. RE 2400 HrsStall Protection System Functional Test27-39-00-221A/F27

In PackageDUE: 12,208.2 Hrs1. RE 2400 HrsFlap Actuator - Outboard flap actuator backlash check27-50-16-224A/F27

In PackageDUE: 12,859 Hrs1. RE 2400 HrsFlap Actuator Torque and Side Play Check27-50-16-237A/F27

In PackageDUE: 13,259.8 Hrs1. RE 2400 HrsFlexible Drive Shaft - Check flexible drive shaft casing / C...27-50-41-301A/F27

In PackageDUE: 12,366.7 Hrs1. RE 2400 HrsSpoiler Control (Pre SB 601-0113) Ground Spoiler/Thrust Reve...27-61-00-233A/F27

In PackageDUE: 12,467.3 Hrs1. RE 2400 HrsFuel Tanks Check Fuel Tanks for Leaks- Visual Check (externa...28-10-11-204A/F28

In PackageDUE: 12,366.7 Hrs1. RE 2400 HrsFirewall Fuel Shutoff Valve Internal leakage check28-21-16-213A/F28

In PackageDUE: 12,859 Hrs1. RE 2400 HrsWing Anti-Icing Check valve condition check30-11-00-201A/F30

In PackageDUE: 12,208.2 Hrs1. RE 2400 HrsExtension and Retraction Priority Valves Functional Test32-30-00-209A/F32

In PackageDUE: 12,725.2 Hrs1. RE 2400 HrsParking Brake Shutoff Valve Functional Test - Parking Brake...32-45-31-224A/F32

In PackageDUE: 12,467.3 Hrs1. RE 2400 HrsWing Structure Visual Check of leading edge external surface57-00-00-202A/F57

In PackageDUE: 12,467.3 Hrs1. RE 2400 HrsPlates/Skins (Upper Wing Box) Visual Check - External57-30-00-212A/F57

In PackageDUE: 12,467.3 Hrs1. RE 2400 HrsAttachment Fittings - Main Gear Side Brace (MLG Actuator Pic...57-40-00-214A/F57

In PackageDUE: 12,467.3 Hrs1. RE 2400 HrsFlaps (Inboard Flap Vane Assembly) Visual Check (Upon remova...57-53-00-224A/F57

In PackageDUE: 13,118 Hrs1. RE 2400 HrsThrust Reverser General Visual Check of the torque box, torq...78-30-00-212A/F78

In PackageDUE: 12,725.2 Hrs1. RE 2400 HrsThrust Reverser Thrust Reverser Warning Circuit Functional T...78-30-00-215A/F78

In PackageDUE: 13,118 Hrs1. RE 2400 HrsBlocker Doors Special Detailed Inspection of Blocker Door Bu...78-30-26-204A/F78

In PackageDUE: 13,118 Hrs1. RE 2400 HrsFlexshafts Special Detailed Inspection of Flexshaft78-30-51-217A/F78

In PackageDUE: 13,118 Hrs1. RE 2400 HrsBallscrew Actuators Inspection Detailed Inspection of Ballsc...78-30-56-214A/F78









≈25-Sep-2016REPKG 300 Eng Hour 300 Engine Hourly Task

10-Feb-2016Mos

300 Hrs (+40)12,437.4-/+4030012,137.4Hrs

6,769Enc

5 ENG1

In PackageDUE: 12,437.4 Hrs1. RE 300 HrsScheduled Servicing - Lubricate variable geometry actuator12-20-00-314ENG112

In PackageDUE: 12,437.4 Hrs1. RE 300 HrsEngine - General - Visual Check of Fan Stator for the follow...72-00-00-201ENG172

In PackageDUE: 12,437.4 Hrs1. RE 300 HrsEngine - General - Carry out a visual check of the following...72-00-00-203ENG172

In PackageDUE: 12,437.4 Hrs1. RE 300 HrsEngine - General - Visual Check of engine external lines, po...72-00-00-206ENG172

In PackageDUE: 12,437.4 Hrs1. RE 300 HrsEngine - General - Visual check of high pressure turbine sec...72-00-00-208ENG172

In PackageDUE: 12,437.4 Hrs1. RE 300 HrsEngine - General - Compressor Waterwash72-00-00-301ENG172

In PackageDUE: 12,437.4 Hrs1. RE 300 HrsEngine - General (Engine model CF34-1A/-3A/-3A2 only) - Powe...72-00-00-302ENG172

In PackageDUE: 12,437.4 Hrs1. RE 300 HrsFuel Heater Assembly - Check for evidence of leakage from fu...73-10-16-208ENG173

In PackageDUE: 12,437.4 Hrs1. RE 300 HrsFuel Filter Assembly - Check bypass indicator and carry out ...73-10-21-202ENG173

In PackageDUE: 12,437.4 Hrs1. RE 300 HrsN1 Speed Control Amplifier - Visual Check of control amplifi...73-20-16-210ENG173

In PackageDUE: 12,437.4 Hrs1. RE 300 HrsIgnition Exciter - Visual Check74-10-11-203ENG174

In PackageDUE: 12,437.4 Hrs1. RE 300 HrsIgniter Plug - Inspect Igniter plugs74-10-16-202ENG174

In PackageDUE: 12,437.4 Hrs1. RE 300 HrsVariable Geometry Control - Visual Check of VG system, payin...75-30-00-201ENG175

≈25-Sep-2016REPKG 300 Eng Hour 300 Engine Hourly Task

10-Feb-2016Mos

300 Hrs (+40)12,320.4-/+4030012,020.4Hrs

6,728Enc

5 ENG2

In PackageDUE: 12,320.4 Hrs1. RE 300 HrsScheduled Servicing - Lubricate variable geometry actuator12-20-00-314ENG212

In PackageDUE: 12,320.4 Hrs1. RE 300 HrsEngine - General - Visual Check of Fan Stator for the follow...72-00-00-201ENG272


In PackageDUE: 12,320.4 Hrs1. RE 300 HrsEngine - General - Visual Check of engine external lines, po...72-00-00-206ENG272

In PackageDUE: 12,320.4 Hrs1. RE 300 HrsEngine - General - Visual check of high pressure turbine sec...72-00-00-208ENG272

In PackageDUE: 12,320.4 Hrs1. RE 300 HrsEngine - General - Compressor Waterwash72-00-00-301ENG272

In PackageDUE: 12,320.4 Hrs1. RE 300 HrsEngine - General (Engine model CF34-1A/-3A/-3A2 only) - Powe...72-00-00-302ENG272

In PackageDUE: 12,320.4 Hrs1. RE 300 HrsFuel Heater Assembly - Check for evidence of leakage from fu...73-10-16-208ENG273

In PackageDUE: 12,320.4 Hrs1. RE 300 HrsFuel Filter Assembly - Check bypass indicator and carry out ...73-10-21-202ENG273

In PackageDUE: 12,320.4 Hrs1. RE 300 HrsN1 Speed Control Amplifier - Visual Check of control amplifi...73-20-16-210ENG273

In PackageDUE: 12,320.4 Hrs1. RE 300 HrsIgnition Exciter - Visual Check74-10-11-203ENG274

In PackageDUE: 12,320.4 Hrs1. RE 300 HrsIgniter Plug - Inspect Igniter plugs74-10-16-202ENG274

In PackageDUE: 12,320.4 Hrs1. RE 300 HrsVariable Geometry Control - Visual Check of VG system, payin...75-30-00-201ENG275

≈18-Sep-2016REPKG 300 Hour 300 Hourly Task

10-Feb-2016Mos

290.8 Hrs (+40)12,332-/+4030012,041.2Hrs

6,326Ldg

5 A/F

(Tol. Adjustment: -9.2 Hrs)

In PackageDUE: 12,332 Hrs1. RE 300 HrsHydraulic System Replenishing (No.1, No.2, and No.3 Systems)...12-10-29-301A/F12

In PackageDUE: 12,332 Hrs1. RE 300 HrsHydraulic System Replenishing (No.1, No.2, and No.3 Systems)...12-10-29-318A/F12

In PackageDUE: 12,332 Hrs1. RE 300 HrsLanding Gear Replenishing - Check main gear shock strut exte...12-10-32-316A/F12

In PackageDUE: 12,332 Hrs1. RE 300 HrsLanding Gear Replenishing - Check nose gear shock strut exte...12-10-32-317A/F12

In PackageDUE: 12,332 Hrs1. RE 300 HrsScheduled Servicing - Lubricate landing gear doors12-20-00-302A/F12

In PackageDUE: 12,332 Hrs1. RE 300 HrsScheduled Servicing - Lubricate dual brake control valve pus...12-20-00-303A/F12

In PackageDUE: 12,332 Hrs1. RE 300 HrsScheduled Servicing - Lubricate servicing doors / Lubricate ...12-20-00-304A/F12

In PackageDUE: 12,332 Hrs1. RE 300 HrsScheduled Servicing - Lubricate main tracks12-20-00-305A/F12

In PackageDUE: 12,332 Hrs1. RE 300 HrsScheduled Servicing - Lubricate pylon tracks12-20-00-306A/F12

In PackageDUE: 12,332 Hrs1. RE 300 HrsScheduled Servicing - Lubricate inboard flap vane mechanism12-20-00-307A/F12









In PackageDUE: 12,332 Hrs1. RE 300 HrsIntegrated Drive Generator System Differential Pressure Chec...24-21-00-202A/F24

In PackageDUE: 12,332 Hrs1. RE 300 HrsIntegrated Drive Generator Oil System Replenishing - Repleni...24-21-00-301A/F24

In PackageDUE: 12,332 Hrs1. RE 300 HrsPower Plant and APU Fire Sensing Cables Visual Check all vis...26-10-11-201A/F26

In PackageDUE: 12,332 Hrs1. RE 300 HrsAuxiliary Power Unit (APU) Fire Extinguishing Functional Tes...26-21-00-204A/F26

In PackageDUE: 12,332 Hrs1. RE 300 HrsPortable Fire Extinguisher - Check pressure26-25-00-212A/F26

In PackageDUE: 12,332 Hrs1. RE 300 HrsAileron, Flap Actuators and Attachments Visual Check27-11-00-201A/F27

In PackageDUE: 12,332 Hrs1. RE 300 HrsAileron Power Control Unit Operational Test27-17-00-208A/F27

In PackageDUE: 12,332 Hrs1. RE 300 HrsRudder Power Control Units Operational Test27-25-00-212A/F27

In PackageDUE: 12,332 Hrs1. RE 300 HrsElevator Power Control Units Operational Test27-37-00-219A/F27

In PackageDUE: 12,332 Hrs1. RE 300 HrsSpoiler Control/Scheduled Servicing Lubricate Flight Spoiler...27-61-00-231A/F27

In PackageDUE: 12,332 Hrs1. RE 300 HrsGround Spoiler Actuators and Manifold Assembly (Pre SB 601-0...27-69-00-228A/F27

In PackageDUE: 12,332 Hrs1. RE 300 HrsFuel and Vent Line Shrouds Visual Check of the Vent and Dist...28-10-31-211A/F28

In PackageDUE: 12,332 Hrs1. RE 300 HrsHydraulic Power Check Filter Differential Pressure Indicator...29-00-00-201A/F29

In PackageDUE: 12,332 Hrs1. RE 300 HrsNose Cowl Anti-Ice/Thrust Reverser Ducting Visual Check, pay...30-20-21-206A/F30

In PackageDUE: 12,332 Hrs1. RE 300 HrsMain Gear and Doors / Main Landing Gear Uplock /Emergency Ex...32-10-00-210A/F32

In PackageDUE: 12,332 Hrs1. RE 300 HrsMain Landing Gear Lubricate Landing Gear32-10-00-241A/F32

In PackageDUE: 12,332 Hrs1. RE 300 HrsNose Gear and Doors Visual Check32-20-00-205A/F32

In PackageDUE: 12,332 Hrs1. RE 300 HrsNose Landing Gear Lubricate Nose Landing Gear32-20-00-242A/F32

In PackageDUE: 12,332 Hrs1. RE 300 HrsNose Landing Gear Uplock Visual Check, paying particular att...32-30-51-211A/F32

In PackageDUE: 12,332 Hrs1. RE 300 HrsAccumulator/Hydraulic System - Replenishing Check accumulato...32-43-16-222A/F32

In PackageDUE: 12,332 Hrs1. RE 300 HrsDual Brake Control Valve Assembly Visual Check visible porti...32-43-21-216A/F32

In PackageDUE: 12,332 Hrs1. RE 300 HrsFunctional Test of Nose Wheel Steering Selector Valve32-47-00-226A/F32

In PackageDUE: 12,332 Hrs1. RE 300 HrsNosewheel Steering Nosewheel Steering Selector and arming va...32-50-00-226A/F32

In PackageDUE: 12,332 Hrs1. RE 300 HrsMain Landing Gear - CPCP CheckC32-10-801A/F32

In PackageDUE: 12,332 Hrs1. RE 300 HrsNose Landing Gear - CPCP CheckC32-20-801A/F32

In PackageDUE: 12,332 Hrs1. RE 300 HrsEmergency Lighting Visual Check- Operational Test33-50-00-202A/F33

In PackageDUE: 12,332 Hrs1. RE 300 HrsPitot Static System and Temperature Sensing System Visual Ch...34-11-00-201A/F34

In PackageDUE: 12,332 Hrs1. RE 300 HrsPitot Static Heads Clean pitot drain holes34-11-11-208A/F34

In PackageDUE: 12,332 Hrs1. RE 300 HrsDoors Visual Check of passenger/crew entrance door seal52-00-00-201A/F52

In PackageDUE: 12,332 Hrs1. RE 300 HrsPassenger/Crew Entrance Door Visual Check that water drains ...52-10-00-202A/F52

In PackageDUE: 12,332 Hrs1. RE 300 HrsDownward Opening Passenger/Crew Entrance Door Scheduled Serv...52-12-00-212A/F52

In PackageDUE: 12,332 Hrs1. RE 300 HrsDownward Opening Passenger/Crew Entrance Door Cam Latch Mech...52-12-00-213A/F52

In PackageDUE: 12,332 Hrs1. RE 300 HrsDoor Warning - Passenger/Crew Entrance Door Switches Operati...52-70-00-214A/F52

In PackageDUE: 12,332 Hrs1. RE 300 HrsFuselage Visual Check (External)53-00-00-201A/F53

In PackageDUE: 12,332 Hrs1. RE 300 HrsNacelles/Pylons Visual Check - External54-00-00-201A/F54

In PackageDUE: 12,332 Hrs1. RE 300 HrsStabilizers Visual Check - External55-00-00-201A/F55

In PackageDUE: 12,332 Hrs1. RE 300 HrsElevators and Rudder Visual Check - External55-20-00-207A/F55

In PackageDUE: 12,332 Hrs1. RE 300 HrsFlight Compartment Windows Visual Check - Internal and Exter...56-10-00-201A/F56

In PackageDUE: 12,332 Hrs1. RE 300 HrsNose Cowl Assembly Visual Check71-10-11-209A/F71

In PackageDUE: 12,332 Hrs1. RE 300 HrsTranslating Cowl Doors Visual Check, paying particular atten...71-10-16-201A/F71

In PackageDUE: 12,332 Hrs1. RE 300 HrsCore Cowl Doors Check Core Cowl71-12-01-202A/F71

In PackageDUE: 12,332 Hrs1. RE 300 HrsThrust Reverser With thrust reversers manually deployed, vis...78-30-00-208A/F78

In PackageDUE: 12,332 Hrs1. RE 300 HrsThrust Reverser (Pre SB 601-1084) Detailed Inspection of the...78-30-16-219A/F78

In PackageDUE: 12,332 Hrs1. RE 300 HrsAir Turbine Starter/Air Turbine Starter Replenishing Visual ...80-10-11-201A/F80









≈22-Feb-2021REPKG 3000 Eng Hour 3000 Engine Hourly Task

05-Jun-2009Mos

2,417.4 Hrs (+40)14,554.8-/+403,00011,554.8Hrs

Enc

5 ENG1

In PackageDUE: 14,554.8 Hrs1. RE 3000 HrsEngine - General - Mid point inspection72-00-00-213ENG172

In PackageDUE: 14,554.8 Hrs1. RE 3000 HrsEngine - General - Borescope Compressor / Visual Check of vi...72-00-00-215ENG172

In PackageDUE: 14,554.8 Hrs1. RE 3000 HrsEngine - General - Detailed Inspection of engine accessory g...72-00-00-218ENG172

In PackageDUE: 14,554.8 Hrs1. RE 3000 HrsEngine - General - Visual Check of 6 o’clock c-sump scavenge...72-00-00-221ENG172

In PackageDUE: 14,554.8 Hrs1. RE 3000 HrsEngine - General - Visual Check of LPT stator assembly P/N 6...72-00-00-222ENG172

In PackageDUE: 14,554.8 Hrs1. RE 3000 HrsEngine - General - Visual Check of HPT stage 1 and stage 2 s...72-00-00-223ENG172

In PackageDUE: 14,554.8 Hrs1. RE 3000 HrsEngine - General - Inspect/Check turbine thermocouple harnes...72-00-00-224ENG172

In PackageDUE: 14,554.8 Hrs1. RE 3000 HrsEngine - General - Visual Check of turbine nozzles72-00-00-225ENG172

In PackageDUE: 14,554.8 Hrs1. RE 3000 HrsEngine - General - Detailed visual inspection of the swirler...72-00-00-226ENG172

In PackageDUE: 14,554.8 Hrs1. RE 3000 HrsEngine - General - Visual Check of primary swirlers, paying ...72-00-00-227ENG172

In PackageDUE: 14,554.8 Hrs1. RE 3000 HrsEngine - General - Visual Check of stage 1 and stage 2 nozzl...72-00-00-228ENG172

In PackageDUE: 14,554.8 Hrs1. RE 3000 HrsEngine - General - Visual Check of combustion liner after di...72-00-00-229ENG172

In PackageDUE: 14,554.8 Hrs1. RE 3000 HrsEngine - General - Check combustion section fuel injector he...72-00-00-230ENG172

In PackageDUE: 14,554.8 Hrs1. RE 3000 HrsEngine - General - Visual Check of fan disk to ensure bushin...72-00-00-231ENG172

In PackageDUE: 13,956 Hrs1. RE 3000 HrsFuel Pump Assembly - General Visual Inspection of the engine...73-10-11-204ENG173

In PackageDUE: 14,554.8 Hrs1. RE 3000 HrsFuel Control Unit - General Visual Inspection of main fuel c...73-20-11-206ENG173

In PackageDUE: 14,554.8 Hrs1. RE 3000 HrsC-Sump Scavenge Screens - Detailed Inspection79-21-01-202ENG179

≈24-Nov-2019REPKG 3000 Eng Hour 3000 Engine Hourly Task

28-Jul-2005Mos

1,818.6 Hrs (+40)13,839-/+403,00010,839Hrs

Enc

5 ENG2

In PackageDUE: 13,839 Hrs1. RE 3000 HrsEngine - General - Mid point inspection72-00-00-213ENG272

In PackageDUE: 13,839 Hrs1. RE 3000 HrsEngine - General - Borescope Compressor / Visual Check of vi...72-00-00-215ENG272

In PackageDUE: 13,839 Hrs1. RE 3000 HrsEngine - General - Detailed Inspection of engine accessory g...72-00-00-218ENG272

In PackageDUE: 13,839 Hrs1. RE 3000 HrsEngine - General - Visual Check of 6 o’clock c-sump scavenge...72-00-00-221ENG272

In PackageDUE: 13,839 Hrs1. RE 3000 HrsEngine - General - Visual Check of LPT stator assembly P/N 6...72-00-00-222ENG272

In PackageDUE: 13,839 Hrs1. RE 3000 HrsEngine - General - Visual Check of HPT stage 1 and stage 2 s...72-00-00-223ENG272

In PackageDUE: 13,839 Hrs1. RE 3000 HrsEngine - General - Inspect/Check turbine thermocouple harnes...72-00-00-224ENG272

In PackageDUE: 13,839 Hrs1. RE 3000 HrsEngine - General - Visual Check of turbine nozzles72-00-00-225ENG272

In PackageDUE: 13,839 Hrs1. RE 3000 HrsEngine - General - Detailed visual inspection of the swirler...72-00-00-226ENG272

In PackageDUE: 13,839 Hrs1. RE 3000 HrsEngine - General - Visual Check of primary swirlers, paying ...72-00-00-227ENG272

In PackageDUE: 13,839 Hrs1. RE 3000 HrsEngine - General - Visual Check of stage 1 and stage 2 nozzl...72-00-00-228ENG272

In PackageDUE: 13,839 Hrs1. RE 3000 HrsEngine - General - Visual Check of combustion liner after di...72-00-00-229ENG272

In PackageDUE: 13,839 Hrs1. RE 3000 HrsEngine - General - Check combustion section fuel injector he...72-00-00-230ENG272

In PackageDUE: 13,839 Hrs1. RE 3000 HrsEngine - General - Visual Check of fan disk to ensure bushin...72-00-00-231ENG272

In PackageDUE: 13,839 Hrs1. RE 3000 HrsFuel Pump Assembly - General Visual Inspection of the engine...73-10-11-204ENG273

In PackageDUE: 13,839 Hrs1. RE 3000 HrsFuel Control Unit - General Visual Inspection of main fuel c...73-20-11-206ENG273

In PackageDUE: 13,839 Hrs1. RE 3000 HrsC-Sump Scavenge Screens - Detailed Inspection79-21-01-202ENG279










11.9 Months (+31

Days)28-Mar-2017-/+13628-Mar-2014Mos

Hrs

Ldg

5 A/F

Also ConsiderDUE: 21-Oct-20161. RE 12 Mos12 Monthly TasksPKG 12 MonthA/F5

In PackageDUE: 28-Mar-20171. RE 36 MosAttachment Fittings Visual Check of the vertical stabilizer ...55-50-00-214A/F55

In PackageDUE: 28-Mar-20171. RE 36 MosAttachment Fittings Visual Check of the rudder actuator/hing...55-50-00-215A/F55

In PackageDUE: 28-Mar-20171. RE 36 MosAttachment Fittings Visual Check of the rudder attachment fi...55-50-00-216A/F55

In PackageDUE: 28-Mar-20171. RE 36 MosAttachment Fittings Visual Check of Hinge Fitting on Horizon...55-50-00-217A/F55

In PackageDUE: 28-Mar-20171. RE 36 MosAttachment Fittings Visual Check of PCU Fittings, Horizontal...55-50-00-218A/F55

In PackageDUE: 28-Mar-20171. RE 36 MosAttachment Fittings Visual Check of PCU and Elevator, paying...55-50-00-219A/F55

In PackageDUE: 28-Mar-20171. RE 36 MosVertical Stabilizer Rear Spar Structure - CPCP Check includi...C55-00-805A/F55

In PackageDUE: 28-Mar-20171. RE 36 MosRudder External Skin, Structure and Attachments - CPCP Check...C55-00-812A/F55

In PackageDUE: 28-Mar-20171. RE 36 MosElevator External Skin, Structure and Attachments - CPCP Che...C55-00-813A/F55


2.5 Years (+30 Days)26-Sep-2018-/+14826-Sep-2014Mos

Hrs

Ldg

5 A/F

Also ConsiderDUE: 30-Jan-20171. RE 24 Mos24 Monthly TasksPKG 24 MonthA/F5

In PackageDUE: 26-Sep-20181. RE 48 MosNose-Radome Lightning Strips Functional Test23-60-00-203A/F23

In PackageDUE: 26-Sep-20181. RE 48 MosPassenger/Crew Entrance Door Structure (External) - CPCP Che...C52-00-803A/F52

In PackageDUE: 26-Sep-20181. RE 48 MosFuselage External Skin Panels, FS621.00 to VS67.5% - CPCP Ch...C53-00-814A/F53

In PackageDUE: 26-Sep-20181. RE 48 MosNose Landing Gear Wheel Well Structure - CPCP Check includin...C53-00-815A/F53

In PackageDUE: 26-Sep-20181. RE 48 MosVertical Stabilizer External Surfaces - CPCP Check including...C55-00-801A/F55

In PackageDUE: 26-Sep-20181. RE 48 MosVertical Stabilizer, Pitch Trim Actuator Attachment Structur...C55-00-804A/F55

In PackageDUE: 26-Sep-20181. RE 48 MosHorizontal Stabilizer Front Spar - CPCP Check including the ...C55-00-806A/F55

In PackageDUE: 26-Sep-20181. RE 48 MosHorizontal and Vertical Stabilizer - CPCP Check including th...C55-00-809A/F55

In PackageDUE: 26-Sep-20181. RE 48 MosHorizontal Stabilizer, Pitch Trim Actuator Attachment - CPCP...C55-00-810A/F55

In PackageDUE: 26-Sep-20181. RE 48 MosHorizontal Stabilizer, External Surfaces - CPCP Check includ...C55-00-811A/F55

In PackageDUE: 26-Sep-20181. RE 48 MosMain Landing Gear Actuator Fitting at Wing Box FS513.00 and ...C57-00-810A/F57









≈24-Aug-2023REPKG 4800 Hour 4800 Hourly Tasks

08-Aug-2005Mos

3,618.6 Hrs (+40)15,659.8-/+404,80010,859.8Hrs

Ldg

5 A/F

Also ConsiderDUE: 12,725.2 Hrs1. RE 2400 Hrs2400 Hourly TasksPKG 2400 HourA/F5

In PackageDUE: 15,659.8 Hrs1. RE 4800 HrsAileron Flutter Dampers - Remove, carry out “Testing and Fau...27-13-21-206A/F27

In PackageDUE: 15,659.8 Hrs1. RE 4800 HrsAileron Flutter Dampers - Remove, carry out “Testing and Fau...27-13-21-206A/F27

In PackageDUE: 15,659.8 Hrs1. RE 4800 HrsElevator Flutter Dampers - Remove, carry out “Testing and Fa...27-33-11-217A/F27




In PackageDUE: 15,659.8 Hrs1. RE 4800 HrsAPU Return Line Check Valve Remove Check Valve and Perform I...28-25-21-223A/F28

In PackageDUE: 15,659.8 Hrs1. RE 4800 HrsMain Systems Remove No.1 and No.2 system hydraulic reservoir...29-10-00-205A/F29

In PackageDUE: 15,659.8 Hrs1. RE 4800 HrsMain Systems Remove No.3 system hydraulic reservoir in-line ...29-10-00-206A/F29

In PackageDUE: 15,659.8 Hrs1. RE 4800 HrsStabilizers Structure NDT Check of the vertical stabilizer t...55-50-00-220A/F55

In PackageDUE: 15,659.8 Hrs1. RE 4800 HrsStabilizers Structure NDT Check of the horizontal stabilizer...55-50-00-221A/F55

In PackageDUE: 15,659.8 Hrs1. RE 4800 HrsWing Structure NDT Check of wing to aileron hinge bolts for ...57-40-00-215A/F57

In PackageDUE: 15,659.8 Hrs1. RE 4800 HrsWing to Flap Hinge Bolts NDT Check57-40-00-216A/F57

REPKG 60 Month 60 Monthly Task

5.8 Months (+30

Days)26-Sep-2016-/+16026-Sep-2011Mos

Hrs

Ldg

5 A/F

In PackageDUE: 26-Sep-20161. RE 60 MosWire Cables - Flight Controls Wire Cable Inspection (straigh...20-40-00-202A/F20

In PackageDUE: 26-Sep-20161. RE 60 MosForward and Aft Auxiliary Fuel Tanks External Check28-10-21-206A/F28

In PackageDUE: 26-Sep-20161. RE 60 MosFuel and Vent Line Shrouds Fuselage tank wall interspace and...28-10-31-205A/F28

In PackageDUE: 26-Sep-20161. RE 60 MosFuel and Vent Line Shrouds Pressure test of the following sh...28-10-31-208A/F28

In PackageDUE: 26-Sep-20161. RE 60 MosFuel and Vent Line Shrouds (Post SB 601-0262) Tail tank fuel...28-10-31-209A/F28

In PackageDUE: 26-Sep-20161. RE 60 MosScavenge Fuel Ejector Visual Check of pump screen28-21-26-215A/F28

In PackageDUE: 26-Sep-20161. RE 60 MosWing Anti-Icing Ducting Visual Check of ducts, brackets, cla...30-11-06-204A/F30

In PackageDUE: 22-Mar-20171. RE 60 MosMain Landing Gear Assembly - Detailed Inspection32-10-00-237A/F32

In PackageDUE: 22-Mar-20171. RE 60 MosMain Landing Gear Assembly - Detailed Inspection32-10-00-237A/F32

In PackageDUE: 26-Sep-20161. RE 60 MosNose Landing Gear Assembly - Detailed Inspection32-20-00-239A/F32

In PackageDUE: 26-Sep-20161. RE 60 MosEmergency Extension Visual Check of the control path (straig...32-35-00-244A/F32

In PackageDUE: 26-Sep-20161. RE 60 MosAccumulator Visual Check of No. 2 and No. 3 System Brake Acc...32-43-16-223A/F32

In PackageDUE: 26-Sep-20161. RE 60 MosOverwing Emergency Exit Visual Check of all structure, payin...52-20-00-209A/F52

In PackageDUE: 26-Sep-20161. RE 60 MosBaggage Compartment Door Visual Check of all structure, payi...52-30-00-210A/F52

In PackageDUE: 26-Sep-20161. RE 60 MosOverwing Emergency Exit Door, External - CPCP Check includin...C52-00-801A/F52

In PackageDUE: 26-Sep-20161. RE 60 MosBaggage Compartment Door Structure - CPCP Check including th...C52-00-802A/F52

In PackageDUE: 26-Sep-20161. RE 60 MosMain Landing Gear Doors - CPCP Check including the following...C52-00-804A/F52

In PackageDUE: 26-Sep-20161. RE 60 MosPassenger/Crew Entrance Door Structure (Internal) - CPCP Che...C52-00-805A/F52

In PackageDUE: 26-Sep-20161. RE 60 MosOverwing Emergency Exit Door (Internal) - CPCP Check includi...C52-00-806A/F52

In PackageDUE: 26-Sep-20161. RE 60 MosFuselage Visual Check - External - along rivet lines, paying...53-00-00-204A/F53

In PackageDUE: 26-Sep-20161. RE 60 MosMain Frame (Pressure Bulkhead FS202.75) Visual Check of the ...53-10-00-205A/F53

In PackageDUE: 26-Sep-20161. RE 60 MosMain Frame (FS625.30 and Engine Support Beam Attachment) Vis...53-10-00-206A/F53

In PackageDUE: 26-Sep-20161. RE 60 MosMain Frame (Keel Longerons) Visual Check of the following it...53-10-00-207A/F53

In PackageDUE: 26-Sep-20161. RE 60 MosMain Frame (FS755.00) Visual Check, paying particular attent...53-10-00-208A/F53

In PackageDUE: 26-Sep-20161. RE 60 MosMain Frame (Floor Beam End Fittings at FS621.00) Visual Chec...53-10-00-209A/F53









In PackageDUE: 26-Sep-20161. RE 60 MosMain Frame (Passenger Door Surround Structure) Visual Check ...53-10-00-210A/F53

In PackageDUE: 26-Sep-20161. RE 60 MosMain Frame (Overwing Emergency Exit Surround Structure) Visu...53-10-00-211A/F53

In PackageDUE: 26-Sep-20161. RE 60 MosMain Frame (Baggage Door Surround Structure) Visual Check of...53-10-00-212A/F53

In PackageDUE: 26-Sep-20161. RE 60 MosMain Frame (Equipment Bay Door Surround Structure) Visual Ch...53-10-00-213A/F53

In PackageDUE: 26-Sep-20161. RE 60 MosMain Frame - Fuselage Floor Beam Splices Visual Check53-10-00-214A/F53

In PackageDUE: 26-Sep-20161. RE 60 MosMain Frame (Frame Assembly FS424.00) Visual Check, paying pa...53-10-00-215A/F53



In PackageDUE: 26-Sep-20161. RE 60 MosMain Frame (Frame Assembly FS640.00 and Engine Support Beam ...53-10-00-218A/F53

In PackageDUE: 26-Sep-20161. RE 60 MosMain Frame (Frame Assembly FS654.50) Visual Check - Internal53-10-00-219A/F53

In PackageDUE: 26-Sep-20161. RE 60 MosMain Frame (FS672.20 and FS682.20) Visual Check - Internal53-10-00-220A/F53

In PackageDUE: 26-Sep-20161. RE 60 MosFloor Structure (Pre or Post SB 601-0372) - Remove Toilet, G...53-10-11-230A/F53

In PackageDUE: 26-Sep-20161. RE 60 MosCabin Window Cut-Outs NDT Check53-30-00-221A/F53

In PackageDUE: 26-Sep-20161. RE 60 MosPlates/Skins (Side Skin Panel FS409.00 and WL73.50) Visual C...53-30-00-222A/F53

In PackageDUE: 26-Sep-20161. RE 60 MosNose Radome Visual Check, paying particular attention to int...53-50-11-227A/F53

In PackageDUE: 26-Sep-20161. RE 60 MosFuselage Upper External Skin, FS169.00 to FS621.00, above WL...C53-00-801A/F53

In PackageDUE: 26-Sep-20161. RE 60 MosFuselage Lower External Skin, FS169.00 to FS621.00 - CPCP Ch...C53-00-802A/F53

In PackageDUE: 26-Sep-20161. RE 60 MosKeel Longerons and Surround Structure - CPCP Check including...C53-00-804A/F53

In PackageDUE: 26-Sep-20161. RE 60 MosFuselage Frame Attachment at FS755.00 and Skin at FS710.00 t...C53-00-805A/F53

In PackageDUE: 26-Sep-20161. RE 60 MosPassenger Door Surround Structure - CPCP Check including the...C53-00-806A/F53

In PackageDUE: 26-Sep-20161. RE 60 MosOverwing Emergency Exit Door Structure - CPCP Check includin...C53-00-807A/F53

In PackageDUE: 26-Sep-20161. RE 60 MosBaggage Door Surround Structure - CPCP Check including the f...C53-00-808A/F53

In PackageDUE: 26-Sep-20161. RE 60 MosMain Frame (Equipment Bay Door Surround Structure) - CPCP Ch...C53-00-809A/F53

In PackageDUE: 26-Sep-20161. RE 60 MosWing to Fuselage Integral Attachment at FS424.00 and BL45.00...C53-00-810A/F53



In PackageDUE: 26-Sep-20161. RE 60 MosCabin Window Cut-Outs and Surround Structure FS364.00 to FS5...C53-00-813A/F53

In PackageDUE: 26-Sep-20161. RE 60 MosTail Cone Assembly (Pre SB 601-0262) - CPCP Check including ...C53-00-816A/F53

In PackageDUE: 26-Sep-20161. RE 60 MosNose Radome - CPCP Check including the following items: (1) ...C53-00-817A/F53

In PackageDUE: 26-Sep-20161. RE 60 MosFloor Structure, FS589.00 to FS621.00 - CPCP Check including...C53-00-818A/F53

In PackageDUE: 26-Sep-20161. T 120 Mos | 2. RE 60 MosTail Cone (Post SB 601-0262) - CPCP Check including the foll...C53-00-822A/F53




In PackageDUE: 26-Sep-20161. RE 60 MosStructure Adjacent to Overboard Lavatory Services (External)...C53-00-826A/F53

In PackageDUE: 26-Sep-20161. RE 60 MosFuselage Frame FS409.00, Aft Face, External - CPCP Check inc...C53-00-827A/F53

In PackageDUE: 26-Sep-20161. RE 60 MosNacelles/Pylons (Pylon Structure) Visual Check - Internal54-00-00-202A/F54

In PackageDUE: 26-Sep-20161. RE 60 MosNacelles/Pylons, Internal (Pylon Structure) - CPCP CheckC54-00-802A/F54

In PackageDUE: 26-Sep-20161. RE 60 MosHorizontal Stabilizer Visual Check of the following items, p...55-10-00-203A/F55

In PackageDUE: 26-Sep-20161. RE 60 MosHorizontal Stabilizer Visual Check - Internal - Structure at...55-10-00-204A/F55

In PackageDUE: 26-Sep-20161. RE 60 MosVertical Stabilizer Visual Check of the following items, pay...55-30-00-210A/F55

In PackageDUE: 26-Sep-20161. RE 60 MosVertical Stabilizer Front Spar - CPCP Check including the fo...C55-00-802A/F55

In PackageDUE: 26-Sep-20161. RE 60 MosVertical Stabilizer Internal Structure - CPCP Check includin...C55-00-803A/F55

In PackageDUE: 26-Sep-20161. RE 60 MosHorizontal Stabilizer Rear Spar - CPCP Check including the f...C55-00-807A/F55

In PackageDUE: 26-Sep-20161. RE 60 MosHorizontal Stabilizer Internal Structure - CPCP Check includ...C55-00-808A/F55

In PackageDUE: 26-Sep-20161. RE 60 MosWing Structure - Wing Box Visual Check of the following item...57-00-00-204A/F57

In PackageDUE: 26-Sep-20161. RE 60 MosMain Frame (Wing Center Section Internal Structure) Visual C...57-10-00-205A/F57

In PackageDUE: 26-Sep-20161. RE 60 MosMain Frame (Front Spar Splice WS29.42) Visual Check (Interna...57-10-00-206A/F57

In PackageDUE: 26-Sep-20161. RE 60 MosMain Frame (Wing Inboard Box Internal Structure WS45.00 to W...57-10-00-207A/F57









In PackageDUE: 26-Sep-20161. RE 60 MosMain Frame (Wing Outboard Box Internal Structure WS148.00 to...57-10-00-208A/F57

In PackageDUE: 26-Sep-20161. RE 60 MosMain Frame (Rear Spar Splice at WS45.00) Visual Check (Inter...57-10-00-209A/F57

In PackageDUE: 26-Sep-20161. RE 60 MosAuxiliary Structure (Winglet) Visual Check (Internal and Ext...57-20-00-210A/F57

In PackageDUE: 26-Sep-20161. RE 60 MosAuxiliary Structure Visual Check of Wing Trailing Edge and W...57-20-00-211A/F57

In PackageDUE: 26-Sep-20161. RE 60 MosAttachment Fittings (Main Gear Trunnion) Visual Check (as ex...57-40-00-217A/F57

In PackageDUE: 26-Sep-20161. RE 60 MosAttachment Fittings (Wing to Fuselage Attach Assembly FS424....57-40-00-218A/F57

In PackageDUE: 26-Sep-20161. RE 60 MosAttachment Fittings (Wing to Fuselage Attachment Fitting FS4...57-40-00-219A/F57

In PackageDUE: 26-Sep-20161. RE 60 MosAttachment Fittings (Hinge/Actuator Aileron) Visual Check (U...57-40-00-220A/F57

In PackageDUE: 26-Sep-20161. RE 60 MosAttachment Fittings (Flap Hinges) Visual Check (Upon extensi...57-40-00-221A/F57

In PackageDUE: 26-Sep-20161. RE 60 MosFlight Control Surfaces (Ailerons, Spoilers and Flaps) Visua...57-50-00-222A/F57

In PackageDUE: 26-Sep-20161. RE 60 MosWing Front Spar and Leading Edge WS50.00 to WS353.00 - CPCP ...C57-00-801A/F57

In PackageDUE: 26-Sep-20161. RE 60 MosWing Upper Surface, BL0.00 to BL50.00 - CPCP Check: (1) Wing...C57-00-803A/F57

In PackageDUE: 26-Sep-20161. RE 60 MosWing Structure Between the Front Spar and Rear Spar, BL0.00 ...C57-00-804A/F57

In PackageDUE: 26-Sep-20161. RE 60 MosWing Front Spar, BL0.00 to WS50.00 - CPCP Check of the follo...C57-00-805A/F57

In PackageDUE: 26-Sep-20161. RE 60 MosWing Structure Between the Front Spar and Rear Spar, WS45.00...C57-00-806A/F57

In PackageDUE: 26-Sep-20161. RE 60 MosWing Rear Spar, BL0.00 to WS66.00 (External) - CPCP Check in...C57-00-807A/F57

In PackageDUE: 26-Sep-20161. RE 60 MosWingtip/Winglet Assembly (Internal/External) - CPCP Check in...C57-00-808A/F57

In PackageDUE: 26-Sep-20161. RE 60 MosWing Rear Spar and Auxiliary Spar, WS50.00 to WS353.00 - CPC...C57-00-809A/F57

In PackageDUE: 26-Sep-20161. RE 60 MosWing Rear Spar and Auxiliary Spar, WS66.00 to WS148.00 - CPC...C57-00-811A/F57

In PackageDUE: 26-Sep-20161. RE 60 MosWing to Fuselage Attachment Fitting, FS424.00 and BL45.00 - ...C57-00-812A/F57

In PackageDUE: 26-Sep-20161. RE 60 MosWing to Fuselage Attachment Fitting, FS473.15 and BL45.00 - ...C57-00-813A/F57

In PackageDUE: 26-Sep-20161. RE 60 MosOutboard Flap (External) - CPCP Check including the followin...C57-00-814A/F57

In PackageDUE: 26-Sep-20161. RE 60 MosInboard Flap (External) - CPCP Check including the following...C57-00-815A/F57

In PackageDUE: 26-Sep-20161. RE 60 MosInboard Flap Vane Actuating Assemblies - CPCP Check includin...C57-00-816A/F57

In PackageDUE: 26-Sep-20161. RE 60 MosAileron (External) - CPCP Check including the following item...C57-00-817A/F57

In PackageDUE: 26-Sep-20161. RE 60 MosFlight Spoiler (External) - CPCP Check including the followi...C57-00-818A/F57

In PackageDUE: 26-Sep-20161. RE 60 MosWing Upper External Surface, WS50.00 to WS353.00 - CPCP Chec...C57-00-819A/F57

In PackageDUE: 26-Sep-20161. RE 60 MosWing to Fuselage Attachment Fitting, WS513.00 and BL45.00 - ...C57-00-820A/F57

In PackageDUE: 26-Sep-20161. RE 60 MosForward Engine Mount - CPCP Check including the following it...C71-00-801A/F71

In PackageDUE: 26-Sep-20161. RE 60 MosAft Engine Mount - CPCP Check including the following items:...C71-00-802A/F71

In PackageDUE: 26-Sep-20161. RE 60 MosForward Nacelle and Nose Cowl Actuator Support Fitting - CPC...C71-00-803A/F71

In PackageDUE: 26-Sep-20161. RE 60 MosThrust Reverser - CPCP Check including the following items: ...C78-00-801A/F78

≈10-May-2017REPKG 600 Eng Hour 600 Engine Hourly Task

10-Feb-2016Mos

600 Hrs (+40)12,737.4-/+4060012,137.4Hrs

6,769Enc

5 ENG1


In PackageDUE: 12,737.4 Hrs1. RE 600 HrsEngine - General - Oil Sample Check72-00-00-219ENG172

In PackageDUE: 12,737.4 Hrs1. RE 600 HrsFuel Filter Assembly - Check Fuel filter element73-10-21-203ENG173

In PackageDUE: 12,728.2 Hrs1. RE 600 HrsPneumatic Drive/Flexshaft Lock Unit (Pre Allied Signal SB 12...78-30-46-206ENG178

In PackageDUE: 12,737.4 Hrs1. RE 600 HrsOil Filter Assembly - Inspect and install new filter element79-20-21-203ENG179

In PackageDUE: 12,737.4 Hrs1. RE 600 HrsOil Filter Impending Bypass Sensor - Functional Test79-30-26-204ENG179









≈03-May-2017REPKG 600 Eng Hour 600 Engine Hourly Task

10-Feb-2016Mos

590.8 Hrs (+40)12,611.2-/+4060012,020.4Hrs

6,728Enc

5 ENG2



In PackageDUE: 12,611.2 Hrs1. RE 600 HrsEngine - General - Oil Sample Check72-00-00-219ENG272

In PackageDUE: 12,611.2 Hrs1. RE 600 HrsFuel Filter Assembly - Check Fuel filter element73-10-21-203ENG273

In PackageDUE: 12,611.2 Hrs1. RE 600 HrsPneumatic Drive/Flexshaft Lock Unit (Pre Allied Signal SB 12...78-30-46-206ENG278

In PackageDUE: 12,611.2 Hrs1. RE 600 HrsOil Filter Assembly - Inspect and install new filter element79-20-21-203ENG279

In PackageDUE: 12,611.2 Hrs1. RE 600 HrsOil Filter Impending Bypass Sensor - Functional Test79-30-26-204ENG279

≈03-May-2017REPKG 600 Hour 600 Hourly Tasks

10-Feb-2016Mos

590.8 Hrs (+40)12,632-/+4060012,041.2Hrs

6,326Ldg

5 A/F


In PackageDUE: 12,632 Hrs1. RE 600 HrsScheduled Servicing - Lubricate BUTE door hinge / Lubricate ...12-20-00-308A/F12

In PackageDUE: 12,632 Hrs1. RE 600 HrsWire Cables - Flight Controls Wire Cable Inspection (except ...20-40-00-201A/F20

In PackageDUE: 12,632 Hrs1. RE 600 HrsDistribution Visual Check of accessible Air Conditioning Plu...21-20-00-201A/F21

In PackageDUE: 12,632 Hrs1. RE 600 HrsPressurization Control Operational Test of Emergency Pressur...21-30-00-204A/F21

In PackageDUE: 12,632 Hrs1. RE 600 HrsPressurization Control Operational Test of Emergency Depress...21-30-00-205A/F21

In PackageDUE: 12,632 Hrs1. RE 600 HrsOutflow Valves - Remove and install new filter element21-30-11-301A/F21

In PackageDUE: 12,632 Hrs1. RE 600 HrsEmergency Ram Air Shutoff Valve Functional Test Emergency Ra...21-53-11-210A/F21

In PackageDUE: 12,632 Hrs1. RE 600 HrsWater Separator - Clean coalescer bag21-70-11-302A/F21

In PackageDUE: 12,632 Hrs1. RE 600 HrsAC Generation Functional Test - Complete Generator System24-20-00-201A/F24

In PackageDUE: 12,632 Hrs1. RE 600 HrsDC Static Conversion System Functional Test24-31-00-211A/F24

In PackageDUE: 12,632 Hrs1. RE 600 HrsCrew Seats/Safety Harness and Inertial Reel Visual Check, pa...25-11-00-201A/F25

In PackageDUE: 12,632 Hrs1. RE 600 HrsPower Plant Firex Discharge Lines Visual Check, paying parti...26-23-21-215A/F26

In PackageDUE: 12,632 Hrs1. RE 600 HrsAileron Control Check aileron backlash27-11-00-202A/F27

In PackageDUE: 12,632 Hrs1. RE 600 HrsTension Regulator Operational Test - Tension Regulator27-11-11-203A/F27

In PackageDUE: 12,632 Hrs1. RE 600 HrsAileron Flutter Dampers - Check aileron flutter damper / Che...27-13-21-205A/F27

In PackageDUE: 12,632 Hrs1. RE 600 HrsAileron Flutter Dampers - Check aileron flutter damper / Che...27-13-21-205A/F27

In PackageDUE: 12,632 Hrs1. RE 600 HrsRoll Disconnect Mechanism Functional Test27-15-00-207A/F27

In PackageDUE: 12,632 Hrs1. RE 600 HrsAileron Power Control Unit Visual Check, paying particular a...27-17-00-209A/F27

In PackageDUE: 12,632 Hrs1. RE 600 HrsRudder Control Check Rudder Backlash- Check PCU Input Load L...27-21-00-210A/F27

In PackageDUE: 12,632 Hrs1. RE 600 HrsElevator Control Check elevator backlash - Check PCU Input J...27-31-00-213A/F27

In PackageDUE: 12,632 Hrs1. RE 600 HrsElevator Flutter Dampers - Check elevator flutter damper27-33-11-216A/F27




In PackageDUE: 12,632 Hrs1. RE 600 HrsPitch Disconnect Mechanism Operational Test27-35-00-218A/F27

In PackageDUE: 12,632 Hrs1. RE 600 HrsStall Protection System Operational Test27-39-00-220A/F27

In PackageDUE: 12,632 Hrs1. RE 600 HrsHorizontal Stabilizer Trim Control Pitch trim actuator backl...27-40-00-222A/F27

In PackageDUE: 12,632 Hrs1. RE 600 HrsPitch Trim Actuator - Inspect pitch trim actuator27-40-16-223A/F27

In PackageDUE: 12,632 Hrs1. RE 600 HrsFlap Actuator Detailed Inspection27-50-16-236A/F27

In PackageDUE: 12,632 Hrs1. RE 600 HrsPower Drive Unit (PDU) Operational Test of flap PDU motor br...27-50-21-225A/F27

In PackageDUE: 12,632 Hrs1. RE 600 HrsAsymmetry/Overspeed Detector and Brake Brake drag torque tes...27-50-26-226A/F27

In PackageDUE: 12,632 Hrs1. RE 600 HrsFlexible Drive Shaft Check flexible drive shaft casing27-50-41-227A/F27

In PackageDUE: 12,632 Hrs1. RE 600 HrsSpoiler Control Visual Check of Flight Spoiler and Ground Sp...27-61-00-229A/F27

In PackageDUE: 12,632 Hrs1. RE 600 HrsSpoiler Control (A/C 3001 to 3059 with SB 601-0113 NOT incor...27-61-00-230A/F27









In PackageDUE: 12,632 Hrs1. RE 600 HrsFlight Spoiler Power Control Units Operational Test27-65-00-234A/F27

In PackageDUE: 12,632 Hrs1. RE 600 HrsFuel Tank Gravity Filler Cap Remove, inspect for condition a...28-10-00-225A/F28

In PackageDUE: 12,632 Hrs1. RE 600 HrsHydraulic Power Internal leakage Check29-00-00-202A/F29

In PackageDUE: 12,632 Hrs1. RE 600 HrsHeat Exchanger Visual Check, paying particular attention to ...29-11-51-211A/F29

In PackageDUE: 12,632 Hrs1. RE 600 HrsNo. 3 Main System Visual Check pump installation areas for c...29-13-00-212A/F29

In PackageDUE: 12,632 Hrs1. RE 600 HrsWing Anti-Ice Coupling (Pre SB 601-0433) Detailed inspection...30-11-06-212A/F30

In PackageDUE: 12,632 Hrs1. RE 600 HrsAural Warning System Operational Test of Fire Detection Warn...31-51-00-201A/F31

In PackageDUE: 12,632 Hrs1. RE 600 HrsWeight on Wheels Functional Test32-05-11-201A/F32

In PackageDUE: 12,632 Hrs1. RE 600 HrsExtension and Retraction Functional Test - Landing Gear Retr...32-30-00-207A/F32

In PackageDUE: 12,632 Hrs1. RE 600 HrsNose Gear Drag Brace Visual Check, paying particular attenti...32-30-26-206A/F32

In PackageDUE: 12,632 Hrs1. RE 600 HrsEmergency Extension Functional Test32-35-00-212A/F32

In PackageDUE: 12,632 Hrs1. RE 600 HrsEmergency Extension Visual Check of the control path (except...32-35-00-243A/F32

In PackageDUE: 12,632 Hrs1. RE 600 HrsDual Brake Control Valve Assembly Brake pressure decay check32-43-21-221A/F32

In PackageDUE: 12,632 Hrs1. RE 600 HrsParking Brake Control Cable Assembly / Pilots and Co-Pilots ...32-45-11-217A/F32

In PackageDUE: 12,632 Hrs1. RE 600 HrsAnti-Skid System Anti-skid system operational test32-47-00-225A/F32

In PackageDUE: 12,632 Hrs1. RE 600 HrsNosewheel Steering - Functional test of Electronic Control M...32-50-00-236A/F32

In PackageDUE: 12,632 Hrs1. RE 600 HrsCrew Oxygen System Functional Test35-10-00-201A/F35

In PackageDUE: 12,632 Hrs1. RE 600 HrsBleed Air Distribution Visual Check - Ducting36-10-00-201A/F36

In PackageDUE: 12,632 Hrs1. RE 600 HrsDownward Opening Passenger/Crew Entrance Door Visual Check o...52-12-00-203A/F52

In PackageDUE: 12,632 Hrs1. RE 600 HrsIgnition System Operational Test - Ignition System74-00-00-204 (Left)A/F74

In PackageDUE: 12,632 Hrs1. RE 600 HrsIgnition System Operational Test - Ignition System74-00-00-204 (Right)A/F74

In PackageDUE: 12,632 Hrs1. RE 600 HrsBallscrew Actuators Lubrication of Ballscrew Actuators and M...78-30-00-218A/F78

In PackageDUE: 12,632 Hrs1. RE 600 HrsCascades/Pylon Tracks Visual Check78-30-11-209A/F78

In PackageDUE: 12,632 Hrs1. RE 600 HrsMain Tracks Visual Check of the main track and attachments78-30-31-210A/F78

In PackageDUE: 12,641.2 Hrs1. RE 600 HrsAir Turbine Starter Air Turbine Starter (ATS) Oil change80-10-11-202 (Left)A/F80

In PackageDUE: 12,641.2 Hrs1. RE 600 HrsAir Turbine Starter Air Turbine Starter (ATS) Oil change80-10-11-202 (Right)A/F80

In PackageDUE: 12,632 Hrs1. RE 600 HrsAir Turbine Starter (Part No. 3505188-9 and Subs) - Detailed...80-10-11-203A/F80


OVD11-Dec-2015-/+19611-Dec-2007Mos

Hrs

Ldg

5 A/F

Also ConsiderDUE: 26-Sep-20181. RE 48 Mos48 Monthly TasksPKG 48 MonthA/F5

In PackageDUE: 11-Dec-20151. RE 96 MosLower Fuselage Skins (External) NDT Check53-30-00-224A/F53

≈29-Dec-2030REPKG 9600 Hour 9600 Hourly Task

05-Aug-2003Mos

7,144.4 Hrs (+40)19,185.6-/+409,6009,585.6Hrs

Ldg

5 A/F

In PackageDUE: 19,185.6 Hrs1. RE 9600 HrsCheck Valves Visual Check of Conditioned Air and Cold Air Ch...21-20-11-203A/F21

In PackageDUE: 19,185.6 Hrs1. RE 9600 HrsCollector Tanks Collector Tank Flapper Check Valves Check28-21-11-212A/F28

In PackageDUE: 19,185.6 Hrs1. RE 9600 HrsWing Anti-Icing Functional Test Wing Anti-Icing30-11-00-202A/F30

In PackageDUE: 19,185.6 Hrs1. RE 9600 HrsTail Cone Visual Check of interior surface, frames, access d...53-50-00-226A/F53

▼ 8 - LEVELING AND WEIGHING.

AMMRE08-10-01-001 Aircraft Weighing and Balancing

1.4 Years18-Aug-20173618-Aug-2014Mos

Hrs

Ldg

8 A/FInspected Date 18-Aug-2014









▼ 11 - PLACARDS AND MARKINGS

RecommendedRE (-)601-0032 Modification - Tires and Airspeed Limitation Placards - 43,100 Pounds Take-off Weight

01-Sep-1983Mos

0Hrs

0Ldg

11 A/FEff: 15-Mar-1984 Complied With

OptionalT (A/R)601-0205 Modification - Flight Compartment Tire Pressure "Caution" Placard - Special Operating Conditions Only

Mos

Hrs

Ldg

11 A/FEff: 05-Oct-1988

OptionalRE (-)601-0280 Modification - Increased MTOW - 44,600 LBS

Mos

Hrs

Ldg

11 A/F

OptionalRE (-)601-0280 Rev 1 Modification - Increased MTOW - 44,600 LBS

Mos

Hrs

Ldg

11 A/F

OptionalRE (-)601-0280 Rev 2 Modification - Increased MTOW - 44,600 LBS

12-Jun-1999Mos

5,934.4Hrs

2,605Ldg

11 A/FEff: 24-Sep-1990 Complied With

OptionalRE (-)601-0360 Modification - Increased MTOW - 45,100 Lbs

Mos

Hrs

Ldg

11 A/F

OptionalRE (-)601-0360 Rev 1 Modification - Increased MTOW - 45,100 Lbs

12-Jun-1999Mos

5,934.4Hrs

2,605Ldg

11 A/FEff: 12-Dec-1990 Complied With

OptionalRE (-)601-0385 Brazilian Registration Requirements - Servicing and Emergency Placards/Cabin Pressure Indication/Overspeed Warning

Mos

Hrs

Ldg

11 A/F

OptionalT (A/R)601-0385 Rev 1 Brazilian Registration Requirements - Servicing and Emergency Placards/Cabin Pressure Indication/Overspeed Warning

Mos

Hrs

Ldg

11 A/FEff: 30-Oct-1998

OptionalT (A/R)601-0467 Modification - Remove MLG Wheel Discs and Add Placard in Flight Compartment

Mos

Hrs

Ldg

11 A/FEff: 30-Nov-1995

OptionalRE (-)601-0511 Modification - Argentinian Certification Requirements

Mos

Hrs

Ldg

11 A/F









OptionalT (A/R)601-0511 Rev 1 Modification - Argentinian Certification Requirements

Mos

Hrs

Ldg

11 A/FEff: 24-Mar-2008

RecommendedRE (-)601-0551 Modification - Fuselage Placards and Markings - Addition of Stow Rod Warning Decal on Upper Core Cowl Door

25-Jul-2008Mos

11,432Hrs

5,881Ldg

11 A/FEff: 30-Aug-2002 Complied With

RecommendedRE (-)601-0552 Special Check/Modification - Wing Placards and Markings - Painted Overwing Anti-Slip Walkway

Mos

Hrs

Ldg

11 A/F

RecommendedT (A/R)601-0552 Rev 1 Special Check/Modification - Wing Placards and Markings - Painted Overwing Anti-Slip Walkway

Mos

Hrs

Ldg

11 A/FEff: 15-Dec-2003

OptionalT (-)601-0638 Stage 4 Noise Levels Standards - Certification

Mos

Hrs

Ldg

11 A/FEff: 29-May-2014

OptionalT (A/R)601-0638 Rev 1 Stage 4 Noise Levels Standards - Certification

Mos

Hrs

Ldg

11 A/FEff: 21-Oct-2015

(AVG MAN HRS: 1) (NOTE: Controlled Effectivity)

RecommendedT (A/R)601-1025 Modification - Engine Cowling - Warning Placard

Mos

Hrs

Ldg

11 A/FEff: 12-Dec-1983

RecommendedRE (-)601-1037 Special Check/Modification - Engine Cowling - Warning Placards

Mos

Hrs

Ldg

11 A/F

RecommendedRE (-)601-1037 Rev 1 Special Check/Modification - Engine Cowling - Warning Placards

26-Jan-1987Mos

1,267Hrs

480Ldg


MandatoryRE (-)85-14-04 Lightning Protection

13-Nov-1992Mos

Hrs

Ldg

11 A/FSB A601-0069Eff: 12-Aug-1985 Complied

With

AlertRE (-)A601-0052 Special Check/Modification - APU - Removal of Restriction

Mos

Hrs

Ldg

11 A/F









AlertRE (-)A601-0052 Rev 1 Special Check/Modification - APU - Removal of Restriction

23-Jan-1985Mos

Hrs

Ldg

11 A/FEff: 02-Nov-1984 Complied With

IsModSumRE (-)IS600-11-0001 REV A Kit - Registration Plate Instl. Pax Door Surround

Mos

Hrs

Ldg

11 A/FEff: 08-Aug-2011

IsModSumT (A/R)IS600-11-0001 REV B Kit - Registration Plate Instl. Pax Door Surround

Mos

Hrs

Ldg

11 A/F

▼ 12 - SERVICING - ROUTINE MAINTENANCE

Servicing - Recommended ≈18-Sep-2016RE12-10-29-301 Hydraulic System Replenishing (No.1, No.2, and No.3 Systems) - Check accumulator charge pressures / Service hydraulic overspill containers

10-Feb-2016Mos

290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs

6,326Ldg

(PKG 300 Hour)

12 A/F

(ZONE: 140, 190, 310) (ACCESS: 144-DZ, 311-BB) (SOURCE: MPD 3.2)

Servicing - Optional ≈18-Sep-2016RE12-10-29-318 Hydraulic System Replenishing (No.1, No.2, and No.3 Systems) - Check reservoir for fluid level

10-Feb-2016Mos

290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs

6,326Ldg

(PKG 300 Hour)

12 A/F

(ZONE: 140, 190, 310) (ACCESS: 144-DZ, 311-BB) (SOURCE: MPD 3.3)

Servicing - Recommended ≈18-Sep-2016RE12-10-32-316 Landing Gear Replenishing - Check main gear shock strut extension

10-Feb-2016Mos

290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs

6,326Ldg

(PKG 300 Hour)

12 A/F

(ZONE: 721, 731) (SOURCE: MPD 3.2)

Servicing - Recommended ≈18-Sep-2016RE12-10-32-317 Landing Gear Replenishing - Check nose gear shock strut extension

10-Feb-2016Mos

290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs

6,326Ldg

(PKG 300 Hour)

12 A/F

(ZONE: 710) (SOURCE: MPD 3.2)

Servicing - Recommended ≈18-Sep-2016RE12-20-00-302 Scheduled Servicing - Lubricate landing gear doors

10-Feb-2016Mos

290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs

6,326Ldg

(PKG 300 Hour)

12 A/F


Servicing - Recommended ≈18-Sep-2016RE12-20-00-303 Scheduled Servicing - Lubricate dual brake control valve push rods

10-Feb-2016Mos

290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs

6,326Ldg

(PKG 300 Hour)

12 A/F

(SOURCE: MPD 3.2)

Servicing - Optional ≈18-Sep-2016RE12-20-00-304 Scheduled Servicing - Lubricate servicing doors / Lubricate baggage compartment door

10-Feb-2016Mos

290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs

6,326Ldg

(PKG 300 Hour)

12 A/F

(ZONE: 100, 200, 812, 815, 824) (ACCESS: 112-BR, 140-FR, 190-DR, 211-AL, 212-AR -BR,) (SOURCE: MPD 3.3) (NOTE: more zone (continued);

311-AL, 312-AR, 815-BL)









Servicing - Recommended ≈18-Sep-2016RE12-20-00-305 Scheduled Servicing - Lubricate main tracks

10-Feb-2016Mos

290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs

6,326Ldg

(PKG 300 Hour)

12 A/F

(ZONE: 410, 420) (ACCESS: 413-AB -AT, 423-AB -AT) (SOURCE: MPD 3.2)

Servicing - Recommended ≈18-Sep-2016RE12-20-00-306 Scheduled Servicing - Lubricate pylon tracks

10-Feb-2016Mos

290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs

6,326Ldg

(PKG 300 Hour)

12 A/F

(ZONE: 410, 420) (ACCESS: 413-AB -AT, 423-AB -AT) (SOURCE: MPD 3.2)

Servicing - Recommended ≈18-Sep-2016RE12-20-00-307 Scheduled Servicing - Lubricate inboard flap vane mechanism

10-Feb-2016Mos

290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs

6,326Ldg

(PKG 300 Hour)

12 A/F

(ZONE: 500, 600) (SOURCE: MPD 3.2)

Servicing - Recommended ≈03-May-2017RE12-20-00-308 Scheduled Servicing - Lubricate BUTE door hinge / Lubricate BUTE door rollers

10-Feb-2016Mos

590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs

6,326Ldg

(PKG 600 Hour)

12 A/F

(ZONE: 500, 600) (Tol. Adjustment: -9.2 Hrs) (SOURCE: MPD 3.2)

Servicing - RecommendedRE12-20-00-309 Scheduled Servicing - Lubricate throttle control inner element and pressure seal

6.6 Months (+31

Days)21-Oct-2016-/+11221-Oct-2015Mos

Hrs

Ldg

(PKG 12 Month)

12 A/F

(ZONE: 200) (ACCESS: 222CZ-DZ) (SOURCE: MPD 3.2)

Servicing - Recommended ≈20-Oct-2017RE12-20-00-311 Scheduled Servicing - Lubricate wing-fuselage pick-up link

29-Oct-2012Mos

812.3 Hrs12,853.51,20011,653.5Hrs

Ldg

(PKG 1200 Hour)

12 A/F

(ZONE: 140, 240) (ACCESS: 140-CL-CR) (SOURCE: MPD 3.2)

Servicing - RecommendedRE12-20-00-312 Scheduled Servicing - Lubricate air driven generator (ADG)

6.6 Months (+31

Days)21-Oct-2016-/+11221-Oct-2015Mos

Hrs

Ldg

(PKG 12 Month)

12 A/F

(ZONE: 112) (ACCESS: 112-AR, 116-AZ) (SOURCE: MPD 3.2)

Servicing - RecommendedRE12-20-00-313 Scheduled Servicing - Lubricate flap actuator

6.6 Months (+31

Days)21-Oct-2016-/+11221-Oct-2015Mos

Hrs

Ldg

(PKG 12 Month)

12 A/F

(ZONE: 500, 600) (SOURCE: MPD 3.2)

Servicing - Recommended ≈25-Sep-2016RE12-20-00-314 Scheduled Servicing - Lubricate variable geometry actuator

10-Feb-2016Mos

300 Hrs (+40)(12,437.4)-/+4030012,137.4Hrs

6,769Enc

(PKG 300 Eng Hour)

12 ENG1

(ZONE: 410, 420) (ACCESS: 412-AB-AT, 414-AB-AT, 422-AB-AT, 424-AB-AT) (SOURCE: MPD 3.2)

Servicing - Recommended ≈25-Sep-2016RE12-20-00-314 Scheduled Servicing - Lubricate variable geometry actuator

10-Feb-2016Mos

300 Hrs (+40)(12,320.4)-/+4030012,020.4Hrs

6,728Enc

(PKG 300 Eng Hour)

12 ENG2

(ZONE: 410, 420) (ACCESS: 412-AB-AT, 414-AB-AT, 422-AB-AT, 424-AB-AT) (SOURCE: MPD 3.2)









Servicing - OptionalRE12-20-00-320 Scheduled Servicing - Lubrication of the Service Door Locks

35 Days11-May-2016611-Nov-2015Mos

Hrs

Ldg

12 A/F

(ZONE: 100, 200, 812, 815) (ACCESS: 112-BR, 140-FR, 190-DR, 211-AL, 212-AR -BR,) (SOURCE: MPD 3.3) (NOTE: more zone (continued); 311-AL,

312-AR, 815-BL)

OptionalT (A/R)601-0147 Modification - Fuel System Replenishing - Level Attitude Indicators

Mos

Hrs

Ldg

12 A/FEff: 08-Jul-1985

OptionalT (A/R)601-0623 Modification – System and Components Replenishing and Hydraulic Power – Introduction of Hydraulic Servicing Placards with Values at Different Ambient

Temperatures

Mos

Hrs

Ldg

12 A/FEff: 04-Mar-2013

▼ 20 - STANDARD PRACTICES – AIRFRAME

MRB ≈03-May-2017RE20-40-00-201 Wire Cables - Flight Controls Wire Cable Inspection (except for straight runs under cabin floor and in vertical stabilizer), paying particular attention to safetying of

turnbuckles and pulleys for freedom of rotation

10-Feb-2016Mos

590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs

6,326Ldg

(PKG 600 Hour)

20 A/F

(Tol. Adjustment: -9.2 Hrs) (SOURCE: TLMC 05-20-15)

MRBRE20-40-00-202 Wire Cables - Flight Controls Wire Cable Inspection (straight runs under cabin floor and invertical stabilizer), paying particular attention to safetying of turnbuckles and

pulleys for freedom of rotation - Check Cable Tensions

5.8 Months (+30

Days)(26-Sep-2016)-/+16024-Oct-2011Mos

Hrs

Ldg

(PKG 60 Month)

20 A/F

(SOURCE: TLMC 05-20-15)

MRBRE20-40-00-203 Wire Cables - Flight Controls Visual Check (using a borescope) of Flight Control Cables located below Toilet/Galley areas (without removal), paying particular attention

to corrosion of cables

6.6 Months (+31

Days)(21-Oct-2016)-/+11221-Oct-2015Mos

Hrs

Ldg

(PKG 12 Month)

20 A/F


RecommendedT (A/R)601-0561 Special Check/Rework - Wiring - Possible Chafing on Electrical Harness Located on the APU Support Structure

Mos

Hrs

Ldg

20 A/FEff: 31-Oct-2003

▼ 21 - AIR CONDITIONING AND PRESSURIZATION

RE (O/C)2 Inch Check Valve

20-Sep-1983Mos

0Hrs0

0Ldg0

Left21 A/FNew3202062-1-1

UNKNOWN

RE (O/C)2 Inch Check Valve

20-Sep-1983Mos

0Hrs0

0Ldg0

Right21 A/FNew3202062-1-1

UNKNOWN









RE (O/C)3 Inch Backup Valve

20-Sep-1983Mos

0Hrs

0Ldg

Left21 A/FUnknownUnknown

RE (O/C)3 Inch Shutoff (Emerg Ram Air) Valve

20-Sep-1983Mos

0Hrs0

0Ldg0

21 A/FNew398724-1-1

UNKNOWN

RE (O/C)AC (LIRS) Blower

20-Sep-1983Mos

0Hrs

0Ldg

No.121 A/FUnknownUnknown

RE (O/C)AC (LIRS) Blower

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Air Pressure Regulator

20-Sep-1983Mos

0Hrs0

0Ldg0

21 A/FNew131402-2

UNKNOWN

RE (O/C)Balancing - 4 Inch Valve

20-Sep-1983Mos

0Hrs0

0Ldg0

Left21 A/FNew600-95278-1

UNKNOWN

RE (O/C)Balancing - 4 Inch Valve

20-Sep-1983Mos

0Hrs0

0Ldg0


UNKNOWN

RE (O/C)Cabin Pressure Controller

20-Sep-1983Mos

0Hrs0

0Ldg0

21 A/FNew2117804-2

UNKNOWN

RE (O/C)Cabin Pressure Indicator

20-Sep-1983Mos

0Hrs0

0Ldg0

21 A/FNew600-59117-7

UNKNOWN

RE (O/C)Cabin Pressure Selector

20-Sep-1983Mos

0Hrs0

0Ldg0

21 A/FNew2117598-3

UNKNOWN

RE (O/C)Cabin Temperature Indicator

20-Sep-1983Mos

0Hrs0

0Ldg0

21 A/FNew115-079

UNKNOWN









RE (O/C)Check Valve

20-Sep-1983Mos

0Hrs0

0Ldg0

No.121 A/FNew123790-1-1

UNKNOWN

RE (O/C)Check Valve

20-Sep-1983Mos

0Hrs0

0Ldg0

No.221 A/FNew3202062-1-1

UNKNOWN

RE (O/C)Check Valve

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Control Unit Air Conditioning ECU

20-Sep-1983Mos

0Hrs0

0Ldg0

No.121 A/FNew2201600-4

UNKNOWN

RE (O/C)Control Unit Air Conditioning ECU

20-Sep-1983Mos

0Hrs0

0Ldg0

No.221 A/FNew2201600-4

UNKNOWN

RE (O/C)Cooling Turbine

20-Sep-1983Mos

0Hrs0

0Ldg0

Left21 A/FNew586110-3

UNKNOWN

RE (O/C)Cooling Turbine

09-Jul-2003Mos

9,566.9Hrs

4,786Ldg

Right21 A/F586110-374-2703

RE (O/C)Diverter Valve

20-Sep-1983Mos

0Hrs0

0Ldg0

21 A/FNew228565-1

UNKNOWN

RE (O/C)Duct Temperature Sensor

20-Sep-1983Mos

0Hrs

0Ldg



20-Sep-1983Mos

0Hrs

0Ldg



20-Sep-1983Mos

0Hrs

0Ldg











20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Ejector Shutoff Valve

20-Sep-1983Mos

0Hrs0

0Ldg0

Left21 A/FNew979142-1-1

UNKNOWN

RE (O/C)Ejector Shutoff Valve

20-Sep-1983Mos

0Hrs0

0Ldg0


UNKNOWN

RE (O/C)Fan Sensor

10-Nov-2004Mos

10,467.3Hrs

5,311Ldg

Cabin21 A/F625692-20470-483

RE (O/C)Fan Sensor

20-Sep-1983Mos

0Hrs0

0Ldg0

Cockpit21 A/FNew625692-2

UNKNOWN

RE (O/C)Low Limit Temperature Control Unit

20-Sep-1983Mos

0Hrs0

0Ldg0


UNKNOWN

RE (O/C)Low Limit Temperature Control Unit

20-Sep-1983Mos

0Hrs0

0Ldg0

Right21 A/FNew625520-2

UNKNOWN

RE (O/C)Modulating/Shutoff Valve

21-Feb-2002Mos

8,126.5Hrs

3,910Ldg

Left21 A/F979558-8976

RE (O/C)Modulating/Shutoff Valve

20-Sep-1983Mos

0Hrs0

0Ldg0


UNKNOWN

RE (O/C)Motor Driven Fan

20-Sep-1983Mos

0Hrs0

0Ldg0

21 A/FNew605385-6-1

UNKNOWN

RE (O/C)Pressure Regulating Primary Valve

29-Jul-2004Mos

10,458.3Hrs

5,306Ldg

21 A/F103632-2102-362









RE (O/C)Pressure Regulating Secondary Valve

29-Jul-2004Mos

10,458.3Hrs

5,306Ldg

21 A/F103664-136-446

RE (O/C)Pressure Regulating Shutoff Valve

25-Jul-2008Mos

11,432Hrs

5,881Ldg

Left21 A/F228845UNKNOWN


20-Sep-1983Mos

0Hrs

0Ldg

Right21 A/FUnknownUnknown

RE (O/C)Pressure Regulating Valve

20-Sep-1983Mos

0Hrs

0Ldg



20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Regulating Valve

20-Sep-1983Mos

0Hrs

0Ldg

21 A/FUnknownUnknown

RE (O/C)Temperature Control

20-Sep-1983Mos

0Hrs

0Ldg



20-Sep-1983Mos

0Hrs0

0Ldg0

No.121 A/FNew625514-2-1

UNKNOWN


20-Sep-1983Mos

0Hrs0

0Ldg0

No.221 A/FNew625514-2-1

UNKNOWN

RE (O/C)Temperature Limiter Valve

20-Sep-1983Mos

0Hrs0

0Ldg0

No.121 A/FNew129580-6

UNKNOWN

RE (O/C)Temperature Limiter Valve

20-Sep-1983Mos

0Hrs0

0Ldg0

No.221 A/FNew129580-6

UNKNOWN









RE (O/C)Torque Motor

20-Sep-1983Mos

0Hrs0

0Ldg0

No.121 A/FNew124904-1-1

UNKNOWN

RE (O/C)Torque Motor

20-Sep-1983Mos

0Hrs0

0Ldg0

No.221 A/FNew124904-1-1

UNKNOWN

RE (O/C)Upper ACU Thermal Switch

20-Sep-1983Mos

0Hrs0

0Ldg0


UNKNOWN

RE (O/C)Upper ACU Thermal Switch

20-Sep-1983Mos

0Hrs0

0Ldg0


UNKNOWN

MRB ≈03-May-2017RE21-20-00-201 Distribution Visual Check of accessible Air Conditioning Plumbing and Ducting, paying particular attention to: (1) Discoloration of insulation tubes and condensation in

the tube area which may indicate leakage / (2) The ram air intake and exhausts for F.O.D. and cracks / (3) Air Conditioning ducts and connections under the cockpit

floor

10-Feb-2016Mos

590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs

6,326Ldg

(PKG 600 Hour)

21 A/F


MRB ≈13-Jul-2017RE21-20-11-202 Check Valves Check Valve inspection

04-May-2004Mos

684 Hrs (+30)(12,725.2)-/+402,40010,325.2Hrs

Ldg

(PKG 2400 Hour)

21 A/F

(SOURCE: TLMC 05-20-15) (NOTE: (Footwarmer/Demist Manifold Check Valve Only))

MRB ≈29-Dec-2030RE21-20-11-203 Check Valves Visual Check of Conditioned Air and Cold Air Check Valves forinternal condition

05-Aug-2003Mos

7,144.4 Hrs (+40)(19,185.6)-/+409,6009,585.6Hrs

Ldg

(PKG 9600 Hour)

21 A/F

(SOURCE: TLMC 05-20-15) (NOTE: The inspection criteria for the “Check Valve Inspection” in the Maintenance Manual are equally applicable to

these valves.)

MRB ≈03-May-2017RE21-30-00-204 Pressurization Control Operational Test of Emergency Pressurization System

10-Feb-2016Mos

590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs

6,326Ldg

(PKG 600 Hour)

21 A/F


MRB ≈03-May-2017RE21-30-00-205 Pressurization Control Operational Test of Emergency Depressurization Control System

10-Feb-2016Mos

590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs

6,326Ldg

(PKG 600 Hour)

21 A/F


MRB ≈13-Jul-2017RE21-30-00-206 Pressurization Control Cabin Low Pressure Warning System Operational Check

24-Feb-2005Mos

684 Hrs (+30)(12,725.2)-/+402,40010,601.2Hrs

Ldg

(PKG 2400 Hour)

21 A/F










MRB ≈13-Jul-2017RE21-30-00-207 Pressurization Control Operational Test of Manual Pressurization Control System - Operational Test of Jet Pump Right Bleed Air Check Valve - Operational Test of Jet

Pump Left Bleed Air Check Valve

04-May-2004Mos

684 Hrs (+30)(12,725.2)-/+402,40010,325.2Hrs

Ldg

(PKG 2400 Hour)

21 A/F


MRB ≈20-Oct-2017RE21-30-11-208 Outflow Valves Outflow valve Functional Test (Using Pressure Test Kit) - Visual Check, paying particular attention to valve seat; (1) Alt Limit Control Poppet Mechanism

/ (2) Overpressure Limiter / (3) Negative Pressure Relief

29-Oct-2012Mos

812.3 Hrs (+40)(12,853.5)-/+401,20011,653.5Hrs

Ldg

(PKG 1200 Hour)

21 A/F


Servicing - Recommended ≈03-May-2017RE21-30-11-301 Outflow Valves - Remove and install new filter element

10-Feb-2016Mos

590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs

6,326Ldg

(PKG 600 Hour)

21 A/F

(Tol. Adjustment: -9.2 Hrs) (SOURCE: MPD 3.2)

MRBRE (N/A)21-51-31-209 Air Conditioning Overheat Switch (A/C 3001 to 3059 Post SB 601-0141, A/C 3060 to 3990) - Functional Test of overheat warning

Mos

Hrs

Ldg

21 A/F


MRB ≈03-May-2017RE21-53-11-210 Emergency Ram Air Shutoff Valve Functional Test Emergency Ram Air Shutoff Valve

10-Feb-2016Mos

590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs

6,326Ldg

(PKG 600 Hour)

21 A/F


Servicing - Optional ≈03-May-2017RE21-70-11-302 Water Separator - Clean coalescer bag

10-Feb-2016Mos

590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs

6,326Ldg

(PKG 600 Hour)

21 A/F

(ZONE: 311, 312) (ACCESS: 311-BB) (Tol. Adjustment: -9.2 Hrs) (SOURCE: MPD 3.3)

OptionalT (A/R)601-0141 Modification - Conditioned Air Ducting - Thermoswitch Addition

Mos

Hrs

Ldg

21 A/FEff: 29-Jan-1987

RecommendedRE (-)601-0151 Modification - Cabin Air and Anti-Ice Ducts - Connections

Mos

Hrs

Ldg

21 A/F

RecommendedRE (-)601-0151 Rev 1 Modification - Cabin Air and Anti-Ice Ducts - Connections

Mos

Hrs

Ldg

21 A/F

RecommendedRE (-)601-0151 Rev 2 Modification - Cabin Air and Anti-Ice Ducts - Connections

27-Jan-1987Mos

0Hrs

Ldg










RecommendedRE (-)601-0197 Emergency Pressurization Shut-Off Valve - Wire Protection

01-Dec-1990Mos

3,058.6Hrs

1,212Ldg


RecommendedRE (-)601-0241 Modification - RAM Air Duct - Insulation Addition

Mos

Hrs

Ldg

21 A/F

RecommendedRE (-)601-0241 Rev 1 Modification - RAM Air Duct - Insulation Addition

28-Mar-1989Mos

2,373Hrs

910Ldg

21 A/FEff: 04-May-1988 Complied With

OptionalT (A/R)601-0282 Modification - Ground Cooling Fan - Addition of Spacer

Mos

Hrs

Ldg

21 A/FEff: 21-Feb-1989

RecommendedRE (-)601-0310 Modification - Air Conditioning Unit (ACU) - Introduction of Water Extractor

Mos

Hrs

Ldg

21 A/F

RecommendedRE (-)601-0310 Rev 1 Modification - Air Conditioning Unit (ACU) - Introduction of Water Extractor

Mos

Hrs

Ldg

21 A/F

RecommendedRE (-)601-0310 Rev 2 Modification - Air Conditioning Unit (ACU) - Introduction of Water Extractor

14-Oct-1992Mos

Hrs

Ldg

21 A/FEff: 10-Jan-1992 Complied With

OptionalRE (-)601-0323 Modification - Temperature Control - Duct Temperature Sensors

Mos

Hrs

Ldg

21 A/F

OptionalT (A/R)601-0323 Rev 1 Modification - Temperature Control - Duct Temperature Sensors

Mos

Hrs

Ldg

21 A/FEff: 30-Aug-1990

RecommendedT (A/R)601-0369 Modification - Water Extractor Drain Hoses - Addition of Clamps and Inline Restrictors

Mos

Hrs

Ldg

21 A/FEff: 10-Jan-1992

RecommendedRE (-)601-0375 Modification - Air Conditioning Unit (ACU) Ducts - Prevention of Connector Separation

Mos

Hrs

Ldg

21 A/FEff: 20-Mar-1992









RecommendedRE (-)601-0442 Special Check/Rework - Pressurization - Outflow Valve - Diaphragm

28-Apr-1995Mos

4,555Hrs

1,824Ldg

21 A/FEff: 15-Feb-1995 Complied With

OptionalT (A/R)601-0448 Modification - Cockpit Air Conditioned - Ducts Replacement Below the Side Consoles

Mos

Hrs

Ldg

21 A/FEff: 29-Feb-1996

OptionalRE (-)601-0450 Modification - Air Conditioning Units (ACU) - ACUs Inhibit During Either Engine Start

12-Nov-1997Mos

5,395Hrs

2,274Ldg

21 A/FComplied With

OptionalT (A/R)601-0450 Rev 1 Modification - Air Conditioning Units (ACU) - ACUs Inhibit During Either Engine Start

Mos

Hrs

Ldg

21 A/FEff: 28-Mar-2002

RecommendedT (A/R)601-0505 Special Check/Rework - Pressurization Control - Check Valves, Part No. 2770080-102 Installation

Mos

Hrs

Ldg

21 A/FEff: 29-May-1998

Nextdue Share EarliestDUE:1. T A/R | 2. RE -Special Check/Rework - Pressurization Control - Check Valves...601-0505 Part AA/F21

Nextdue Share EarliestDUE:1. T A/R | 2. RE -Special Check/Rework - Pressurization Control - Check Valves...601-0505 Part BA/F21

RecommendedRE (-)601-0505 Part A Special Check/Rework - Pressurization Control - Check Valves, Part No. 2770080-102 Installation - Special Check

05-Nov-1998Mos

5,824Hrs

2,521Ldg


RecommendedT (A/R)601-0505 Part B Special Check/Rework - Pressurization Control - Check Valves, Part No. 2770080-102 Installation - Rework

Mos

Hrs

Ldg

21 A/FEff: 29-May-1998

OptionalT (A/R)601-0518 Modification - Temperature Control - Prevention of Ice Formation Downstream of Air Conditioning Units (ACU)

Mos

Hrs

Ldg

21 A/FEff: 31-Jan-2001

RecommendedT (A/R)601-0533 Modification - Air Conditioning Units - Replacement of Existing Relays K2000HG and K2001HG With 5 Second Delay Relays

Mos

Hrs

Ldg

21 A/FEff: 28-Feb-2002

RecommendedRE (-)601-0607 Special Check/Rework – Corrosion Prevention – ACU Exhaust Duct Flange & Fuselage Skin Mating Surfaces

Mos

Hrs

Ldg

21 A/F









RecommendedRE (-)601-0607 Rev 1 Special Check/Rework – Corrosion Prevention – ACU Exhaust Duct Flange & Fuselage Skin Mating Surfaces

Mos

Hrs

Ldg

21 A/F

RecommendedT (A/R)601-0607 Rev 2 Special Check/Rework – Corrosion Prevention – ACU Exhaust Duct Flange & Fuselage Skin Mating Surfaces

Mos

Hrs

Ldg

21 A/FEff: 24-Jul-2015

AlertRE (-)A601-0016 Modification - Cabin Air Duct - Support Clamps

Mos

Hrs

Ldg

21 A/FEff: 25-Jul-1983

▼ 22 - AUTOFLIGHT

RE (O/C)Autopilot Computer

15-May-2004Mos

10,352.6Hrs

5,241Ldg

22 A/F4029377-91184080661

RE (O/C)Autopilot Controller

16-Nov-2001Mos

7,861.9Hrs

3,759Ldg

22 A/F4018639-904C80030161

RE (O/C)Autopilot-Status Controller

26-Mar-2007Mos

11,045.9Hrs

5,659Ldg

22 A/F4031474-90385020542

RE (O/C)Duplex Aileron Servo

25-Jul-2008Mos

11,432Hrs

5,881Ldg

22 A/F4015373-71381070567

RE (O/C)Duplex Elevator Servo

25-Jul-2008Mos

11,432Hrs

5,881Ldg

22 A/F4015373-71680090415

RE (O/C)Linear Yaw Damper Actuator

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Linear Yaw Damper Actuator

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Roll Rate Monitor

20-Sep-1983Mos

0Hrs0

0Ldg0

Left22 A/FNew4015901-921

UNKNOWN









RE (O/C)Roll Rate Monitor

20-Sep-1983Mos

0Hrs0

0Ldg0


UNKNOWN

RE (O/C)Stability Augmentation Computer

18-Dec-2014Mos

11,854.6Hrs

Ldg

22 A/F4031475-80585040359

MRB ≈03-May-2017RE22-10-00-201 Autopilot System (Post SB 601-0048 and A/C 3022 to 3066) - Roll Rate Monitors Operational Test

10-Feb-2016Mos

590.8 Hrs (+40)12,632-/+4060012,041.2Hrs

6,326Ldg

22 A/F


RecommendedRE (-)601-0048 Modification - Autopilot System - Aileron Channel

Mos

Hrs

Ldg

22 A/F

RecommendedRE (-)601-0048 Rev 1 Modification - Autopilot System - Aileron Channel

30-Jan-1987Mos

Hrs

Ldg

22 A/FEff: 10-Jun-1984 Complied With

RecommendedRE (-)601-0125 Modification - Auto Pilot System - A.F.C.S. Light

28-Mar-1989Mos

2,373Hrs

910Ldg

22 A/FEff: 03-Jul-1986 Complied With

OptionalRE (-)601-0143 Modification - Automatic Flight Control System - Improvements

Mos

Hrs

Ldg

22 A/F

OptionalRE (-)601-0143 Rev 1 Modification - Automatic Flight Control System - Improvements

26-Jan-1987Mos

1,267Hrs

480Ldg


OptionalT (A/R)601-0166 Modification - Autopilot/Vert Nav Valid Lines - Protection

Mos

Hrs

Ldg

22 A/FEff: 24-Mar-1986

RecommendedRE (-)601-0276 Modification - Flight Guidance Computers - Replacement

Mos

Hrs

Ldg

22 A/F

OptionalT (A/R)601-0403 Modification - Dual-Channel Synchro-Transmitter - Replacement

Mos

Hrs

Ldg

22 A/FEff: 15-Jan-1997









RecommendedRE (-)601-0411 Special Check/Rework/Modification - Autopilot System - Wire Splices, Ground Studs and Flight Guidance Computer

Mos

Hrs

Ldg

22 A/F

RecommendedRE (-)601-0570 Modification - General - Conversion of Servo Drive Assemblies from Part No. 4015373-813 and -816 to Part No. 4015373-713 and -716 to Ensure Retention of Clutch

Screws

25-Jul-2008Mos

11,432Hrs

5,881Ldg


▼ 23 - COMMUNICATIONS

RE (O/C)Audio Amplifier

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Audio Amplifier Filter

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Audio Panel

20-Sep-1983Mos

0Hrs

0Ldg

Copilot23 A/FUnknownUnknown

RE (O/C)Audio Panel

04-Mar-2015Mos

11,879.4Hrs

6,207Ldg

Pilot23 A/FM1045-MLAL-GFE7840355 REPAIR

RE (O/C)Audio Unit

16-Nov-2001Mos

7,861.9Hrs

3,759Ldg

23 A/F990-6800-00100120010799

RE (O/C)Cockpit Voice recorder (CVR)

20-Sep-1983Mos

0Hrs0

0Ldg0

23 A/FNewUNKNOWN

UNKNOWN

Assembly SubDUE: 04-Mar-20211. RE DueCockpit Voice Recorder (CVR) Underwater Locating DeviceDK120 / SD40876A/F23

Life LimitRE (Due)Cockpit Voice Recorder (CVR) Underwater Locating Device

4.9 Years04-Mar-202104-Mar-2015Mos

Hrs

Ldg

23 A/F

Expiration Date 04-Mar-2021

DK120SD40876

RE (O/C)Com-2/Nav-2 Controller

20-Sep-1983Mos

0Hrs

0Ldg










RE (O/C)CVR Inertia Switch

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Handset

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)HF Coupler/PWR Amplifier

26-Sep-2006Mos

10,897.5Hrs

5,558Ldg

No.123 A/F064-1017-0211990

RE (O/C)HF Coupler/PWR Amplifier

19-Dec-2003Mos

9,982.2Hrs

5,021Ldg

No.223 A/F064-1017-0210725

RE (O/C)HF Receiver/Transmitter

26-Sep-2006Mos

10,897.5Hrs1,622.8

5,558Ldg941

No.123 A/FOverhauled064-1015-01

32389

RE (O/C)HF Receiver/Transmitter

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)VHF Antenna

20-Sep-1983Mos

0Hrs0

0Ldg0

No.123 A/FNewS65-8280

UNKNOWN

RE (O/C)VHF Antenna

25-Jul-2008Mos

11,432Hrs

5,881Ldg

No.223 A/FS65-8280-102799

RE (O/C)VHF Communications Control

15-Apr-2003Mos

9,393.4Hrs

4,682Ldg

No.123 A/F822-1120-0056540


06-Aug-2002Mos

8,695.2Hrs

4,260Ldg

No.223 A/F822-1120-00518010


20-Sep-1983Mos

0Hrs

0Ldg










RE (O/C)VHF Transceiver

08-Nov-2003Mos

9,866.8Hrs

4,961Ldg

No.123 A/F822-1113-00135906


30-Oct-2003Mos

9,838.7Hrs

4,941Ldg

No.223 A/F822-1113-001UNKNOWN


20-Sep-1983Mos

0Hrs

0Ldg


MandatoryRE (-)2005-11-04 Microphone jack assemblies.

25-Jul-2008Mos

11,432Hrs

5,881Ldg

23 A/FEff: 27-May-2005 Not Applicable

MRB ≈20-Oct-2017RE23-60-00-201 Static Dischargers Visual Check - Static Dischargers Functional Test

29-Oct-2012Mos

812.3 Hrs (+40)(12,853.5)-/+401,20011,653.5Hrs

Ldg

(PKG 1200 Hour)

23 A/F


MRBRE23-60-00-203 Nose-Radome Lightning Strips Functional Test

2.5 Years (+30 Days)(26-Sep-2018)-/+14826-Sep-2014Mos

Hrs

Ldg

(PKG 48 Month)

23 A/F


Custom TaskRE23-CUS-003 Cockpit Voice Recorder ULB Battery - Check

11.1 Months04-Mar-20172404-Mar-2015Mos

11,879.4Hrs

6,207Ldg

23 A/F

RecommendedRE (-)601-0281 Modification - Audio Electronic Unit (AEU) - Cockpit Voice Recorder (CVR) Audio Levels

Mos

Hrs

Ldg

23 A/F

RecommendedRE (-)601-0281 Rev 1 Modification - Audio Electronic Unit (AEU) - Cockpit Voice Recorder (CVR) Audio Levels

Mos

Hrs

Ldg

23 A/F

RecommendedRE (-)601-0383 Modification - HF Communications System - Introduction of Improved Fiber-Optic Cables

Mos

Hrs

Ldg

23 A/F

OptionalT (A/R)601-0390 Modification - Audio Electronic Unit (AEU) - Cockpit Voice Recorder (CVR) Continuous Recording (”Hot Mic") Capability

Mos

Hrs

Ldg

23 A/FEff: 06-Sep-1991









RecommendedRE (-)601-0405 Modification - Fuel Tank Water Drains - Improved Protective Finish

Mos

Hrs

Ldg

23 A/F

RecommendedRE (-)601-0405 Rev 1 Modification - Fuel Tank Water Drains - Improved Protective Finish

26-Jan-1996Mos

4,785Hrs

1,932Ldg


OptionalT (A/R)601-0486 Modification - Interphone - Addition of Shock Mounts to Ground Crew Interphone Unit

Mos

Hrs

Ldg

23 A/FEff: 15-Nov-1996

▼ 24 - ELECTRICAL POWER

AWL - Life LimitREADG Uplock Actuator Assy (Squib)

2.6 Years01-Nov-20186001-Nov-2013Mos

11,854.6Hrs

Ldg

24 A/F

Manufactured Date 01-Nov-2013

055046B575 11/2013

(NOTE: NOTE:Life limit is 60 months from date of manufacture or 42 months from date of installation whichever comes first.)

Component Inspection SimpleDUE: 18-Jun-20181. RE 42 MosADG Uplock Actuator Assy (Squib) - In Service Limit05-10-20A/F24

RE (O/C)Air Driven Gen Auto Deploy Controller

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Air Driven Generator (ADG)

23-Feb-2003Mos

9,253.9Hrs

4,606Ldg

24 A/F720848-A0552

RE (O/C)Air Driven Generator Control

19-Apr-2002Mos

8,358.5Hrs

4,045Ldg

24 A/F72831081113

RE (O/C)Air Driven Generator Eject Jack

20-Sep-1983Mos

0Hrs0

0Ldg0

24 A/FNew728431B

UNKNOWN

RE (O/C)Air Driven Turbine Assy

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)AMPS-500 Battery

21-Nov-2004Mos

10,477.5Hrs

5,321Ldg

No.124 A/F171BS101-1079










20-Sep-1983Mos

0Hrs

0Ldg



20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)APU Generator Control Unit (GCU)

20-Sep-1983Mos

0Hrs0

0Ldg0

24 A/FNew720846B

UNKNOWN

RE (O/C)Battery Charger

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Fan Cooled (TRU) Converter

20-Sep-1983Mos

0Hrs0

0Ldg0

No.124 A/FNewMS17976-2

UNKNOWN


20-Sep-1983Mos

0Hrs0

0Ldg0

No.224 A/FNewMS17976-2

UNKNOWN


21-Nov-2002Mos

9,021.9Hrs

4,466Ldg

No.324 A/F28V550Y3573A

RE (O/C)Frequency/Voltage Sensor

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Generator Contactor

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Generator Control Unit (GCU)

16-Nov-2003Mos

9,901.1Hrs

4,981Ldg

No.124 A/F720846B0884

RE (O/C)Generator Control Unit (GCU)

20-Sep-1983Mos

0Hrs0

0Ldg0

No.224 A/FNew720846B

UNKNOWN









RE (O/C)Hand Air Driven Generator Pump

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Heat IDG Exchanger

20-Sep-1983Mos

0Hrs0

0Ldg0

No.124 A/FNew24E26-1

UNKNOWN

RE (O/C)Heat IDG Exchanger

20-Sep-1983Mos

0Hrs0

0Ldg0

No.224 A/FNew24E26-1

UNKNOWN

RE (O/C)IDG Generator

15-Sep-2007Mos

11,184.3Hrs

5,748Ldg

No.124 A/F720845E537

RE (O/C)IDG Generator

15-Sep-2007Mos

11,184.3Hrs

5,748Ldg

No.224 A/F720845E0740

RE (O/C)IRS Battery

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Main Battery

28-Mar-2014Mos

11,824.5Hrs

6,169Ldg

24 A/F9750W05383060W0020

RE (O/C)Monitor - External Power Relay

20-Sep-1983Mos

0Hrs

0Ldg


AWL - Life LimitRE05-10-20 ADG Uplock Actuator Assy (Squib) - In Service Limit

2.2 Years18-Jun-20184218-Dec-2014Mos

11,854.6Hrs

Ldg

24 A/F055046B575 11/2013

(NOTE: NOTE:Life limit is 60 months from date of manufacture or 42 months from date of installation whichever comes first.)

MandatoryRE (-)2009-23-09 Electrical power

22-Mar-2012Mos

11,578.6Hrs

6,004Ldg

24 A/FSB 601-0591Eff: 14-Dec-2009 Complied

With

Compliance Share DoubleDUE:1. T A/R | 2. RE -Special Check/Modification – Air-Driven Generator System – R...601-0591A/F24









Mandatory ≈27-Nov-2016T2015-25-05 Detect and Correct Broken Support Brackets of the Hydraulic Lines - Perform a One Time Detailed Inspection of the IDG Power Cables

1.3 Years28-Jul-201718Mos

382.67 Hrs≈12,423.87400Hrs

Ldg

24 A/FEff: 28-Jan-2016

Compliance Share DoubleDUE: 12,039.2 Hrs1. T 400 Hrs | 2. RE -Special Check/Rework – Integrated Drive Generator (IDG) and ...601-0625 Rev 1A/F24

Servicing - RecommendedRE24-00-00-301 Battery System - Operational Test (Cycling) of the Thermal Circuit Breakers

6.6 Months (+31

Days)21-Oct-2016-/+11221-Oct-2015Mos

Hrs

Ldg

(PKG 12 Month)

24 A/F

(ZONE: 221, 223, 232, 311) (SOURCE: MPD 3.2)

MRB ≈03-May-2017RE24-20-00-201 AC Generation Functional Test - Complete Generator System

10-Feb-2016Mos

590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs

6,326Ldg

(PKG 600 Hour)

24 A/F


MRB ≈18-Sep-2016RE24-21-00-202 Integrated Drive Generator System Differential Pressure Check

10-Feb-2016Mos

290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs

6,326Ldg

(PKG 300 Hour)

24 A/F


Servicing - Recommended ≈18-Sep-2016RE24-21-00-301 Integrated Drive Generator Oil System Replenishing - Replenishing

10-Feb-2016Mos

290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs

6,326Ldg

(PKG 300 Hour)

24 A/F

Ref Ch.5:12-11-24 (ZONE: 410, 412) (ACCESS: 412-AB, 422-AB) (SOURCE: MPD 3.2)

MRB ≈13-Jul-2017RE24-21-16-204 IDG Oil-in Filter Assembly Remove, inspect and install new filter element

04-May-2004Mos

684 Hrs (+30)(12,725.2)-/+402,40010,325.2Hrs

Ldg

(PKG 2400 Hour)

24 A/F


MRB ≈13-Jul-2017RE24-21-21-205 IDG Oil-out Filter Assembly Remove, inspect and install new filter element

04-May-2004Mos

684 Hrs (+30)(12,725.2)-/+402,40010,325.2Hrs

Ldg

(PKG 2400 Hour)

24 A/F


MRB ≈15-Feb-2019RE24-22-00-206 Auxiliary Generator System GTCP36-100 APU (Pre SB 601-0568 or SB 601-0581) - Roll Rate Monitors Operational Test

08-Aug-2005Mos

1,520 Hrs (+40)9,379-/+402,4006,979Hrs

APUS

24 APU1


MRB ≈03-Apr-2016RE24-22-00-214 Auxiliary Generator System - APU Generator Adaptor Dry Cavity - Drain Oil

10-Jan-2008Mos

145 Hrs (+40)8,004-/+404007,604Hrs

APUS

24 APU1

(SOURCE: TLMC 05-20-15) (NOTE: • GTCP36-100 APU (P/N 722882B and subsequent) and/or)

MRB ≈15-Feb-2019RE24-22-16-207 APU Generator Adapter Filter Element - Remove, inspect and install new filter element

08-Aug-2005Mos

1,520 Hrs (+40)9,379-/+402,4006,979Hrs

APUS

24 APU1










MRBRE24-23-00-208 Air Driven Generator System Oil level check- Oil leakage check

15 Days (+30)21-Apr-2016-/+1621-Oct-2015Mos

Hrs

Ldg

24 A/F

(SOURCE: TLMC 05-20-15) (NOTE: The checks in section 5-50-09 of this manual apply immediately after any in-flight deployment of the ADG,

including the annual operational test. The checks aboveare to be carried out 6 months after the last in-flightdeployment)

MRBRE24-23-00-209 Air Driven Generator System Operational Test - ADG

10 Months (+29

Days)(30-Jan-2017)-/+12430-Jan-2015Mos

Hrs

Ldg

(PKG 24 Month)

24 A/F


MRBRE24-23-46-210 ADG Auto-Deploy Control Unit Operational Test - ADG Auto-Deploy Control Unit

6.6 Months (+31

Days)(21-Oct-2016)-/+11221-Oct-2015Mos

Hrs

Ldg

(PKG 12 Month)

24 A/F


MRB ≈03-May-2017RE24-31-00-211 DC Static Conversion System Functional Test

10-Feb-2016Mos

590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs

6,326Ldg

(PKG 600 Hour)

24 A/F


MRBRE24-33-00-212 Battery System - Battery Capacity and Electrolyte Check

1 Year23-Apr-201755021-Oct-2015Days

3,959.9 Hrs16,001.14,00012,001.1Hrs

6,291Ldg

24 A/F

Ref.:CMM/PSP 608/608A 24-30-99 or 24-32-05 (SOURCE: TLMC 05-20-15)

MRBRE24-33-00-213 Battery System Functional Test - Main Battery Charger Thermal Sensor

6.6 Months (+31

Days)(21-Oct-2016)-/+11221-Oct-2015Mos

Hrs

Ldg

(PKG 12 Month)

24 A/F


Servicing - Recommended ≈26-Jun-1985RE24-33-00-302 Battery System - Visual check of battery, paying particular attention to cells, case and vent system for deposits, leakage and corrosion

Mos

OVD100-/+40100Hrs

Ldg

24 A/F


OptionalRE (-)601-0107 Modification - DC Power Generation - TRU 3 Replacement

Mos

Hrs

Ldg

24 A/F

OptionalT (A/R)601-0107 Rev 1 Modification - DC Power Generation - TRU 3 Replacement

Mos

Hrs

Ldg

24 A/FEff: 02-May-1986

RecommendedRE (-)601-0198 Modification - Air Driven Generator - Manual Release Handle

15-Apr-1988Mos

1,995Hrs

756Ldg










RecommendedRE (-)601-0302 Special Check/Rectification - Battery Connector - Wire Connections

28-Mar-1989Mos

2,373Hrs

910Ldg


RecommendedRE (-)601-0322 Modification - ADG Restow Pump - Addition of Warning Placard

21-Feb-1991Mos

3,142Hrs

1,250Ldg


RecommendedRE (-)601-0356 Modification - Main Battery and AFT Equipment Bay - Venting and Drainage

Mos

Hrs

Ldg

24 A/F

RecommendedRE (-)601-0356 Rev 1 Modification - Main Battery and AFT Equipment Bay - Venting and Drainage

Mos

Hrs

Ldg

24 A/F


Mos

Hrs

Ldg

24 A/F


26-Jan-1995Mos

Hrs

Ldg


RecommendedRE (-)601-0422 Special Check/Rework - Junction Box No. 5 (JB5) - Terminal Block Pin Sizes

30-Sep-1994Mos

4,399Hrs

1,768Ldg


RecommendedRE (-)601-0428 Special Check/Rework - Shielded Wire - Wire Insulation

Mos

Hrs

Ldg

24 A/F

RecommendedRE (-)601-0428 Rev 1 Special Check/Rework - Shielded Wire - Wire Insulation

26-Jan-1996Mos

4,785Hrs

1,932Ldg


RecommendedRE (-)601-0430 Special Check and Modification - Air Driven Generator - Uplock Assembly Replacement

30-Sep-1994Mos

4,399Hrs

1,768Ldg

24 A/FEff: 25-Apr-1994 Complied With

OptionalT (A/R)601-0445 Modification - Air-Driven Generator (ADG) System - Ecology Bottle Addition

Mos

Hrs

Ldg

24 A/FEff: 30-Apr-1996









OptionalT (A/R)601-0480 Modification - Aircraft Air-Driven Generator - Addition of a Time Delay Relay

Mos

Hrs

Ldg

24 A/FEff: 30-Aug-1996

RecommendedRE (-)601-0509 Modification - Battery System - Addition of Protective Resistor

Mos

Hrs

Ldg

24 A/F

RecommendedT (A/R)601-0509 Rev 1 Modification - Battery System - Addition of Protective Resistor

Mos

Hrs

Ldg

24 A/FEff: 15-Sep-2000

OptionalT (A/R)601-0515 Modification - Static Discharger - Installation of Additional Winglet Static Discharger

Mos

Hrs

Ldg

24 A/FEff: 30-Apr-1999

RecommendedRE (-)601-0516 Modification - Battery System - Installation of Battery Charger Output Protection

Mos

Hrs

Ldg

24 A/F

RecommendedT (A/R)601-0516 Rev 1 Modification - Battery System - Installation of Battery Charger Output Protection

Mos

Hrs

Ldg

24 A/FEff: 30-Jun-2000

RecommendedRE (-)601-0521 Modification - Integrated Drive Generator (IDG) System - Protection of IDG Harness Inside Pylon

Mos

Hrs

Ldg

24 A/F

RecommendedT (A/R)601-0534 Modification - Battery System - Conversion of the Main Battery, Part No. 600-59151-11 to a -13

Mos

Hrs

Ldg

24 A/FEff: 28-Sep-2001

RecommendedT (A/R)601-0548 Special Check/Rework - Integrated Drive Generator (IDG) System and Auxiliary AC Generation System - Replacement of Faultily Manufactured IDG and APU Generators

Mos

Hrs

Ldg

24 A/FEff: 31-Jan-2002

Nextdue Share EarliestDUE:1. T A/R | 2. RE -Special Check/Rework - Integrated Drive Generator (IDG) Syst...601-0548 Part AA/F24

Nextdue Share EarliestDUE:1. T A/R | 2. RE -Special Check/Rework - Integrated Drive Generator (IDG) Syst...601-0548 Part BA/F24

Nextdue Share EarliestDUE:1. T A/R | 2. RE -Special Check/Rework - Integrated Drive Generator (IDG) Syst...601-0548 Part CA/F24

RecommendedT (A/R)601-0548 Part A Special Check/Rework - Integrated Drive Generator (IDG) System and Auxiliary AC Generation System - Inspect IDG and APU Generators

Mos

Hrs

Ldg

24 A/FEff: 31-Jan-2002









RecommendedT (A/R)601-0548 Part B Special Check/Rework - Integrated Drive Generator (IDG) System and Auxiliary AC Generation System - Replacement of Faultily Manufactured IDG

Mos

Hrs

Ldg

24 A/FEff: 31-Jan-2002

RecommendedT (A/R)601-0548 Part C Special Check/Rework - Integrated Drive Generator (IDG) System and Auxiliary AC Generation System - Replacement of Faultily Manufactured APU Generators

Mos

Hrs

Ldg

24 A/FEff: 31-Jan-2002

RecommendedRE (-)601-0591 Special Check/Modification – Air-Driven Generator System – Replacement of Chafing ADG Power Feed Wire

22-Mar-2012Mos

11,578.6Hrs

6,004Ldg


Nextdue Share EarliestDUE:1. T A/R | 2. RE -Special Check/Modification – Air-Driven Generator System – I...601-0591 Part AA/F24

Nextdue Share EarliestDUE:1. T A/R | 2. RE -Special Check/Modification – Air-Driven Generator System – R...601-0591 Part BA/F24

RecommendedT (A/R)601-0591 Part A Special Check/Modification – Air-Driven Generator System – Inspect the ADG Power Feed Wire

Mos

Hrs

Ldg

24 A/FEff: 23-Jul-2007

RecommendedT (A/R)601-0591 Part B Special Check/Modification – Air-Driven Generator System – Replacement of Chafing ADG Power Feed Wire

Mos

Hrs

Ldg

24 A/FEff: 23-Jul-2007

RecommendedRE (-)601-0625 Special Check/Rework – Integrated Drive Generator (IDG) and Hydraulic Systems No.1 and No. 2 – Aft Equipment Bay Right IDG Power Cable and Adjacent Hydraulic

Lines Support Brackets

Mos

Hrs

Ldg

24 A/F

Recommended ≈09-Feb-2016T601-0625 Rev 1 Special Check/Rework – Integrated Drive Generator (IDG) and Hydraulic Systems No.1 and No. 2 – Aft Equipment Bay Right IDG Power Cable and Adjacent Hydraulic

Lines Support Brackets

Mos

OVD[12,039.2]400Hrs

Ldg

24 A/FEff: 13-Jan-2014

RecommendedT (A/R)601-1085 Modification - Engine Standard Configuration - Thrust Reverser and IDG Cable Clamps

Mos

Hrs

Ldg

24 A/FEff: 15-Sep-1994

Mandatory (Appliance AD)RE (-)82-21-04 JET ELECTRONICS AND TECHNOLOGY, INC. All Model PS-835 Series Emergency Power Supply Installations

18-Sep-1985Mos

Hrs

Ldg

24 A/FBY DATE OF MANUFACTUREEff: 21-Oct-1982 Not

Applicable

MandatoryRE (-)83-07-09 Wire Overheating

18-Sep-1985Mos

Hrs

Ldg

24 A/FComplied With









MandatoryT (A/R)83-07-09 R1 Wire Overheating

Mos

Hrs

Ldg

24 A/FEff: 12-Nov-1993

Mandatory (Appliance AD)RE (-)87-06-09 MECHANICAL PRODUCTS, INC. Model 4001, 4200, 4310, and 8500 Series Circuit Breakers

29-Apr-1988Mos

Hrs

Ldg

24 A/FEff: 27-Apr-1987 Not Applicable

MandatoryRE (-)91-19-01 Air Driven Generator

18-Mar-1992Mos

Hrs

Ldg


MandatoryRE (-)95-10-06 Shaft Pin

05-Nov-1998Mos

Hrs

Ldg

24 A/FSI 601-0430Eff: 12-Jun-1995 Complied

With

AlertRE (-)A601-0028 Special Check/Modification - AC Voltage and Frequency Sensor - Release Time

Mos

Hrs

Ldg

24 A/FEff: 05-Jul-1983

RecommendedT (A/R)A601-0069 Special Check/Rework - External Finish - Lightning Protection

Mos

Hrs

Ldg

24 A/FEff: 30-Jul-1984

AlertRE (-)A601-0097 Special Check/Replacement - IDG and APU - Generators

Mos

Hrs

Ldg

24 A/F

AlertT (A/R)A601-0097 Rev 1 Special Check/Replacement - IDG and APU - Generators

Mos

Hrs

Ldg

24 A/FEff: 22-Apr-1985

AlertRE (-)A601-0174 Special Check/Modification - Nacelle/Pylon Services - Elimination of Possible Chafing

Mos

Hrs

Ldg

24 A/F

AlertRE (-)A601-0174 Rev 1 Special Check/Modification - Nacelle/Pylon Services - Elimination of Possible Chafing

11-Apr-1985Mos

0Hrs

Ldg


RecommendedRE (-)A601-0219 Special Check/Modification - Air Driven Generator - Harness Rerouting

11-Apr-1988Mos

Hrs

Ldg










AlertRE (-)A601-0370 Special Check/Modification - Air-Driven Generator - Output Harness Chafing

24-Mar-1992Mos

Hrs

Ldg

24 A/FComplied With

AlertT (A/R)A601-0370 Rev 1 Special Check/Modification - Air-Driven Generator - Output Harness Chafing

Mos

Hrs

Ldg

24 A/FEff: 15-Apr-1993

AlertRE (-)A601-0416 Special Operational and Rigging Check - Air-Driven Generator - ADG Uplock Assembly

01-Nov-1993Mos

Hrs

Ldg


AlertT (A/R)A601-0547 Special Check/Rework - AC Load Distribution - Replacement of Faultily Manufactured Leach "H" Series Relays

Mos

Hrs

Ldg

24 A/FEff: 28-Sep-2001

Nextdue Share EarliestDUE:1. T 100 Hrs | 2. RE -Special Check/Rework - AC Load Distribution - Replacement of...A601-0547 Part AA/F24

Nextdue Share EarliestDUE:1. T 200 Hrs | 2. RE -Special Check/Rework - AC Load Distribution - Replacement of...A601-0547 Part BA/F24

Nextdue Share EarliestDUE:1. T 300 Hrs | 2. RE -Special Check/Rework - AC Load Distribution - Replacement of...A601-0547 Part CA/F24

Nextdue Share EarliestDUE:1. T 500 Hrs | 2. RE -Special Check/Rework - AC Load Distribution - Replacement of...A601-0547 Part DA/F24

AlertRE (-)A601-0547 Part A Special Check/Rework - AC Load Distribution - Replacement of Faultily Manufactured Leach "H" Series Relays

Mos

Hrs

Ldg

24 A/FEff: 28-Sep-2001

(NOTE: NOTE: There are limited available quantities of “H” series relays,that are required for the incorporation of PART B, C and/or D.For this

reason, the special check in PART A is intended toverify if the suspect relays are installed in the aircraft beforeordering the relays and planning

the incorporation of PART B,C and/or D.)

AlertRE (-)A601-0547 Part B Special Check/Rework - AC Load Distribution - Replacement of Faultily Manufactured Leach "H" Series Relays

Mos

Hrs

Ldg

24 A/FEff: 28-Sep-2001

AlertRE (-)A601-0547 Part C Special Check/Rework - AC Load Distribution - Replacement of Faultily Manufactured Leach "H" Series Relays

Mos

Hrs

Ldg

24 A/FEff: 28-Sep-2001

AlertRE (-)A601-0547 Part D Special Check/Rework - AC Load Distribution - Replacement of Faultily Manufactured Leach "H" Series Relays

Mos

Hrs

Ldg

24 A/FEff: 28-Sep-2001

▼ 25 - EQUIPMENT/FURNISHINGS

RE (O/C)Emergency Locator Transmitter (ELT)

20-Sep-1983Mos

0Hrs

0Ldg


Assembly SubDUE: 31-Jul-20171. RE DueEmergency Locator Transmitter (ELT) BatteryBP-1030 / N/AA/F25

Component Inspection SimpleDUE: 17-Apr-20161. RE 12 MosEmergency Locator Transmitter Inspection and Test per FAR 91...FAR 91.207A/F25









Life LimitRE (Due)Emergency Locator Transmitter (ELT) Battery

1.3 Years31-Jul-201731-Jul-2015Mos

11,905.8Hrs

6,221Ldg

25 A/F

Expiration Date 31-Jul-2017

BP-1030N/A

RE (O/C)First Aid Kit

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Galley Control Panel

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Hi Temp Oven

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Lap Belt

20-Sep-1983Mos

0Hrs0

0Ldg0

Pilot25 A/FNew1101020-29

UNKNOWN

RE (O/C)Life Raft

06-Sep-2001Mos

7,694.9Hrs

3,648Ldg

Aft25 A/FRAF1210-105T1135HP

RE (O/C)Life Raft

06-Sep-2001Mos

7,694.9Hrs

3,648Ldg

Fwd25 A/FRAF1210-105T1130HP

RE (O/C)Life Vest

Mos

Hrs

Ldg


Component Inspection SimpleDUE: 16-Feb-20201. RE DueLife Vest - Recertification25-61-CUS-001A/F25

RE (O/C)Life Vest

Mos

Hrs

Ldg



RE (O/C)Life Vest

Mos

Hrs

Ldg











RE (O/C)Life Vest

Mos

Hrs

Ldg



RE (O/C)Life Vest

Mos

Hrs

Ldg



RE (O/C)Life Vest

Mos

Hrs

Ldg



RE (O/C)Life Vest

Mos

Hrs

Ldg



RE (O/C)Life Vest

Mos

Hrs

Ldg



RE (O/C)Life Vest

Mos

Hrs

Ldg



RE (O/C)Life Vest

Mos

Hrs

Ldg



RE (O/C)Life Vest

Mos

Hrs

Ldg











RE (O/C)Life Vest (Crew)

Mos

Hrs

Ldg


Component Inspection SimpleDUE: 16-Feb-20201. RE DueLife Vest (Crew) - Recertification25-61-CUS-001A/F25

RE (O/C)Life Vest (Crew)

Mos

Hrs

Ldg

Pilot25 A/FUnknownUnknown

Component Inspection SimpleDUE: 16-Feb-20201. RE DueLife Vest (Crew) - Recertification25-61-CUS-001A/F25

RE (O/C)Oven Controller

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Panel

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Reel And Control Harness

20-Sep-1983Mos

0Hrs0

0Ldg0

No.125 A/FNew1S20B25A4X21

UNKNOWN

RE (O/C)Reel And Control Harness

20-Sep-1983Mos

0Hrs0

0Ldg0

No.225 A/FNew1S20B25A4X21

UNKNOWN

RE (O/C)Seat

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Seat

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Seat Belt

20-Sep-1983Mos

0Hrs0

0Ldg0

Copilot25 A/FNew1101020-31

UNKNOWN

Mandatory (Appliance AD)RE (-)2011-21-08 Paragraph (f)(1) SICMA AERO SEAT - Equipment/Furnishings - Passenger Seat Assemblies - do a general visual inspection of the backrest links having P/Ns 90-000200-104-1 and 90-

000200-104-2, in accordance with Part One of Sicma Aero Seat Service Bulletin 90-25-013, Issue 4

13-Jul-2012Mos

11,613.3Hrs

6,021Ldg

25 A/FBY PART NUMBER INSTALLEDEff: 23-Nov-2011 Not

Applicable









Mandatory (Appliance AD)RE (-)2011-21-08 Paragraph (f)(4)(5) SICMA AERO SEAT - Equipment/Furnishings - Passenger Seat Assemblies - replace the links, P/Ns 90-000200-104-1 and 90-000200-104-2, with new improved links,

P/Ns 90-100200-104-1 and 90-100200-104-2

13-Jul-2012Mos

11,613.3Hrs

6,021Ldg

25 A/FBY PART NUMBER INSTALLEDEff: 23-Nov-2011 Not

Applicable

Mandatory (Appliance AD)T (A/R)2012-08-07 Equipment/Furnishings - To Detect Cracks in the Central and Lateral Spreaders on Passenger Seats

Mos

Hrs

Ldg

25 A/FEff: 09-May-2012

Mandatory (Appliance AD)T (A/R)2014-20-11 Zodiac Seats France - Equipment/Furnishings - Seats

Mos

Hrs

Ldg

25 A/FEff: 22-Oct-2014

MRB ≈03-May-2017RE25-11-00-201 Crew Seats/Safety Harness and Inertial Reel Visual Check, paying particular attention to the seat tracks, trackstops and adjustment cables

10-Feb-2016Mos

590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs

6,326Ldg

(PKG 600 Hour)

25 A/F


RE (Due)25-61-CUS-001 Life Vest - Recertification

3.9 Years16-Feb-202016-Feb-2010Mos

Hrs

Ldg

No.125 A/F

Expiration Date 16-Feb-2020

UnknownUnknown



Hrs

Ldg

No.1025 A/F


UnknownUnknown



Hrs

Ldg

No.1125 A/F


UnknownUnknown



Hrs

Ldg

No.225 A/F


UnknownUnknown



Hrs

Ldg

No.325 A/F


UnknownUnknown



Hrs

Ldg

No.425 A/F


UnknownUnknown











Hrs

Ldg

No.525 A/F


UnknownUnknown



Hrs

Ldg

No.625 A/F


UnknownUnknown



Hrs

Ldg

No.725 A/F


UnknownUnknown



Hrs

Ldg

No.825 A/F


UnknownUnknown



Hrs

Ldg

No.925 A/F


UnknownUnknown

RE (Due)25-61-CUS-001 Life Vest (Crew) - Recertification


Hrs

Ldg

Copilot25 A/F


UnknownUnknown

RE (Due)25-61-CUS-001 Life Vest (Crew) - Recertification


Hrs

Ldg

Pilot25 A/F


UnknownUnknown

ICARE25-CUS-011 Aircraft First Aid Kit - Inspection

44 Days20-May-20161220-May-2015Mos

Hrs

Ldg

25 A/F

(NOTE: 12 Month Inspection Per Manufacture's Instructions)

OptionalT (A/R)601-0071 Modification - Cockpit Headlining - Drainage Provision

Mos

Hrs

Ldg

25 A/FEff: 10-Jul-1985

OptionalT (A/R)601-0168 Modification - Pilots Eye Locator - Improved Mounting

Mos

Hrs

Ldg

25 A/FEff: 26-May-1987









RecommendedRE (-)601-0191 Modification - Aft Distribution Box (JB4) - Vent Screen Cover

23-Mar-1992Mos

Hrs

Ldg

25 A/FComplied With

RecommendedT (A/R)601-0191 Rev 1 Modification - Aft Distribution Box (JB4) - Vent Screen Cover

Mos

Hrs

Ldg

25 A/FEff: 20-Jun-1988

RecommendedT (A/R)601-0567 Modification - Flight Compartment - Replacement of Camloc Fasteners on Rudder Pedal Protection Panels

Mos

Hrs

Ldg

25 A/FEff: 29-Oct-2004

Mandatory ≈23-Dec-2016RE74-08-09 R3 Equipment/furnishings - Equipment/furnishings - improper disposal of smoking materials in lavatory waste receptacles

05-Jun-2009Mos

417.4 Hrs12,458.61,00011,458.6Hrs

Ldg

25 A/FEff: 28-Mar-2012

Mandatory (Appliance AD)RE (-)83-11-03 Attendant Restraint System Rotary Buckle Assemblies

18-Sep-1985Mos

Hrs

Ldg

25 A/FEQUIPMENT NOT INSTALLEDEff: 18-Jul-1983 Not

Applicable

Mandatory (Appliance AD)RE (-)87-17-06 Occupant Restraint System Assemblies

29-Apr-1988Mos

1,995Hrs

756Ldg

25 A/FEff: 22-Sep-1987 Not Applicable

FAR91, FAR 91REFAR 91.207 Emergency Locator Transmitter Inspection and Test per FAR 91.207 (d)

11 Days17-Apr-20161217-Apr-2015Mos

Hrs

Ldg


▼ 26 - FIRE PROTECTION

RE (O/C)Auxiliary Power Unit Firex Container

24-Oct-2011Mos

11,543.4Hrs

5,985Ldg

26 A/F89788-299058EK

Component Inspection SimpleDUE: 21-Oct-20161. RE 12 MosAuxiliary Power Unit Firex Container - Check APU Firex Conta...26-21-11-206A/F26

Component Inspection Tso To

TsiDUE: 24-Oct-20161. RE 60 MosAuxiliary Power Unit Firex Container - Hydrostatic Test26-21-11-207A/F26

RE (O/C)Fire Detection Control

20-Sep-1983Mos

0Hrs0

0Ldg0

No.126 A/FNew377-02836

UNKNOWN


20-Sep-1983Mos

0Hrs0

0Ldg0

No.226 A/FNew377-02836

UNKNOWN










20-Sep-1983Mos

0Hrs

0Ldg



20-Sep-1983Mos

0Hrs

0Ldg



20-Sep-1983Mos

0Hrs

0Ldg



20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Fire Sensing Element

20-Sep-1983Mos

0Hrs0

0Ldg0

No.126 A/FNew244-21086

UNKNOWN


20-Sep-1983Mos

0Hrs

0Ldg



20-Sep-1983Mos

0Hrs

0Ldg



20-Sep-1983Mos

0Hrs

0Ldg



20-Sep-1983Mos

0Hrs

0Ldg



20-Sep-1983Mos

0Hrs

0Ldg



20-Sep-1983Mos

0Hrs

0Ldg











20-Sep-1983Mos

0Hrs

0Ldg



20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Fire Sensing Mlg Element

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Fire Sensing Mlg Element

20-Sep-1983Mos

0Hrs

0Ldg


AWL - Life LimitRE (O/C)Portable Fire Extinguisher

08-Jul-2011Mos

11,523.8Hrs

Ldg

Aft - Cabin26 A/FC352TSW-790480


Component Inspection SimpleDUE: 21-Oct-20161. RE 12 MosPortable Fire Extinguisher - Check weight26-25-00-213A/F26


TsiDUE: 08-Jul-20231. RE 144 MosPortable Fire Extinguisher - Hydrostatic Test26-25-00-214A/F26


26-Jan-2011Mos

11,460.7Hrs

Ldg

Cockpit26 A/FC352TSUnknown


Component Inspection SimpleDUE: 21-Oct-20161. RE 12 MosPortable Fire Extinguisher - Check weight26-25-00-213A/F26


TsiDUE: 26-Jan-20231. RE 144 MosPortable Fire Extinguisher - Hydrostatic Test26-25-00-214A/F26


20-Sep-1983Mos

0Hrs

0Ldg

Fwd - Cabin26 A/FUnknownUnknown



20-Sep-1983Mos

0Hrs

0Ldg

Fwd - Closet26 A/FUnknownUnknown










RE (O/C)Power Plant Firex Container

24-Oct-2011Mos

11,543.4Hrs

5,985Ldg

Left26 A/F8990745765U

Component Inspection SimpleDUE: 21-Oct-20161. RE 12 MosPower Plant Firex Container - Check Power Plant Firex Contai...26-23-11-210A/F26


TsiDUE: 24-Oct-20161. RE 60 MosPower Plant Firex Containers - Hydrostatic Test26-23-11-211A/F26

RE (O/C)Power Plant Firex Container

24-Oct-2011Mos

11,543.4Hrs

5,985Ldg

Right26 A/F89907430292EL

Component Inspection SimpleDUE: 21-Oct-20161. RE 12 MosPower Plant Firex Container - Check Power Plant Firex Contai...26-23-11-210A/F26


TsiDUE: 24-Oct-20161. RE 60 MosPower Plant Firex Containers - Hydrostatic Test26-23-11-211A/F26

Mandatory (Appliance AD)RE (-)2001-22-14 Overland Aviation Services - Fire Extinguishing System Bottle Cartridges

11-Jan-2002Mos

7,973.5Hrs

3,823Ldg

26 A/FSB 22-09-97Eff: 10-Dec-2001 Complied

With

MRB ≈18-Sep-2016RE26-10-11-201 Power Plant and APU Fire Sensing Cables Visual Check all visible portions of the firewires, particularly around mountings and runs through bulkheads

10-Feb-2016Mos

290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs

6,326Ldg

(PKG 300 Hour)

26 A/F


MRB ≈20-Oct-2017RE26-10-21-203 Main Landing Gear Bay Overheat Detection System Functional Test

29-Oct-2012Mos

812.3 Hrs (+40)(12,853.5)-/+401,20011,653.5Hrs

Ldg

(PKG 1200 Hour)

26 A/F


MRB ≈18-Sep-2016RE26-21-00-204 Auxiliary Power Unit (APU) Fire Extinguishing Functional Test APU Fire Extinguishing System

10-Feb-2016Mos

290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs

6,326Ldg

(PKG 300 Hour)

26 A/F


MRBRE26-21-11-206 Auxiliary Power Unit Firex Container - Check APU Firex Container

6.6 Months (+31

Days)21-Oct-2016-/+11221-Oct-2015Mos

Hrs

Ldg

(PKG 12 Month)

26 A/F

89788-299058EK


MRBRE26-21-11-207 Auxiliary Power Unit Firex Container - Hydrostatic Test

6.7 Months (+31

Days)24-Oct-2016-/+16024-Oct-2011Mos

Hrs

Ldg

26 A/F

Hydrostatic Tested Date 24-Oct-2011

89788-299058EK

Ref.:CMM/PSP 608/608A 26-21-28, Ref.:Section 5-20-05 Para 10 Program Note B (SOURCE: TLMC 05-20-15)

MRBRE26-21-21-205 Auxiliary Power Unit Firex Discharge Line Visual Check

6.6 Months (+31

Days)(21-Oct-2016)-/+11221-Oct-2015Mos

Hrs

Ldg

(PKG 12 Month)

26 A/F










MRBRE (N/A)26-23-00-208 Power Plant Fire Extinguishing (Pre SB 601-0171) Functional Test Power Plant Fire Extinguishing System

Mos

Hrs

Ldg

26 A/F


MRB ≈29-Feb-2016RE26-23-00-209 Power Plant Fire Extinguishing (Post SB 601-0171) Functional Test Power Plant Fire Extinguishing System

05-Apr-2013Mos

26.3 Hrs (+40)12,067.5-/+4030011,767.5Hrs

Ldg

26 A/F


MRBRE26-23-11-210 Power Plant Firex Container - Check Power Plant Firex Container

6.6 Months (+31

Days)21-Oct-2016-/+11221-Oct-2015Mos

Hrs

Ldg

Left

(PKG 12 Month)

26 A/F

8990745765U


MRBRE26-23-11-210 Power Plant Firex Container - Check Power Plant Firex Container

6.6 Months (+31

Days)21-Oct-2016-/+11221-Oct-2015Mos

Hrs

Ldg

Right

(PKG 12 Month)

26 A/F

89907430292EL


MRBRE26-23-11-211 Power Plant Firex Containers - Hydrostatic Test

6.7 Months (+31

Days)24-Oct-2016-/+16024-Oct-2011Mos

Hrs

Ldg

Left26 A/F


8990745765U


MRBRE26-23-11-211 Power Plant Firex Containers - Hydrostatic Test

6.7 Months (+31

Days)24-Oct-2016-/+16024-Oct-2011Mos

Hrs

Ldg

Right26 A/F


89907430292EL


MRB ≈03-May-2017RE26-23-21-215 Power Plant Firex Discharge Lines Visual Check, paying particular attention for any chafing with the PRSOV sensing line

10-Feb-2016Mos

590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs

6,326Ldg

(PKG 600 Hour)

26 A/F


MRB ≈18-Sep-2016RE26-25-00-212 Portable Fire Extinguisher - Check pressure

10-Feb-2016Mos

290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs

6,326Ldg

(PKG 300 Hour)

26 A/F


MRBRE26-25-00-213 Portable Fire Extinguisher - Check weight

6.6 Months (+31

Days)21-Oct-2016-/+11221-Oct-2015Mos

Hrs

Ldg

Aft - Cabin

(PKG 12 Month)

26 A/F

Weighted Date 21-Oct-2015

C352TSW-790480










MRBRE26-25-00-213 Portable Fire Extinguisher - Check weight

6.6 Months (+31

Days)21-Oct-2016-/+11221-Oct-2015Mos

Hrs

Ldg

Cockpit

(PKG 12 Month)

26 A/F

Weighted Date 21-Oct-2015

C352TSUnknown


MRBRE26-25-00-214 Portable Fire Extinguisher - Hydrostatic Test

7.3 Years (+31 Days)08-Jul-2023-/+114408-Jul-2011Mos

Hrs

Ldg

Aft - Cabin26 A/F

Hydrostatic Tested Date 08-Jul-2011

C352TSW-790480


MRBRE26-25-00-214 Portable Fire Extinguisher - Hydrostatic Test

6.8 Years (+31 Days)26-Jan-2023-/+114426-Jan-2011Mos

Hrs

Ldg

Cockpit26 A/F

Hydrostatic Tested Date 26-Jan-2011

C352TSUnknown


VendorRE26-NFPA-10 Portable Fire Extinguisher • 6 Years Inspection

1.3 Years08-Jul-20177208-Jul-2011Mos

Hrs

Ldg

26 A/FInspected Date 08-Jul-2011

VendorRE26-NFPA-10 Portable Fire Extinguisher • 6 Years Inspection

9.8 Months26-Jan-20177226-Jan-2011Mos

Hrs

Ldg

26 A/FInspected Date 26-Jan-2011

RecommendedRE (-)601-0123 Modification - Power Plant - Relocation of FIREX Bottle

17-Sep-1985Mos

607Hrs

262Ldg


RecommendedRE (-)601-0171 Modification - Engine Fire Push and Master Caution Reset Switches - Replacement

23-Mar-1992Mos

Hrs

Ldg


OptionalT (A/R)601-0315 Modification - APU Firex Container - Support Bracket

Mos

Hrs

Ldg

26 A/FEff: 08-Mar-1991

RecommendedRE (-)601-0321 Special Check/Modification - Power Plant Fire Extinguishing System - Two-Way Check Tee

25-Mar-1991Mos

3,182Hrs

1,266Ldg


RecommendedRE (-)601-0574 Modification/Inspection - Fire Detection System - Improved Harness Routing for Jet Pipe Sensing Element

Mos

Hrs

Ldg

26 A/F









RecommendedT (A/R)601-0589 Special Check/Modification - Fire Detection - Resistance Test and Replacement of Combustion Zone Sensing Elements Where Required

Mos

Hrs

Ldg

26 A/FEff: 26-Feb-2007

Nextdue Share EarliestDUE:1. T 400 Hrs | 2. RE -Special Check/Modification - Fire Detection - Resistance Tes...601-0589 Part AA/F26

Nextdue Share EarliestDUE:1. T 800 Hrs | 2. RE -Special Check/Modification - Fire Detection - Resistance Tes...601-0589 Part BA/F26

RecommendedRE (-)601-0589 Part A Special Check/Modification - Fire Detection - Resistance Test and Replacement of Combustion Zone Sensing Elements Where Required

Mos

Hrs

Ldg

26 A/FEff: 26-Feb-2007

RecommendedRE (-)601-0589 Part B Special Check/Modification - Fire Detection - Resistance Test and Replacement of Combustion Zone Sensing Elements Where Required

Mos

Hrs

Ldg

26 A/FEff: 26-Feb-2007

OptionalRE (-)601-1050 Modification - Engine Fire Sensing Cable - Support Bracket

Mos

Hrs

Ldg

26 A/F

OptionalT (A/R)601-1050 Rev 1 Modification - Engine Fire Sensing Cable - Support Bracket

Mos

Hrs

Ldg

26 A/FEff: 12-Jan-1987

RecommendedRE (-)601-1059 Modification - Firex Line Assembly - Clearance

02-May-1988Mos

1,995Hrs

756Ldg

26 A/FEff: 12-Oct-1987 Complied With

RecommendedRE (-)601-1068 Modification - Exhaust Nozzle Fairing - Fire Sensing Cable

Mos

Hrs

Ldg

26 A/F

RecommendedRE (-)601-1068 Rev 1 Modification - Exhaust Nozzle Fairing - Fire Sensing Cable

23-Mar-1992Mos

3,584Hrs

1,446Ldg


MandatoryRE (-)92-13-09 Engine Fire Extinguishing System

24-Dec-2002Mos

9,122.1Hrs

4,527Ldg

26 A/FSB A601-0309Eff: 23-Jul-1992 Complied

With

Compliance Share DoubleDUE:1. T 50 Hrs | 2. RE -Special Check/Modification - Engine Fire Protection - Sensor...A601-0309A/F26

AlertRE (-)A601-0309 Special Check/Modification - Engine Fire Protection - Sensor System Wiring and Fire Extinguishing Bottle Squib Wiring

Mos

Hrs

Ldg

26 A/FEff: 08-Sep-1989









AlertT (A/R)A601-1087 Modification - Fire Protection - Harness Re-Routing

Mos

Hrs

Ldg

26 A/FEff: 25-Apr-1994

▼ 27 - FLIGHT CONTROLS

RE (O/C)(Inner Flap) Actuator

20-Sep-1983Mos

0Hrs

0Ldg

Left Inboard27 A/FUnknownUnknown


20-Sep-1983Mos

0Hrs

0Ldg

Left Outboard27 A/FUnknownUnknown


20-Sep-1983Mos

0Hrs

0Ldg

Right Inboard27 A/FUnknownUnknown


20-Sep-1983Mos

0Hrs

0Ldg

Right Outboard27 A/FUnknownUnknown

RE (O/C)Aileron Cable Tension Regulator

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Aileron Cable Tension Regulator

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Aileron Flutter Damper

08-Aug-2003Mos

9,585.6Hrs

4,797Ldg

Left27 A/F600-75142-3HA13712

Component Inspection SimpleDUE:1. RE 600 HrsAileron Flutter Dampers - Check aileron flutter damper / Che...27-13-21-205A/F27

Component Inspection SimpleDUE:1. RE 4800 HrsAileron Flutter Dampers - Remove, carry out “Testing and Fau...27-13-21-206A/F27

RE (O/C)Aileron Flutter Damper

08-Aug-2003Mos

9,585.6Hrs

4,797Ldg

Right27 A/F600-75142-9HA13913

Component Inspection SimpleDUE:1. RE 600 HrsAileron Flutter Dampers - Check aileron flutter damper / Che...27-13-21-205A/F27

Component Inspection SimpleDUE:1. RE 4800 HrsAileron Flutter Dampers - Remove, carry out “Testing and Fau...27-13-21-206A/F27

RE (O/C)Aileron Trim (Roll) Actuator

20-Sep-1983Mos

0Hrs

0Ldg










RE (O/C)Altitude Transducer

20-Sep-1983Mos

0Hrs0

0Ldg0

Left27 A/FNew7001648-902

UNKNOWN

RE (O/C)Altitude Transducer

17-Sep-2001Mos

7,697.4Hrs

3,650Ldg

Right27 A/F7001648-90295081379

RE (O/C)Angle-of-Attack (AOA) Transducer

20-Sep-1983Mos

0Hrs

0Ldg


Component Inspection SimpleDUE: 12,055.3 Hrs1. RE 300 HrsAngle-of-Attack Vane Transducer Linearity - Functional Test ...27-39-11-101 *A/F27


TsiDUE:1. RE N/AAngle-of-Attack Vane Transducer, Restoration - Overhaul of t...27-39-11-102 *A/F27

RE (O/C)Angle-of-Attack (AOA) Transducer

27-Feb-2005Mos

10,601.2Hrs

5,392Ldg

Right27 A/F600-59154-1247-098

Component Inspection SimpleDUE: 12,055.3 Hrs1. RE 300 HrsAngle-of-Attack Vane Transducer Linearity - Functional Test ...27-39-11-101 *A/F27


TsiDUE:1. RE N/AAngle-of-Attack Vane Transducer, Restoration - Overhaul of t...27-39-11-102 *A/F27

RE (O/C)Control Column Wheel

20-Sep-1983Mos

0Hrs0

0Ldg0

Copilot27 A/FNew720-5716

UNKNOWN

RE (O/C)Control Column Wheel

20-Sep-1983Mos

0Hrs0

0Ldg0

Pilot27 A/FNew720-5715

UNKNOWN

RE (O/C)Control Surface Position Indicator

25-Jul-2008Mos

11,432Hrs

5,881Ldg

27 A/F600-50930-5147

RE (O/C)Elevator Flutter Damper

08-Aug-2003Mos

9,585.6Hrs

4,797Ldg

Left Inboard27 A/F1018100-7HA13933

Component Inspection SimpleDUE:1. RE 600 HrsElevator Flutter Dampers - Check elevator flutter damper27-33-11-216A/F27

Component Inspection SimpleDUE:1. RE 4800 HrsElevator Flutter Dampers - Remove, carry out “Testing and Fa...27-33-11-217A/F27










08-Aug-2003Mos

9,585.6Hrs

4,797Ldg

Left Outboard27 A/F1018100-7HA13911




08-Aug-2003Mos

9,585.6Hrs

4,797Ldg

Right Inboard27 A/F1018100-7HA13910




08-Aug-2003Mos

9,585.6Hrs

4,797Ldg

Right Outboard27 A/F1018100-7HA13919



RE (O/C)Elevator Load Limiter

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Elevator Load Limiter

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Flap Brake Detector Unit

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Flap Brake Detector Unit

01-Dec-2002Mos

9,037.1Hrs

4,479Ldg

Right27 A/F2022280-6102-469M

RE (O/C)Flap Control Unit

28-Nov-2002Mos

9,032.5Hrs

4,475Ldg

27 A/F8-341-02125-339

RE (O/C)Flap Control Unit

20-Sep-1983Mos

0Hrs

0Ldg










RE (O/C)Flap Drive Potentiometer (PDU)

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Flap Position Indicator

04-Mar-2003Mos

9,274.7Hrs

4,617Ldg

27 A/F600-59179-186110177

RE (O/C)Flap Position Transmitter

20-Sep-1983Mos

0Hrs0

0Ldg0

Left27 A/FNew600-93030-1

N/A

RE (O/C)Flap Position Transmitter

20-Sep-1983Mos

0Hrs0

0Ldg0


N/A

RE (O/C)Flap System Control Lever

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Flexible Drive Shaft

20-Sep-1983Mos

0Hrs

0Ldg



20-Sep-1983Mos

0Hrs

0Ldg



20-Sep-1983Mos

0Hrs

0Ldg



20-Sep-1983Mos

0Hrs

0Ldg



20-Sep-1983Mos

0Hrs

0Ldg



20-Sep-1983Mos

0Hrs

0Ldg











20-Sep-1983Mos

0Hrs

0Ldg



20-Sep-1983Mos

0Hrs

0Ldg



20-Sep-1983Mos

0Hrs

0Ldg



20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Flight Control Monitor Unit

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Flight Spoiler Load Limiter

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Flight Spoiler Load Limiter

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Flight Spoiler Proximity Switch

20-Sep-1983Mos

0Hrs

0Ldg


AWL - Life Limit ≈02-Nov-2016REGround Spoiler PCU

10-Nov-2000Mos

7,089.9Hrs

262 Ldg6,5883,3003,288Ldg0

Left27 A/F600-75106-3307

AWL - Life Limit ≈02-Nov-2016REGround Spoiler PCU

10-Nov-2000Mos

7,089.9Hrs

262 Ldg6,5883,3003,288Ldg0

Right27 A/F600-75106-3308

RE (O/C)Ground Spoiler Select Manifold

20-Sep-1983Mos

0Hrs0

0Ldg0

27 A/FNew62130-7

UNKNOWN









RE (O/C)Horizontal Stab Trim Control Unit

28-Mar-2014Mos

11,824.5Hrs

6,169Ldg

27 A/F56417-005370

AWL - Life Limit ≈04-Jun-2137REHSTA Inst Pin, Lower Attach

20-Sep-1983Mos

0Hrs0

43,674 Ldg50,00050,0000Ldg0

Left27 A/FNewUNKNOWN

UNKNOWN

AWL - Life Limit ≈04-Jun-2137REHSTA Inst Pin, Lower Attach

20-Sep-1983Mos

0Hrs0

43,674 Ldg50,00050,0000Ldg0

Right27 A/FNewUNKNOWN

UNKNOWN

AWL - Life Limit ≈04-Jun-2137REHSTA Inst Pin, Upper Attach

20-Sep-1983Mos

0Hrs0

43,674 Ldg50,00050,0000Ldg0

Left27 A/FNew600-93033-1

UNKNOWN

AWL - Life Limit ≈04-Jun-2137REHSTA Inst Pin, Upper Attach

20-Sep-1983Mos

0Hrs0

43,674 Ldg50,00050,0000Ldg0


UNKNOWN

RE (O/C)Lateral Stall Warning Accelerometer

20-Sep-1983Mos

0Hrs0

0Ldg0

Left27 A/FNew4383A0-5P10

UNKNOWN

RE (O/C)Lateral Stall Warning Accelerometer

20-Sep-1983Mos

0Hrs0

0Ldg0

Right27 A/FNew4383A0-5P10

UNKNOWN

RE (O/C)Load Limiter

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Outboard Flap Actuator

12-May-2010Mos

Hrs

5,910Ldg

Left Inboard27 A/F600-93000-82UNKNOWN


TsiDUE: 7,910 Ldg1. RE 2000 LdgOutboard Flap Actuator - Restoration of the Outboard Flap Ac...27-50-16-101 *A/F27


12-May-2010Mos

Hrs

5,910Ldg

Left Outboard27 A/F600-93000-93UNKNOWN












12-May-2010Mos

Hrs

5,910Ldg

Right Inboard27 A/F600-93000-82UNKNOWN




12-May-2010Mos

Hrs

5,910Ldg

Right Outboard27 A/F600-93000-93UNKNOWN



RE (O/C)Pitch Feel Simulator

20-Sep-1983Mos

0Hrs

0Ldg


Component Inspection SimpleDUE: 12,397.5 Hrs1. RE 1500 HrsPitch Feel Simulator - Functional Test of the Pitch Feel Sim...27-31-11-101A/F27

RE (O/C)Pitch Feel Simulator

20-Sep-1983Mos

0Hrs

0Ldg


Component Inspection SimpleDUE: 12,397.5 Hrs1. RE 1500 HrsPitch Feel Simulator - Functional Test of the Pitch Feel Sim...27-31-11-101A/F27

AWL - Life Limit ≈19-Dec-2031REPitch Trim Actuator

11-Mar-2000Mos

7,611.7 Hrs19,652.913,2006,452.9Hrs0

2,899Ldg0

27 A/FNew600-92301-65

346E


TsiDUE: 13,052.9 Hrs1. T 6600 Hrs | 2. RE 6600 HrsPitch Trim Actuator - Overhaul27-40-16-101 *A/F27

RE (O/C)Position Transmitter

20-Sep-1983Mos

0Hrs

0Ldg



20-Sep-1983Mos

0Hrs

0Ldg



20-Sep-1983Mos

0Hrs

0Ldg



20-Sep-1983Mos

0Hrs

0Ldg











20-Sep-1983Mos

0Hrs

0Ldg



20-Sep-1983Mos

0Hrs

0Ldg



20-Sep-1983Mos

0Hrs

0Ldg



20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Power Control Aileron (PCU)

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Power Control Aileron (PCU)

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Power Control Flight Spoiler Unit

20-Sep-1983Mos

0Hrs

0Ldg



20-Sep-1983Mos

0Hrs

0Ldg



20-Sep-1983Mos

0Hrs

0Ldg



20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Power Control Ground Spoiler Unit

20-Sep-1983Mos

0Hrs

0Ldg










RE (O/C)Power Control Ground Spoiler Unit

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Power Control Rudder (PCU)

20-Sep-1983Mos

0Hrs

0Ldg

Lower27 A/FUnknownUnknown


20-Sep-1983Mos

0Hrs

0Ldg

Mid27 A/FUnknownUnknown


20-Sep-1983Mos

0Hrs

0Ldg

Upper27 A/FUnknownUnknown

RE (O/C)Power Control Unit Elevator (PCU)

20-Sep-1983Mos

0Hrs

0Ldg



20-Sep-1983Mos

0Hrs

0Ldg



20-Sep-1983Mos

0Hrs

0Ldg



20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Power Drive Flap Control Unit

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Rudder Load Limiter

20-Sep-1983Mos

0Hrs

0Ldg

Lower27 A/FUnknownUnknown


20-Sep-1983Mos

0Hrs

0Ldg

Mid27 A/FUnknownUnknown










20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Rudder Position Transmitter

15-Dec-2004Mos

10,499.3Hrs

53,310Ldg

27 A/FLMT-199V11211690

RE (O/C)Spoiler Control Lever

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Stall Margin Indicator

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Stall Margin Indicator

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Stall Protection System (SPS), Stick Pusher Capstan Shaft

20-Sep-1983Mos

0Hrs

0Ldg


Component Inspection SimpleDUE: 12,397.5 Hrs1. RE 1500 HrsStall Protection System (SPS), Stick Pusher Capstan Shaft - ...27-39-00-104 *A/F27

RE (O/C)Stall Warning Computer

24-Mar-2009Mos

11,458.6Hrs

5,902Ldg

27 A/F600-59152-29014-0148 MI-60

RE (O/C)Stick Pusher Actuator

20-Sep-1983Mos

0Hrs0

0Ldg0

27 A/FNew501-1259-03

014-0148 MI-60

RE (O/C)Stick Shaker

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Stick Shaker

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Surface Trim Indicator

20-Sep-1983Mos

0Hrs

0Ldg










RE (O/C)Total Position Transducer

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Trim (Roll & Yaw) Actuator

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Yaw Damper Load Limiter

20-Sep-1983Mos

0Hrs

0Ldg


MandatoryRE (-)2003-22-12 Electronic flight instrument system (EFIS)

Mos

Hrs

Ldg

27 A/FEff: 12-Dec-2003

Nextdue Share EarliestDUE: 12,055.3 Hrs1. T 300 Hrs | 2. RE 300 HrsElectronic flight instrument system (EFIS) - Measurement, Re...2003-22-12 (Left) Paragraph (h)A/F27

Nextdue Share EarliestDUE: 12,055.3 Hrs1. T 300 Hrs | 2. RE 300 HrsElectronic flight instrument system (EFIS) - Measurement, Re...2003-22-12 (Right) Paragraph (h)A/F27

Nextdue Share EarliestDUE:1. T A/R | 2. RE -Electronic flight instrument system (EFIS) - Revision of Air...2003-22-12 Paragraph (a)A/F27

Nextdue Share EarliestDUE:1. T A/R | 2. RE -Electronic flight instrument system (EFIS) - All AOA Vane An...2003-22-12 Paragraph (d)A/F27

Nextdue Share EarliestDUE:1. T A/R | 2. RE -Electronic flight instrument system (EFIS) - One or More AOA...2003-22-12 Paragraph (e)A/F27

Nextdue Share EarliestDUE:1. T A/R | 2. RE -Electronic flight instrument system (EFIS) - Any AOA Vane An...2003-22-12 Paragraph (f)A/F27

Nextdue Share EarliestDUE:1. T A/R | 2. RE -Electronic flight instrument system (EFIS) - inspect the le...2003-22-12 Paragraph (j)(1)A/F27

Nextdue Share EarliestDUE:1. T A/R | 2. RE -Electronic flight instrument system (EFIS) - Concurrent Requ...2003-22-12 Paragraph (k)A/F27

Nextdue Share EarliestDUE:1. T A/R | 2. RE -Electronic flight instrument system (EFIS) - Concurrent Requ...2003-22-12 Paragraph (l)A/F27

Nextdue Share EarliestDUE:1. T A/R | 2. RE -Electronic flight instrument system (EFIS) - Alternative Met...2003-22-12 Paragraph (n)A/F27

Mandatory ≈20-Feb-2016RE2003-22-12 (Left) Paragraph

(h)

Electronic flight instrument system (EFIS) - Measurement, Repetitive Measurement and Corrective Actions

22-Mar-2013Mos

14.1 Hrs12,055.330011,755.3Hrs

Ldg

27 A/FSBEff: 12-Dec-2003 Complied

With

Compliance Share DoubleDUE:1. T A/R | 2. RE -Special Check/Rework - Stall Protection System - Angle-of-At...A601-0550 Rev 1A/F27

Mandatory ≈20-Feb-2016RE2003-22-12 (Right) Paragraph

(h)

Electronic flight instrument system (EFIS) - Measurement, Repetitive Measurement and Corrective Actions

22-Mar-2013Mos

14.1 Hrs12,055.330011,755.3Hrs

Ldg

27 A/FSBEff: 12-Dec-2003 Complied

With


MandatoryT (A/R)2003-22-12 Paragraph (a) Electronic flight instrument system (EFIS) - Revision of Airplane Flight Manual (AFM)

Mos

Hrs

Ldg

27 A/FEff: 12-Dec-2003









MandatoryT (A/R)2003-22-12 Paragraph (d) Electronic flight instrument system (EFIS) - All AOA Vane Angles Within Tolerances: Disconnection and Measurement

Mos

Hrs

Ldg

27 A/FEff: 12-Dec-2003


MandatoryT (A/R)2003-22-12 Paragraph (e) Electronic flight instrument system (EFIS) - One or More AOA Vane Angles Outside Tolerances, but All AOA Vane Angles Within Expanded Tolerances.

Mos

Hrs

Ldg

27 A/FEff: 12-Dec-2003


MandatoryT (A/R)2003-22-12 Paragraph (f) Electronic flight instrument system (EFIS) - Any AOA Vane Angle Outside Tolerances

Mos

Hrs

Ldg

27 A/FEff: 12-Dec-2003


MandatoryT (A/R)2003-22-12 Paragraph (j)(1) Electronic flight instrument system (EFIS) - inspect the left- and right-side AOA vane decal to verify that the correct decal is installed. For Model Cl-600-2A12 (CL-601)

and CL-600-2B16 (CL-601-3A and 3R)

Mos

Hrs

Ldg

27 A/FEff: 12-Dec-2003

Compliance Share DoubleDUE:1. T A/R | 2. RE -Special Check/Rework - Stall Protection System - Inspection ...A601-0519A/F27

MandatoryT (A/R)2003-22-12 Paragraph (k) Electronic flight instrument system (EFIS) - Concurrent Requirements: Corrective Actions - Replace the AOA vane decal(s) with new vane decal(s), and ensure that the

new decal(s) is the correct type.

Mos

Hrs

Ldg

27 A/FEff: 12-Dec-2003

Compliance Share DoubleDUE:1. T A/R | 2. RE -Special Check/Rework - Stall Protection System - Inspection ...A601-0519A/F27

MandatoryT (A/R)2003-22-12 Paragraph (l) Electronic flight instrument system (EFIS) - Concurrent Requirements: Corrective Actions - Remove existing decal(s), and do the alignment check(s) of the AOA vane

transducer.

Mos

Hrs

Ldg

27 A/FEff: 12-Dec-2003


MandatoryT (A/R)2003-22-12 Paragraph (n) Electronic flight instrument system (EFIS) - Alternative Methods of Compliance.(refer to TLMC Chapter 5 task 27-35-04-101* for recurring inspection)

Mos

Hrs

Ldg

27 A/FEff: 12-Dec-2003

MandatoryRE (-)2004-09-37 Inboard flap actuator beam

05-Jun-2009Mos

11,458.6Hrs

5,902Ldg

27 A/FSB A601-0532Eff: 11-Jun-2004 Complied

With

Nextdue Share EarliestDUE: 6,565 Ldg1. T 1300 Ldg | 2. RE 100 LdgInboard flap actuator beam - Inspection/Repetitive Inspectio...2004-09-37 Paragraph (a)(b)A/F27

Nextdue Share EarliestDUE:1. RE -Inboard flap actuator beam - Terminating Actions (using para...2004-09-37 Paragraph (d)(e)A/F27

Nextdue Share EarliestDUE:1. RE -Inboard flap actuator beam - Terminating Actions (using para...2004-09-37 Paragraph (d)(f)A/F27









Mandatory ≈09-Oct-2016T2004-09-37 Paragraph (a)(b) Inboard flap actuator beam - Inspection/Repetitive Inspection

Mos

Hrs

239 Ldg≈6,5651,300Ldg

27 A/FEff: 11-Jun-2004

Compliance Share DoubleDUE:1. T A/R | 2. RE -Special Check/Modification - Flaps - Inspect Vane Brackets f...A601-0532 Rev 1A/F27

MandatoryRE (-)2004-09-37 Paragraph (d)(e) Inboard flap actuator beam - Terminating Actions (using paragraph (e))

Mos

Hrs

Ldg

27 A/FEff: 11-Jun-2004


MandatoryRE (-)2004-09-37 Paragraph (d)(f) Inboard flap actuator beam - Terminating Actions (using paragraph (f))

Mos

Hrs

Ldg

27 A/FEff: 11-Jun-2004


MandatoryRE (-)2004-25-19 Premature wear of the potentiometers in AOA transducers having a certain part number.

15-Apr-2005Mos

10,732.6Hrs

5,457Ldg

27 A/FBY AOA TRANSDUCER P/NEff: 04-Jan-2005 Not

Applicable

Nextdue Share EarliestDUE:1. T 7 Days | 2. RE -Premature wear of the potentiometers in AOA transducers havi...2004-25-19 Paragraph (f)A/F27

Nextdue Share EarliestDUE:1. RE -Premature wear of the potentiometers in AOA transducers havi...2004-25-19 Paragraph (g) LeftA/F27

Nextdue Share EarliestDUE:1. RE -Premature wear of the potentiometers in AOA transducers havi...2004-25-19 Paragraph (g) RightA/F27

MandatoryRE (-)2004-25-19 Paragraph (f) Premature wear of the potentiometers in AOA transducers having a certain part number - Airplane Flight Manual (AFM) Revisions.

15-Apr-2005Mos

10,732.6Hrs

5,457Ldg

27 A/FREVISED AFMEff: 04-Jan-2005 Complied

With

MandatoryRE (-)2004-25-19 Paragraph (g) Left Premature wear of the potentiometers in AOA transducers having certain part number - Repetitive Tests

Mos

Hrs

Ldg

27 A/FEff: 04-Jan-2004

Compliance Share DoubleDUE:1. T A/R | 2. RE -Special Check - Stall Protection System - Angle-of-Attack (A...A601-0571A/F27

MandatoryRE (-)2004-25-19 Paragraph (g)

Right

Premature wear of the potentiometers in AOA transducers having certain part number - Repetitive Tests

Mos

Hrs

Ldg

27 A/FEff: 04-Jan-2005

Compliance Share DoubleDUE:1. T A/R | 2. RE -Special Check - Stall Protection System - Angle-of-Attack (A...A601-0571A/F27

MandatoryRE (-)2005-26-04 Lower Gimbal Pin

26-Sep-2006Mos

10,897.5Hrs

5,558Ldg

27 A/FASB A601-0555Eff: 25-Jan-2006 Complied

With

Compliance Share DoubleDUE:1. T A/R | 2. RE -Special Check/Modification - Horizontal Stabilizer Trim Cont...601-0555A/F27









MandatoryRE (-)2006-02-04 Rudder balance spring assembly

20-Jan-2007Mos

10,976.2Hrs

5,614Ldg

27 A/FASB 601-0549Eff: 24-Feb-2006 Complied

With

Compliance Share DoubleDUE:1. T A/R | 2. RE -Modification - Rudder Control - Introduction of an Adjustabl...601-0549A/F27

MandatoryRE (-)2009-14-03 Flight Controls

23-Sep-2009Mos

11,459.7Hrs

5,904Ldg

27 A/FAFM REVISIONEff: 12-Aug-2009 Complied

With

MRB ≈18-Sep-2016RE27-11-00-201 Aileron, Flap Actuators and Attachments Visual Check

10-Feb-2016Mos

290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs

6,326Ldg

(PKG 300 Hour)

27 A/F


MRB ≈03-May-2017RE27-11-00-202 Aileron Control Check aileron backlash

10-Feb-2016Mos

590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs

6,326Ldg

(PKG 600 Hour)

27 A/F


MRB ≈03-May-2017RE27-11-11-203 Tension Regulator Operational Test - Tension Regulator

10-Feb-2016Mos

590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs

6,326Ldg

(PKG 600 Hour)

27 A/F


MRB ≈20-Oct-2017RE27-13-11-204 Anti-Float Mechanism Operational Test - Anti-Float Mechanism

29-Oct-2012Mos

812.3 Hrs (+40)(12,853.5)-/+401,20011,653.5Hrs

Ldg

(PKG 1200 Hour)

27 A/F


MRB ≈03-May-2017RE27-13-21-205 Aileron Flutter Dampers - Check aileron flutter damper / Check flutter damper shear pin

10-Feb-2016Mos

590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs

6,326Ldg

Left

(PKG 600 Hour)

27 A/F

600-75142-3HA13712


MRB ≈03-May-2017RE27-13-21-205 Aileron Flutter Dampers - Check aileron flutter damper / Check flutter damper shear pin

10-Feb-2016Mos

590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs

6,326Ldg

Right

(PKG 600 Hour)

27 A/F

600-75142-9HA13913


MRB ≈24-Aug-2023RE27-13-21-206 Aileron Flutter Dampers - Remove, carry out “Testing and Fault Isolation” of Flutter Dampers and reinstall

08-Aug-2005Mos

3,618.6 Hrs (+40)(15,659.8)-/+404,80010,859.8Hrs

Ldg

Left

(PKG 4800 Hour)

27 A/F

600-75142-3HA13712

Ref.:CMM/PSP 608/608A 27-09-01, Ref.:CMM/PSP 608/608A 27-13-21, Ref.:CMM/PSP 608/608A 27-13-22 (SOURCE: TLMC 05-20-15)









MRB ≈24-Aug-2023RE27-13-21-206 Aileron Flutter Dampers - Remove, carry out “Testing and Fault Isolation” of Flutter Dampers and reinstall

08-Aug-2005Mos

3,618.6 Hrs (+40)(15,659.8)-/+404,80010,859.8Hrs

Ldg

Right

(PKG 4800 Hour)

27 A/F

600-75142-9HA13913


MRB ≈03-May-2017RE27-15-00-207 Roll Disconnect Mechanism Functional Test

10-Feb-2016Mos

590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs

6,326Ldg

(PKG 600 Hour)

27 A/F


MRB ≈18-Sep-2016RE27-17-00-208 Aileron Power Control Unit Operational Test

10-Feb-2016Mos

290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs

6,326Ldg

(PKG 300 Hour)

27 A/F


MRB ≈03-May-2017RE27-17-00-209 Aileron Power Control Unit Visual Check, paying particular attention for hydraulic fluidleakage

10-Feb-2016Mos

590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs

6,326Ldg

(PKG 600 Hour)

27 A/F


MRB ≈03-May-2017RE27-21-00-210 Rudder Control Check Rudder Backlash- Check PCU Input Load Limiter Travel - Visual Check of the following: (1) Load limiter balancing spring / (2) PCU input and

centering mechanism / (3) Rudder centering, preload and feel springs / (4) PCU’s for hydraulic fluid leakage

10-Feb-2016Mos

590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs

6,326Ldg

(PKG 600 Hour)

27 A/F


MRB ≈13-Jul-2017RE27-21-00-211 Rudder Control Rudder Anti-Jam Mechanism Functional Test

18-Oct-2003Mos

684 Hrs (+30)(12,725.2)-/+402,4009,808.2Hrs

Ldg

(PKG 2400 Hour)

27 A/F


MRB ≈18-Sep-2016RE27-25-00-212 Rudder Power Control Units Operational Test

10-Feb-2016Mos

290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs

6,326Ldg

(PKG 300 Hour)

27 A/F


MRB ≈13-Jul-2017RE27-30-00-235 Pitch Control System Pitch Trim Suppressor Unit - Bench Check

24-Oct-2004Mos

684 Hrs (+30)(12,725.2)-/+402,40010,459Hrs

Ldg

(PKG 2400 Hour)

27 A/F

Ref.:CMM/PSP 608/608A 27-30-04 (SOURCE: TLMC 05-20-15)

MRB ≈03-May-2017RE27-31-00-213 Elevator Control Check elevator backlash - Check PCU Input Jam Tolerant Mechanism Travel - Visual Check of the following: (1) Load limiter balancing springs (2 per

side) / (2) PCU input and centering mechanisms / (3) PCU’s for hydraulic fluid leakage

10-Feb-2016Mos

590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs

6,326Ldg

(PKG 600 Hour)

27 A/F


MRB ≈20-Oct-2017RE27-31-00-214 Elevator Control (Pre SB 601-0304) Visual Check of elevator control levers, Part Numbers 600-92354-7, 600-92358-1 and 600-92359-1, paying particular attention for

cracks in the hub area where the taper pinis installed

29-Oct-2012Mos

812.3 Hrs (+40)(12,853.5)-/+401,20011,653.5Hrs

Ldg

(PKG 1200 Hour)

27 A/F










MRB ≈24-Oct-2017RE27-31-00-215 Elevator Control Elevator load limiters test

21-Oct-2004Mos

817.8 Hrs (+40)12,859-/+402,40010,459Hrs

Ldg

(PKG 2400 Hour)

27 A/F


AWL ≈07-Nov-2016RE27-31-11-101 Pitch Feel Simulator - Functional Test of the Pitch Feel Simulator

26-Sep-2006Mos

356.3 Hrs12,397.51,50010,897.5Hrs

Ldg



AWL ≈07-Nov-2016RE27-31-11-101 Pitch Feel Simulator - Functional Test of the Pitch Feel Simulator

26-Sep-2006Mos

356.3 Hrs12,397.51,50010,897.5Hrs

Ldg



MRB ≈03-May-2017RE27-33-11-216 Elevator Flutter Dampers - Check elevator flutter damper

10-Feb-2016Mos

590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs

6,326Ldg

Left Inboard

(PKG 600 Hour)

27 A/F

1018100-7HA13933



10-Feb-2016Mos

590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs

6,326Ldg

Left Outboard

(PKG 600 Hour)

27 A/F

1018100-7HA13911



10-Feb-2016Mos

590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs

6,326Ldg

Right Inboard

(PKG 600 Hour)

27 A/F

1018100-7HA13910



10-Feb-2016Mos

590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs

6,326Ldg

Right Outboard

(PKG 600 Hour)

27 A/F

1018100-7HA13919


MRB ≈24-Aug-2023RE27-33-11-217 Elevator Flutter Dampers - Remove, carry out “Testing and Fault Isolation” of Flutter Damper and reinstall

08-Aug-2005Mos

3,618.6 Hrs (+40)(15,659.8)-/+404,80010,859.8Hrs

Ldg

Left Inboard

(PKG 4800 Hour)

27 A/F

1018100-7HA13933



08-Aug-2005Mos

3,618.6 Hrs (+40)(15,659.8)-/+404,80010,859.8Hrs

Ldg

Left Outboard

(PKG 4800 Hour)

27 A/F

1018100-7HA13911











08-Aug-2005Mos

3,618.6 Hrs (+40)(15,659.8)-/+404,80010,859.8Hrs

Ldg

Right Inboard

(PKG 4800 Hour)

27 A/F

1018100-7HA13910



08-Aug-2005Mos

3,618.6 Hrs (+40)(15,659.8)-/+404,80010,859.8Hrs

Ldg

Right Outboard

(PKG 4800 Hour)

27 A/F

1018100-7HA13919


MRB ≈03-May-2017RE27-35-00-218 Pitch Disconnect Mechanism Operational Test

10-Feb-2016Mos

590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs

6,326Ldg

(PKG 600 Hour)

27 A/F


MRB ≈18-Sep-2016RE27-37-00-219 Elevator Power Control Units Operational Test

10-Feb-2016Mos

290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs

6,326Ldg

(PKG 300 Hour)

27 A/F


AWLRE (N/A)27-39-00-101 Stall Protection System (SPS) (Pre SB 601-0510) - Functional Test of the Flap Input

Mos

Hrs

Ldg

27 A/F


AWLRE (N/A)27-39-00-102 Stall Protection System (SPS) (Pre SB 601-0510) - Functional Test of the Phase Advance and Sideslip Compensation

Mos

Hrs

Ldg

27 A/F


AWL ≈03-Nov-2024RE27-39-00-103 Stall Protection System (SPS) (Post SB 601-0510) - Functional Test of the Flap and Sideslip Compensation Monitor

25-Jul-2008Mos

4,190.8 Hrs16,2324,80011,432Hrs

Ldg

27 A/F


AWL ≈07-Nov-2016RE27-39-00-104 * Stall Protection System (SPS), Stick Pusher Capstan Shaft - Functional Test of the Stick Pusher Capstan Shaft, Part No. 600-59156-7 (Vendor Part No. 501-1258-01)

26-Sep-2006Mos

356.3 Hrs12,397.51,50010,897.5Hrs

Ldg



MRB ≈03-May-2017RE27-39-00-220 Stall Protection System Operational Test

10-Feb-2016Mos

590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs

6,326Ldg

(PKG 600 Hour)

27 A/F


MRB ≈13-Jul-2017RE27-39-00-221 Stall Protection System Functional Test

04-May-2004Mos

684 Hrs (+30)(12,725.2)-/+402,40010,325.2Hrs

Ldg

(PKG 2400 Hour)

27 A/F










AWL ≈20-Feb-2016RE27-39-11-101 * Angle-of-Attack Vane Transducer Linearity - Functional Test of the Angle-of-Attack (AOA) Transducer Linearity

22-Mar-2013Mos

14.1 Hrs12,055.330011,755.3Hrs

Ldg



AWL ≈20-Feb-2016RE27-39-11-101 * Angle-of-Attack Vane Transducer Linearity - Functional Test of the Angle-of-Attack (AOA) Transducer Linearity

22-Mar-2013Mos

14.1 Hrs12,055.330011,755.3Hrs

Ldg

Right27 A/F600-59154-1247-098


AWLRE (N/A)27-39-11-102 * Angle-of-Attack Vane Transducer, Restoration - Overhaul of the Angle-of-Attack (AOA) Transducer,

Mos

Hrs

Ldg



AWLRE (N/A)27-39-11-102 * Angle-of-Attack Vane Transducer, Restoration - Overhaul of the Angle-of-Attack (AOA) Transducer,

Mos

Hrs

Ldg

Right27 A/F600-59154-1247-098


AWL ≈03-May-2017RE27-40-00-102 * Trim System Actuator Brake - Operational Test

10-Feb-2016Mos

590.8 Hrs12,63260012,041.2Hrs

6,326Ldg

27 A/F


MRB ≈03-May-2017RE27-40-00-222 Horizontal Stabilizer Trim Control Pitch trim actuator backlash check

10-Feb-2016Mos

590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs

6,326Ldg

(PKG 600 Hour)

27 A/F


MRB ≈20-Oct-2017RE27-40-00-238 Pitch Trim Actuator - Lubricate horizontal stabilizer pitch trim actuator

29-Oct-2012Mos

812.3 Hrs (+40)(12,853.5)-/+401,20011,653.5Hrs

Ldg

(PKG 1200 Hour)

27 A/F


AWL ≈19-Mar-2018RE27-40-16-101 * Pitch Trim Actuator - Overhaul

11-Mar-2000Mos

1,011.7 Hrs13,052.96,6006,452.9Hrs

Ldg

27 A/F600-92301-65346E

Ref:MM/PSP 608/608A (SOURCE: TLMC 05-10-30)

MRB ≈03-May-2017RE27-40-16-223 Pitch Trim Actuator - Inspect pitch trim actuator

10-Feb-2016Mos

590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs

6,326Ldg

(PKG 600 Hour)

27 A/F


AWL ≈04-Jul-2020RE27-50-16-101 * Outboard Flap Actuator - Restoration of the Outboard Flap Actuator

12-May-2010Mos

Hrs

1,584 Ldg7,9102,0005,910Ldg

Left Inboard27 A/F600-93000-82UNKNOWN

(SOURCE: TLMC 05-10-30) (NOTE: For Component where flight cycles are Unknown)










12-May-2010Mos

Hrs

1,584 Ldg7,9102,0005,910Ldg

Left Outboard27 A/F600-93000-93UNKNOWN



12-May-2010Mos

Hrs

1,584 Ldg7,9102,0005,910Ldg

Right Inboard27 A/F600-93000-82UNKNOWN



12-May-2010Mos

Hrs

1,584 Ldg7,9102,0005,910Ldg

Right Outboard27 A/F600-93000-93UNKNOWN


MRB ≈15-Jun-2016RE27-50-16-224 Flap Actuator - Outboard flap actuator backlash check

18-Oct-2003Mos

167 Hrs (+40)12,208.2-/+402,4009,808.2Hrs

Ldg

(PKG 2400 Hour)

27 A/F

(SOURCE: TLMC 05-20-15) (NOTE: Both the inboard and outboard actuators of the outboard flap are to be checked.)

MRB ≈03-May-2017RE27-50-16-236 Flap Actuator Detailed Inspection

10-Feb-2016Mos

590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs

6,326Ldg

(PKG 600 Hour)

27 A/F


MRB ≈24-Oct-2017RE27-50-16-237 Flap Actuator Torque and Side Play Check

23-Oct-2004Mos

817.8 Hrs (+40)12,859-/+402,40010,459Hrs

Ldg

(PKG 2400 Hour)

27 A/F


MRB ≈03-May-2017RE27-50-21-225 Power Drive Unit (PDU) Operational Test of flap PDU motor brake

10-Feb-2016Mos

590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs

6,326Ldg

(PKG 600 Hour)

27 A/F


MRB ≈03-May-2017RE27-50-26-226 Asymmetry/Overspeed Detector and Brake Brake drag torque test

10-Feb-2016Mos

590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs

6,326Ldg

(PKG 600 Hour)

27 A/F


MRB ≈03-May-2017RE27-50-41-227 Flexible Drive Shaft Check flexible drive shaft casing

10-Feb-2016Mos

590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs

6,326Ldg

(PKG 600 Hour)

27 A/F


Servicing - Recommended ≈24-Aug-2018RE27-50-41-301 Flexible Drive Shaft - Check flexible drive shaft casing / Check flexible drive shaft inner core

08-Aug-2005Mos

1,218.6 Hrs (+40)13,259.8-/+402,40010,859.8Hrs

Ldg

(PKG 2400 Hour)

27 A/F

(ZONE: 500, 600) (ACCESS: 571/671-CB-FB, 581/681-AB-BB-CB-DB-EB-FB-GB) (SOURCE: MPD 3.2)









MRB ≈03-May-2017RE27-61-00-229 Spoiler Control Visual Check of Flight Spoiler and Ground Spoiler Actuators, Attachments and Mechanisms, paying particular attention to the flight spoiler track roller,

cam and detent assembly for wear and freedom of movement

10-Feb-2016Mos

590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs

6,326Ldg

(PKG 600 Hour)

27 A/F


MRB ≈03-May-2017RE27-61-00-230 Spoiler Control (A/C 3001 to 3059 with SB 601-0113 NOT incorporated) - Operational Test of throttle switches

10-Feb-2016Mos

590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs

6,326Ldg

(PKG 600 Hour)

27 A/F


MRB ≈18-Sep-2016RE27-61-00-231 Spoiler Control/Scheduled Servicing Lubricate Flight Spoilers Flexshaft and Controlex Cable end

10-Feb-2016Mos

290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs

6,326Ldg

(PKG 300 Hour)

27 A/F


MRB ≈14-Oct-2016RE27-61-00-233 Spoiler Control (Pre SB 601-0113) Ground Spoiler/Thrust Reverser Separation Diode Test

11-Dec-2003Mos

325.5 Hrs (+40)12,366.7-/+402,4009,966.7Hrs

Ldg

(PKG 2400 Hour)

27 A/F


MRB ≈03-May-2017RE27-65-00-234 Flight Spoiler Power Control Units Operational Test

10-Feb-2016Mos

590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs

6,326Ldg

(PKG 600 Hour)

27 A/F


MRB ≈18-Sep-2016RE27-69-00-228 Ground Spoiler Actuators and Manifold Assembly (Pre SB 601-0224) Check Mechanical Locking Mechanism

10-Feb-2016Mos

290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs

6,326Ldg

(PKG 300 Hour)

27 A/F


RecommendedRE (-)601-0020 Modification - Ground Spoiler Position Indication - Wiring Changes

Mos

Hrs

Ldg

27 A/F

RecommendedT (A/R)601-0020 Rev 1 Modification - Ground Spoiler Position Indication - Wiring Changes

Mos

Hrs

Ldg

27 A/FEff: 23-Oct-1984

OptionalRE (-)601-0035 Modification - Stall Protection System - Angle-of-Attack Vane Decal

Mos

Hrs

Ldg

27 A/F

OptionalRE (-)601-0035 Rev 1 Modification - Stall Protection System - Angle-of-Attack Vane Decal

01-Sep-1983Mos

0Hrs

0Ldg


RecommendedRE (-)601-0036 Modification - Flight Spoiler Push/Pull Controls, Aileron Cables and and Flap Flexible Drive Shafts - Improved Clearances

Mos

Hrs

Ldg

27 A/F









RecommendedRE (-)601-0036 Rev 1 Modification - Flight Spoiler Push/Pull Controls, Aileron Cables and and Flap Flexible Drive Shafts - Improved Clearances

Mos

Hrs

Ldg

27 A/F

RecommendedRE (-)601-0036 Rev 2 Modification - Flight Spoiler Push/Pull Controls, Aileron Cables and and Flap Flexible Drive Shafts - Improved Clearances

17-Sep-1983Mos

0Hrs

0Ldg


RecommendedRE (-)601-0037 Modification - Flight Spoilers - Fillers and Toggles

Mos

Hrs

Ldg

27 A/FEff: 23-Jan-1984

OptionalRE (-)601-0040 Modification - Warning System - Flight Spoilers

17-Sep-1983Mos

0Hrs

0Ldg

27 A/FComplied With

OptionalT (A/R)601-0040 Rev 1 Modification - Warning System - Flight Spoilers

Mos

Hrs

Ldg

27 A/FEff: 09-Apr-1985

RecommendedRE (-)601-0055 Modification - Proximity Sensors - Rework

21-Feb-1995Mos

3,142Hrs

1,250Ldg

27 A/FComplied With

RecommendedT (A/R)601-0055 Rev 1 Modification - Proximity Sensors - Rework

Mos

Hrs

Ldg

27 A/FEff: 30-Jan-1986

RecommendedT (A/R)601-0058 Modification - Inboard Flaps - Forward Fairing Support Structure

Mos

Hrs

Ldg

27 A/FEff: 05-Apr-1985

RecommendedRE (-)601-0083 Special Check/Modification - Ailerons - Mixer Support Brackets

04-Sep-1985Mos

607Hrs

261Ldg


RecommendedRE (-)601-0085 Modification - Elevator Controls - Replacement of Guard Pin and Addition of Rub Strip

12-Sep-1985Mos

607Hrs

261Ldg


RecommendedRE (-)601-0090 Modification - Proximity Sensors - Improved Sealing

Mos

Hrs

Ldg

27 A/F









RecommendedRE (-)601-0090 Rev 1 Modification - Proximity Sensors - Improved Sealing

28-Mar-1989Mos

2,373Hrs

910Ldg


RecommendedRE (-)601-0095 Modification - Flight Spoiler Warning System - Elimination of Spurious Warnings

18-Sep-1985Mos

607Hrs

261Ldg


RecommendedRE (-)601-0102 Modification - Lateral Accelerometers - Improved Installation

Mos

Hrs

Ldg

27 A/F

RecommendedRE (-)601-0102 Rev 1 Modification - Lateral Accelerometers - Improved Installation

23-Mar-1992Mos

Hrs

Ldg


OptionalRE (-)601-0113 Modification - Ground Spoilers - Auto-Deployment

Mos

Hrs

Ldg

27 A/F

OptionalRE (-)601-0113 Rev 1 Modification - Ground Spoilers - Auto-Deployment

Mos

Hrs

Ldg

27 A/F

OptionalT (A/R)601-0113 Rev 2 Modification - Ground Spoilers - Auto-Deployment

Mos

Hrs

Ldg

27 A/FEff: 14-Dec-1987

RecommendedRE (-)601-0133 Modification - Outboard Flap Bute Doors - Hinge Pin Retention

16-Jul-1986Mos

952Hrs

403Ldg


RecommendedRE (-)601-0136 Modification - Horizontal Stabilizer Trim Control - Transient Suppression Addition

Mos

Hrs

Ldg

27 A/F

RecommendedRE (-)601-0136 Rev 1 Modification - Horizontal Stabilizer Trim Control - Transient Suppression Addition

26-Jan-1987Mos

1,267Hrs

480Ldg


RecommendedRE (-)601-0170 Special Check/Modification - Aileron Controls Pulley Brackets - Attachment Bolts

26-Jan-1987Mos

1,267Hrs

480Ldg










OptionalRE (-)601-0176 Stall Protection System - Stick Shaker

Mos

Hrs

Ldg

27 A/F

OptionalRE (-)601-0176 Rev 1 Stall Protection System - Stick Shaker

Mos

Hrs

Ldg

27 A/F

OptionalRE (-)601-0176 Rev 2 Stall Protection System - Stick Shaker

Mos

Hrs

Ldg

27 A/F

OptionalT (A/R)601-0176 Rev 3 Stall Protection System - Stick Shaker

Mos

Hrs

Ldg

27 A/FEff: 31-Aug-1995

RecommendedRE (-)601-0189 Special Check/Modification - Horizontal Stabilizer - Pitch Trim Actuator

Mos

Hrs

Ldg

27 A/FEff: 18-Aug-1986

RecommendedRE (-)601-0199 Special Check/Adjustment - Elevator - Wire Harness Reroute

01-Dec-1990Mos

3,058.6Hrs

1,212Ldg


RecommendedRE (-)601-0204 Special Check/Modification - Rudder Control Yokes - Stop Bolt Clearance

07-Mar-1989Mos

2,373Hrs

910Ldg


OptionalRE (-)601-0224 Modification - Ground Spoiler Actuators - Deletion of Life-Limiting Locks

Mos

Hrs

Ldg

27 A/F

OptionalT (A/R)601-0224 Rev 1 Modification - Ground Spoiler Actuators - Deletion of Life-Limiting Locks

Mos

Hrs

Ldg

27 A/FEff: 13-Jul-1990

RecommendedRE (-)601-0228 Wing Outboard Flaps - Identification Plates

Mos

Hrs

Ldg

27 A/FEff: 06-Oct-1987

RecommendedRE (-)601-0237 Modification - Stall Protection System - Computer Reliability Improvement

25-Apr-1988Mos

1,995Hrs

756Ldg

27 A/FComplied With









RecommendedT (A/R)601-0237 Rev 1 Modification - Stall Protection System - Computer Reliability Improvement

Mos

Hrs

Ldg

27 A/FEff: 21-Dec-1989

OptionalT (A/R)601-0243 Modification - Aileron and Flight Spoiler Control Cables - Turnbuckle Relocation

Mos

Hrs

Ldg

27 A/FEff: 14-Mar-1988

RecommendedRE (-)601-0304 Special Check/Modification - Elevator Control Levers - Stress Corrosion

Mos

Hrs

Ldg

27 A/F

RecommendedRE (-)601-0304 Rev 1 Special Check/Modification - Elevator Control Levers - Stress Corrosion

21-Nov-1997Mos

Hrs

Ldg


RecommendedRE (-)601-0312 Flap Actuators - Retaining Ring

24-Jan-1990Mos

2,653Hrs

1,022Ldg


OptionalRE (-)601-0319 Modification - Aileron Flutter Dampers - Replacement

05-Aug-2003Mos

9,585.6Hrs

4,797Ldg


RecommendedRE (-)601-0426 Special Check/Modification - Rudder Quadrant Assembly - Introduction of Sub-Assembly, Part No. K600-92600-3 or -7

Mos

Hrs

Ldg

27 A/F

RecommendedRE (-)601-0426 Rev 1 Special Check/Modification - Rudder Quadrant Assembly - Introduction of Sub-Assembly, Part No. K600-92600-3 or -7

28-Apr-1995Mos

4,555Hrs

1,824Ldg


RecommendedRE (-)601-0438 Modification - Flap System - Asymmetry/Overspeed Detector and Brake Unit Wiring Harness

30-Sep-1994Mos

4,399Hrs

1,768Ldg


RecommendedRE (-)601-0440 Modification - Flap Actuators - Attachment Bolt Replacement

26-Jan-1996Mos

4,785Hrs

1,932Ldg


RecommendedRE (-)601-0457 Modification - Stall Protection System - Safety Stick Shaker Connector with Lockwire

06-Oct-1995Mos

4,704Hrs

1,894Ldg










OptionalT (A/R)601-0458 Modification - Flap Control Unit - Addition of Ground Studs and Shielded Wires

Mos

Hrs

Ldg

27 A/FEff: 15-Sep-1995

RecommendedRE (-)601-0477 Modification - Flap System - Introduction of New Proximity Switches in the Brake Detector Unit (BDU)

12-Nov-1997Mos

5,395Hrs

2,274Ldg


OptionalRE (-)601-0479 Modification - Stall Protection System Addition of a Time Delay Relay

Mos

Hrs

Ldg

27 A/F

OptionalRE (-)601-0479 Rev 1 Modification - Stall Protection System Addition of a Time Delay Relay

23-Mar-2001Mos

Hrs

Ldg


RecommendedRE (-)601-0498 Special Check/Rework - Control-Column Torque-Tube - Support Bearings and Pitch Disconnect Cable

05-Jan-2000Mos

Hrs

Ldg


Nextdue Share EarliestDUE:1. T 400 Hrs | 2. RE -Special Check/Rework - Control-Column Torque-Tube - Support ...601-0498 Part AA/F27

Nextdue Share EarliestDUE:1. T 400 Hrs | 2. RE -Special Check/Rework - Control-Column Torque-Tube - Support ...601-0498 Part BA/F27

Nextdue Share EarliestDUE:1. T 1200 Hrs | 2. RE -Special Check/Rework - Control-Column Torque-Tube - Support ...601-0498 Part CA/F27

Nextdue Share EarliestDUE:1. T A/R | 2. RE -Special Check/Rework - Control-Column Torque-Tube - Support ...601-0498 Part DA/F27

RecommendedRE (-)601-0498 Part A Special Check/Rework - Control-Column Torque-Tube - Support Bearings and Pitch Disconnect Cable

Mos

Hrs

Ldg

27 A/FEff: 29-Oct-1999

RecommendedRE (-)601-0498 Part B Special Check/Rework - Control-Column Torque-Tube - Support Bearings and Pitch Disconnect Cable

Mos

Hrs

Ldg

27 A/FEff: 29-Oct-1999

RecommendedRE (-)601-0498 Part C Special Check/Rework - Control-Column Torque-Tube - Support Bearings and Pitch Disconnect Cable

Mos

Hrs

Ldg

27 A/FEff: 29-Oct-1999

(NOTE: Recommended in less than 1,200 flight hours after the ServiceBulletin release date, if necessary as a result of PART A)

RecommendedT (A/R)601-0498 Part D Special Check/Rework - Control-Column Torque-Tube - Support Bearings and Pitch Disconnect Cable

Mos

Hrs

Ldg

27 A/FEff: 29-Oct-1999

(NOTE: Recommended before the next flight, if necessary as a resultof PART B.)

RecommendedRE (-)601-0510 Modification - Stall Protection System - Dormant Failures in the Stall Protection system (SPS) Computer

05-Jun-2009Mos

11,458.6Hrs

5,902Ldg










RecommendedRE (-)601-0549 Modification - Rudder Control - Introduction of an Adjustable Balance Spring Assembly for the Rudder Control Surface

20-Jan-2007Mos

10,976.2Hrs

5,614Ldg


RecommendedRE (-)601-0553 Modification - Wing Flap System - Serialization of Flap Actuator Beams

05-Aug-2003Mos

9,585.6Hrs

4,797Ldg


RecommendedRE (-)601-0555 Special Check/Modification - Horizontal Stabilizer Trim Control - Possible Migration of the Horizontal Stabilizer Trim Actuator (HSTA) Lower Gimbal Pin

26-Sep-2006Mos

10,897.5Hrs

5,558Ldg


RecommendedRE (-)601-0563 Special Check/Rework - Elevator System - Pitch Feel Simulator Disconnect Check and Replacement of Bearing and Lever Assembly

Mos

Hrs

Ldg

27 A/F

Nextdue Share EarliestDUE:1. RE -Special Check/Rework - Elevator System - Pitch Feel Simulato...601-0563 Part AA/F27

Nextdue Share EarliestDUE:1. RE -Special Check/Rework - Elevator System - Pitch Feel Simulato...601-0563 Part BA/F27

Nextdue Share EarliestDUE:1. RE -Special Check/Rework - Elevator System - Pitch Feel Simulato...601-0563 Part CA/F27

Nextdue Share EarliestDUE:1. RE -Special Check/Rework - Elevator System - Pitch Feel Simulato...601-0563 Part DA/F27

RecommendedRE (-)601-0563 Part A Special Check/Rework - Elevator System - Pitch Feel Simulator - Do a check of PFS serial number

25-Jul-2008Mos

11,432Hrs

5,881Ldg


RecommendedRE (-)601-0563 Part B Special Check/Rework - Elevator System - Pitch Feel Simulator Disconnect Check

25-Jul-2008Mos

11,432Hrs

5,881Ldg


RecommendedRE (-)601-0563 Part C Special Check/Rework - Elevator System - Pitch Feel Simulator Disconnect Check - Repeat check

25-Jul-2008Mos

11,432Hrs

5,881Ldg

27 A/FEff: 27-Feb-2004 Not Applicable

RecommendedRE (-)601-0563 Part D Special Check/Rework - Elevator System - Pitch Feel Simulator Disconnect Check and Replacement of Bearing and Lever Assembly

25-Jul-2008Mos

11,432Hrs

5,881Ldg


RecommendedT (A/R)601-0563 Rev 1 Special Check/Rework - Elevator System - Pitch Feel Simulator Disconnect Check and Replacement of Bearing and Lever Assembly

Mos

Hrs

Ldg

27 A/FEff: 07-Nov-2005

Nextdue Share EarliestDUE:1. T A/R | 2. RE -Special Check/Rework - Elevator System - Pitch Feel Simulato...601-0563 Rev 1 Part AA/F27

Nextdue Share EarliestDUE:1. T A/R | 2. RE -Special Check/Rework - Elevator System - Pitch Feel Simulato...601-0563 Rev 1 Part BA/F27

Nextdue Share EarliestDUE:1. T A/R | 2. RE -Special Check/Rework - Elevator System - Pitch Feel Simulato...601-0563 Rev 1 Part CA/F27

Nextdue Share EarliestDUE:1. T A/R | 2. RE -Special Check/Rework - Elevator System - Pitch Feel Simulato...601-0563 Rev 1 Part DA/F27









RecommendedT (A/R)601-0563 Rev 1 Part A Special Check/Rework - Elevator System - Pitch Feel Simulator - Do a check of PFS serial number

Mos

Hrs

Ldg

27 A/FEff: 07-Nov-2005

RecommendedT (A/R)601-0563 Rev 1 Part B Special Check/Rework - Elevator System - Pitch Feel Simulator Disconnect Check

Mos

Hrs

Ldg

27 A/FEff: 07-Nov-2005

RecommendedT (A/R)601-0563 Rev 1 Part C Special Check/Rework - Elevator System - Pitch Feel Simulator Disconnect Check - Repeat check

Mos

Hrs

Ldg

27 A/FEff: 07-Nov-2005

RecommendedT (A/R)601-0563 Rev 1 Part D Special Check/Rework - Elevator System - Pitch Feel Simulator Disconnect Check and Replacement of Bearing and Lever Assembly

Mos

Hrs

Ldg

27 A/FEff: 07-Nov-2005

RecommendedT (A/R)601-0566 Special Check/Rework - Wing Flap System - Outboard Flap Actuators with Non-Conformant Trunnion Block Rotation

Mos

Hrs

Ldg

27 A/FEff: 31-Mar-2004

RecommendedRE (-)601-0576 Modification - Rudder - Replacement of Rudder System Stop Bolt Part No. 600-92689-1

Mos

Hrs

Ldg

27 A/F

RecommendedT (A/R)601-0576 Rev 1 Modification - Rudder - Replacement of Rudder System Stop Bolt Part No. 600-92689-1

Mos

Hrs

Ldg

27 A/FEff: 30-Aug-2006

OptionalRE (-)601-0577 Modification – Stall Protection System (SPS) – Introduction of Improved AOA Transducer Mounting and Sealing Installation

Mos

Hrs

Ldg

27 A/F

OptionalT (A/R)601-0577 Rev 1 Modification – Stall Protection System (SPS) – Introduction of Improved AOA Transducer Mounting and Sealing Installation

Mos

Hrs

Ldg

27 A/FEff: 27-Apr-2009

RecommendedT (A/R)601-0626 Modification – Horizontal Stabilizer Trim-Actuating System (HSTA) –Serialization of the Actuator Pins

1.9 Years[25-Feb-2018]Mos

689.6 Hrs[12,730.8]Hrs

Ldg

27 A/FEff: 25-Feb-2013

RecommendedT (-)601-0643 Special Check/Modification - Rudder Control System - Replace the Pilot's Rudder Pedal Bar Assembly or Rudder Pedal Assembly

Mos

Hrs

Ldg

27 A/FEff: 31-Aug-2015









RecommendedRE (-)601-0643 Rev 1 Special Check/Modification - Rudder Control System - Replace the Pilot's Rudder Pedal Bar Assembly or Rudder Pedal Assembly

Mos

Hrs

Ldg

27 A/FEff: 31-Mar-2016

(AVG MAN HRS: 12)

MandatoryRE (-)82-01-01 Left and Right Controlex Cables

18-Sep-1985Mos

Hrs

Ldg

27 A/FBY AIRCRAFT SERIAL NUMBEREff: 04-Jan-1982 Not

Applicable

MandatoryRE (-)82-04-05 Aileron Power Control Unit

18-Sep-1985Mos

607Hrs

261Ldg

27 A/FBY AIRCRAFT SERIAL NUMBEREff: 04-Mar-1982 Not

Applicable

MandatoryRE (-)82-06-06 Flap Drive Shafts

18-Sep-1985Mos

607Hrs

261Ldg


Applicable

MandatoryRE (-)83-07-51 R1 Flap Vane Support Assembly

18-Sep-1985Mos

Hrs

Ldg


Compliance Share DoubleDUE:1. RE -Special Check/Modification - Wing Inboard Flap - Vane and As...A601-0010 Rev 2A/F27

MandatoryRE (-)94-08-15 Inspect Shoulder Bolts & Flap Actuator Housings

17-Jun-1994Mos

Hrs

Ldg

27 A/FASB A601-0415Eff: 20-May-1994 Complied

With

Compliance Share DoubleDUE:1. T 10 Hrs | 2. RE -Special Check - Flap Actuators - Attachment BoltsA601-0415A/F27

Mandatory ≈21-Feb-2016RE95-17-14 Horizontal Stabilizer Trim Actuator

07-Sep-2008Mos

14.5 Hrs12,055.760011,455.7Hrs

5,898Ldg

27 A/FSI A601-0443Complied With

Compliance Share DoubleDUE:1. RE -Special Check/Modification - Horizontal Stabilizer Trim Actu...A601-0443A/F27

MandatoryRE (-)95-18-07 Inspect Rudder Control Quadrant

30-Nov-1995Mos

Hrs

Ldg

27 A/FSI A601-0426Eff: 30-Oct-1995 Complied

With

Compliance Share DoubleDUE:1. T A/R | 2. RE -Special Check/Modification - Rudder Quadrant Assembly - Intr...601-0426 Rev 1A/F27

AlertRE (-)A601-0004 Special Check/Modificatiopn – Flap Structure – Wing Outboard Flap Vane and Associated Structure

06-Jan-2005Mos

11,613.3Hrs

6,021Ldg

27 A/FPART A - VISUAL INSPECTIONComplied With

AlertRE (-)A601-0004 Rev 1 Special Check/Modificatiopn – Flap Structure – Wing Outboard Flap Vane and Associated Structure

Mos

Hrs

Ldg

27 A/F









AlertRE (-)A601-0004 Rev 2 Special Check/Modificatiopn – Flap Structure – Wing Outboard Flap Vane and Associated Structure

Mos

Hrs

Ldg

27 A/F

Alert ≈28-Feb-2017RE (-)A601-0004 Rev 3 Special Check/Modificatiopn – Flap Structure – Wing Outboard Flap Vane and Associated Structure

13-Nov-2015Mos

Hrs

379 Ldg[6,705]6,305Ldg

27 A/FEff: 22-Nov-1984

AlertRE (-)A601-0010 Special Check/Modification - Wing Inboard Flap - Vane and Associated Structure

20-Sep-1983Mos

0Hrs

0Ldg

27 A/FAT MANUFACTUTREComplied With

AlertRE (-)A601-0010 Rev 1 Special Check/Modification - Wing Inboard Flap - Vane and Associated Structure

Mos

Hrs

Ldg

27 A/F

AlertRE (-)A601-0010 Rev 2 Special Check/Modification - Wing Inboard Flap - Vane and Associated Structure

Mos

Hrs

Ldg

27 A/FEff: 22-Dec-1983

AlertT (A/R)A601-0056 Modification - Surface Trim Indicator - Replacement

Mos

Hrs

Ldg

27 A/FEff: 16-Mar-1984

AlertT (A/R)A601-0081 Special Check/Modification - No. 3 Hydraulic System Lines and Fittings - Clearance with Rudder

Mos

Hrs

Ldg

27 A/FEff: 14-Sep-1984

AlertRE (-)A601-0145 Modification - Pitch Trim Actuator - Yoke Pin Retention

27-Jan-1987Mos

0Hrs

Ldg


AlertRE (-)A601-0332 Modification - Stall Protection System - Stick Pusher

Mos

Hrs

Ldg

27 A/F

AlertRE (-)A601-0332 Rev 1 Modification - Stall Protection System - Stick Pusher

04-Oct-1990Mos

Hrs

Ldg


AlertRE (-)A601-0415 Special Check - Flap Actuators - Attachment Bolts

21-May-1993Mos

Hrs

Ldg










AlertRE (-)A601-0421 Special Check/Modification - Rudder Control Quadrant Assembly

Mos

Hrs

Ldg

27 A/F

AlertRE (-)A601-0421 Rev 1 Special Check/Modification - Rudder Control Quadrant Assembly

Mos

Hrs

Ldg

27 A/F

AlertRE (-)A601-0421 Rev 2 Special Check/Modification - Rudder Control Quadrant Assembly

31-Oct-1993Mos

Hrs

Ldg


AlertRE (-)A601-0443 Special Check/Modification - Horizontal Stabilizer Trim Actuator (HSTA) - Overspeed Condition

Mos

Hrs

Ldg

27 A/F

Nextdue Share EarliestDUE:1. RE -Special Check/Modification - Horizontal Stabilizer Trim Actu...A601-0443 Part AA/F27

Nextdue Share EarliestDUE:1. RE -Special Check/Modification - Horizontal Stabilizer Trim Actu...A601-0443 Part BA/F27

Nextdue Share EarliestDUE:1. RE -Special Check/Modification - Horizontal Stabilizer Trim Actu...A601-0443 Part CA/F27

AlertRE (-)A601-0443 Part A Special Check/Modification - Horizontal Stabilizer Trim Actuator (HSTA) - HSTA brake operational check, if necessary do trouble-shooting of HSTA brake.

Mos

Hrs

Ldg

27 A/FEff: 11-Jan-1995

AlertRE (-)A601-0443 Part B Special Check/Modification - Horizontal Stabilizer Trim Actuator (HSTA) - Do a trouble-Shooting of the Pitch trim Overspeed Condition

Mos

Hrs

Ldg

27 A/FEff: 11-Jan-1995

AlertRE (-)A601-0443 Part C Special Check/Modification - Horizontal Stabilizer Trim Actuator (HSTA) - HSTA Replacement

Mos

Hrs

Ldg

27 A/FEff: 11-Jan-1995

AlertRE (-)A601-0443 Rev 1 Special Check/Modification - Horizontal Stabilizer Trim Actuator (HSTA) - Overspeed Condition

Mos

Hrs

Ldg

27 A/F

Nextdue Share EarliestDUE:1. RE -Special Check/Modification - Horizontal Stabilizer Trim Actu...A601-0443 Rev 1 Part AA/F27

Nextdue Share EarliestDUE:1. RE -Special Check/Modification - Horizontal Stabilizer Trim Actu...A601-0443 Rev 1 Part BA/F27

Nextdue Share EarliestDUE:1. RE -Special Check/Modification - Horizontal Stabilizer Trim Actu...A601-0443 Rev 1 Part CA/F27

AlertRE (-)A601-0443 Rev 1 Part A Special Check/Modification - Horizontal Stabilizer Trim Actuator (HSTA) - HSTA brake operational check, if necessary do trouble-shooting of HSTA brake.

Mos

Hrs

Ldg

27 A/F









AlertRE (-)A601-0443 Rev 1 Part B Special Check/Modification - Horizontal Stabilizer Trim Actuator (HSTA) - Do a trouble-Shooting of the Pitch trim Overspeed Condition

Mos

Hrs

Ldg

27 A/F

AlertRE (-)A601-0443 Rev 1 Part C Special Check/Modification - Horizontal Stabilizer Trim Actuator (HSTA) - HSTA Replacement

Mos

Hrs

Ldg

27 A/F

AlertRE (-)A601-0443 Rev 2 Special Check/Modification - Horizontal Stabilizer Trim Actuator (HSTA) - Overspeed Condition

07-Sep-2008Mos

11,455.7Hrs

5,898Ldg


Nextdue Share EarliestDUE:1. T A/R | 2. RE -Special Check/Modification - Horizontal Stabilizer Trim Actu...A601-0443 Rev 2 Part AA/F27

Nextdue Share EarliestDUE:1. T A/R | 2. RE -Special Check/Modification - Horizontal Stabilizer Trim Actu...A601-0443 Rev 2 Part BA/F27

Nextdue Share EarliestDUE:1. T A/R | 2. RE -Special Check/Modification - Horizontal Stabilizer Trim Actu...A601-0443 Rev 2 Part CA/F27

AlertT (A/R)A601-0443 Rev 2 Part A Special Check/Modification - Horizontal Stabilizer Trim Actuator (HSTA) - HSTA brake operational check, if necessary do trouble-shooting of HSTA brake.

Mos

Hrs

Ldg

27 A/FEff: 15-May-1996

AlertT (A/R)A601-0443 Rev 2 Part B Special Check/Modification - Horizontal Stabilizer Trim Actuator (HSTA) - Do a trouble-Shooting of the Pitch trim Overspeed Condition

Mos

Hrs

Ldg

27 A/FEff: 15-May-1996

AlertT (A/R)A601-0443 Rev 2 Part C Special Check/Modification - Horizontal Stabilizer Trim Actuator (HSTA) - HSTA Replacement

Mos

Hrs

Ldg

27 A/FEff: 15-May-1996

AlertRE (-)A601-0519 Special Check/Rework - Stall Protection System - Inspection and Replacement of Angle-of-Attack (AOA) Vane Decals

18-Nov-2003Mos

Hrs

Ldg


AlertRE (-)A601-0532 Special Check/Modification - Flaps - Inspect Vane Brackets for Cracks, Replace Brackets and Remove Gaps Between Brackets and Mating Surfaces

05-Aug-2003Mos

9,585.6Hrs

4,797Ldg

27 A/FComplied With

Nextdue Share EarliestDUE:1. RE -Special Check/Modification - Flaps - Inspect Vane Brackets f...A601-0532 Part AA/F27

Nextdue Share EarliestDUE:1. RE -Special Check/Modification - Flaps - Inspect Vane Brackets f...A601-0532 Part BA/F27

Nextdue Share EarliestDUE:1. RE -Special Check/Modification - Flaps - Inspect Vane Brackets f...A601-0532 Part CA/F27

AlertRE (-)A601-0532 Part A Special Check/Modification - Flaps - Inspect Vane Brackets for Cracks, Replace Brackets and Remove Gaps Between Brackets and Mating Surfaces - Visual Inpection

Mos

Hrs

Ldg

27 A/FEff: 29-Nov-2001









AlertRE (-)A601-0532 Part B Special Check/Modification - Flaps - Inspect Vane Brackets for Cracks, Replace Brackets and Remove Gaps Between Brackets and Mating Surfaces - do a nondestructive

inspection (NDI)

Mos

Hrs

Ldg

27 A/FEff: 29-Nov-2001

AlertRE (-)A601-0532 Part C Special Check/Modification - Flaps - Inspect Vane Brackets for Cracks, Replace Brackets and Remove Gaps Between Brackets and Mating Surfaces - Replace all 12 vane

brackets aned remove all gaps.

Mos

Hrs

Ldg

27 A/FEff: 29-Nov-2001

AlertT (A/R)A601-0532 Rev 1 Special Check/Modification - Flaps - Inspect Vane Brackets for Cracks, Replace Brackets and Remove Gaps Between Brackets and Mating Surfaces

Mos

Hrs

Ldg

27 A/FEff: 08-Jul-2002

Nextdue Share EarliestDUE:1. T A/R | 2. RE -Special Check/Modification - Flaps - Inspect Vane Brackets f...A601-0532 Rev 1 Part AA/F27

Nextdue Share EarliestDUE:1. T A/R | 2. RE -Special Check/Modification - Flaps - Inspect Vane Brackets f...A601-0532 Rev 1 Part BA/F27

Nextdue Share EarliestDUE:1. T A/R | 2. RE -Special Check/Modification - Flaps - Inspect Vane Brackets f...A601-0532 Rev 1 Part CA/F27

AlertT (A/R)A601-0532 Rev 1 Part A Special Check/Modification - Flaps - Inspect Vane Brackets for Cracks, Replace Brackets and Remove Gaps Between Brackets and Mating Surfaces - Visual Inpection

Mos

Hrs

Ldg

27 A/FEff: 08-Jul-2002

AlertT (A/R)A601-0532 Rev 1 Part B Special Check/Modification - Flaps - Inspect Vane Brackets for Cracks, Replace Brackets and Remove Gaps Between Brackets and Mating Surfaces - do a nondestructive

inspection (NDI)

Mos

Hrs

Ldg

27 A/FEff: 08-Jul-2002

AlertT (A/R)A601-0532 Rev 1 Part C Special Check/Modification - Flaps - Inspect Vane Brackets for Cracks, Replace Brackets and Remove Gaps Between Brackets and Mating Surfaces - Replace all 12 vane

brackets aned remove all gaps.

Mos

Hrs

Ldg

27 A/FEff: 08-Jul-2002

AlertRE (-)A601-0540 Special Check - Flaps - Visually Examine Flap Actuator Beam Vane Brackets for Possible Cracks

01-Mar-2009Mos

Hrs

Ldg


AlertRE (-)A601-0550 Special Check/Rework - Stall Protection System - Angle-of-Attack (AOA) Transducer Tolerance Check and Rework of Out-of-Tolerance AOA Transducer Assemblies

Mos

Hrs

Ldg

27 A/F

Nextdue Share EarliestDUE:1. RE -Special Check/Rework - Stall Protection System - Angle-of-At...A601-0550 Part AA/F27

Nextdue Share EarliestDUE:1. RE -Special Check/Rework - Stall Protection System - Rework of O...A601-0550 Part BA/F27

AlertRE (-)A601-0550 Part A Special Check/Rework - Stall Protection System - Angle-of-Attack (AOA) Transducer Tolerance Check

18-Nov-2003Mos

9,901.1Hrs

4,981Ldg










AlertRE (-)A601-0550 Part B Special Check/Rework - Stall Protection System - Rework of Out-of-Tolerance AOA Transducer Assemblies

Mos

Hrs

Ldg

27 A/FEff: 07-Jan-2002

AlertT (A/R)A601-0550 Rev 1 Special Check/Rework - Stall Protection System - Angle-of-Attack (AOA) Transducer Tolerance Check and Rework of Out-of-Tolerance AOA Transducer Assemblies

Mos

Hrs

Ldg

27 A/FEff: 27-Feb-2004

Nextdue Share EarliestDUE:1. T A/R | 2. RE -Special Check/Rework - Stall Protection System - Angle-of-At...A601-0550 Rev 1 Part AA/F27

Nextdue Share EarliestDUE:1. T A/R | 2. RE -Special Check/Rework - Stall Protection System - Rework of O...A601-0550 Rev 1 Part BA/F27

AlertT (A/R)A601-0550 Rev 1 Part A Special Check/Rework - Stall Protection System - Angle-of-Attack (AOA) Transducer Tolerance Check

Mos

Hrs

Ldg

27 A/FEff: 27-Feb-2004

AlertT (A/R)A601-0550 Rev 1 Part B Special Check/Rework - Stall Protection System - Rework of Out-of-Tolerance AOA Transducer Assemblies

Mos

Hrs

Ldg

27 A/FEff: 27-Feb-2004

AlertT (A/R)A601-0571 Special Check - Stall Protection System - Angle-of-Attack (AOA) Transducer Linearity Check

Mos

Hrs

Ldg

27 A/FEff: 14-Oct-2004

MandatoryRE (-)CF-2002-05R1 Paragraph 1 Bombardier CL-600 “Challenger” – Angle of Attack Transducer, AFM Temporary Revision

Mos

Hrs

Ldg

27 A/FEff: 30-Jul-2004

MandatoryRE (-)CF-2002-05R1 PART A Bombardier CL-600 “Challenger” – Angle of Attack Transducer - Special Check

Mos

Hrs

Ldg

27 A/FEff: 30-Jul-2004

MandatoryRE (-)CF-2004-22 PART B Bombardier CL-600 “Challenger” – Angle of Attack Vane, Transducer Linearity Check

Mos

Hrs

Ldg

27 A/FEff: 26-Oct-2004

▼ 28 - FUEL

RE (O/C)2-Way APU Fuel Valve

20-Sep-1983Mos

0Hrs0

0Ldg0

28 A/FNewAV16E1295

UNKNOWN

RE (O/C)3-Way APU Fuel Valve

20-Sep-1983Mos

0Hrs0

0Ldg0

28 A/FNewAV23B1149-1

UNKNOWN









RE (O/C)Aux Fuel Quantity Transmitter

20-Sep-1983Mos

0Hrs0

0Ldg0

Left28 A/FNew391002-421

UNKNOWN

RE (O/C)Aux Fuel Quantity Transmitter

20-Sep-1983Mos

0Hrs0

0Ldg0


UNKNOWN

RE (O/C)Float Valve

20-Sep-1983Mos

0Hrs

0Ldg

Auxiliary28 A/FUnknownUnknown

RE (O/C)Float Valve

16-Aug-2002Mos

8,715.1Hrs

4,273Ldg

No.128 A/F2760131-1030813

RE (O/C)Float Valve

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Fuel Ejector Pump

20-Sep-1983Mos

0Hrs0

0Ldg0

Left28 A/FNew2780602-104

UNKNOWN

RE (O/C)Fuel Ejector Pump

20-Sep-1983Mos

0Hrs0

0Ldg0


UNKNOWN

RE (O/C)Fuel Motorized Shutoff Valve

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Fuel Pump DC Cartridge

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Fuel Pump DC Cartridge

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Fuel Quantity Indicator

06-Apr-2004Mos

10,270.9Hrs

5,187Ldg

28 A/F478-286-102186









RE (O/C)Fuel Quantity Transmitter

20-Sep-1983Mos

0Hrs

0Ldg



20-Sep-1983Mos

0Hrs

0Ldg



20-Sep-1983Mos

0Hrs

0Ldg



20-Sep-1983Mos

0Hrs

0Ldg



20-Sep-1983Mos

0Hrs

0Ldg



20-Sep-1983Mos

0Hrs

0Ldg



20-Sep-1983Mos

0Hrs

0Ldg



20-Sep-1983Mos

0Hrs

0Ldg



20-Sep-1983Mos

0Hrs0

0Ldg0

No.328 A/FNew391002-438

UNKNOWN


20-Sep-1983Mos

0Hrs

0Ldg



20-Sep-1983Mos

0Hrs

0Ldg











20-Sep-1983Mos

0Hrs

0Ldg



20-Sep-1983Mos

0Hrs

0Ldg



20-Sep-1983Mos

0Hrs

0Ldg



20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Fuel Scavenger Ejector Pump

20-Sep-1983Mos

0Hrs0

0Ldg0

Left28 A/FNew2780472-102

UNKNOWN

RE (O/C)Fuel Scavenger Ejector Pump

20-Sep-1983Mos

0Hrs0

0Ldg0


UNKNOWN

RE (O/C)Fuel Shutoff Valve

26-Sep-2006Mos

10,897.5Hrs

5,558Ldg

Left28 A/F601-62900-1P80257

RE (O/C)Fuel Shutoff Valve

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Fuel Tank Vent Valve

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Fuel Transfer Ejector Pump

26-Sep-2006Mos

10,897.5Hrs

5,558Ldg

Left28 A/F2780473-1030200

RE (O/C)Fuel Transfer Ejector Pump

26-Sep-2006Mos

10,897.5Hrs

5,558Ldg

Right28 A/F2780473-103010









RE (O/C)No. 1 Pressure Switch

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)No. 2 Pressure Switch

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Shutoff Valve

20-Sep-1983Mos

0Hrs

0Ldg

Auxiliary28 A/FUnknownUnknown


20-Sep-1983Mos

0Hrs0

0Ldg0

Left28 A/FNew2760129-101

UNKNOWN


20-Sep-1983Mos

0Hrs0

0Ldg0


UNKNOWN

RE (O/C)Signal Conditioner

20-Sep-1983Mos

0Hrs0

0Ldg0

28 A/FNew473382

UNKNOWN

RE (O/C)Tank Fuel Vent Valve

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Tank Fuel Vent Valve

20-Sep-1983Mos

0Hrs0

0Ldg0

No.228 A/FNew2780491-105

UNKNOWN

RE (O/C)Transfer Float Valve

26-Mar-2007Mos

11,045.9Hrs

5,659Ldg

Left28 A/F2950022-1020857

RE (O/C)Transfer Float Valve

20-Sep-1983Mos

0Hrs

0Ldg


MRBRE (N/A)28-10-00-201 Fuel Storage (Post SB 601-0262) Visual Check of tail tank vent line (external to tank)

Mos

Hrs

Ldg

28 A/F










MRBRE (N/A)28-10-00-202 Fuel Storage (Post SB 601-0262) Visual Check of aft cone and lower fairing, paying particularattention for fuel leakage, damage to Strobe Light/Power Supply/Dump

Valve Wiring

Mos

Hrs

Ldg

28 A/F


MRBRE (N/A)28-10-00-203 Fuel Storage (Post SB 601-0262) Visual Check of tail tank internal and external structure andcomponents, paying particular attention for corrosion andleakage

Mos

Hrs

Ldg

28 A/F


MRB ≈03-May-2017RE28-10-00-225 Fuel Tank Gravity Filler Cap Remove, inspect for condition and re-install

10-Feb-2016Mos

590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs

6,326Ldg

(PKG 600 Hour)

28 A/F


MRB ≈30-Dec-2016RE28-10-11-204 Fuel Tanks Check Fuel Tanks for Leaks- Visual Check (external), paying particular attention for corrosion

05-Feb-2004Mos

426.1 Hrs (+40)12,467.3-/+402,40010,067.3Hrs

Ldg

(PKG 2400 Hour)

28 A/F


MRBRE28-10-21-206 Forward and Aft Auxiliary Fuel Tanks External Check

5.8 Months (+30

Days)(26-Sep-2016)-/+16024-Oct-2011Mos

Hrs

Ldg

(PKG 60 Month)

28 A/F


MRBRE28-10-21-207 Forward and Aft Auxiliary Fuel Tanks External Check (Using Borescope)

5.8 Months (+30

Days)26-Sep-2016-/+112026-Sep-2006Mos

Hrs

Ldg

28 A/F


MRBRE28-10-31-205 Fuel and Vent Line Shrouds Fuselage tank wall interspace and associated shrouds pressuretest

5.8 Months (+30

Days)(26-Sep-2016)-/+16024-Oct-2011Mos

Hrs

Ldg

(PKG 60 Month)

28 A/F


MRBRE28-10-31-208 Fuel and Vent Line Shrouds Pressure test of the following shrouds: (1) APU Negative G Fuel Feed Line / (2) APU Fuel Return Line / (3) APU Fuel Feed Line / (4) Engine

Fuel Feed Line / (5) Motive Flow Line / (6) Fuselage Vent Lines

5.8 Months (+30

Days)(26-Sep-2016)-/+16024-Oct-2011Mos

Hrs

Ldg

(PKG 60 Month)

28 A/F


MRBRE28-10-31-209 Fuel and Vent Line Shrouds (Post SB 601-0262) Tail tank fuel shroud pressure test

5.8 Months (+30

Days)(26-Sep-2016)6024-Oct-2011Mos

Hrs

Ldg

(PKG 60 Month)

28 A/F


MRB ≈18-Sep-2016RE28-10-31-211 Fuel and Vent Line Shrouds Visual Check of the Vent and Distribution Shroud Drains forBlockage and Leakage

10-Feb-2016Mos

290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs

6,326Ldg

(PKG 300 Hour)

28 A/F










MRBRE (N/A)28-10-36-210 Tail Tank Vent System (Post SB 601-0262) Vent line check valve inspection

Mos

Hrs

Ldg

28 A/F


MRB ≈29-Dec-2030RE28-21-11-212 Collector Tanks Collector Tank Flapper Check Valves Check

05-Aug-2003Mos

7,144.4 Hrs (+40)(19,185.6)-/+409,6009,585.6Hrs

Ldg

(PKG 9600 Hour)

28 A/F


MRB ≈14-Oct-2016RE28-21-16-213 Firewall Fuel Shutoff Valve Internal leakage check

11-Dec-2003Mos

325.5 Hrs (+40)12,366.7-/+402,4009,966.7Hrs

Ldg

(PKG 2400 Hour)

28 A/F


MRBRE28-21-26-215 Scavenge Fuel Ejector Visual Check of pump screen

5.8 Months (+30

Days)(26-Sep-2016)-/+16024-Oct-2011Mos

Hrs

Ldg

(PKG 60 Month)

28 A/F


MRBRE (N/A)28-22-00-216 Tail Tank Fuel Transfer System/Pressure Refuel/Defuel System (Post SB 601-0262) Visual Check of all tail tank fuel lines at R.H.belly fairing (wing fillet), paying

particular attention for fuel leakage and corrosion

Mos

Hrs

Ldg

28 A/F


MRBRE (N/A)28-22-00-217 Tail Tank Fuel Transfer System (Post SB 601-0262) Fuel transfer functional test

Mos

Hrs

Ldg

28 A/F


MRBRE (N/A)28-22-05-218 Tail Tank Fuel Transfer Line Check Valve (Post SB 601-0262) Remove and install new valve

Mos

Hrs

Ldg

28 A/F


MRBRE (N/A)28-22-11-219 Rotor Burst Detection System (Post SB 601-0262) Rotor burst detection system - shroud pressure check

Mos

Hrs

Ldg

28 A/F


MRBRE (N/A)28-22-11-220 Rotor Burst Detection System (Post SB 601-0262) Functional Test

Mos

Hrs

Ldg

28 A/F


MRBRE (N/A)28-22-16-221 Tail Tank System Level Switches (Post SB 601-0262) Warning system before fuel operational test

Mos

Hrs

Ldg

28 A/F










MRBRE (N/A)28-22-21-222 Tail Tank Shutoff Valves (Post SB 601-0262) Shutoff valves internal leakage check

Mos

Hrs

Ldg

28 A/F


MRB ≈24-Aug-2023RE28-25-21-223 APU Return Line Check Valve Remove Check Valve and Perform Internal Leakage Test

08-Aug-2005Mos

3,618.6 Hrs (+40)(15,659.8)-/+404,80010,859.8Hrs

Ldg

(PKG 4800 Hour)

28 A/F


MRBRE (N/A)28-30-11-224 Fuel Jettison System (Post SB 601-0262) Fuel jettison system functional test

Mos

Hrs

Ldg

28 A/F


RecommendedRE (-)601-0018 Modification - Main Auxiliary Fuel Tank - Level Control Valve (LCV)

Mos

Hrs

Ldg

28 A/F

RecommendedRE (-)601-0018 Rev 1 Modification - Main Auxiliary Fuel Tank - Level Control Valve (LCV)

Mos

Hrs

Ldg

28 A/FEff: 23-Apr-1984

RecommendedRE (-)601-0033 Special Check/Modification - Main and Auxiliary Fuel Tanks - Fuel Capacity

Mos

Hrs

Ldg

28 A/F

RecommendedT (A/R)601-0033 Rev 1 Special Check/Modification - Main and Auxiliary Fuel Tanks - Fuel Capacity

Mos

Hrs

Ldg

28 A/FEff: 13-Feb-1987

OptionalRE (-)601-0063 Modification - Fuel Booster Pumps - Replacement of Fuel Pump Canisters and Cartridges

Mos

Hrs

Ldg

28 A/F

OptionalRE (-)601-0063 Rev 1 Modification - Fuel Booster Pumps - Replacement of Fuel Pump Canisters and Cartridges

Mos

Hrs

Ldg

28 A/F

OptionalT (A/R)601-0063 Rev 2 Modification - Fuel Booster Pumps - Replacement of Fuel Pump Canisters and Cartridges

Mos

Hrs

Ldg

28 A/FEff: 06-Jul-1988

RecommendedRE (-)601-0075 Special Check/Modification - Fuel Quantity System - Wiring

Mos

Hrs

Ldg

28 A/FEff: 04-May-1985









RecommendedRE (-)601-0114 Modification - Fuel Pressure Switches - Replacement

18-Sep-1985Mos

607Hrs

261Ldg


RecommendedT (A/R)601-0117 Modification - Forward Auxiliary Fuel Tank - Transfer Drain Line

Mos

Hrs

Ldg

28 A/FEff: 30-Apr-1985

OptionalT (A/R)601-0160 Modification - Forward and Aft Auxiliary Fuel Tanks - Vent Shroud Line Sealing Plugs

Mos

Hrs

Ldg

28 A/FEff: 29-Apr-1987

RecommendedRE (-)601-0209 Modification - Transfer Ejector Screens - Addition

23-Mar-1992Mos

3,584Hrs

1,446Ldg


RecommendedRE (-)601-0213 Modification - Main Fuel Tank Level Control Valves - Wiring Conduits

Mos

Hrs

Ldg

28 A/F

RecommendedT (A/R)601-0213 Rev 1 Modification - Main Fuel Tank Level Control Valves - Wiring Conduits

Mos

Hrs

Ldg

28 A/FEff: 21-Jun-1988

RecommendedRE (-)601-0217 Modification - Refuel/Defuel System - Fuel Spillage Prevention

Mos

Hrs

Ldg

28 A/F

RecommendedRE (-)601-0217 Rev 1 Modification - Refuel/Defuel System - Fuel Spillage Prevention

Mos

Hrs

Ldg

28 A/F


Mos

Hrs

Ldg

28 A/F


01-Oct-1991Mos

Hrs

Ldg


RecommendedRE (-)601-0220 Modification - Motive Flow Fuel Line - Rerouting

Mos

Hrs

Ldg

28 A/FEff: 11-May-1988









RecommendedRE (-)601-0222 Modification - Motive Flow Line Fittings - Identification

Mos

Hrs

Ldg

28 A/F

RecommendedRE (-)601-0222 Rev 1 Modification - Motive Flow Line Fittings - Identification

28-Mar-1989Mos

2,373Hrs

910Ldg


RecommendedRE (-)601-0223 Modification - Refuel/Defuel System - Fuel Line Clearance

Mos

Hrs

Ldg

28 A/FEff: 24-Aug-1987

OptionalRE (-)601-0225 Modification - Fuel Balancing System - Powered Crossfeed System

Mos

Hrs

Ldg

28 A/F

OptionalT (A/R)601-0225 Rev 1 Modification - Fuel Balancing System - Powered Crossfeed System

Mos

Hrs

Ldg

28 A/FEff: 23-Mar-1990

RecommendedRE (-)601-0229 Modification - Motive Flow Lines - Addition of Spiral Wrap

Mos

Hrs

Ldg

28 A/F

RecommendedRE (-)601-0229 Rev 1 Modification - Motive Flow Lines - Addition of Spiral Wrap

Mos

Hrs

Ldg

28 A/F

RecommendedRE (-)601-0229 Rev 2 Modification - Motive Flow Lines - Addition of Spiral Wrap

28-Mar-1989Mos

2,373Hrs

910Ldg


OptionalRE (-)601-0262 Modification - Fuel Storage - Tail Cone Fuel Tank Addition

Mos

Hrs

Ldg

28 A/F

OptionalRE (-)601-0262 Rev 1 Modification - Fuel Storage - Tail Cone Fuel Tank Addition

Mos

Hrs

Ldg

28 A/F

OptionalRE (-)601-0262 Rev 2 Modification - Fuel Storage - Tail Cone Fuel Tank Addition

Mos

Hrs

Ldg

28 A/F









OptionalT (A/R)601-0262 Rev 3 Modification - Fuel Storage - Tail Cone Fuel Tank Addition

Mos

Hrs

Ldg

28 A/FEff: 23-Jan-1992

OptionalT (A/R)601-0274 Modification - Refuel/Defuel Control Panel - Cover Assembly Rework

Mos

Hrs

Ldg

28 A/FEff: 14-Jul-1988

RecommendedRE (-)601-0318 Modification - NACA Scoop Vent Line - Deletion of Check Valve

Mos

Hrs

Ldg

28 A/F

RecommendedRE (-)601-0318 Rev 1 Modification - NACA Scoop Vent Line - Deletion of Check Valve

Mos

Hrs

Ldg

28 A/F

RecommendedRE (-)601-0318 Rev 2 Modification - NACA Scoop Vent Line - Deletion of Check Valve

02-Nov-1992Mos

Hrs

Ldg


RecommendedRE (-)601-0320 Modification - Primary Ejector Pump and Fuel Feed Tube - Connector Assembly

Mos

Hrs

Ldg

28 A/F

RecommendedRE (-)601-0320 Rev 1 Modification - Primary Ejector Pump and Fuel Feed Tube - Connector Assembly

06-Oct-1992Mos

Hrs

Ldg


RecommendedRE (-)601-0355 Modification - Tail Cone Fuel Tank - Addition of Back Up Pump

Mos

Hrs

Ldg

28 A/FEff: 27-Mar-1992

RecommendedRE (-)601-0361 Modification - Auxiliary Tank Fuel Lines - Elimination of Possible Chafing

Mos

Hrs

Ldg

28 A/F

RecommendedRE (-)601-0361 Rev 1 Modification - Auxiliary Tank Fuel Lines - Elimination of Possible Chafing

21-Feb-1991Mos

3,142Hrs

1,250Ldg


RecommendedRE (-)601-0362 Modification - Tail Cone Fuel Tank - Improvements Double Click For Further Effectivity

Mos

Hrs

Ldg

28 A/FEff: 27-Mar-1992









RecommendedRE (-)601-0364 Special Check/Modification - Wing Tank Fuel Access Panels - Introduction of Conductive Gasket

12-Oct-1992Mos

3,754Hrs

1,519Ldg


OptionalRE (-)601-0371 Fuel Tanks - Replacement Of Float Switches

Mos

Hrs

Ldg

28 A/FEff: 27-Mar-1992

RecommendedRE (-)601-0386 Modification - Tail Cone Fuel Tank - Replacement of Dump Valve Support Bracket and/or Flanged Fitting

Mos

Hrs

Ldg

28 A/FEff: 27-Mar-1992

RecommendedRE (-)601-0391 Special Check/Rework - Tail Cone Fuel Tank - Lightning Protection

Mos

Hrs

Ldg

28 A/FEff: 27-Jan-1992

RecommendedRE (-)601-0392 Special Check/Modification - RH Engine Fuel Feed Line - Clearance with Fourteenth (14th) Stage Bleed Air Shutoff Valve

Mos

Hrs

Ldg

28 A/F

RecommendedT (A/R)601-0392 Rev 1 Special Check/Modification - RH Engine Fuel Feed Line - Clearance with Fourteenth (14th) Stage Bleed Air Shutoff Valve

Mos

Hrs

Ldg

28 A/FEff: 15-Jan-1993

RecommendedRE (-)601-0435 Modification - Wing Tank Fuel Access Panels, Part No. 601R10906-17 and Conductive Gasket Part No. 600-10910-3

28-Apr-1995Mos

4,555Hrs

1,824Ldg


OptionalT (A/R)601-0508 Modification - Tail Tank System - Prevent False Low Fuel Indication

Mos

Hrs

Ldg

28 A/FEff: 31-May-1999

RecommendedRE (-)601-0513 Modification - Engine Standby and Auxiliary Power Unit (APU) Fuel Feed Systems - Replacement of Flexible Fuel Hoses

11-Dec-2001Mos

7,908.6Hrs

3,787Ldg


RecommendedT (A/R)601-0525 Special Check/Modification - Fuel Feed System - Examine For Chafing on the Fuel Feed Lines and Add Brackets and Clamps

Mos

Hrs

Ldg

28 A/FEff: 30-Nov-1999

Nextdue Share EarliestDUE:1. T A/R | 2. RE -Special Check/Modification - Fuel Feed System - Examine For ...601-0525 Part AA/F28

Nextdue Share EarliestDUE:1. T A/R | 2. RE -Special Check/Modification - Fuel Feed System - Examine For ...601-0525 Part BA/F28


Generated: 6-Apr-2016 1:16 PM100/429







RecommendedT (A/R)601-0525 Part A Special Check/Modification - Fuel Feed System - Examine For Chafing on the Fuel Feed Lines and Add Brackets and Clamps - Special Check

Mos

Hrs

Ldg

28 A/FEff: 30-Nov-1999

RecommendedT (A/R)601-0525 Part B Special Check/Modification - Fuel Feed System - Examine For Chafing on the Fuel Feed Lines and Add Brackets and Clamps - Rework

Mos

Hrs

Ldg

28 A/FEff: 30-Nov-1999

OptionalRE (-)601-0530 Modification - Fuel Storage - Removal of forward Auxiliary Fuel tank

Mos

Hrs

Ldg

28 A/FEff: 17-Dec-1999

OptionalT (A/R)601-0535 Modification - Fuel Storage - Deactivation of Forward Auxiliary Fuel Tank

Mos

Hrs

Ldg

28 A/FEff: 26-Feb-2007

OptionalRE (-)601-0536 Modification - Fuel Storage - Sustain Flight Operations with the Removal of the Forward Auxiliary Fuel Tank

Mos

Hrs

Ldg

28 A/F

OptionalT (A/R)601-0536 Rev 1 Modification - Fuel Storage - Sustain Flight Operations with the Removal of the Forward Auxiliary Fuel Tank

Mos

Hrs

Ldg

28 A/FEff: 12-Feb-2007

OptionalT (A/R)601-0605 Modification – Vent System Enhancement

Mos

Hrs

Ldg

28 A/FEff: 23-Nov-2009

RecommendedT601-0640 Special Check/Modification - Auxiliary Power Unit (APU) Fuel-Feed System - Possible Chafing of the APU Negative-G Fuel-Feed Drain Line

1.1 Years19-May-201724Mos

Hrs

Ldg

28 A/FEff: 19-May-2015

Nextdue Share EarliestDUE: 19-May-20171. T 24 Mos | 2. RE -Special Check - Auxiliary Power Unit (APU) Fuel-Feed System ...601-0640 Part AA/F28

Nextdue Share EarliestDUE: 19-May-20171. T 24 Mos | 2. RE -Modification - Auxiliary Power Unit (APU) Fuel-Feed System -...601-0640 Part BA/F28

RecommendedT601-0640 Part A Special Check - Auxiliary Power Unit (APU) Fuel-Feed System - Possible Chafing of the APU Negative-G Fuel-Feed Drain Line


Hrs

Ldg

28 A/FEff: 19-May-2015

(AVG MAN HRS: 0.5)

RecommendedT601-0640 Part B Modification - Auxiliary Power Unit (APU) Fuel-Feed System - Possible Chafing of the APU Negative-G Fuel-Feed Drain Line


Hrs

Ldg

28 A/FEff: 19-May-2015

(AVG MAN HRS: 8)


Generated: 6-Apr-2016 1:16 PM101/429







MandatoryRE (-)92-20-04 Tail Cone Fuel Tank

18-Mar-1992Mos

Hrs

Ldg

28 A/FBY CONFIGURATIONEff: 17-Nov-1992 Not

Applicable

Compliance Share DoubleDUE:1. RE -Special Check/Modification - Pressure Refuel/Defuel System -...A601-0381 Rev 2A/F28

MandatoryRE (-)98-03-02 Anti-Noise Filter on Standby & APU

30-Dec-2002Mos

9,147Hrs

4,540Ldg

28 A/FSB A601-0441Eff: 06-Mar-1998 Complied

With

AlertRE (-)A601-0175 Special Check/Modification - Scavenge Ejector Screens - Addition

Mos

Hrs

Ldg

28 A/F

AlertRE (-)A601-0175 Rev 1 Special Check/Modification - Scavenge Ejector Screens - Addition

Mos

Hrs

Ldg

28 A/F

AlertRE (-)A601-0175 Rev 2 Special Check/Modification - Scavenge Ejector Screens - Addition

26-Jan-1987Mos

1,267Hrs

480Ldg


AlertRE (-)A601-0330 Special Check/Modification - Powered Crossfeed System - Fuel Line Cap Assembly Safetying

01-Oct-1991Mos

Hrs

Ldg

28 A/FEff: 07-May-1990 Not Applicable

AlertRE (-)A601-0381 Special Check/Modification - Pressure Refuel/Defuel System - Relocation of Sensing Line

Mos

Hrs

Ldg

28 A/F

AlertRE (-)A601-0381 Rev 1 Special Check/Modification - Pressure Refuel/Defuel System - Relocation of Sensing Line

Mos

Hrs

Ldg

28 A/F

AlertRE (-)A601-0381 Rev 2 Special Check/Modification - Pressure Refuel/Defuel System - Relocation of Sensing Line

Mos

Hrs

Ldg

28 A/FEff: 27-Jan-1992

AlertRE (-)A601-0441 Modification - Standby and APU Fuel Pump Assemblies - Sealing External Surfaces/Replacement of Anti-Noise (EMI) Filter

Mos

Hrs

Ldg

28 A/F

AlertRE (-)A601-0441 Rev 1 Modification - Standby and APU Fuel Pump Assemblies - Sealing External Surfaces/Replacement of Anti-Noise (EMI) Filter

28-Apr-1995Mos

4,555Hrs

1,824Ldg



Generated: 6-Apr-2016 1:16 PM102/429







▼ 29 - HYDRAULIC POWER

RE (O/C)Acoustic Filter

28-Feb-2007Mos

11,006.2Hrs

5,640Ldg

Left29 A/FAC9607F10Y3UNKNOWN

RE (O/C)Acoustic Filter

28-Feb-2007Mos

11,006.2Hrs

5,640Ldg

Right29 A/FAC2358F1279JUNKNOWN

RE (O/C)Air Pressure Indicator Gauge

20-Sep-1983Mos

0Hrs

0Ldg



20-Sep-1983Mos

0Hrs

0Ldg



20-Sep-1983Mos

0Hrs

0Ldg



20-Sep-1983Mos

0Hrs

0Ldg



20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Electric Motor Driven Pump

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Engine Driven Hydraulic Pump

20-Sep-1983Mos

0Hrs0

0Ldg0

Left29 A/FNew601-75100-5

UNKNOWN

RE (O/C)Engine Driven Hydraulic Pump

18-Apr-2004Mos

10,295.1Hrs

5,200Ldg

Right29 A/F601-75100-5MX509255A

RE (O/C)Firewall Shut-Off Valve

20-Sep-1983Mos

0Hrs0

0Ldg0

Left29 A/FNewAV16B2069B1

N/A


Generated: 6-Apr-2016 1:16 PM103/429







RE (O/C)Firewall Shut-Off Valve

20-Sep-1983Mos

0Hrs0

0Ldg0

Right29 A/FNewAV16B2069B1

N/A

RE (O/C)Heat Hydraulic Fluid Exchanger

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Hydraulic Accumulator

20-Sep-1983Mos

0Hrs

0Ldg



20-Sep-1983Mos

0Hrs

0Ldg



20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Hydraulic Assy Reservoir

20-Sep-1983Mos

0Hrs0

0Ldg0

No.129 A/FNew7301

UNKNOWN


20-Sep-1983Mos

0Hrs0

0Ldg0

No.229 A/FNew7302

UNKNOWN


20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Hydraulic Motor

20-Sep-1983Mos

0Hrs

0Ldg



20-Sep-1983Mos

0Hrs

0Ldg



25-Jul-2008Mos

11,432Hrs

5,881Ldg

No.329 A/F9008D15-2XP2230


Generated: 6-Apr-2016 1:16 PM104/429








20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Hydraulic Pressure Indicator

20-Sep-1983Mos

0Hrs

0Ldg



20-Sep-1983Mos

0Hrs

0Ldg



20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Hydraulic Pressure Switch

20-Sep-1983Mos

0Hrs

0Ldg



20-Sep-1983Mos

0Hrs

0Ldg



20-Sep-1983Mos

0Hrs

0Ldg



20-Sep-1983Mos

0Hrs

0Ldg



20-Sep-1983Mos

0Hrs

0Ldg



20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Hydraulic Pressure Transducer

20-Sep-1983Mos

0Hrs0

0Ldg0

No.129 A/FNew600-59174-17

UNKNOWN


Generated: 6-Apr-2016 1:16 PM105/429








20-Sep-1983Mos

0Hrs

0Ldg



20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Hydraulic Pump

20-Sep-1983Mos

0Hrs

0Ldg



26-Sep-2006Mos

10,897.5Hrs

5,558Ldg

No.229 A/F63108-03184787


25-Jul-2008Mos

11,432Hrs

5,881Ldg

No.329 A/F63108-06180773

RE (O/C)Hydraulic Quantity Indicator

25-May-2004Mos

10,384.9Hrs

5,260Ldg

No.129 A/F115-080-380E0119


20-Sep-1983Mos

0Hrs0

0Ldg0

No.229 A/FNew115-080-3

80E0119


20-Sep-1983Mos

0Hrs0

0Ldg0

No.329 A/FNew115-080-3

80E0119

RE (O/C)Relief Valve

20-Sep-1983Mos

0Hrs

0Ldg



20-Sep-1983Mos

0Hrs

0Ldg



20-Sep-1983Mos

0Hrs

0Ldg



Generated: 6-Apr-2016 1:16 PM106/429







MandatoryRE (-)2010-14-05 Hydraulic power

08-Jul-2011Mos

11,523.8Hrs

5,970Ldg


Nextdue Share EarliestDUE:1. RE -Hydraulic power - inspect to determine the part numbers of ...2010-14-05 Paragraph (g)(1)A/F29

Nextdue Share EarliestDUE:1. RE -Hydraulic power - Replace the accumulator with a new, over...2010-14-05 Paragraph (g)(2) Brake No.2A/F29

Nextdue Share EarliestDUE:1. RE -Hydraulic power - Replace the accumulator with a new, over...2010-14-05 Paragraph (g)(2) Brake No.3A/F29

Nextdue Share EarliestDUE:1. RE -Hydraulic power - Replace the accumulator with a new, over...2010-14-05 Paragraph (g)(2) Hyd.Sys

No.1A/F29


No.2A/F29


No.3A/F29

MandatoryRE (-)2010-14-05 Paragraph (g)(1) Hydraulic power - inspect to determine the part numbers of the system accumulators numbers 1, 2, and 3 and brake accumulators numbers 2 and 3 that are installed

on the airplane.

Mos

Hrs

Ldg

29 A/FEff: 05-Aug-2010

MandatoryRE (-)2010-14-05 Paragraph (g)(2)

Brake No.2

Hydraulic power - Replace the accumulator with a new, overhauled, or refurbished accumulator with the same part number.

Mos

Hrs

Ldg

29 A/FEff: 05-Aug-2010

Compliance Share DoubleDUE:1. RE -Modification – Hydraulic Power and Landing Gear – Replacemen...601-0597 Rev 2A/F29


Brake No.3


Mos

Hrs

Ldg

29 A/FEff: 05-Aug-2010



Hyd.Sys No.1


Mos

Hrs

Ldg

29 A/FEff: 05-Aug-2010



Hyd.Sys No.2


Mos

Hrs

Ldg

29 A/FEff: 05-Aug-2010



Generated: 6-Apr-2016 1:16 PM107/429








Hyd.Sys No.3


Mos

Hrs

Ldg

29 A/FEff: 05-Aug-2010


MRB ≈18-Sep-2016RE29-00-00-201 Hydraulic Power Check Filter Differential Pressure Indicators on the following: (1) Case Drain Filters - No. 1, No. 2 and No. 3 Hydraulic Systems (6 locations) / (2)

Pressure and Return Manifold Filters - No. 1, No. 2 and No. 3 Hydraulic Systems (6 locations)

10-Feb-2016Mos

290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs

6,326Ldg

(PKG 300 Hour)

29 A/F


MRB ≈03-May-2017RE29-00-00-202 Hydraulic Power Internal leakage Check

10-Feb-2016Mos

590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs

6,326Ldg

(PKG 600 Hour)

29 A/F


Servicing - OptionalRE29-00-00-301 Hydraulic Power - Hydraulic fluid acidity check

10 Months (+29

Days)30-Jan-2017-/+12430-Jan-2015Mos

Hrs

Ldg

(PKG 24 Month)

29 A/F

(ZONE: 140, 310) (ACCESS: 112-BR, 190-DR, 311-BB) (SOURCE: MPD 3.3)

MRB ≈20-Oct-2017RE29-10-00-204 Main Systems Functional Test of Reservoir-Mounted Return Line Check Valve

29-Oct-2012Mos

812.3 Hrs (+40)(12,853.5)-/+401,20011,653.5Hrs

Ldg

(PKG 1200 Hour)

29 A/F


MRB ≈24-Aug-2023RE29-10-00-205 Main Systems Remove No.1 and No.2 system hydraulic reservoir in-line check valves for bench check or install new valves

08-Aug-2005Mos

3,618.6 Hrs (+40)(15,659.8)-/+404,80010,859.8Hrs

Ldg

(PKG 4800 Hour)

29 A/F


MRB ≈24-Aug-2023RE29-10-00-206 Main Systems Remove No.3 system hydraulic reservoir in-line check valve forbench check or installnew valve

08-Aug-2005Mos

3,618.6 Hrs (+40)(15,659.8)-/+404,80010,859.8Hrs

Ldg

(PKG 4800 Hour)

29 A/F


MRB ≈20-Oct-2017RE29-11-31-208 Case Drain Filter Check Filter Elements in No. 1, No. 2 and No. 3 HydraulicSystems (6 locations)

29-Oct-2012Mos

812.3 Hrs (+40)(12,853.5)-/+401,20011,653.5Hrs

Ldg

(PKG 1200 Hour)

29 A/F


MRB ≈20-Oct-2017RE29-11-36-209 Pressure Manifold Check Filter Elements in No. 1, No. 2 and No. 3 HydraulicSystems (3 locations)

29-Oct-2012Mos

812.3 Hrs (+40)(12,853.5)-/+401,20011,653.5Hrs

Ldg

(PKG 1200 Hour)

29 A/F


MRB ≈20-Oct-2017RE29-11-41-210 Return Manifold Check Filter Elements in No. 1, No. 2 and No. 3 HydraulicSystems (3 locations)

29-Oct-2012Mos

812.3 Hrs (+40)(12,853.5)-/+401,20011,653.5Hrs

Ldg

(PKG 1200 Hour)

29 A/F



Generated: 6-Apr-2016 1:16 PM108/429







MRB ≈03-May-2017RE29-11-51-211 Heat Exchanger Visual Check, paying particular attention to security ofattachment

10-Feb-2016Mos

590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs

6,326Ldg

(PKG 600 Hour)

29 A/F


MRB ≈03-May-2017RE29-13-00-212 No. 3 Main System Visual Check pump installation areas for contamination by hydraulic fluid

10-Feb-2016Mos

590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs

6,326Ldg

(PKG 600 Hour)

29 A/F

(Tol. Adjustment: -9.2 Hrs) (SOURCE: TLMC 05-20-15) (NOTE: In case of shock mount contamination, refer to Section 5-50-10)

OptionalRE (-)601-0007 Modification - Hydraulic Systems No. 1 and No. 2 - Overboard Drains

01-Sep-1983Mos

Hrs

Ldg

29 A/FComplied With

OptionalT (A/R)601-0007 Rev 1 Modification - Hydraulic Systems No. 1 and No. 2 - Overboard Drains

Mos

Hrs

Ldg

29 A/FEff: 19-Dec-1985

RecommendedRE (-)601-0044 Modification - Main Systems - Replacement of Tube Assemblies

01-Sep-1983Mos

0Hrs

0Ldg


OptionalRE (-)601-0066 Modification - No. 3 Hydraulic System - Cabin Noise Reduction

Mos

Hrs

Ldg

29 A/F

OptionalT (A/R)601-0066 Rev 1 Modification - No. 3 Hydraulic System - Cabin Noise Reduction

Mos

Hrs

Ldg

29 A/FEff: 06-Feb-1987

RecommendedRE (-)601-0077 Special Check/Modification - Underfloor Hydraulic Lines - Clearance with Fuel Line

Mos

Hrs

Ldg

29 A/FEff: 17-Aug-1984

RecommendedRE (-)601-0080 Special Check/Modification - Hydraulic Accumulator - Support Bracket

Mos

Hrs

Ldg

29 A/FEff: 09-Oct-1984

RecommendedRE (-)601-0088 Modification - No. 3 Hydraulic System - Reservoir Bleed Line

28-Mar-1989Mos

2,373Hrs

910Ldg

29 A/FComplied With

RecommendedT (A/R)601-0088 Rev 1 Modification - No. 3 Hydraulic System - Reservoir Bleed Line

Mos

Hrs

Ldg

29 A/FEff: 05-Sep-1985


Generated: 6-Apr-2016 1:16 PM109/429







RecommendedRE (-)601-0089 Modification - No. 3 Hydraulic System Reservoir - AFT Mounting Pad

Mos

Hrs

Ldg

29 A/F

RecommendedT (A/R)601-0089 Rev 1 Modification - No. 3 Hydraulic System Reservoir - AFT Mounting Pad

Mos

Hrs

Ldg

29 A/FEff: 16-Sep-1985

RecommendedT (A/R)601-0098 Modification - Hydraulic Disconnect Fittings - Locking

Mos

Hrs

Ldg

29 A/FEff: 23-Aug-1984

RecommendedRE (-)601-0159 Modification - Hydraulic Hoses - Support Brackets

27-Jan-1987Mos

1,267Hrs

470Ldg


RecommendedRE (-)601-0163 Modification - No. 3 Hydraulic System Pumps - Drain Reorientation

21-Feb-1991Mos

3,142Hrs

1,250Ldg


RecommendedRE (-)601-0180 Modification - Hydraulic System Components - Protection Covers

Mos

Hrs

Ldg

29 A/F

RecommendedRE (-)601-0180 Rev 1 Modification - Hydraulic System Components - Protection Covers

Mos

Hrs

Ldg

29 A/FEff: 05-Feb-1988

RecommendedRE (-)601-0211 Modification - No. 3 Hydraulic System - Ecology Drain Bottles

29-Apr-1988Mos

1,995Hrs

756Ldg


RecommendedRE (-)601-0269 Special Check/Modification - Pressure Manifold - Relief Valve Replacement

03-Mar-1989Mos

2,373Hrs

910Ldg


RecommendedRE (-)601-0307 Modification - Main Systems - Replacement of Tube Assembly

31-Oct-1993Mos

4,142Hrs

1,668Ldg


RecommendedRE (-)601-0328 Modification - Run-Around/Bypass Valve - Screw Replacement

04-Oct-1990Mos

2,979Hrs

1,177Ldg



Generated: 6-Apr-2016 1:16 PM110/429







RecommendedRE (-)601-0388 Modification - No. 3 Hydraulic System - Replacement of Bulkhead Tee Reducers

14-Oct-1992Mos

3,754Hrs

1,519Ldg


RecommendedRE (-)601-0414 Modification - Pressure Transducers - Introduction of Safety Lock-Wire

30-Sep-1994Mos

4,399Hrs

1,768Ldg


RecommendedRE (-)601-0482 Modification – Hydraulic Tubes, Main Landing Gear Bay - Install New Re-Routed Tubes

12-Nov-1997Mos

5,395Hrs

2,274Ldg


RecommendedRE (-)601-0541 Modification - Hydraulic System No. 1 and No. 2 - Replacement of Pressure Hose Assemblies at The Pylon Firewall

Mos

Hrs

Ldg

29 A/F

RecommendedT (A/R)601-0592 Modification – No. 3 Main System – Addition of Spacers for Accumulator Part No. 601R75138-3 Installation

Mos

Hrs

Ldg

29 A/FEff: 17-Dec-2007

RecommendedRE (-)601-0597 Modification – Hydraulic Power and Landing Gear – Replacement of System Accumulators No. 1, No. 2 and No. 3 and Brake Accumulators No. 2 and No. 3 or Part Nos

08-60163-002 and 08-60164-002

Mos

Hrs

Ldg

29 A/F

Nextdue Share EarliestDUE:1. RE -Modification – Hydraulic Power and Landing Gear – Replacemen...601-0597 (Brake 2)A/F29

Nextdue Share EarliestDUE:1. RE -Modification – Hydraulic Power and Landing Gear – Replacemen...601-0597 (Brake 3)A/F29

Nextdue Share EarliestDUE:1. RE -Modification – Hydraulic Power and Landing Gear – Replacemen...601-0597 (Hyd Sys 1)A/F29



RecommendedRE (-)601-0597 (Brake 2) Modification – Hydraulic Power and Landing Gear – Replacement of Brake Accumulators No. 2 for Part Nos 08-60163-002 and 08-60164-002

Mos

Hrs

Ldg

29 A/FEff: 10-Nov-2008

RecommendedRE (-)601-0597 (Brake 3) Modification – Hydraulic Power and Landing Gear – Replacement of Brake Accumulators No. 3 for Part Nos 08-60163-002 and 08-60164-002

Mos

Hrs

Ldg

29 A/FEff: 10-Nov-2008

RecommendedRE (-)601-0597 (Hyd Sys 1) Modification – Hydraulic Power and Landing Gear – Replacement of System Accumulators No. 1 Hydraulic System for Part Nos 08-60163-002 and 08-60164-002

Mos

Hrs

Ldg

29 A/FEff: 10-Nov-2008


Generated: 6-Apr-2016 1:16 PM111/429








Mos

Hrs

Ldg

29 A/FEff: 10-Nov-2008


Mos

Hrs

Ldg

29 A/FEff: 10-Nov-2008

RecommendedRE (-)601-0597 Rev 1 Modification – Hydraulic Power and Landing Gear – Replacement of System Accumulators No. 1, No. 2 and No. 3 and Brake Accumulators No. 2 and No. 3 or Part Nos

08-60163-002 and 08-60164-002

Mos

Hrs

Ldg

29 A/F

Nextdue Share EarliestDUE:1. RE -Modification – Hydraulic Power and Landing Gear – Replacemen...601-0597 Rev 1 (Brake 2)A/F29


Nextdue Share EarliestDUE:1. RE -Modification – Hydraulic Power and Landing Gear – Replacemen...601-0597 Rev 1 (Hyd Sys 1)A/F29



RecommendedRE (-)601-0597 Rev 1 (Brake 2) Modification – Hydraulic Power and Landing Gear – Replacement of Brake Accumulators No. 2 for Part Nos 08-60163-002 and 08-60164-002

Mos

Hrs

Ldg

29 A/FEff: 06-Jul-2009


Mos

Hrs

Ldg

29 A/FEff: 06-Jul-2009

RecommendedRE (-)601-0597 Rev 1 (Hyd Sys 1) Modification – Hydraulic Power and Landing Gear – Replacement of System Accumulators No. 1 Hydraulic System for Part Nos 08-60163-002 and 08-60164-002

Mos

Hrs

Ldg

29 A/FEff: 06-Jul-2009


Mos

Hrs

Ldg

29 A/FEff: 06-Jul-2009


Mos

Hrs

Ldg

29 A/FEff: 06-Jul-2009


Generated: 6-Apr-2016 1:16 PM112/429








08-60163-002 and 08-60164-002

Mos

Hrs

Ldg

29 A/F







Mos

Hrs

Ldg

29 A/FEff: 10-May-2010


Mos

Hrs

Ldg

29 A/FEff: 10-May-2010


Mos

Hrs

Ldg

29 A/FEff: 10-May-2010


Mos

Hrs

Ldg

29 A/FEff: 10-May-2010


Mos

Hrs

Ldg

29 A/FEff: 10-May-2010


08-60163-002 and 08-60164-002

Mos

Hrs

Ldg

29 A/F







Mos

Hrs

Ldg

29 A/FEff: 10-Apr-2012


Generated: 6-Apr-2016 1:16 PM113/429








Mos

Hrs

Ldg

29 A/FEff: 10-Apr-2012


Mos

Hrs

Ldg

29 A/FEff: 10-Apr-2012


Mos

Hrs

Ldg

29 A/FEff: 10-Apr-2012


Mos

Hrs

Ldg

29 A/FEff: 10-Apr-2012

RecommendedT (A/R)601-0597 Rev 4 Modification – Hydraulic Power and Landing Gear – Replacement of System Accumulators No. 1, No. 2 and No. 3 and Brake Accumulators No. 2 and No. 3 or Part Nos

08-60163-002 and 08-60164-002

Mos

Hrs

Ldg

29 A/FEff: 11-Jun-2015







Mos

Hrs

Ldg

29 A/FEff: 11-Jun-2015


Mos

Hrs

Ldg

29 A/FEff: 11-Jun-2015


Mos

Hrs

Ldg

29 A/FEff: 11-Jun-2015


Mos

Hrs

Ldg

29 A/FEff: 11-Jun-2015


Generated: 6-Apr-2016 1:16 PM114/429








Mos

Hrs

Ldg

29 A/FEff: 11-Jun-2015

OptionalT (A/R)601-0618 Modification – No. 1 and No. 2 Main System – Replacement of the Hydraulic System No. 1 Accumulator

Mos

Hrs

Ldg

29 A/FEff: 14-May-2012

OptionalT (A/R)601-0619 Modification – No. 1 and No. 2 Main System – Replacement of the Hydraulic System No. 2 Accumulator

Mos

Hrs

Ldg

29 A/FEff: 14-May-2012

OptionalT (A/R)601-0620 Modification – No. 3 Main System – Replacement of the Hydraulic System No. 3 Accumulator

Mos

Hrs

Ldg

29 A/FEff: 14-May-2012

RecommendedT601-0633 Modification - No. 1 and No. 2 Main Systems - Relocation of the Hydraulic System No. 1 and No. 2 Accumulators

7.5 Years08-Oct-202396Mos

Hrs

Ldg

29 A/FEff: 08-Oct-2015

MandatoryRE (-)86-10-02 R1 Aileron And Elevator Flutter Dampers

18-Sep-1985Mos

Hrs

Ldg

29 A/FBY PART NUMBER INSTALLEDEff: 09-Feb-1990 Not

Applicable

MandatoryRE (-)86-10-02 R1 (1) Left Aileron Flutter Damper Fluid Check

18-Sep-1985Mos

Hrs

Ldg


Applicable

MandatoryRE (-)86-10-02 R1 (2) Right Aileron Flutter Damper Fluid Check

18-Sep-1985Mos

Hrs

Ldg


Applicable

MandatoryRE (-)86-10-02 R1 (3) Left Outboard Elevator Flutter Damper Fluid Check

18-Sep-1985Mos

Hrs

Ldg


Applicable

MandatoryRE (-)86-10-02 R1 (4) Left Inboard Elevator Flutter Damper Fluid Check

18-Sep-1985Mos

Hrs

Ldg


Applicable

MandatoryRE (-)86-10-02 R1 (5) Right Inboard Elevator Flutter Damper Fluid Check

18-Sep-1985Mos

Hrs

Ldg


Applicable


Generated: 6-Apr-2016 1:16 PM115/429







MandatoryRE (-)86-10-02 R1 (6) Right Outboard Elevator Flutter Damper Fluid Check

18-Sep-1985Mos

Hrs

Ldg


Applicable

MandatoryRE (-)99-26-16 MLG Hydraulic And Fuel Lines

30-Dec-2002Mos

9,147Hrs

4,540Ldg

29 A/FSB 601-0482Eff: 01-Feb-2000 Complied

With

Compliance Share DoubleDUE:1. T A/R | 2. RE -Modification – Hydraulic Tubes, Main Landing Gear Bay - Inst...601-0482A/F29

AlertRE (-)A601-0082 Modification - No. 1 and 2 System Return Lines - Addition of Check Valve

20-Nov-1984Mos

Hrs

Ldg


AlertT (A/R)A601-0108 Special Check/Modification - Hydraulic Line - Clearance with Left Main Wheel Bin

Mos

Hrs

Ldg

29 A/FEff: 24-Aug-1984

AlertT (A/R)A601-0138 Special Check/Modification - Tube Assemblies - Clearance

Mos

Hrs

Ldg

29 A/FEff: 15-Oct-1985

IsModSumT (A/R)IS600-29-0002 REV A Kit – Intro of Elbow Fitting on Ecology Bottle for the Hydraulic Resevoir #3

Mos

Hrs

Ldg

29 A/F

▼ 30 - ICE AND RAIN PROTECTION

RE (O/C)ADS Heater Control Unit

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Anti-Ice Controller

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Anti-Ice Modulating/Shutoff Valve

20-Sep-1983Mos

0Hrs0

0Ldg0


N/A

RE (O/C)Anti-Ice Modulating/Shutoff Valve

20-Sep-1983Mos

0Hrs0

0Ldg0


N/A


Generated: 6-Apr-2016 1:16 PM116/429







RE (O/C)Cowl Anti-Ice Pressure Switch

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Cowl Anti-Ice Pressure Switch

07-Jun-2003Mos

9,559.7Hrs

4,782Ldg

No.230 A/F98505-126811244

RE (O/C)Cowl Anti-Ice Valve

26-Mar-2007Mos

11,045.9Hrs

5,659Ldg

Left30 A/F300013000-0030284T

RE (O/C)Cowl Anti-Ice Valve

26-Mar-2005Mos

10,699.3Hrs

5,441Ldg

Right30 A/F734027B0496

RE (O/C)Ejector Interface Duct Assy

20-Sep-1983Mos

0Hrs0

0Ldg0

No.130 A/FNew228-56345-135

UNKNOWN

RE (O/C)Ejector Interface Duct Assy

20-Sep-1983Mos

0Hrs0

0Ldg0

No.230 A/FNew228-56345-135

UNKNOWN

RE (O/C)Ice Detector

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Ice Detector

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Over Pressure Relief Valve

28-Jan-2005Mos

10,580.3Hrs

5,376Ldg

Left30 A/F228-56480-801SB/3157

RE (O/C)Over Pressure Relief Valve

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Side Window Temperature Controller

20-Sep-1983Mos

0Hrs0

0Ldg0

Left30 A/FNew600-59100-13

UNKNOWN


Generated: 6-Apr-2016 1:16 PM117/429







RE (O/C)Side Window Temperature Controller

20-Sep-1983Mos

0Hrs0

0Ldg0

Right30 A/FNew600-59100-13

UNKNOWN

RE (O/C)Windshield Temperature Controller

20-Sep-1983Mos

0Hrs0

0Ldg0

Left30 A/FNew600-59100-11

UNKNOWN

RE (O/C)Windshield Temperature Controller

20-Sep-1983Mos

0Hrs0

0Ldg0

Right30 A/FNew600-59100-11

UNKNOWN

MandatoryRE (-)2005-04-07 Revision to Airplane Flight Manual (AFM) - New cold weather operations limitation - CANCELLED

20-Feb-2005Mos

10,595.3Hrs

5,386Ldg

30 A/FREVISED AFMEff: 22-Feb-2005 Complied

With

MandatoryRE (-)2008-08-06 Revision to Airplane Flight Manual (AFM) - New cold weather operations limitations - CANCELLED

25-Jul-2008Mos

11,432Hrs

5,881Ldg

30 A/FREVISED AFMEff: 21-Apr-2008 Complied

With

MandatoryRE (-)2008-21-09 Cold weather operation limitations

18-Mar-2009Mos

11,458.6Hrs

5,902Ldg

30 A/FFOUND P/C/WEff: 31-Oct-2008 Complied

With

MandatoryT (A/R)2009-06-05 Wing anti-ice piccolo duct failure

Mos

Hrs

Ldg

30 A/FEff: 28-Apr-2009

MandatoryRE (-)2009-06-05 R1 Wing anti-ice piccolo duct failure

17-Apr-2015Mos

11,905.8Hrs

6,221Ldg

30 A/FREPLACED ON 8/1/2000Eff: 28-Apr-2009 Complied

With

Nextdue Share EarliestDUE:1. T 1 Mos | 2. RE -Wing anti-ice piccolo duct failure - Airplane Flight Manual ...2009-06-05 R1 Paragraph (f) (1)A/F30

Nextdue Share EarliestDUE:1. RE -Wing anti-ice piccolo duct failure - Review the airplane mai...2009-06-05 R1 Paragraph (f) (2)A/F30

Nextdue Share EarliestDUE:1. T A/R | 2. RE -Wing anti-ice piccolo duct failure - Identification of S/N's...2009-06-05 R1 Paragraph (f) (3)A/F30

MandatoryRE (-)2009-06-05 R1 Paragraph (f)

(1)

Wing anti-ice piccolo duct failure - Airplane Flight Manual (AFM) Revise

23-Sep-2009Mos

11,459.7Hrs

5,904Ldg

30 A/FREVISED AFMEff: 01-Apr-2010 Complied

With

(AVG MAN HRS: 37) (APX COST [USD]: 3,145)


Generated: 6-Apr-2016 1:16 PM118/429







MandatoryRE (-)2009-06-05 R1 Paragraph (f)

(2)

Wing anti-ice piccolo duct failure - Review the airplane maintenance records

Mos

Hrs

Ldg

30 A/FEff: 01-Apr-2010

Compliance Share SingleDUE:1. T A/R | 2. RE -Wing anti-ice piccolo duct failure - Identification of S/N's...2009-06-05 R1 Paragraph (f) (3)A/F30

MandatoryT (A/R)2009-06-05 R1 Paragraph (f)

(3)

Wing anti-ice piccolo duct failure - Identification of S/N's affected and Replacement

Mos

Hrs

Ldg

30 A/FEff: 01-Apr-2010

Compliance Share DoubleDUE: 12,932 Hrs1. T A/R | 2. RE -Special Check/Modification - Wing Anti-Icing - Anti-Ice Picc...601-0585A/F30

MandatoryRE (-)2011-09-09 Ice and Rain Protection and Pneumatic, respectively

13-May-2014Mos

11,839.6Hrs

6,172Ldg

30 A/FSB 590 NOT COMPLIED WITHEff: 19-Aug-2011 Not

Applicable

Not SetDUE:1. T A/R | 2. RE -Ice and Rain Protection and Pneumatic, respectively - Revise...2011-09-09 Paragraph (g)A/F30

Not SetDUE:1. T 4800 Hrs | 2. RE -Ice and Rain Protection and Pneumatic, respectively - Initia...2011-09-09 Paragraph (h)A/F30

MandatoryT (A/R)2011-09-09 Paragraph (g) Ice and Rain Protection and Pneumatic, respectively - Revise the Airworthiness Limitations Section of the Instructions for Continued Airworthiness

13-May-2014Mos

11,839.6Hrs

6,172Ldg

30 A/FSB 590 NOT COMPLIED WITHEff: 19-Aug-2011 Not

Applicable

MandatoryRE (-)2011-09-09 Paragraph (h) Ice and Rain Protection and Pneumatic, respectively - Initial Compliance Times for Airworthiness Limitations Tasks.

13-May-2014Mos

11,839.6Hrs

6,172Ldg

30 A/FSB 590 NOT COMPLIED WITHNot Applicable

AWLRE (N/A)30-11-00-101 * Wing Anti-Icing - Detailed Inspection of the Wing Duct Piccolo Tube (Post SB 601-0590)

Mos

Hrs

Ldg

30 A/F


AWLRE (N/A)30-11-00-102 * Wing Anti-Icing - Functional Test of the Thermal Switches and Sensors (Post SB 601-0590)

Mos

Hrs

Ldg

30 A/F


MRB ≈24-Oct-2017RE30-11-00-201 Wing Anti-Icing Check valve condition check

23-Oct-2004Mos

817.8 Hrs (+40)12,859-/+402,40010,459Hrs

Ldg

(PKG 2400 Hour)

30 A/F


MRB ≈29-Dec-2030RE30-11-00-202 Wing Anti-Icing Functional Test Wing Anti-Icing

05-Aug-2003Mos

7,144.4 Hrs (+40)(19,185.6)-/+409,6009,585.6Hrs

Ldg

(PKG 9600 Hour)

30 A/F



Generated: 6-Apr-2016 1:16 PM119/429







MRBRE30-11-06-204 Wing Anti-Icing Ducting Visual Check of ducts, brackets, clamps and associated wiring, underfloor and in wing leading edge

5.8 Months (+30

Days)(26-Sep-2016)-/+16024-Oct-2011Mos

Hrs

Ldg

(PKG 60 Month)

30 A/F


MRB ≈03-May-2017RE30-11-06-212 Wing Anti-Ice Coupling (Pre SB 601-0433) Detailed inspection of the wing anti-ice expansion couplingbearings

10-Feb-2016Mos

590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs

6,326Ldg

(PKG 600 Hour)

30 A/F


MRBRE30-13-00-205 Anti-Icing Bleed Air Leak Detection Functional Test of thermal switches

5.8 Months (+30

Days)26-Sep-2016-/+112026-Sep-2006Mos

Hrs

Ldg

30 A/F


MRB ≈18-Sep-2016RE30-20-21-206 Nose Cowl Anti-Ice/Thrust Reverser Ducting Visual Check, paying particular attention for hot spots and discoloration

10-Feb-2016Mos

290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs

6,326Ldg

(PKG 300 Hour)

30 A/F


MRB ≈27-Jul-2016RE30-40-00-213 Windshield - Functional Test of the windshield rain repellant layer

30-Jan-2015Mos

221.5 Hrs12,262.740011,862.7Hrs

Ldg

Left30 A/F600-33030-259415

(SOURCE: TLMC 05-20-15) (NOTE: This task applies to Sully Glass Faceply Windshields, Part No. 270-462-00-XX and Sierracin Glass Faceply /

Windshields Part No. 158700-57 and Subs.)

MRB ≈27-Jul-2016RE30-40-00-213 Windshield - Functional Test of the windshield rain repellant layer

30-Jan-2015Mos

221.5 Hrs (+40)12,262.7-/+4040011,862.7Hrs

Ldg

Right30 A/F604-33030-2611030 REPAIR

(SOURCE: TLMC 05-20-15) (NOTE: This task applies to Sully Glass Faceply Windshields, Part No. 270-462-00-XX and Sierracin Glass Faceply /

Windshields Part No. 158700-57 and Subs.)

Servicing - Optional ≈25-Aug-2016RE30-40-00-301 Windshield/Side Window Aerodynamic Seal - Detailed Inspection

6.6 Months (+31

Days)21-Oct-2016-/+11221-Oct-2015Mos

259.9 Hrs (+40)12,301.1-/+4030012,001.1Hrs

6,291Ldg

30 A/F

(ZONE: 221, 223) (SOURCE: MPD 3.3)

MRB ≈20-Oct-2017RE30-41-00-210 Electrical Anti-Icing Functional Test of Heating Element - Functional Test of Sensors

29-Oct-2012Mos

812.3 Hrs (+40)(12,853.5)-/+401,20011,653.5Hrs

Ldg

(PKG 1200 Hour)

30 A/F


MRB ≈20-Oct-2017RE30-41-16-211 Varistor Suppressor Nominal varistor voltage test - DC standby current test

29-Oct-2012Mos

812.3 Hrs (+40)(12,853.5)-/+401,20011,653.5Hrs

Ldg

(PKG 1200 Hour)

30 A/F


RecommendedRE (-)601-0015 Modification - Wing Anti-Icing System - Activation

Mos

Hrs

Ldg

30 A/F


Generated: 6-Apr-2016 1:16 PM120/429







RecommendedRE (-)601-0015 Rev 1 Modification - Wing Anti-Icing System - Activation

Mos

Hrs

Ldg

30 A/FEff: 23-Apr-1984

RecommendedRE (-)601-0120 Modification - Anti-Ice System - Addition of Blocking Diodes

23-Mar-1992Mos

3,584Hrs

1,446Ldg


OptionalRE (-)601-0142 Modification - Airfoil Anti-Icing - Removal of Guides

28-Oct-1988Mos

2,159Hrs

825Ldg


RecommendedRE (-)601-0165 Modification - Windshield Anti-Icing and Demisting - Dual Heat Control

28-Mar-1989Mos

2,373Hrs

910Ldg


RecommendedRE (-)601-0183 Modification - Anti-Ice Ducting - Insulation Boots

28-Mar-1989Mos

2,373Hrs

910Ldg


RecommendedRE (-)601-0188 Modification - Leak Detection Elements - Dual Clip Assembly

28-Mar-1989Mos

2,373Hrs

910Ldg


RecommendedRE (-)601-0190 Special Check/Rework - Bleed Air Leak Detector - Routing

28-Mar-1989Mos

2,373Hrs

910Ldg


OptionalRE (-)601-0256 Modification - Ice Detector Light - Conversion for Certification

Mos

Hrs

Ldg

30 A/F

OptionalT (A/R)601-0256 Rev 1 Modification - Ice Detector Light - Conversion for Certification

Mos

Hrs

Ldg

30 A/FEff: 22-Feb-1991

RecommendedRE (-)601-0433 Modification - Wing Anti-Ice System - Coupling Assembly

Mos

Hrs

Ldg

30 A/F

RecommendedRE (-)601-0433 Rev 1 Modification - Wing Anti-Ice System - Coupling Assembly

26-Jan-1996Mos

4,785Hrs

1,932Ldg



Generated: 6-Apr-2016 1:16 PM121/429







RecommendedRE (-)601-0471 Special Check/Rework - Wing Anti-Icing - Coupling/Boot-Cover Position at FS559.00

01-May-1996Mos

4,891Hrs

1,989Ldg


Recommended ≈18-Dec-2017T (A/R)601-0585 Special Check/Modification - Wing Anti-Icing - Anti-Ice Piccolo Ducts Inspection/Replacement

Mos

890.8 Hrs[12,932]Hrs

Ldg

30 A/FEff: 30-Nov-2006

RecommendedRE (-)601-0608 Modification – Wing Anti-Icing – Take-Off Safety Enhancement (TOSE) Wing Anti-Ice Wiring Modification to Prevent Nuisance Indication on Take-Off

Mos

Hrs

Ldg

30 A/F

RecommendedT (A/R)601-0608 Rev 1 Modification – Wing Anti-Icing – Take-Off Safety Enhancement (TOSE) Wing Anti-Ice Wiring Modification to Prevent Nuisance Indication on Take-Off

Mos

Hrs

Ldg

30 A/FEff: 27-Jun-2011

RecommendedRE (-)601-1022 Special Check/Modification - Air Intake Anti-Icing - Valve Replacement

Mos

Hrs

Ldg

30 A/F

RecommendedT (A/R)601-1022 Rev 1 Special Check/Modification - Air Intake Anti-Icing - Valve Replacement

Mos

Hrs

Ldg

30 A/FEff: 02-Apr-1984

RecommendedRE (-)601-1064 Special Check/Modification - Anti-Ice System - Pressure Relief Valve

23-Feb-1990Mos

2,687Hrs

1,034Ldg


AlertRE (-)A601-0008 Modification - Windshield Anti-Icing and Demisting - Addition of Suppressors

Mos

Hrs

Ldg

30 A/F

AlertRE (-)A601-0008 Rev 1 Modification - Windshield Anti-Icing and Demisting - Addition of Suppressors

Mos

Hrs

Ldg

30 A/FEff: 10-Feb-1984

AlertRE (-)A601-0556 Special Check/Rework - Wing Anti-Icing - Examine Piccolo Tube and Connecting Duct Installation on Left and Right Wings

05-Aug-2003Mos

9,585.6Hrs

4,797Ldg


Nextdue Share EarliestDUE:1. T 6 Mos, 250 Hrs | 2. RE -Special Check/Rework - Wing Anti-Icing - Examine Piccolo Tub...A601-0556 Part AA/F30

Nextdue Share EarliestDUE:1. T 6 Mos, 250 Hrs | 2. RE -Special Check/Rework - Wing Anti-Icing - Examine Piccolo Tub...A601-0556 Part BA/F30

Nextdue Share EarliestDUE:1. T 6 Mos, 250 Hrs | 2. RE -Special Check/Rework - Wing Anti-Icing - Examine Piccolo Tub...A601-0556 Part CA/F30

Nextdue Share EarliestDUE:1. T 6 Mos, 250 Hrs | 2. RE -Special Check/Rework - Wing Anti-Icing - Examine Piccolo Tub...A601-0556 Part DA/F30


Generated: 6-Apr-2016 1:16 PM122/429







AlertRE (-)A601-0556 Part A Special Check/Rework - Wing Anti-Icing - Examine Piccolo Tube and Connecting Duct Installation on Left and Right Wings

Mos

Hrs

Ldg

30 A/FEff: 23-Jan-2003

AlertRE (-)A601-0556 Part B Special Check/Rework - Wing Anti-Icing - Examine Piccolo Tube and Connecting Duct Installation on Left and Right Wings

Mos

Hrs

Ldg

30 A/FEff: 23-Jan-2003

AlertRE (-)A601-0556 Part C Special Check/Rework - Wing Anti-Icing - Examine Piccolo Tube and Connecting Duct Installation on Left and Right Wings

Mos

Hrs

Ldg

30 A/FEff: 23-Jan-2003

AlertRE (-)A601-0556 Part D Special Check/Rework - Wing Anti-Icing - Examine Piccolo Tube and Connecting Duct Installation on Left and Right Wings

Mos

Hrs

Ldg

30 A/FEff: 23-Jan-2003

▼ 31 - INDICATING / RECORDING SYSTEM

RE (O/C)Aural Warning Test Panel

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Aural Warning Unit

30-Jan-2015Mos

11,862.7Hrs

6,194Ldg

31 A/F7001433-90182020233

RE (O/C)Circuit Breaker Box

20-Sep-1983Mos

0Hrs0

0Ldg0

31 A/FNew70-0197-3

UNKNOWN

RE (O/C)Dimming Module Assy

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Dimming Module Assy

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Flight Data Recorder (FDR)

20-Sep-1983Mos

0Hrs

0Ldg


Assembly SubDUE:1. RE N/AFlight Data Recorder (FDR) Underwater Locating DeviceUnknown / UnknownA/F31


Generated: 6-Apr-2016 1:16 PM123/429







Life LimitRE (N/A)Flight Data Recorder (FDR) Underwater Locating Device

Mos

Hrs

Ldg


RE (O/C)Master Warning Caution Panel 10-Channel

07-Nov-2004Mos

10,460.5Hrs

5,308Ldg

31 A/F843347-3226

RE (O/C)Master Warning Caution Panel 8-Channel

20-Sep-1983Mos

0Hrs

0Ldg


MRB ≈03-May-2017RE31-51-00-201 Aural Warning System Operational Test of Fire Detection Warning (Bell) - Functional Test of: (1) Landing gear warning (Horn) / (2) Take-off configuration (TOC)

warning (Intermittent Horn)

10-Feb-2016Mos

590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs

6,326Ldg

(PKG 600 Hour)

31 A/F


MRBRE31-51-00-202 Aural Warning System Functional Test of: (1) Overspeed warning (Clacker) / (2) Flap overspeed warning (Wailer) (3) Altitude advisory (C Chord)

10 Months (+29

Days)(30-Jan-2017)-/+12430-Jan-2015Mos

Hrs

Ldg

(PKG 24 Month)

31 A/F


RecommendedT (A/R)601-0119 Modification - Master Caution and Warning Light System - Legend Light Wiring

Mos

Hrs

Ldg

31 A/FEff: 20-Jan-1986

OptionalRE (-)601-0148 Modification - Master Caution and Warning System - Blocking Diode

26-Jan-1987Mos

1,267Hrs

480Ldg


OptionalRE (-)601-0162 Modification - Master Caution and Warning System - Load Resistors

Mos

Hrs

Ldg

31 A/F

OptionalT (A/R)601-0162 Rev 1 Modification - Master Caution and Warning System - Load Resistors

Mos

Hrs

Ldg

31 A/FEff: 15-Apr-1992

RecommendedRE (-)601-0263 Modification - Pilots Facia Panel Flood Light - EMI Correction

21-Feb-1991Mos

3,142Hrs

1,250Ldg



Generated: 6-Apr-2016 1:16 PM124/429







OptionalT (A/R)601-0396 Modification - Aural Warning System - Take-off Configuration Warning (TOCW) Back Up

Mos

Hrs

Ldg

31 A/FEff: 15-Aug-1994

▼ 32 - LANDING GEAR

RE (O/C)Box Antiskid Control

15-Sep-2007Mos

11,184.3Hrs

5,748Ldg

32 A/F600-87000-103OCT92-0212

RE (O/C)Brake Control Valve

26-Jan-1996Mos

4,785Hrs

1,932Ldg

No.132 A/F600-75115-51542

RE (O/C)Brake Control Valve

26-Jan-1996Mos

4,785Hrs

1,932Ldg

No.232 A/F600-75115-51247

RE (O/C)Brake Hydraulic Accumulator

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Brake Hydraulic Accumulator

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Brake Hydraulic Fuse

20-Sep-1983Mos

0Hrs0

0Ldg0

No.132 A/FNew6190

UNKNOWN


20-Sep-1983Mos

0Hrs0

0Ldg0

No.232 A/FNew6190

UNKNOWN


20-Sep-1983Mos

0Hrs0

0Ldg0

No.332 A/FNew6190

UNKNOWN


20-Sep-1983Mos

0Hrs0

0Ldg0

No.432 A/FNew6190

UNKNOWN

RE (O/C)Brake Pressure Indicator

20-Sep-1983Mos

0Hrs

0Ldg



Generated: 6-Apr-2016 1:16 PM125/429







RE (O/C)Brake Pressure Transducer

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Brake Pressure Transducer

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Extension and Retraction - Main Landing Gear Selector Valve

20-Sep-1983Mos

0Hrs

0Ldg



TsiDUE:1. RE N/AExtension and Retraction - Main Landing Gear Selector Valve ...32-00-00-245A/F32

AWL - Life LimitRE (O/C)Hydraulic Accumulator Assy

20-Sep-1983Mos

0Hrs

0Ldg



20-Sep-1983Mos

0Hrs

0Ldg



20-Sep-1983Mos

0Hrs

0Ldg


AWL - Life LimitRE (O/C)Hydraulic Brake Control Valve

26-Jan-1996Mos

4,785Hrs0

1,932Ldg0

No.132 A/FNew600-75115-5

1542

AWL - Life LimitRE (O/C)Hydraulic Brake Control Valve

26-Jan-1996Mos

4,785Hrs0

1,932Ldg0

No.232 A/FNew600-75115-5

1247

RE (O/C)Inboard Brake Anti-Skid Valve

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Landing Gear Unit Control

20-Sep-1983Mos

0Hrs

0Ldg



Generated: 6-Apr-2016 1:16 PM126/429







RE (O/C)Main Gear Beam

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Main Gear Beam

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Main Landing Gear Assembly

22-Mar-2012Mos

Hrs

6,004Ldg2,278

Left32 A/FOverhauled601-85082-7

DCL272/00

Component Inspection SimpleDUE: 22-Mar-20171. RE 60 MosMain Landing Gear Assembly - Detailed Inspection32-10-00-237A/F32


TsiDUE: 22-Mar-20221. RE 120 MosMain Landing Gear Assembly - Restoration32-10-00-238A/F32

RE (O/C)Main Landing Gear Assembly

22-Mar-2012Mos

Hrs

6,004Ldg2,278

Right32 A/FOverhauled601-85082-8

DCL269/00

Component Inspection SimpleDUE: 22-Mar-20171. RE 60 MosMain Landing Gear Assembly - Detailed Inspection32-10-00-237A/F32


TsiDUE: 22-Mar-20221. RE 120 MosMain Landing Gear Assembly - Restoration32-10-00-238A/F32

RE (O/C)Main Wheel Assy

26-Sep-2006Mos

10,897.5Hrs

5,558Ldg

Left Inboard32 A/F5009029-1JAN93-0617

Assembly SubDUE:1. RE O/CMain Wheel TireUnknown / UnknownA/F32

Component Inspection SimpleDUE:1. RE T/CMain Wheel - NDT Check32-41-11-231A/F32

Component Inspection SimpleDUE: 6,358 Ldg1. T 1600 Ldg | 2. RA 1600 Ldg | 3. RA 1600 Ldg | 4. RE

800 LdgMain Wheel - Carry out all maintenance requirements in the “...32-41-11-232A/F32


25-Jul-2008Mos

11,432Hrs

5,881Ldg

Left Outboard32 A/F5007045-2JAN84-235









25-Jul-2008Mos

11,432Hrs

5,881Ldg

Right Inboard32 A/F5009029-1JUN85-R494



Generated: 6-Apr-2016 1:16 PM127/429








26-Sep-2006Mos

10,897.5Hrs

5,558Ldg

Right Outboard32 A/F5009029-1NOV95-1044





RE (O/C)Main Wheel Brake Unit

28-Jun-2004Mos

10,421.6Hrs

5,281Ldg

Left Inboard32 A/F5009027-5UNKNOWN

Component Inspection SimpleDUE:1. RE T/CMain Wheel Brake Unit - Brake channel check32-43-11-220A/F32


28-Jun-2004Mos

10,421.6Hrs

5,281Ldg

Left Outboard32 A/F5009027-5AUG82-495



28-Jun-2004Mos

10,421.6Hrs

5,281Ldg

Right Inboard32 A/F5009027-5OCT83-691



04-Dec-2003Mos

9,966.7Hrs

5,011Ldg

Right Outboard32 A/F5009027-5MAY82-426


AWL - Life LimitRE (O/C)Main Wheel Tire

20-Sep-1983Mos

0Hrs

0Ldg



20-Sep-1983Mos

0Hrs

0Ldg



20-Sep-1983Mos

0Hrs

0Ldg



20-Sep-1983Mos

0Hrs

0Ldg



Generated: 6-Apr-2016 1:16 PM128/429







AWL - Life Limit ≈10-Oct-2147REMLG Axle

22-Mar-2012Mos

Hrs

47,400 Ldg53,72650,0006,004Ldg2,278

Left32 A/FOverhauled6433-1

MBM1029

AWL - Life Limit ≈10-Oct-2147REMLG Axle

22-Mar-2012Mos

Hrs

47,400 Ldg53,72650,0006,004Ldg2,278

Right32 A/FOverhauled6433-1

MBM1050

AWL - Life Limit ≈31-Oct-2016REMLG Door Hinge Fasteners

17-May-2013Mos

347.6 Hrs12,388.860011,788.8Hrs0

6,143Ldg0

Left32 A/FNew104467705

UNKNOWN

(NOTE: (Hinge Sector 600-31587-1/-2 not installed))

AWL - Life Limit ≈31-Oct-2016REMLG Door Hinge Fasteners

17-May-2013Mos

347.6 Hrs12,388.860011,788.8Hrs0

6,143Ldg0

Right32 A/FNew104467705

UNKNOWN

(NOTE: (Hinge Sector 600-31587-1/-2 not installed))

AWL - Life Limit ≈10-Oct-2147REMLG Door Stud

22-Mar-2012Mos

Hrs

47,400 Ldg53,72650,0006,004Ldg2,278


1-3013/12

AWL - Life Limit ≈10-Oct-2147REMLG Door Stud

22-Mar-2012Mos

Hrs

47,400 Ldg53,72650,0006,004Ldg2,278


2-3013/12

RE (O/C)MLG Downlock Assist Actuator

20-Sep-1983Mos

0Hrs0

0Ldg0

Left32 A/FNew600-85001-29

UNKNOWN

RE (O/C)MLG Downlock Assist Actuator

20-Sep-1983Mos

0Hrs0

0Ldg0

Right32 A/FNew600-85001-29

UNKNOWN

AWL - Life Limit ≈15-Sep-2179REMLG Eye Bolt

22-Mar-2012Mos

Hrs

58,895 Ldg65,22163,5366,004Ldg4,319


DCL358

AWL - Life Limit ≈10-Oct-2182REMLG Eye Bolt

22-Mar-2012Mos

Hrs

60,997 Ldg67,32363,5366,004Ldg2,217


MBM1083

AWL - Life LimitRE (O/C)MLG Main Fitting

20-Sep-1983Mos

0Hrs

0Ldg



Generated: 6-Apr-2016 1:16 PM129/429







AWL - Life LimitRE (O/C)MLG Main Fitting

20-Sep-1983Mos

0Hrs

0Ldg


AWL - Life Limit ≈06-Jan-2137REMLG Main Fitting Assy

22-Mar-2012Mos

Hrs

43,526 Ldg49,85246,1266,004Ldg2,278


DER-1035

Assembly SubDUE:1. RE O/CMLG Main FittingUnknown / UnknownA/F32

AWL - Life Limit ≈06-Jan-2137REMLG Main Fitting Assy

22-Mar-2012Mos

Hrs

43,526 Ldg49,85246,1266,004Ldg2,278


DER-1047

Assembly SubDUE:1. RE O/CMLG Main FittingUnknown / UnknownA/F32

AWL - Life Limit ≈24-Jun-2141REMLG Pintle Pin

22-Mar-2012Mos

Hrs

45,134 Ldg51,46047,7346,004Ldg2,278


MBM0704

AWL - Life Limit ≈24-Jun-2141REMLG Pintle Pin

22-Mar-2012Mos

Hrs

45,134 Ldg51,46047,7346,004Ldg2,278


PLT1010

AWL - Life Limit ≈10-Oct-2147REMLG Pivot Pin

22-Mar-2012Mos

Hrs

47,400 Ldg53,72650,0006,004Ldg2,278


MBM0537

AWL - Life Limit ≈10-Oct-2147REMLG Pivot Pin

22-Mar-2012Mos

Hrs

47,400 Ldg53,72650,0006,004Ldg2,278


MBM0524

RE (O/C)MLG Shock Strut

22-Mar-2012Mos

Hrs

6,004Ldg2,278


DCL552/00

RE (O/C)MLG Shock Strut

22-Mar-2012Mos

Hrs

6,004Ldg2,278


DCL553/00

AWL - Life Limit ≈10-Oct-2147REMLG Shock Strut Cylinder

22-Mar-2012Mos

Hrs

47,400 Ldg53,72650,0006,004Ldg2,278


DER1022


Generated: 6-Apr-2016 1:16 PM130/429







AWL - Life Limit ≈10-Oct-2147REMLG Shock Strut Cylinder

22-Mar-2012Mos

Hrs

47,400 Ldg53,72650,0006,004Ldg2,278


DER1007

AWL - Life Limit ≈10-Oct-2147REMLG Shock Strut Lower Pin

22-Mar-2012Mos

Hrs

47,400 Ldg53,72650,0006,004Ldg2,278


DCL007

AWL - Life Limit ≈10-Oct-2147REMLG Shock Strut Lower Pin

22-Mar-2012Mos

Hrs

47,400 Ldg53,72650,0006,004Ldg2,278


2-3013/06

AWL - Life Limit ≈10-Oct-2147REMLG Shock Strut Piston

22-Mar-2012Mos

Hrs

47,400 Ldg53,72650,0006,004Ldg2,278


DCL618

AWL - Life Limit ≈10-Oct-2147REMLG Shock Strut Piston

22-Mar-2012Mos

Hrs

47,400 Ldg53,72650,0006,004Ldg2,278


DCL622

AWL - Life Limit ≈21-Sep-2148REMLG Shock Strut Upper Pin

22-Mar-2012Mos

Hrs

47,741 Ldg54,06750,3416,004Ldg2,278


MBM0071

AWL - Life Limit ≈23-Oct-2153REMLG Shock Strut Upper Pin

26-Sep-2006Mos

10,897.5Hrs0

49,573 Ldg55,89950,3415,558Ldg0


UNKNOWN

AWL - Life Limit ≈21-May-2092REMLG Side Brace to A/C Fitting Pin

22-Mar-2012Mos

Hrs

27,461 Ldg33,78730,0006,004Ldg2,217


1-3013/12

AWL - Life Limit ≈21-May-2092REMLG Side Brace to A/C Fitting Pin

22-Mar-2012Mos

Hrs

27,461 Ldg33,78730,0006,004Ldg2,217

Right32 A/F600-10237-12-3013/12

RE (O/C)MLG Side Stay (W/ Harness) Actuator Assembly

22-Mar-2012Mos

Hrs

6,004Ldg4,319


DCL114/89/95

RE (O/C)MLG Side Stay (W/ Harness) Actuator Assembly

22-Mar-2012Mos

Hrs

6,004Ldg8,072


DCL104/89/00R


Generated: 6-Apr-2016 1:16 PM131/429







AWL - Life Limit ≈09-Feb-2142REMLG Side Stay Cylinder

22-Mar-2012Mos

Hrs

45,359 Ldg51,68550,0006,004Ldg4,319

Left32 A/FOverhauled104467734

DCL328

AWL - Life Limit ≈11-Dec-2147REMLG Side Stay Cylinder

22-Mar-2012Mos

Hrs

47,461 Ldg53,78750,0006,004Ldg2,217

Right32 A/FOverhauled104467734

DER1052

AWL - Life Limit ≈11-Jan-2130REMLG Side Stay Pin

22-Mar-2012Mos

Hrs

41,011 Ldg47,33743,6116,004Ldg2,278


MBM2111

AWL - Life Limit ≈11-Jan-2130REMLG Side Stay Pin

22-Mar-2012Mos

Hrs

41,011 Ldg47,33743,6116,004Ldg2,278


MBM2143

AWL - Life Limit ≈03-Nov-2138REMLG Side Stay Piston Rod

22-Mar-2012Mos

Hrs

44,183 Ldg50,50950,0006,004Ldg5,495


DCL352

AWL - Life Limit ≈06-Sep-2131REMLG Side Stay Piston Rod

22-Mar-2012Mos

Hrs

41,606 Ldg47,93250,0006,004Ldg8,072


DCL308

AWL - Life Limit ≈10-Oct-2147REMLG Trailing Arm

22-Mar-2012Mos

Hrs

47,400 Ldg53,72650,0006,004Ldg2,278


DCL641

AWL - Life Limit ≈10-Oct-2147REMLG Trailing Arm

22-Mar-2012Mos

Hrs

47,400 Ldg53,72650,0006,004Ldg2,278


MBM1021

AWL - Life Limit ≈02-Jan-2168REMLG Uplock Actuator Assembly

20-Sep-1983Mos

0Hrs0

54,682 Ldg61,00861,0080Ldg0

Left32 A/FNew200815001

UNKNOWN

AWL - Life Limit ≈02-Jan-2168REMLG Uplock Actuator Assembly

20-Sep-1983Mos

0Hrs0

54,682 Ldg61,00861,0080Ldg0

Right32 A/FNew200815001

UNKNOWN

AWL - Life Limit ≈31-Dec-2062RENLG Attachment Pin (Main Fitting to Drag Brace)

22-Mar-2012Mos

Hrs

16,880 Ldg23,20619,4806,004Ldg2,278

32 A/FOverhauled200811721

MY808750


Generated: 6-Apr-2016 1:16 PM132/429







AWL - Life LimitRE (O/C)NLG Axle Assy

20-Sep-1983Mos

0Hrs

0Ldg


Assembly SubDUE: 23,206 Ldg1. RE 19480 LdgNLG Axle Fitting200811308 / DCL0606A/F32

AWL - Life Limit ≈31-Dec-2062RENLG Axle Fitting

22-Mar-2012Mos

Hrs

16,880 Ldg23,20619,4806,004Ldg2,278


DCL0606

RE (O/C)NLG Drag Brace Assembly

22-Mar-2012Mos

Hrs

6,004Ldg2,278

32 A/FOverhauled600-85002-45

DCL284/00

AWL - Life Limit ≈31-Dec-2062RENLG Drag Brace Lower Link

22-Mar-2012Mos

Hrs

16,880 Ldg23,20619,4806,004Ldg2,278


MIL-0011

AWL - Life Limit ≈31-Dec-2062RENLG Drag Brace Upper Hinge Pin

22-Mar-2012Mos

Hrs

16,880 Ldg23,20619,4806,004Ldg2,278


PEG1141

AWL - Life Limit ≈31-Dec-2062RENLG Drag Brace Upper Link

22-Mar-2012Mos

Hrs

16,880 Ldg23,20619,4806,004Ldg2,278

32 A/FOverhauled7202-3

DER-1030

AWL - Life Limit ≈31-Dec-2062RENLG Drag Brace Upper Pivot Pin

22-Mar-2012Mos

Hrs

16,880 Ldg23,20619,4806,004Ldg2,278


PEG1051

AWL - Life Limit ≈31-Dec-2062RENLG Drag Brace Upper Pivot Pin

22-Mar-2012Mos

Hrs

16,880 Ldg23,20619,4806,004Ldg2,278


PEG1093

AWL - Life Limit ≈31-Dec-2062RENLG Main Fitting

22-Mar-2012Mos

Hrs

16,880 Ldg23,20619,4806,004Ldg2,278


TA1071

AWL - Life Limit ≈31-Dec-2062RENLG Pivot (Trunion) Pin

22-Mar-2012Mos

Hrs

16,880 Ldg23,20619,4806,004Ldg2,278


1/3013/12

AWL - Life Limit ≈31-Dec-2062RENLG Pivot (Trunion) Pin

22-Mar-2012Mos

Hrs

16,880 Ldg23,20619,4806,004Ldg2,278


2/3013/12


Generated: 6-Apr-2016 1:16 PM133/429







RE (O/C)NLG Proximity Switch

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)NLG Retraction Actuator

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)NLG Retraction Actuator, Lower Pin

20-Sep-1983Mos

0Hrs0

0Ldg0

32 A/FNew200811773

UNKNOWN

RE (O/C)NLG Shock Strut

22-Mar-2012Mos

Hrs

6,004Ldg2,278

32 A/FOverhauled601-85002-13

DCL376/00

AWL - Life Limit ≈31-Dec-2062RENLG Shock Strut Sliding Tube

22-Mar-2012Mos

Hrs

16,880 Ldg23,20619,4806,004Ldg2,278


MBM0106

AWL - Life Limit ≈28-Apr-2069RENLG Sliding Tube to End Fitting Pin

22-Mar-2012Mos

Hrs0

19,158 Ldg25,48419,4806,004Ldg0

32 A/FNew200811602

11EXC0593

RE (O/C)NLG Steering Compensator

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)NLG Steering Selector Valve

23-Feb-2003Mos

9,253.9Hrs

4,606Ldg

32 A/F150446002576

AWL - Life Limit ≈28-Feb-2143RENLG Uplock Assy

20-Sep-1983Mos

0Hrs0

45,739 Ldg52,06552,0650Ldg0

32 A/FNew600-85002-9

UNKNOWN

RE (O/C)Nose Landing Gear Assembly

20-Sep-1983Mos

0Hrs

0Ldg


Component Inspection SimpleDUE:1. RE 60 MosNose Landing Gear Assembly - Detailed Inspection32-20-00-239A/F32


TsiDUE: 24-Oct-20211. RE 120 MosNose Landing Gear Assembly - Detailed Inspection32-20-00-240A/F32


Generated: 6-Apr-2016 1:16 PM134/429







RE (O/C)Nose Landing Gear Doors Actuator

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Nose Landing Gear Selector Valve

20-Sep-1983Mos

0Hrs0

0Ldg0

No.132 A/FNew55540-2

UNKNOWN

RE (O/C)Nose Landing Gear Selector Valve

27-Apr-2002Mos

8,378.4Hrs

4,058Ldg

No.232 A/F55540-5250

RE (O/C)Nose Wheel Assy

15-Sep-2007Mos

11,184.3Hrs

5,748Ldg

Left32 A/F5006450-1MAR98-8484

Assembly SubDUE:1. RE O/CNose Wheel Tire184F23-2 / 60581162A/F32

Component Inspection SimpleDUE:1. RE T/CNose Wheel (Part Number 600-85003 All Dash Numbers) - NDT Ch...32-41-16-234A/F32


800 LdgNose Wheel (Part Number 600-85003 All Dash Numbers) - Carry ...32-41-16-235A/F32

RE (O/C)Nose Wheel Assy

15-Sep-2007Mos

11,184.3Hrs

5,748Ldg

Right32 A/F5006450-1MAY90-0599

Assembly SubDUE:1. RE O/CNose Wheel Tire184F23-2 / 60581160A/F32

Component Inspection SimpleDUE:1. RE T/CNose Wheel (Part Number 600-85003 All Dash Numbers) - NDT Ch...32-41-16-234A/F32


800 LdgNose Wheel (Part Number 600-85003 All Dash Numbers) - Carry ...32-41-16-235A/F32

RE (O/C)Nose Wheel Tire

26-Sep-2006Mos

10,897.5Hrs

5,558Ldg

Left32 A/F184F23-260581162

RE (O/C)Nose Wheel Tire

26-Sep-2006Mos

10,897.5Hrs

5,558Ldg

Right32 A/F184F23-260581160

RE (O/C)Nosewheel Steering Handwheel

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Nosewheel Steering, Electronic Control Module

20-Sep-1983Mos

0Hrs0

0Ldg0

32 A/FNew7040-11

UNKNOWN

Component Inspection SimpleDUE:1. RE 600 HrsNosewheel Steering - Functional test of Electronic Control M...32-50-00-236A/F32


Generated: 6-Apr-2016 1:16 PM135/429







RE (A/R)NW Steering Arming Valve

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)NWS Control Manifold

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Outboard Brake Anti-Skid Valve

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Parking Brake SOV Valve

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Proximity Switch

20-Sep-1983Mos

0Hrs

0Ldg



05-Mar-2008Mos

11,387.8Hrs

5,856Ldg

Left Inboard32 A/F256K43-370377113


25-Jul-2008Mos

11,432Hrs

5,881Ldg

Left Outboard32 A/F256K43-380727106


25-Jul-2008Mos

11,432Hrs

5,881Ldg

Right Inboard32 A/F256K43-380767095


05-Mar-2008Mos

11,387.8Hrs

5,856Ldg

Right Outboard32 A/F256K43-361657040

RE (O/C)Sector Mlg Door Hinge

20-Sep-1983Mos

0Hrs0

0Ldg0

Left32 A/FNew600-31195-7

UNKNOWN

RE (O/C)Sector Mlg Door Hinge

20-Sep-1983Mos

0Hrs0

0Ldg0


UNKNOWN


Generated: 6-Apr-2016 1:16 PM136/429







RE (O/C)Sensor, Nosewheel Steering, RVT

20-Sep-1983Mos

0Hrs

0Ldg

NLG32 A/FUnknownUnknown

AWL - Life Limit ≈24-Aug-2052RESliding Tube/End Fitting Special Bolt

20-Sep-1983Mos

0Hrs

13,154 Ldg19,48019,4800Ldg0


RE (O/C)Steering Potentiometer Control

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Wheel Speed - Anti-Skid System Sensor

15-Sep-2007Mos

11,184.3Hrs

5,748Ldg

Left Inboard32 A/F600-87000-5JUN89-3019


15-Sep-2007Mos

11,184.3Hrs

5,748Ldg

Left Outboard32 A/F600-87000-5JAN81-1404


20-Sep-1983Mos

0Hrs

0Ldg



26-Mar-2007Mos

11,045.9Hrs

5,659Ldg

Right Outboard32 A/F6002504NOV86-1835

MandatoryRE (-)2000-19-01 Main Landing Gear

22-Mar-2001Mos

7,444.3Hrs

3,496Ldg

32 A/FSB 601-0024Eff: 25-Oct-2000 Complied

With

MandatoryRE (-)2000-24-01 Main Landing Gear Wheel Bay Protection Shields

31-Dec-2002Mos

9,154.3Hrs

4,543Ldg

32 A/FSB 601-0507Eff: 19-Dec-2000 Complied

With

Compliance Share DoubleDUE:1. T A/R | 2. RE -Modification - Main Landing Gear Bay Fairing - Add a Protect...601-0507A/F53

MandatoryRE (-)2005-15-04 Landing gear parts

11-Nov-2015Mos

12,012.8Hrs

6,303Ldg

32 A/F03/09/2012, 11578.6 previouslyEff: 30-Aug-2005 Complied

With

(NOTE: Superseded By FAA AD 2014-15-13)

Nextdue Share EarliestDUE:1. RE -Landing gear parts - Add Serial Numbers or Part Numbers2005-15-04 Paragraph (f)(1)A/F32

Nextdue Share EarliestDUE:1. RE -Landing gear parts - Add Serial Numbers or Part Numbers2005-15-04 Paragraph (f)(2)A/F32

Nextdue Share EarliestDUE:1. RE -Landing gear parts - Revise the Airworthiness Limitations Se...2005-15-04 Paragraph (h)A/F32


Generated: 6-Apr-2016 1:16 PM137/429







MandatoryRE (-)2005-15-04 Paragraph (f)(1) Landing gear parts - Add Serial Numbers or Part Numbers

Mos

Hrs

Ldg

32 A/FEff: 30-Aug-2005

Compliance Share DoubleDUE:1. T A/R | 2. RE -Modification - Nose Landing Gear (NLG) and Main Landing Gear...601-0546 Rev 3A/F32

MandatoryRE (-)2005-15-04 Paragraph (f)(2) Landing gear parts - Add Serial Numbers or Part Numbers

Mos

Hrs

Ldg

32 A/FEff: 30-Aug-2005


MandatoryRE (-)2005-15-04 Paragraph (h) Landing gear parts - Revise the Airworthiness Limitations Section (ALS)

Mos

Hrs

Ldg

32 A/FEff: 30-Aug-2005

MandatoryRE (-)2007-14-02 Uncommanded partial retractions of the nose landing gear (NLG) - Prevent internal leakage of the selector valve - CANCELLED

25-Jul-2008Mos

11,432Hrs

5,881Ldg

32 A/FBY PART NUMBER INSTALLEDEff: 16-Aug-2007 Not

Applicable

MandatoryRE (-)2010-10-26 Landing Gear

02-Dec-2009Mos

11,460.7Hrs

5,905Ldg

32 A/FFOUND P/C/WEff: 25-Jun-2010 Complied

With

Compliance Share DoubleDUE:1. T A/R | 2. RE -Special Check/Rework - Extension and Retraction - End Caps o...601-0558 Rev 3A/F32

MandatoryRE (-)2014-15-13 Landing Gear

23-Dec-2014Mos

11,855.8Hrs

6,191Ldg

32 A/F03/09/12, 11578.6 previouslyEff: 25-Sep-2014 Complied

With

Nextdue Share EarliestDUE:1. T 60 Mos | 2. RE -Landing Gear - add serial numbers and part numbers, as appl...2014-15-13 Paragraph (g)(1)A/F32

Nextdue Share EarliestDUE:1. T 120 Mos | 2. RE -Landing Gear - add serial numbers and part numbers, as appl...2014-15-13 Paragraph (g)(2)A/F32

Nextdue Share EarliestDUE:1. T A/R | 2. RE -Landing Gear - if a component does not have a serial numbe...2014-15-13 Paragraph (h)A/F32

Nextdue Share EarliestDUE:1. RE -Landing Gear - ALS Revision2014-15-13 Paragraph (i)A/F32

Nextdue Share EarliestDUE: 25-Sep-20191. T 60 Mos | 2. RE -Landing Gear - add serial numbers and part numbers, to to l...2014-15-13 Paragraph (l) (2)A/F32

Nextdue Share EarliestDUE: 25-Sep-20241. T 120 Mos | 2. RE -Landing Gear - add serial numbers and part numbers, as appli...2014-15-13 Paragraph (l) (3)A/F32

MandatoryRE (-)2014-15-13 Paragraph (g)(1) Landing Gear - add serial numbers and part numbers, as applicable, to the parts identified in Part A of the applicable service bulletin.

26-Sep-2006Mos

10,897.5Hrs

5,558Ldg

32 A/FASB A600-0710,A601-0546Eff: 30-Aug-2005 Complied

With


MandatoryRE (-)2014-15-13 Paragraph (g)(2) Landing Gear - add serial numbers and part numbers, as applicable, to the parts identified in Part B of the applicable service bulletin.

26-Sep-2006Mos

10,897.5Hrs

5,558Ldg


With



Generated: 6-Apr-2016 1:16 PM138/429







MandatoryT (A/R)2014-15-13 Paragraph (h) Landing Gear - if a component does not have a serial number and the CSN or TSN were not tracked, use the formula in the applicable Messier-Dowty service bulletin

to paragraph (g) of this AD to establish the TSN or CSN, and record the newly calculated TSN or CSN.in the airplane log books.

Mos

Hrs

Ldg

32 A/FEff: 25-Sep-2014

MandatoryRE (-)2014-15-13 Paragraph (i) Landing Gear - ALS Revision

26-Sep-2006Days

10,897.5Hrs

5,558Ldg


With

MandatoryT2014-15-13 Paragraph (l) (2) Landing Gear - add serial numbers and part numbers, to to left and right MLG side strut pins having P/N 6318-1 or 6318-3; and to left and right MLG hinge pins having

P/N 6329-3

3.5 Years25-Sep-201960Mos

Hrs

Ldg

32 A/FEff: 25-Sep-2014


MandatoryT2014-15-13 Paragraph (l) (3) Landing Gear - add serial numbers and part numbers, as applicable, to NLG main fitting/drag stay pins having P/N 200811721; NLG drag brace pivot pins having P/N

200814601; and left and right MLG pintle pins having P/N 6324-1

8.5 Years25-Sep-2024120Mos

Hrs

Ldg

32 A/FEff: 25-Sep-2014


MRBRE (N/A)32-00-00-245 Extension and Retraction - Main Landing Gear Selector Valve (Part No. 61750-1) - Restoration

Mos

Hrs

Ldg



Servicing - RecommendedRE (See Note)32-00-00-301 Landing Gear - Cleaning of the Landing Gear

Mos

Hrs

Ldg

32 A/F

(ZONE: 710, 740) (SOURCE: MPD 3.2) (NOTE: This task is required after operation in airports that usepotassium acetate-based Runway De-

Icing fluid. Thecleaning and lubrication of the landing gears should beaccomplished at the earliest convenience after operationin such an

environment.)

MRB ≈03-May-2017RE32-05-11-201 Weight on Wheels Functional Test

10-Feb-2016Mos

590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs

6,326Ldg

(PKG 600 Hour)

32 A/F


MRB ≈18-Sep-2016RE32-10-00-210 Main Gear and Doors / Main Landing Gear Uplock /Emergency Extension Visual Check

10-Feb-2016Mos

290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs

6,326Ldg

(PKG 300 Hour)

32 A/F

Ref.:PSP 612 Part 9 VC-32-10-01 for Landing Gear check (SOURCE: TLMC 05-20-15)

Also ConsiderDUE: (12,332 Hrs)1. RE 300 HrsMain Landing Gear - CPCP CheckC32-10-801A/F32

MRBRE32-10-00-237 Main Landing Gear Assembly - Detailed Inspection

11.7 Months (+31

Days)22-Mar-2017-/+16022-Mar-2012Mos

Hrs

Ldg

Left

(PKG 60 Month)

32 A/F

601-85082-7DCL272/00



Generated: 6-Apr-2016 1:16 PM139/429







MRBRE32-10-00-237 Main Landing Gear Assembly - Detailed Inspection

11.7 Months (+31

Days)22-Mar-2017-/+16022-Mar-2012Mos

Hrs

Ldg

Right

(PKG 60 Month)

32 A/F

601-85082-8DCL269/00


MRBRE32-10-00-238 Main Landing Gear Assembly - Restoration

6 Years (+31 Days)22-Mar-2022-/+112022-Mar-2012Mos

Hrs

Ldg

Left32 A/F601-85082-7DCL272/00


MRBRE32-10-00-238 Main Landing Gear Assembly - Restoration

6 Years (+31 Days)22-Mar-2022-/+112022-Mar-2012Mos

Hrs

Ldg

Right32 A/F601-85082-8DCL269/00


MRB ≈18-Sep-2016RE32-10-00-241 Main Landing Gear Lubricate Landing Gear

10-Feb-2016Mos

290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs

6,326Ldg

(PKG 300 Hour)

32 A/F


MRBRE32-10-36-204 Main Gear Trailing Arm Check transverse shear bolt

6.6 Months (+31

Days)(21-Oct-2016)-/+11221-Oct-2015Mos

Hrs

Ldg

(PKG 12 Month)

32 A/F


MRB ≈18-Sep-2016RE32-20-00-205 Nose Gear and Doors Visual Check

10-Feb-2016Mos

290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs

6,326Ldg

(PKG 300 Hour)

32 A/F


Also ConsiderDUE: (12,332 Hrs)1. RE 300 HrsNose Landing Gear - CPCP CheckC32-20-801A/F32

MRBRE32-20-00-239 Nose Landing Gear Assembly - Detailed Inspection

5.8 Months (+30

Days)(26-Sep-2016)-/+16024-Oct-2011Mos

Hrs

Ldg

(PKG 60 Month)

32 A/F

UnknownUnknown


MRBRE32-20-00-240 Nose Landing Gear Assembly - Detailed Inspection

5.6 Years (+31 Days)24-Oct-2021-/+112024-Oct-2011Mos

Hrs

Ldg



MRB ≈18-Sep-2016RE32-20-00-242 Nose Landing Gear Lubricate Nose Landing Gear

10-Feb-2016Mos

290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs

6,326Ldg

(PKG 300 Hour)

32 A/F



Generated: 6-Apr-2016 1:16 PM140/429







MRB ≈03-May-2017RE32-30-00-207 Extension and Retraction Functional Test - Landing Gear Retraction System - Functional Test - Landing Gear Extension System

10-Feb-2016Mos

590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs

6,326Ldg

(PKG 600 Hour)

32 A/F


MRB ≈20-Oct-2017RE32-30-00-208 Extension and Retraction Landing gear control unit - check for zero output to selectorvalves

29-Oct-2012Mos

812.3 Hrs (+40)(12,853.5)-/+401,20011,653.5Hrs

Ldg

(PKG 1200 Hour)

32 A/F


MRB ≈15-Jun-2016RE32-30-00-209 Extension and Retraction Priority Valves Functional Test

18-Oct-2003Mos

167 Hrs (+40)12,208.2-/+402,4009,808.2Hrs

Ldg

(PKG 2400 Hour)

32 A/F


MRB ≈03-May-2017RE32-30-26-206 Nose Gear Drag Brace Visual Check, paying particular attention to the hinge and attachment pin

10-Feb-2016Mos

590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs

6,326Ldg

(PKG 600 Hour)

32 A/F


MRB ≈18-Sep-2016RE32-30-51-211 Nose Landing Gear Uplock Visual Check, paying particular attention to the tension springand latch jaws. Ensure the latch jaws and the engaging pin on the leg are free

of contamination, corrosion and significant contact damage. Do not lubricate

10-Feb-2016Mos

290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs

6,326Ldg

(PKG 300 Hour)

32 A/F


MRB ≈03-May-2017RE32-35-00-212 Emergency Extension Functional Test

10-Feb-2016Mos

590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs

6,326Ldg

(PKG 600 Hour)

32 A/F


MRB ≈03-May-2017RE32-35-00-243 Emergency Extension Visual Check of the control path (except for straight runs undercabin floor), paying particular attention to security of the manul release cables

(per 20-40-00 Wire Cables - Inspection Procedures), pulleys and attachment linkages

10-Feb-2016Mos

590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs

6,326Ldg

(PKG 600 Hour)

32 A/F


MRBRE32-35-00-244 Emergency Extension Visual Check of the control path (straight runs under cabin floor), paying particular attention to security of the manua release cables (per 20-40-

00 Wire Cables - Inspection Procedures), turnbuckles and pulley

5.8 Months (+30

Days)(26-Sep-2016)-/+16024-Oct-2011Mos

Hrs

Ldg

(PKG 60 Month)

32 A/F


MRBRE (T/C)32-41-11-231 Main Wheel - NDT Check

Mos

Hrs

Ldg


Ref.:PSP 612 Part 6 ET-32-41-01, Ref.:PSP 612 Part 7 MT-32-41-01 (SOURCE: TLMC 05-20-15) (NOTE: [1] Check interval is every 400 Wheel

Landings up to 4800 (except at 1600, 3200 and 4800), then at each subsequent tire change. [2] If any defects are found, a complete wheel

assembly inspection must be performed as per CMM/PSP 608/608A. [3] For 1600, 3200 and 4800 Wheel Landing checks refer to Chapter 5 Ref.

No. 32-41-11-232.)


Generated: 6-Apr-2016 1:16 PM141/429








Mos

Hrs

Ldg





No. 32-41-11-232.)


Mos

Hrs

Ldg

Right Inboard32 A/F5009029-1JUN85-R494




No. 32-41-11-232.)


Mos

Hrs

Ldg





No. 32-41-11-232.)

MRB ≈12-Mar-2016RE32-41-11-232 Main Wheel - Carry out all maintenance requirements in the “CHECK” section of the CMM

26-Sep-2006Mos

Hrs

32 Ldg (+40)6,358-/+408005,558Ldg


Ref.:CMM/PSP 608/608A (SOURCE: TLMC 05-20-15) (NOTE: Check interval is every 1600, 3200 and 4800 Wheel Landings, then at each

subsequent 800 Wheel Landings.)

MRB ≈05-Feb-2017RE32-41-11-232 Main Wheel - Carry out all maintenance requirements in the “CHECK” section of the CMM

25-Jul-2008Mos

Hrs

355 Ldg (+40)6,681-/+408005,881Ldg




MRB ≈05-Feb-2017RE32-41-11-232 Main Wheel - Carry out all maintenance requirements in the “CHECK” section of the CMM

25-Jul-2008Mos

Hrs

355 Ldg (+40)6,681-/+408005,881Ldg




MRB ≈12-Mar-2016RE32-41-11-232 Main Wheel - Carry out all maintenance requirements in the “CHECK” section of the CMM

26-Sep-2006Mos

Hrs

32 Ldg (+40)6,358-/+408005,558Ldg





Generated: 6-Apr-2016 1:16 PM142/429







MRBRE (T/C)32-41-16-234 Nose Wheel (Part Number 600-85003 All Dash Numbers) - NDT Check

Mos

Hrs

Ldg

Left32 A/F5006450-1MAR98-8484



assembly inspection must be performed as per the respective vendor component maintenance manual. [3] For 1600, 3200 and 4800 Wheel

Landing checks refer to Chapter 5 Ref. No. (32-41-16-235).)

MRBRE (T/C)32-41-16-234 Nose Wheel (Part Number 600-85003 All Dash Numbers) - NDT Check

Mos

Hrs

Ldg

Right32 A/F5006450-1MAY90-0599



assembly inspection must be performed as per the respective vendor component maintenance manual. [3] For 1600, 3200 and 4800 Wheel

Landing checks refer to Chapter 5 Ref. No. (32-41-16-235).)

MRB ≈12-Mar-2016RE32-41-16-235 Nose Wheel (Part Number 600-85003 All Dash Numbers) - Carry out all maintenance requirements in the “CHECK” section of the CMM

26-Sep-2006Mos

Hrs

32 Ldg (+40)6,358-/+408005,558Ldg

Left32 A/F5006450-1MAR98-8484

Ref.:CMM/PSP 608/608A (SOURCE: TLMC 05-20-15)

MRB ≈12-Mar-2016RE32-41-16-235 Nose Wheel (Part Number 600-85003 All Dash Numbers) - Carry out all maintenance requirements in the “CHECK” section of the CMM

26-Sep-2006Mos

Hrs

32 Ldg (+40)6,358-/+408005,558Ldg

Right32 A/F5006450-1MAY90-0599

Ref.:CMM/PSP 608/608A (SOURCE: TLMC 05-20-15)

MRBRE (T/C)32-43-11-220 Main Wheel Brake Unit - Brake channel check

Mos

Hrs

Ldg

Left Inboard32 A/F5009027-5UNKNOWN



Mos

Hrs

Ldg

Left Outboard32 A/F5009027-5AUG82-495



Mos

Hrs

Ldg

Right Inboard32 A/F5009027-5OCT83-691



Mos

Hrs

Ldg

Right Outboard32 A/F5009027-5MAY82-426


MRB ≈18-Sep-2016RE32-43-16-222 Accumulator/Hydraulic System - Replenishing Check accumulator charge pressure (Brake Accumulators Only)

10-Feb-2016Mos

290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs

6,326Ldg

(PKG 300 Hour)

32 A/F



Generated: 6-Apr-2016 1:16 PM143/429







MRBRE32-43-16-223 Accumulator Visual Check of No. 2 and No. 3 System Brake Accumulators

5.8 Months (+30

Days)(26-Sep-2016)-/+16024-Oct-2011Mos

Hrs

Ldg

(PKG 60 Month)

32 A/F


MRB ≈18-Sep-2016RE32-43-21-216 Dual Brake Control Valve Assembly Visual Check visible portions of brake plungers, all linkages and push-pull cables forward of pressure bulkhead (FS202.75)

10-Feb-2016Mos

290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs

6,326Ldg

(PKG 300 Hour)

32 A/F


MRB ≈03-May-2017RE32-43-21-221 Dual Brake Control Valve Assembly Brake pressure decay check

10-Feb-2016Mos

590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs

6,326Ldg

(PKG 600 Hour)

32 A/F


MRB ≈03-May-2017RE32-45-11-217 Parking Brake Control Cable Assembly / Pilots and Co-Pilots Push Pull Brake Cables Visual Check of input mechanisms to brake control valve aft ofpressure bulkhead

FS202.75

10-Feb-2016Mos

590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs

6,326Ldg

(PKG 600 Hour)

32 A/F


MRB ≈13-Jul-2017RE32-45-31-224 Parking Brake Shutoff Valve Functional Test - Parking Brake Shut-Off Valve

11-Dec-2003Mos

684 Hrs (+30)(12,725.2)-/+402,4009,966.7Hrs

Ldg

(PKG 2400 Hour)

32 A/F


MRB ≈03-May-2017RE32-47-00-225 Anti-Skid System Anti-skid system operational test

10-Feb-2016Mos

590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs

6,326Ldg

(PKG 600 Hour)

32 A/F


≈18-Sep-2016RE32-47-00-226 Functional Test of Nose Wheel Steering Selector Valve

10-Feb-2016Mos

290.8 Hrs (+40)(12,332)30012,041.2Hrs

Ldg

(PKG 300 Hour)

32 A/F

MRB ≈18-Sep-2016RE32-50-00-226 Nosewheel Steering Nosewheel Steering Selector and arming valves functional test

10-Feb-2016Mos

290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs

6,326Ldg

(PKG 300 Hour)

32 A/F


MRB ≈03-May-2017RE32-50-00-236 Nosewheel Steering - Functional test of Electronic Control Module, Part No.601-86100-9/-13, Vendor Part No. 7040-9/-11/-13/-15

10-Feb-2016Mos

590.8 Hrs (+40)(12,632)60012,041.2Hrs

6,326Ldg

(PKG 600 Hour)

32 A/F

7040-11UNKNOWN


MRBRE (N/A)32-70-00-202 Gravel Runway Protection (Post SB 601-0112) Visual Check

Mos

Hrs

Ldg

32 A/F



Generated: 6-Apr-2016 1:16 PM144/429







RecommendedRE (-)601-0019 Modification - N.L.G. Downlock No. 2 - Wiring Change

Mos

Hrs

Ldg

32 A/FEff: 14-Jun-1983

RecommendedRE (-)601-0022 Modification - Nose Landing Gear - Downlock Microswitch

Mos

Hrs

Ldg

32 A/FEff: 06-Sep-1983

RecommendedRE (-)601-0024 Modification - Main Landing Gear - Wheel Discs Sealing Cap (Blanking Plate), Brake Shields and Deflectors

Mos

Hrs

Ldg

32 A/F

RecommendedRE (-)601-0024 Rev 1 Modification - Main Landing Gear - Wheel Discs Sealing Cap (Blanking Plate), Brake Shields and Deflectors

Mos

Hrs

Ldg

32 A/F

RecommendedRE (-)601-0024 Rev 2 Modification - Main Landing Gear - Wheel Discs Sealing Cap (Blanking Plate), Brake Shields and Deflectors

Mos

Hrs

Ldg

32 A/F

RecommendedT (A/R)601-0024 Rev 3 Modification - Main Landing Gear - Wheel Discs Sealing Cap (Blanking Plate), Brake Shields and Deflectors

Mos

Hrs

Ldg

32 A/FEff: 27-Nov-1984

RecommendedRE (-)601-0034 Anti-Skid System - Wheel Spin-Up

Mos

Hrs

Ldg

32 A/F

RecommendedRE (-)601-0034 Rev 1 Anti-Skid System - Wheel Spin-Up

Mos

Hrs

Ldg

32 A/FEff: 16-Aug-1984

OptionalRE (-)601-0039 Modification - Landing Gear - Alternate Downlock Indication

Mos

Hrs

Ldg

32 A/F

OptionalT (A/R)601-0039 Rev 1 Modification - Landing Gear - Alternate Downlock Indication

Mos

Hrs

Ldg

32 A/FEff: 23-Jun-1986

RecommendedRE (-)601-0041 Modification - Nose Wheel Steering - Control Unit

Mos

Hrs

Ldg

32 A/FEff: 22-Dec-1983


Generated: 6-Apr-2016 1:16 PM145/429







RecommendedRE (-)601-0079 Special Check/Modification - Parking Brake Valve - Fouling on APU Fuel Line

Mos

Hrs

Ldg

32 A/FEff: 24-Jul-1984

RecommendedRE (-)601-0091 Special Check/Modification - Electrical Harnesses - Installation

Mos

Hrs

Ldg

32 A/F

RecommendedT (A/R)601-0091 Rev 1 Special Check/Modification - Electrical Harnesses - Installation

Mos

Hrs

Ldg

32 A/FEff: 27-Jan-1986

RecommendedRE (-)601-0092 Modification - Steer-by-Wire System – Improvements

Mos

Hrs

Ldg

32 A/F

RecommendedRE (-)601-0092 Rev 1 Modification - Steer-by-Wire System – Improvements

Mos

Hrs

Ldg

32 A/F


Mos

Hrs

Ldg

32 A/F


Mos

Hrs

Ldg

32 A/F


26-Jan-1987Mos

1,267Hrs

480Ldg


RecommendedRE (-)601-0093 Special Check/Modification - Manual Release Cable - Grommets

Mos

Hrs

Ldg

32 A/FEff: 05-Jun-1984

OptionalRE (-)601-0100 Modification - Manual Release System - Handle and Lever Assemblies

Mos

Hrs

Ldg

32 A/F

OptionalRE (-)601-0100 Rev 1 Modification - Manual Release System - Handle and Lever Assemblies

25-Nov-2000Mos

Hrs

Ldg



Generated: 6-Apr-2016 1:16 PM146/429







OptionalRE (-)601-0112 Modification - Operation from Unpaved/Gravel Runways - Protection

Mos

Hrs

Ldg

32 A/F

OptionalT (A/R)601-0112 Rev 1 Modification - Operation from Unpaved/Gravel Runways - Protection

Mos

Hrs

Ldg

32 A/FEff: 16-Jun-1989

RecommendedRE (-)601-0146 Modification - Main Landing Gear - Door Hinge

02-May-1988Mos

1,995Hrs

756Ldg


OptionalRE (-)601-0177 Modification - Nose Gear - Introduction of Earthing Point

Mos

Hrs

Ldg

32 A/F

OptionalRE (-)601-0177 Rev 1 Modification - Nose Gear - Introduction of Earthing Point

Mos

Hrs

Ldg

32 A/F

OptionalT (A/R)601-0177 Rev 2 Modification - Nose Gear - Introduction of Earthing Point

Mos

Hrs

Ldg

32 A/FEff: 21-Jun-1989

OptionalT (A/R)601-0203 Modification - Brake Control Mechanism - Plunger Assembly Replacement

Mos

Hrs

Ldg

32 A/FEff: 24-Feb-1989

RecommendedRE (-)601-0206 Modification - Priority Valve - Relocation to Aft MLG Bay Bulkhead

28-Mar-1989Mos

2,373Hrs

910Ldg


RecommendedRE (-)601-0242 Modification - Steer-by-Wire - Reliability Improvements

28-Mar-1989Mos

2,373Hrs

910Ldg

32 A/FComplied With

RecommendedRE (-)601-0242 Rev 1 Modification - Steer-by-Wire - Reliability Improvements

28-Mar-1989Mos

2,373Hrs

910Ldg


OptionalRE (-)601-0266 Modification - Nose Gear Doors - External Ground Operation

Mos

Hrs

Ldg

32 A/F


Generated: 6-Apr-2016 1:16 PM147/429







OptionalRE (-)601-0266 Rev 1 Modification - Nose Gear Doors - External Ground Operation

12-Nov-1997Mos

Hrs

Ldg


RecommendedRE (-)601-0267 Modification - Nose Landing Gear - Shock Strut

Mos

Hrs

Ldg

32 A/F

RecommendedRE (-)601-0267 Rev 1 Modification - Nose Landing Gear - Shock Strut

Mos

Hrs

Ldg

32 A/F

RecommendedRE (-)601-0267 Rev 2 Modification - Nose Landing Gear - Shock Strut

01-Dec-1990Mos

3,058.6Hrs

1,212Ldg


RecommendedRE (-)601-0285 Special Check/Modification - NLG and MLG Harness Assemblies - Replacement/Rerouting

Mos

Hrs

Ldg

32 A/F

RecommendedRE (-)601-0285 Rev 1 Special Check/Modification - NLG and MLG Harness Assemblies - Replacement/Rerouting

Mos

Hrs

Ldg

32 A/F

RecommendedT (A/R)601-0285 Rev 2 Special Check/Modification - NLG and MLG Harness Assemblies - Replacement/Rerouting

Mos

Hrs

Ldg

32 A/FEff: 15-Dec-1997

RecommendedRE (-)601-0299 Modification - Manual Release System - Cable Support Bracket Relocation

Mos

Hrs

Ldg

32 A/FEff: 15-Nov-1989

RecommendedRE (-)601-0303 Special Check/Modification - Main Landing Gear - Shock Strut Rebound Ring

01-Dec-1990Mos

3,058.6Hrs

1,212Ldg


OptionalRE (-)601-0331 Modification - Main Landing Gear - Removal of Wheel Speed Sensor Set-Screw

12-Nov-1992Mos

3,754Hrs

1,519Ldg


OptionalRE (-)601-0363 Modification - Landing Lights - Pulsating Light System

Mos

Hrs

Ldg

32 A/F


Generated: 6-Apr-2016 1:16 PM148/429







OptionalRE (-)601-0363 Rev 1 Modification - Landing Lights - Pulsating Light System

Mos

Hrs

Ldg

32 A/F

OptionalT (A/R)601-0363 Rev 2 Modification - Landing Lights - Pulsating Light System

Mos

Hrs

Ldg

32 A/FEff: 07-Jun-1993

RecommendedRE (-)601-0373 Special Check/Modification - Emergency Extension - Main Landing Gear Manual Release Cable and Dump Valve Lever

31-Oct-1993Mos

4,142Hrs

1,668Ldg


RecommendedRE (-)601-0398 Special Check/Modification - Nose Gear Downlock Indication - Wire Correction

23-Oct-1992Mos

3,754Hrs

1,519Ldg


OptionalT (A/R)601-0444 Modification - Main Landing Gear Priority Valve and Hydraulic Lines

Mos

Hrs

Ldg

32 A/FEff: 30-Apr-1996

RecommendedRE (-)601-0446 Modification - Nose-Gear Door Actuator Improvement to Ground Locking Capability

18-Nov-1996Mos

5,001Hrs

2,052Ldg


OptionalT (A/R)601-0461 Modification - Left Nose Landing Gear (NLG) Door - Installation of Rubber Stop at Aft Hinge

Mos

Hrs

Ldg

32 A/FEff: 31-Oct-1995

OptionalRE (-)601-0469 Modification - Navigation Lights - Replace Navigation Light at Vertical Stabilizer

Mos

Hrs

Ldg

32 A/F

OptionalRE (-)601-0469 Rev 1 Modification - Navigation Lights - Replace Navigation Light at Vertical Stabilizer

Mos

Hrs

Ldg

32 A/F

OptionalT (A/R)601-0469 Rev 2 Modification - Navigation Lights - Replace Navigation Light at Vertical Stabilizer

Mos

Hrs

Ldg

32 A/FEff: 30-Apr-2004

RecommendedRE (-)601-0472 Special Check/Modification - MLG Door Mechanism - Possible Fouling Between Crank and Door Strut Link

18-Nov-1996Mos

5,001Hrs

2,052Ldg



Generated: 6-Apr-2016 1:16 PM149/429







RecommendedRE (-)601-0494 Modification - Replace the Nose Landing Gear Selector Valve and Nose Gear Door Selector Valve, Part No. 55540-2 with Part No. 55540-5

12-Nov-1997Mos

5,395Hrs

2,274Ldg


OptionalRE (-)601-0500 Brake System - Introduction of Restrictor in Nose Landing Gear (NLG) Retraction Line to Brake Metering Valve

05-Nov-1998Mos

5,824Hrs

2,521Ldg


RecommendedRE (-)601-0526 Special Check/Modification - Weight-on- Wheel Proximity Switches - Prevent Uncommanded Deployment of the Air Driven Generator on the Ground

Mos

Hrs

Ldg

32 A/F

RecommendedRE (-)601-0526 Rev 1 Special Check/Modification - Weight-on- Wheel Proximity Switches - Prevent Uncommanded Deployment of the Air Driven Generator on the Ground

26-Sep-2006Mos

10,897.5Hrs

5,558Ldg


OptionalT (A/R)601-0531 Modification - Nose Landing Gear - Introduction of Allowable Wear Limits and Replacement of the Structural Support Bushings for the NLG Trunnion and the NLG Drag

Brace Attachments

Mos

Hrs

Ldg

32 A/FEff: 30-Sep-2004

RecommendedRE (-)601-0545 Special Check/Rework - Nose Landing Gear (NLG) Extension and Retraction - examine NLG Uplock Pin For Jammed Condition

09-Sep-2001Mos

7,697.4Hrs

3,650Ldg


RecommendedRE (-)601-0546 Modification - Nose Landing Gear (NLG) and Main Landing Gear (MLG) System - NLG and MLG Component Serialization

26-Sep-2006Mos

10,897.5Hrs

5,558Ldg

32 A/FComplied With

Nextdue Share EarliestDUE:1. RE -Modification - Nose Landing Gear (NLG) and Main Landing Gear...601-0546 Part AA/F32

Nextdue Share EarliestDUE:1. RE -Modification - Nose Landing Gear (NLG) and Main Landing Gear...601-0546 Part BA/F32

RecommendedRE (-)601-0546 Part A Modification - Nose Landing Gear (NLG) and Main Landing Gear (MLG) System - NLG and Left MLG Component Serialization

Mos

Hrs

Ldg

32 A/FEff: 31-May-2002

RecommendedRE (-)601-0546 Part B Modification - Nose Landing Gear (NLG) and Main Landing Gear (MLG) System - NLG and Right MLG Component Serialization

Mos

Hrs

Ldg

32 A/FEff: 31-May-2002

RecommendedRE (-)601-0546 Rev 1 Modification - Nose Landing Gear (NLG) and Main Landing Gear (MLG) System - NLG and MLG Component Serialization

Mos

Hrs

Ldg

32 A/F

Nextdue Share EarliestDUE:1. RE -Modification - Nose Landing Gear (NLG) and Main Landing Gear...601-0546 Rev 1 Part AA/F32

Nextdue Share EarliestDUE:1. RE -Modification - Nose Landing Gear (NLG) and Main Landing Gear...601-0546 Rev 1 Part BA/F32


Generated: 6-Apr-2016 1:16 PM150/429







RecommendedRE (-)601-0546 Rev 1 Part A Modification - Nose Landing Gear (NLG) and Main Landing Gear (MLG) System - NLG and Left MLG Component Serialization

Mos

Hrs

Ldg

32 A/FEff: 15-Dec-2003

RecommendedRE (-)601-0546 Rev 1 Part B Modification - Nose Landing Gear (NLG) and Main Landing Gear (MLG) System - NLG and Right MLG Component Serialization

Mos

Hrs

Ldg

32 A/FEff: 15-Dec-2003

RecommendedRE (-)601-0546 Rev 2 Modification - Nose Landing Gear (NLG) and Main Landing Gear (MLG) System - NLG and MLG Component Serialization

Mos

Hrs

Ldg

32 A/F

Nextdue Share EarliestDUE:1. RE -Modification - Nose Landing Gear (NLG) and Main Landing Gear...601-0546 Rev 2 Part AA/F32

Nextdue Share EarliestDUE:1. RE -Modification - Nose Landing Gear (NLG) and Main Landing Gear...601-0546 Rev 2 Part BA/F32

RecommendedRE (-)601-0546 Rev 2 Part A Modification - Nose Landing Gear (NLG) and Main Landing Gear (MLG) System - NLG and Left MLG Component Serialization

Mos

Hrs

Ldg

32 A/FEff: 29-Oct-2007

RecommendedRE (-)601-0546 Rev 2 Part B Modification - Nose Landing Gear (NLG) and Main Landing Gear (MLG) System - NLG and Right MLG Component Serialization

Mos

Hrs

Ldg

32 A/FEff: 29-Oct-2007

RecommendedT (A/R)601-0546 Rev 3 Modification - Nose Landing Gear (NLG) and Main Landing Gear (MLG) System - NLG and MLG Component Serialization

Mos

Hrs

Ldg

32 A/FEff: 09-May-2011

Nextdue Share EarliestDUE:1. T A/R | 2. RE -Modification - Nose Landing Gear (NLG) and Main Landing Gear...601-0546 Rev 3 Part AA/F32

Nextdue Share EarliestDUE:1. T A/R | 2. RE -Modification - Nose Landing Gear (NLG) and Main Landing Gear...601-0546 Rev 3 Part BA/F32

RecommendedT (A/R)601-0546 Rev 3 Part A Modification - Nose Landing Gear (NLG) and Main Landing Gear (MLG) System - NLG and Left MLG Component Serialization

Mos

Hrs

Ldg

32 A/FEff: 09-May-2011

RecommendedT (A/R)601-0546 Rev 3 Part B Modification - Nose Landing Gear (NLG) and Main Landing Gear (MLG) System - NLG and Right MLG Component Serialization

Mos

Hrs

Ldg

32 A/FEff: 09-May-2011

RecommendedRE (-)601-0558 Special Check/Rework - Extension and Retraction - End Caps on Nose Landing Gear (NLG) Selector Valve and Nose Gear Door Selector Valve Could Have Been

Incorrectly Lockwired During Assembly

Mos

Hrs

Ldg

32 A/F


Generated: 6-Apr-2016 1:16 PM151/429







RecommendedRE (-)601-0558 Rev 1 Special Check/Rework - Extension and Retraction - End Caps on Nose Landing Gear (NLG) Selector Valve and Nose Gear Door Selector Valve Could Have Been


Mos

Hrs

Ldg

32 A/F



Mos

Hrs

Ldg

32 A/F



02-Dec-2009Mos

11,460.7Hrs

5,905Ldg


OptionalT (A/R)601-0569 Modification - Position and Warning - Installation and Rerouting of a New Nose Landing Gear Harness

Mos

Hrs

Ldg

32 A/FEff: 20-Feb-2006

OptionalRE (-)601-0598 Modification – Nose Landing Gear (NLG) – Towing Strap Placard Installation

Mos

Hrs

Ldg

32 A/F

OptionalT (A/R)601-0598 Rev 1 Modification – Nose Landing Gear (NLG) – Towing Strap Placard Installation

Mos

Hrs

Ldg

32 A/FEff: 14-Oct-2008

RecommendedT (A/R)601-0616 Modification – Nose Gear and Doors – Addition of Guides to Nose Landing Gear Unpaved/Gravel Runway Kit

Mos

Hrs

Ldg

32 A/FEff: 31-Oct-2011

OptionalT (A/R)601-0621 Modification – Main Brake System – Replacement of the Hydraulic System No. 2 Brake Accumulator

Mos

Hrs

Ldg

32 A/FEff: 14-May-2012

OptionalT (A/R)601-0622 Modification – Main Brake System – Replacement of the Hydraulic System No. 3 Brake Accumulator

Mos

Hrs

Ldg

32 A/FEff: 14-May-2012

OptionalT (A/R)601-0632 Modification – Brake Control Valve (BCV) – Incorporation of Optional BCV

Mos

Hrs

Ldg

32 A/FEff: 18-Mar-2014


Generated: 6-Apr-2016 1:16 PM152/429







MandatoryRE (-)81-13-51 Wheel Brake Assembly

20-Sep-1983Mos

0Hrs

0Ldg

32 A/FBY AIRCRAFT MODELEff: 07-Dec-1981 Not

Applicable

MandatoryRE (-)82-06-05 Main Landing Gear Release Control System

18-Sep-1985Mos

Hrs

Ldg


Applicable

MandatoryRE (-)82-09-51 R1 AFM, Supplement 2 Changes

18-Sep-1985Mos

Hrs

Ldg

32 A/FBY AIRCRAFT SERIAL NUMBEREff: 09-Sep-1982 Not

Applicable

AlertRE (-)A601-0072 Special Check/Adjustment - Main Landing Gear Harnesses - Location

Mos

Hrs

Ldg

32 A/FEff: 19-Jul-1984

AlertRE (-)A601-0115 Special Check/Modification - Main Landing Gear Harnesses - Routing

05-Sep-1985Mos

Hrs

Ldg


AlertRE (-)A601-0329 Special Check/Modification - Main Landing Gear Door - Hinge and Fasteners

Mos

Hrs

Ldg

32 A/F

AlertRE (-)A601-0329 Rev 1 Special Check/Modification - Main Landing Gear Door - Hinge and Fasteners

Mos

Hrs

Ldg

32 A/F

AlertRE (-)A601-0329 Rev 2 Special Check/Modification - Main Landing Gear Door - Hinge and Fasteners

17-May-2013Mos

11,788.8Hrs

6,143Ldg


CPCP ≈18-Sep-2016REC32-10-801 Main Landing Gear - CPCP Check

10-Feb-2016Mos

290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs

6,326Ldg

(PKG 300 Hour)

32 A/F

(SOURCE: TLMC 05-30-20) (NOTE: This task can be done in conjunction with the Scheduled Maintenance Instruction Task 32-10-00-210)

CPCP ≈18-Sep-2016REC32-20-801 Nose Landing Gear - CPCP Check

10-Feb-2016Mos

290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs

6,326Ldg

(PKG 300 Hour)

32 A/F

(SOURCE: TLMC 05-30-20) (NOTE: This task can be done in conjunction with the Scheduled Maintenance Instruction Task 32-20-00-205)

▼ 33 - LIGHTS

RE (O/C)Dimmer

20-Sep-1983Mos

0Hrs0

0Ldg0

Left33 A/FNew600-51519-1

UNKNOWN


Generated: 6-Apr-2016 1:16 PM153/429







RE (O/C)Dimmer

20-Sep-1983Mos

0Hrs0

0Ldg0


UNKNOWN

RE (O/C)Dimmer Control Assembly

20-Sep-1983Mos

0Hrs0

0Ldg0

Left33 A/FNew70-0180-3

UNKNOWN

RE (O/C)Dimmer Control Assembly

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Downwash Light Inverter

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Downwash Light Inverter

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Emergency Exit Light Battery Pack

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Emergency Exit Light Battery Pack

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Emergency Lighting Power Supplie

18-Dec-2014Mos

11,854.6Hrs

Ldg

Aft33 A/F60-1321-118594

Component Inspection SimpleDUE:1. RE 12 MosEmergency Lighting Inspect Power Supplies per Check section ...33-50-00-203A/F33

RE (O/C)Emergency Lighting Power Supplie

18-Dec-2014Mos

11,854.6Hrs

Ldg

Fwd33 A/F60-1321-122411

Component Inspection SimpleDUE:1. RE 12 MosEmergency Lighting Inspect Power Supplies per Check section ...33-50-00-203A/F33

RE (O/C)Fluorescent Light Inverter

20-Sep-1983Mos

0Hrs0

0Ldg0

Center33 A/FNew55-0521-4

UNKNOWN


Generated: 6-Apr-2016 1:16 PM154/429








20-Sep-1983Mos

0Hrs

0Ldg



20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Incandescent Dimmer

20-Sep-1983Mos

0Hrs0

0Ldg0

Center33 A/FNew2-459-06

UNKNOWN


20-Sep-1983Mos

0Hrs0

0Ldg0


UNKNOWN


11-Nov-2002Mos

7,968.7Hrs

3,821Ldg

Right33 A/F2-459-060697

RE (O/C)Overhead Power Supply Unit

20-Sep-1983Mos

0Hrs0

0Ldg0

33 A/FNew449-2

UNKNOWN

RE (O/C)Strobe Power Supply Unit

20-Sep-1983Mos

0Hrs0

0Ldg0


UNKNOWN

RE (O/C)Strobe Power Supply Unit

20-Sep-1983Mos

0Hrs0

0Ldg0


UNKNOWN

RE (O/C)Tail Anti-Collision/Pos Light Assembly

20-Sep-1983Mos

0Hrs0

0Ldg0

33 A/FNew30-1192-7

UNKNOWN

RE (O/C)Tail Strobe Power Supply Unit

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Upper Strobe Light

20-Sep-1983Mos

0Hrs

0Ldg



Generated: 6-Apr-2016 1:16 PM155/429







RE (O/C)Upper Tail Nav Light Assembly

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Wing Anti-Collision Light Assembly

20-Sep-1983Mos

0Hrs0

0Ldg0


UNKNOWN

RE (O/C)Wing Anti-Collision Light Assembly

31-Dec-2002Mos

9,155.9Hrs

4,544Ldg

Right33 A/F30-1467-19967

≈29-Feb-2016RE33-40-00-201 Exterior Lighting Visual and Operational Test

05-Apr-2013Mos

26.3 Hrs12,067.530011,767.5Hrs

Ldg

33 A/F

MRB ≈18-Sep-2016RE33-50-00-202 Emergency Lighting Visual Check- Operational Test

10-Feb-2016Mos

290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs

6,326Ldg

(PKG 300 Hour)

33 A/F


MRBRE33-50-00-203 Emergency Lighting Inspect Power Supplies per Check section and carry out Capacity Check per Repair section of CMM/PSP 608/608A33-50-42, or install new Power

Supplies

6.6 Months (+31

Days)(21-Oct-2016)-/+11221-Oct-2015Mos

Hrs

Ldg

Aft

(PKG 12 Month)

33 A/F

60-1321-118594


MRBRE33-50-00-203 Emergency Lighting Inspect Power Supplies per Check section and carry out Capacity Check per Repair section of CMM/PSP 608/608A33-50-42, or install new Power

Supplies

6.6 Months (+31

Days)(21-Oct-2016)-/+11221-Oct-2015Mos

Hrs

Ldg

Fwd

(PKG 12 Month)

33 A/F

60-1321-122411


RecommendedRE (-)601-0067 Modification - Emergency Light Drains - Introduction

Mos

Hrs

Ldg

33 A/F

RecommendedRE (-)601-0067 Rev 1 Modification - Emergency Light Drains - Introduction

26-Jan-1987Mos

1,267Hrs

470Ldg


RecommendedRE (-)601-0070 Modification - External Emergency Light Wiring - Protection

26-Jan-1987Mos

1,267Hrs

470Ldg



Generated: 6-Apr-2016 1:16 PM156/429







OptionalRE (-)601-0137 Modification - Rear Navigation Light - Shock Mount Addition

23-Feb-1990Mos

2,687Hrs

1,034Ldg


OptionalT (A/R)601-0193 Modification - Center Pedestal - Third Light Dimmer

Mos

Hrs

Ldg

33 A/FEff: 15-Jun-1989

RecommendedRE (-)601-0227 Modification - Recognition/Taxi and Landing Lights - Wiring

23-Mar-1992Mos

3,584Hrs

1,446Ldg


OptionalT (A/R)601-0294 Modification - Integral Lighting - Lamp Dimmer Power Supply Circuit Breaker and Wiring Replacement

Mos

Hrs

Ldg

33 A/FEff: 05-Jan-1990

OptionalT (A/R)601-0490 Modification - Power Supplies for AC Incandescent Lamp Dimmers - Separation of AC and DC Ground Connections

Mos

Hrs

Ldg

33 A/FEff: 31-Mar-1998

RecommendedRE (-)601-0527 Modification - Navigation Lights - Change of Circuit Breaker Rating From 3 AMPS to 2 AMPS

08-Feb-2000Mos

6,204.1Hrs

3,181Ldg


OptionalT (A/R)601-0594 Modification – Navigation Lights – Introduction of Wing Tip Halogen Navigation Lights to Improve Reliability

Mos

Hrs

Ldg

33 A/FEff: 31-Mar-2008

IsModSumT (A/R)IS600-33-0001 REV A Kit - Introduction, Rear Navigation Light Spiral Cord / Boot (Service Loop)

Mos

Hrs

Ldg

33 A/F

▼ 34 - NAVIGATION

RE (O/C)ADF Antenna

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)ADF Control

11-Jan-2003Mos

9,193.3Hrs

4,567Ldg

No.134 A/FG7026-0576

RE (O/C)ADF Receiver

20-Sep-1983Mos

0Hrs0

0Ldg0

No.134 A/FNew622-2362-001

UNKNOWN


Generated: 6-Apr-2016 1:16 PM157/429







RE (O/C)ADF Receiver

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Air Data Computer

20-Sep-1983Mos

0Hrs0

0Ldg0

Left34 A/FNew7000700-637

01109199

Component Inspection SimpleDUE: 30-Jan-20171. RE 24 MosFunctional Test of the Air Data Computer34-13-00-101*A/F34

Component Inspection SimpleDUE: 30-Jan-20171. RE 24 MosAir Data Computer tests and inspections per FAR 91.411 Appen...FAR 91.411A/F34

RE (O/C)Air Data Computer

20-Sep-1983Mos

0Hrs0

0Ldg0


86091747

Component Inspection SimpleDUE: 30-Jan-20171. RE 24 MosFunctional Test of the Air Data Computer34-13-00-101*A/F34

Component Inspection SimpleDUE: 30-Jan-20171. RE 24 MosAir Data Computer tests and inspections per FAR 91.411 Appen...FAR 91.411A/F34

RE (O/C)Altimeter

20-Sep-1983Mos

0Hrs

0Ldg


Component Inspection SimpleDUE: 30-Jan-20171. RE 24 MosAltimeter test and inspect per FAR 91.411 Appendix E part 43FAR 91.411A/F34

RE (O/C)Altimeter

20-Sep-1983Mos

0Hrs

0Ldg


Component Inspection SimpleDUE: 30-Jan-20171. RE 24 MosAltimeter test and inspect per FAR 91.411 Appendix E part 43FAR 91.411A/F34

RE (O/C)Altimeter

20-Sep-1983Mos

0Hrs0

0Ldg0

StandBy34 A/FNew8047-10

7536B

Component Inspection SimpleDUE: 30-Jan-20171. RE 24 MosAltimeter Standby Indicator tests and inspections per FAR 91...FAR 91.411A/F34

RE (O/C)Antenna

20-Sep-1983Mos

0Hrs0

0Ldg0

No.134 A/FNewS65-5366-7L

UNKNOWN

RE (O/C)Antenna

20-Sep-1983Mos

0Hrs0

0Ldg0

No.234 A/FNewS65-5366-7L

UNKNOWN

RE (O/C)Antenna

20-Sep-1983Mos

0Hrs

0Ldg



Generated: 6-Apr-2016 1:16 PM158/429







RE (O/C)Antenna

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)ATC Control

23-Feb-2002Mos

8,131.2Hrs

3,914Ldg

34 A/F622-6523-20510222

RE (O/C)ATC Transponder System

24-Apr-2003Mos

9,417.5Hrs

4,702Ldg

No.134 A/F622-9210-0033731

Component Inspection SimpleDUE:1. RE 24 MosATC Transponder System - Functional Test34-54-00-207A/F34

Component Inspection SimpleDUE: 30-Jan-20171. RE 24 MosATC Transponder test and inspections per FAR 91.413 Appendix...FAR 91.413A/F34

RE (O/C)ATC Transponder System

20-Sep-1983Mos

0Hrs0

0Ldg0

No.234 A/FNew622-6210-003

3707

Component Inspection SimpleDUE:1. RE 24 MosATC Transponder System - Functional Test34-54-00-207A/F34

Component Inspection SimpleDUE: 30-Jan-20171. RE 24 MosATC Transponder test and inspections per FAR 91.413 Appendix...FAR 91.413A/F34

RE (O/C)Attitude Direction Indicator

08-Mar-2005Mos

0Hrs0

0Ldg0

No.134 A/FNew7000466-905

82031445

RE (O/C)Attitude Direction Indicator

26-Sep-2006Mos

10,897.5Hrs

5,558Ldg

No.234 A/F7000466-90580080258

RE (O/C)Battery, INS

21-Oct-2015Mos

12,001.1Hrs

Ldg

No.134 A/F27826-0028902788

Component Inspection SimpleDUE: 21-Apr-20161. RE 6 MosCapacity Check of INS Battery34-CUS-010A/F34

RE (O/C)Battery, INS

21-Oct-2015Mos

12,001.1Hrs

Ldg

No.234 A/F27826-0029805842

Component Inspection SimpleDUE: 21-Apr-20161. RE 6 MosCapacity Check of INS Battery.34-CUS-010A/F34

RE (O/C)Comparator Monitor Indicator

20-Sep-1983Mos

0Hrs0

0Ldg0

34 A/FNew2594732-601

UNKNOWN


Generated: 6-Apr-2016 1:16 PM159/429







RE (O/C)Course Deviation Indicator

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Data Management, AFIS Unit

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Digital Clock

26-Nov-2001Mos

7,890Hrs

3,779Ldg

Left34 A/F811B24652

Component Inspection SimpleDUE: 30-Jan-20171. RE 24 MosDigital Clocks - Remove and install new batteries34-62-00-303A/F34

RE (O/C)Digital Clock

30-Jan-2015Mos

11,862.7Hrs

6,194Ldg

Right34 A/F811BUNKNOWN

Component Inspection SimpleDUE: 30-Jan-20171. RE 24 MosDigital Clocks - Remove and install new batteries34-62-00-303A/F34

RE (O/C)Directional Gyro

18-Mar-2003Mos

9,319.8Hrs

4,641Ldg

No.134 A/F2587193-435055183

RE (O/C)Directional Gyro

20-Sep-1983Mos

0Hrs0

0Ldg0

No.234 A/FNew2587193-43

UNKNOWN

RE (O/C)DME Transceiver

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)DME Transceiver

14-Oct-2003Mos

9,787.8Hrs

4,918Ldg

Right34 A/F622-1233-0017699

RE (O/C)EFIS Display

20-Sep-1983Mos

0Hrs

0Ldg



18-Dec-2014Mos

11,854.6Hrs

Ldg

No.234 A/FCG1121AB03050


Generated: 6-Apr-2016 1:16 PM160/429








20-Sep-1983Mos

0Hrs

0Ldg



20-Sep-1983Mos

0Hrs

0Ldg



20-Sep-1983Mos

0Hrs

0Ldg



20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)EFIS Symbol Generator

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)EFIS Symbol Generator

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Flight Director Computer

05-May-2002Mos

8,407.3Hrs

4,077Ldg

No.134 A/F4018369-90785014708

RE (O/C)Flight Director Computer

20-Sep-1983Mos

0Hrs0

0Ldg0

No.234 A/FNew4018369-905

UNKNOWN

RE (O/C)Flux Valve

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Flux Valve

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)FMS CDI Unit

20-Sep-1983Mos

0Hrs

0Ldg



Generated: 6-Apr-2016 1:16 PM161/429







RE (O/C)Glideslope Antenna

20-Sep-1983Mos

0Hrs0

0Ldg0

34 A/FNewS41422-2

UNKNOWN

RE (O/C)GPWS Computer

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Gyro Compass Dual Remote Compensator

20-Sep-1983Mos

0Hrs0

0Ldg0

34 A/FNew2593379-1

UNKNOWN

RE (O/C)Horizon Situation Indicator

07-Mar-2002Mos

8,174.5Hrs

3,939Ldg

No.134 A/F7000469-90381020563

RE (O/C)Horizon Situation Indicator

20-Sep-1983Mos

0Hrs0

0Ldg0

No.234 A/FNew7000469-903

81040711

RE (O/C)Inertial Reference Unit (IRU)

20-Sep-1983Mos

0Hrs

0Ldg



18-Dec-2014Mos

11,854.6Hrs

Ldg

No.234 A/FHG1066AD03099 REPAIR


20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Mach Airspeed Indicator

26-Sep-2006Mos

10,897.5Hrs

5,558Ldg

No.134 A/F35405-013123

RE (O/C)Mach Airspeed Indicator

26-Sep-2006Mos

10,897.5Hrs

5,558Ldg

No.234 A/F35405-013122

RE (O/C)Marker Beacon Antenna

20-Sep-1983Mos

0Hrs0

0Ldg0

34 A/FNewS35-1000-2

UNKNOWN


Generated: 6-Apr-2016 1:16 PM162/429







RE (O/C)MFD Symbol Generator

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Nav Controller

11-Nov-2004Mos

10,470.9Hrs

5,316Ldg

No.134 A/FG7024-07110

RE (O/C)Navigation Receiver

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Navigation Receiver

20-Sep-1983Mos

0Hrs

0Ldg


AWL - RVSM, Life Limit ≈04-Nov-2018REPitot-Static Head

09-Oct-1992Mos

1,312.8 Hrs13,3549,6003,754Hrs0

1,519Ldg0

Left34 A/FNew856KV10

UNKNOWN

TLMC:34-11-11-101* (SOURCE: TLMC 05-10-13)

AWL - RVSM, Life Limit ≈04-Nov-2018REPitot-Static Head

09-Oct-1992Mos

1,312.8 Hrs13,3549,6003,754Hrs0

1,519Ldg0

Right34 A/FNew856KV10

UNKNOWN

TLMC:34-11-11-101* (SOURCE: TLMC 05-10-13)

RE (O/C)Radar Controller

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Radar Indicator

26-Sep-2006Mos

10,897.5Hrs

5,558Ldg

34 A/FMI-5853431258

RE (O/C)Radar Pedestal Antenna

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Radar Waveguide Assy

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Radio Altimeter

06-Apr-2005Mos

10,718Hrs

5,449Ldg

No.134 A/F622-2855-0022663


Generated: 6-Apr-2016 1:16 PM163/429







RE (O/C)Radio Altimeter

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Radio Altimeter Antenna

20-Sep-1983Mos

0Hrs0

0Ldg0

No.134 A/FNewS67-2002

UNKNOWN

RE (O/C)Radio Altimeter Antenna

20-Sep-1983Mos

0Hrs0

0Ldg0

No.234 A/FNewS67-2002

UNKNOWN

RE (O/C)Radio Magnetic Indicator

20-Aug-2003Mos

9,608.2Hrs

4,812Ldg

Left34 A/F3117LB2-1A3773

RE (O/C)Radio Magnetic Indicator

14-Oct-2003Mos

9,787.8Hrs

4,918Ldg

Right34 A/F3117LB2-1A2949

RE (O/C)Rate Gyro

06-Feb-2005Mos

10,582.5Hrs

5,379Ldg

No.134 A/F7007453-90302065494

RE (O/C)Rate Gyro

06-Feb-2005Mos

10,582.5Hrs

5,379Ldg

No.234 A/F7007453-90390112657

RE (O/C)Remote Controller

20-Sep-1983Mos

0Hrs0

0Ldg0

34 A/FNew4026206-904

UNKNOWN

RE (O/C)RMI Adapter

28-Jul-2004Mos

10,458.3Hrs

5,308Ldg

Left34 A/F622-1032-0014574

RE (O/C)RMI Adapter

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Standby Airspeed Indicator

20-Sep-1983Mos

0Hrs

0Ldg



Generated: 6-Apr-2016 1:16 PM164/429







RE (O/C)Standby Horizon Indicator

14-Dec-2003Mos

9,966.7Hrs

5,011Ldg

34 A/F501-1197-053501

RE (O/C)Standby Magnetic Compass

26-Sep-2006Mos

10,897.5Hrs

5,558Ldg

34 A/FPA170060345

Component Inspection SimpleDUE:1. RE 12 MosStandby Magnetic Compass - Compass Swing34-27-00-206A/F34

RE (O/C)Static Pressure Port

20-Sep-1983Mos

0Hrs0

0Ldg0

Left34 A/FNewST300-3HA

UNKNOWN

RE (O/C)Static Pressure Port

20-Sep-1983Mos

0Hrs0

0Ldg0

Right34 A/FNewST300-3HA

UNKNOWN

RE (O/C)TAS/TAT Indicator

21-Apr-2005Mos

10,740.1Hrs

5,462Ldg

34 A/F4031609-90483050462

RE (O/C)TCAS Antenna

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)TCAS Computer

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Total Temperature Sensor

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Vertical Gyro

08-Jul-2004Mos

10,455Hrs

5,305Ldg

No.134 A/F7000622-90280041424

RE (O/C)Vertical Gyro

20-Sep-1983Mos

0Hrs0

0Ldg0

No.234 A/FNew7000622-901

UNKNOWN

RE (O/C)Vertical Navigation Computer

03-Aug-2004Mos

10,458.3Hrs

5,306Ldg

34 A/F7004577-90285080284


Generated: 6-Apr-2016 1:16 PM165/429







RE (O/C)VOR Receiver

27-Jun-2004Mos

10,421.6Hrs

5,281Ldg

Left34 A/F622-0876-20115207

RE (O/C)VOR Receiver

23-Nov-2004Mos

10,487.6Hrs83.4

5,325Ldg60

Right34 A/F622-0876-2018969

RE (O/C)VOR/ILS Antenna

20-Sep-1983Mos

0Hrs0

0Ldg0

Left34 A/FNewDMN4-17-1A

UNKNOWN

RE (O/C)VOR/ILS Antenna

20-Sep-1983Mos

0Hrs0

0Ldg0

Right34 A/FNewDMN4-17-1A

UNKNOWN

RE (O/C)VSI/TRA Indicator

09-Jul-2002Mos

8,603.4Hrs

4,190Ldg

Left34 A/F922-9728-3221444

RE (O/C)VSI/TRA Indicator

10-Nov-2003Mos

9,873.2Hrs

4,964Ldg

Right34 A/F922-9728-3221493

RE (O/C)Weather Radar Transceiver

05-Jun-2015Mos

11,940.5Hrs

6,249Ldg

34 A/FMI5582002695

Mandatory (Appliance AD)RE (-)2001-15-17 Rockwell Collins. CTL-92 - Transponder Control Panels

05-Sep-2001Mos

Hrs

Ldg

34 A/FBY PART S/N INSTALLEDEff: 20-Aug-2001 Not

Applicable

Mandatory (Appliance AD)RE (-)2002-13-07 Honeywell - Inertial Reference Units (IRU)

19-Jul-2002Mos

8,644.4Hrs

4,214Ldg

34 A/FBY IRU'S PART NUMBER INSTALLEDEff: 09-Aug-2002 Not

Applicable

Mandatory (Appliance AD)T2014-18-01 Rockwell Collins, Inc. - Navigation - inspect the airplane type code category strapping setting for a value of zero (0) or one (1) following Rockwell Collins, Inc. Service

Information Letter 07-2, 523-0810069-101000, TDR-94() SIL 07-02.

6.4 Months14-Oct-201624Mos

Hrs

Ldg

34 A/FEff: 14-Oct-2014

(AVG MAN HRS: 1) (APX COST [USD]: 85)

Mandatory (Appliance AD)T2015-0093 Paragraph (2) NORTHROP GRUMMAN LITEF GmbH - Navigation – Attitude Heading Reference System – Modification / Replacement

1.2 Years10-Jun-201724Mos

Hrs

Ldg

34 A/FEff: 10-Jun-2015


Generated: 6-Apr-2016 1:16 PM166/429







Mandatory (Appliance AD)RE (-)2015-10-51-E EMERGENCY AD - Avidyne Integrated Flight Display (IFD) - Navigation - Incorporate Operational Limitations into Airplane Flight Manual (AFM) or Airplane Flight

Manual Supplement (AFMS) Limitation

11-Nov-2015Mos

12,012.8Hrs

6,303Ldg

34 A/FEQUIPMENT NOT INSTALLEDEff: 18-May-2015 Not

Applicable

MRB ≈18-Sep-2016RE34-11-00-201 Pitot Static System and Temperature Sensing System Visual Check

10-Feb-2016Mos

290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs

6,326Ldg

(PKG 300 Hour)

34 A/F


MRBRE34-11-00-202 Pitot Static System and Temperature Sensing System Pitot static system moisture and contamination check

6.6 Months (+31

Days)(21-Oct-2016)-/+11221-Oct-2015Mos

Hrs

Ldg

(PKG 12 Month)

34 A/F


MRBRE34-11-00-203 Pitot Static System and Temperature Sensing System Pressure leak tests

10 Months (+29

Days)(30-Jan-2017)-/+12430-Jan-2015Mos

Hrs

Ldg

(PKG 24 Month)

34 A/F


MRBRE34-11-00-205 Pitot Static System and Temperature Sensing System Altimeter calibration check

10 Months (+29

Days)(30-Jan-2017)-/+12430-Jan-2015Mos

Hrs

Ldg

(PKG 24 Month)

34 A/F

Ref.:Section 5-20-05 Paragraph 10 Program Note G (SOURCE: TLMC 05-20-15)


10 Months (+29

Days)(30-Jan-2017)-/+12430-Jan-2015Mos

Hrs

Ldg

(PKG 24 Month)

34 A/F



10 Months (+29

Days)(30-Jan-2017)-/+12430-Jan-2015Mos

Hrs

Ldg

(PKG 24 Month)

34 A/F


MRB ≈18-Sep-2016RE34-11-11-208 Pitot Static Heads Clean pitot drain holes

10-Feb-2016Mos

290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs

6,326Ldg

(PKG 300 Hour)

34 A/F


AWL - RVSMRE34-13-00-101* Functional Test of the Air Data Computer

10 Months (+29

Days)30-Jan-2017-/+12430-Jan-2015Mos

Hrs

Ldg

Left34 A/F7000700-63701109199



Generated: 6-Apr-2016 1:16 PM167/429







AWL - RVSMRE34-13-00-101* Functional Test of the Air Data Computer

10 Months (+29

Days)30-Jan-2017-/+12430-Jan-2015Mos

Hrs

Ldg

Right34 A/F7000700-63786091747


MRBRE34-27-00-206 Standby Magnetic Compass - Compass Swing

6.6 Months (+31

Days)(21-Oct-2016)-/+11221-Oct-2015Mos

Hrs

Ldg

(PKG 12 Month)

34 A/F

PA170060345


Servicing - RecommendedRE (N/A)34-41-00-302 Weather Radar System (Aircraft 3050 and Subs and Post SB 601-0111) - Pressure line desiccator

11-Nov-2015Mos

Hrs

Ldg

34 A/F


MRBRE34-54-00-207 ATC Transponder System - Functional Test

10 Months (+29

Days)(30-Jan-2017)-/+12430-Jan-2015Mos

Hrs

Ldg

No.1

(PKG 24 Month)

34 A/F

622-9210-0033731


MRBRE34-54-00-207 ATC Transponder System - Functional Test

10 Months (+29

Days)(30-Jan-2017)-/+12430-Jan-2015Mos

Hrs

Ldg

No.2

(PKG 24 Month)

34 A/F

622-6210-0033707


Servicing - RecommendedRE34-62-00-303 Digital Clocks - Remove and install new batteries

10 Months (+29

Days)30-Jan-2017-/+12430-Jan-2015Mos

11,862.7Hrs

6,194Ldg

Left

(PKG 24 Month)

34 A/F

811B24652


Servicing - RecommendedRE34-62-00-303 Digital Clocks - Remove and install new batteries

10 Months (+29

Days)30-Jan-2017-/+12430-Jan-2015Mos

Hrs

Ldg

Right

(PKG 24 Month)

34 A/F

811BUNKNOWN


Custom TaskRE34-CUS-005 24 Month RVSM Inspection Requirements

10 Months30-Jan-20172430-Jan-2015Mos

Hrs

Ldg

34 A/F

(NOTE: KSR Report R02-529 Page 1.2)

RE34-CUS-010 Capacity Check of INS Battery

15 Days21-Apr-2016621-Oct-2015Mos

12,001.1Hrs

Ldg

No.134 A/F27826-0028902788


Generated: 6-Apr-2016 1:16 PM168/429







RE34-CUS-010 Capacity Check of INS Battery.

15 Days21-Apr-2016621-Oct-2015Mos

12,001.1Hrs

Ldg

No.234 A/F27826-0029805842

OptionalRE (-)601-0053 Modification - Flight Director System - Localizer Mode

26-Jan-1987Mos

1,267Hrs

470Ldg

34 A/FComplied With

OptionalT (A/R)601-0053 Rev 1 Modification - Flight Director System - Localizer Mode

Mos

Hrs

Ldg

34 A/FEff: 29-May-1984

OptionalRE (-)601-0111 Modification - Pressurization - Waveguide Desiccator Addition

Mos

Hrs

Ldg

34 A/F

OptionalRE (-)601-0111 Rev 1 Modification - Pressurization - Waveguide Desiccator Addition

20-Jan-1987Mos

Hrs

Ldg


OptionalRE (-)601-0118 Modification - Reduced Bank Angle Limit - Introduction

Mos

Hrs

Ldg

34 A/F

OptionalT (A/R)601-0118 Rev 1 Modification - Reduced Bank Angle Limit - Introduction

Mos

Hrs

Ldg

34 A/FEff: 17-Sep-1986

OptionalT (A/R)601-0128 Modification - Attitude Director Indicator - Radio Altimeter Display Range

Mos

Hrs

Ldg

34 A/FEff: 27-Sep-1985

OptionalT (A/R)601-0129 Modification - DME/Flight Director - Interface

Mos

Hrs

Ldg

34 A/FEff: 26-Sep-1985

RecommendedRE (-)601-0150 Special Check/Modification - Pitot Static System - Line Clearance

19-Jan-1987Mos

1,267Hrs

480Ldg


OptionalRE (-)601-0182 Modification - Tacan System - Placard

Mos

Hrs

Ldg

34 A/FEff: 07-Apr-1986


Generated: 6-Apr-2016 1:16 PM169/429







RecommendedRE (-)601-0226 Modification - Mach/Airspeed Indicator and Air Data Computer - VMO Warning

Mos

Hrs

Ldg

34 A/F

RecommendedRE (-)601-0226 Rev 1 Modification - Mach/Airspeed Indicator and Air Data Computer - VMO Warning

28-Oct-1988Mos

Hrs

Ldg


RecommendedRE (-)601-0246 Modification - Symbol Generators - Speed Trend Vector Display

Mos

Hrs

Ldg

34 A/F

OptionalT (A/R)601-0273 Modification - Attitude and Direction Systems - Radio Magnetic and Horizontal Situation Indicators

Mos

Hrs

Ldg

34 A/FEff: 07-Dec-1988

RecommendedRE (-)601-0275 Modification - Electronic Flight Instrument System - Unit Replacement and Wiring Rework

Mos

Hrs

Ldg

34 A/F

RecommendedRE (-)601-0284 Modification - Waveguide Desiccator - Hardware Change

23-Mar-1992Mos

3,584Hrs

1,446Ldg


RecommendedRE (-)601-0334 Modification - Pitot Static Lines - Improved Drainage

Mos

Hrs

Ldg

34 A/F

RecommendedRE (-)601-0334 Rev 1 Modification - Pitot Static Lines - Improved Drainage

23-Mar-1992Mos

3,584Hrs

1,446Ldg


RecommendedRE (-)601-0377 Modification - Pitot-Static System - Introduction of Pitot-Static Head with Heated Base

Mos

Hrs

Ldg

34 A/F

RecommendedRE (-)601-0377 Rev 1 Modification - Pitot-Static System - Introduction of Pitot-Static Head with Heated Base

09-Oct-1992Mos

3,754Hrs

1,519Ldg


RecommendedRE (-)601-0393 Pitot-Static Drain Line - Addition of Clamps and Clamping Plate

Mos

Hrs

Ldg

34 A/F


Generated: 6-Apr-2016 1:16 PM170/429







OptionalRE (-)601-0484 Reduced Vertical Separation Minimum (RVSM) to 1000 FT. Aircraft Qualification Requirements

14-Nov-1997Mos

5,395Hrs

2,274Ldg

34 A/FComplied With

OptionalRE (-)601-0484 Rev 1 Reduced Vertical Separation Minimum (RVSM) to 1000 FT. Aircraft Qualification Requirements

Mos

Hrs

Ldg

34 A/F

OptionalT (A/R)601-0484 Rev 2 Reduced Vertical Separation Minimum (RVSM) to 1000 FT. Aircraft Qualification Requirements

Mos

Hrs

Ldg

34 A/FEff: 30-Apr-2001

OptionalRE (-)601-0595 Modification – Standby Altitude Indicator (SAI) – Introduction of New AD20 Standby Altimeter

Mos

Hrs

Ldg

34 A/F

RecommendedRE (-)601-0617 Modification – Pitot-Static and Temperature Sensing System – Replacement of Pitot-Static Visual Drain Bottles to Larger Capacity Bottles

Mos

Hrs

Ldg

34 A/F

RecommendedRE (-)601-0617 Rev 1 Modification – Pitot-Static and Temperature Sensing System – Replacement of Pitot-Static Visual Drain Bottles to Larger Capacity Bottles

Mos

Hrs

Ldg

34 A/F

RecommendedRE (-)601-0617 Rev 2 Modification – Pitot-Static and Temperature Sensing System – Replacement of Pitot-Static Visual Drain Bottles to Larger Capacity Bottles

Mos

Hrs

Ldg

34 A/F

MandatoryT (A/R)91-10-01 Traffic Alert and Collision Avoidance Systems

Mos

Hrs

Ldg

34 A/FEff: 10-Mar-1992

FAR91RE (-)FAR 91.171 VOR - Test and Inspection per FAR 91.171

Mos

Hrs

Ldg

34 A/F

FAR91, FAR 91REFAR 91.411 Air Data Computer tests and inspections per FAR 91.411 Appendix E of Part 43


Hrs

Ldg

Left34 A/F

Inspected Date 30-Jan-2015

7000700-63701109199

FAR91, FAR 91REFAR 91.411 Air Data Computer tests and inspections per FAR 91.411 Appendix E of Part 43


Hrs

Ldg

Right34 A/F


7000700-63786091747


Generated: 6-Apr-2016 1:16 PM171/429







FAR91, FAR 91REFAR 91.411 Altimeter Standby Indicator tests and inspections per FAR 91.411


Hrs

Ldg

StandBy34 A/F8047-107536B

FAR91, FAR 91REFAR 91.411 Altimeter test and inspect per FAR 91.411 Appendix E part 43


Hrs

Ldg

Left34 A/F


UnknownUnknown

FAR91, FAR 91REFAR 91.411 Altimeter test and inspect per FAR 91.411 Appendix E part 43


Hrs

Ldg

Right34 A/F


UnknownUnknown

FAR91, FAR 91REFAR 91.413 ATC Transponder test and inspections per FAR 91.413 Appendix F of Part 43


Hrs

Ldg

No.134 A/F


622-9210-0033731

FAR91, FAR 91REFAR 91.413 ATC Transponder test and inspections per FAR 91.413 Appendix F of Part 43


Hrs

Ldg

No.234 A/F


622-6210-0033707

IsModSumT (A/R)IS600-34-0001 REV A Kit – Introduction of Alternate Antenna Installations with Conductive Gaskets

Mos

Hrs

Ldg

34 A/F

▼ 35 - OXYGEN

MRB, Life LimitRECrew Oxygen System , Cylinder

6.6 Years (+30 Days)05-Nov-2022-/+1m2405-Nov-1998Yrs

0Hrs0

0Ldg0

No.135 A/F

Manufactured Date 05-Nov-1998

New895-01077281-7086

TLMC:35-10-00-204, Ref:05-10-20 (SOURCE: TLMC 05-20-15, TLMC 05-10-20) (NOTE: Note: (As per CFR title 49, chapter 180.205 or in

accordance with the operator’s national requirements)


TsiDUE: 20-Jan-20191. RE 60 MosOxygen Cylinder Assembly - Hydrostatic Test and Functional T...35-10-11-203A/F35

RE (O/C)Crew Oxygen System, Mask Assy

18-Dec-2014Mos

11,854.6Hrs

Ldg

No.135 A/FMC10-13-032252


TsiDUE: 18-Dec-20201. RE 72 MosCrew Oxygen System - Restoration of the Oxygen Regulator Mas...35-10-00-205A/F35


Generated: 6-Apr-2016 1:16 PM172/429








18-Dec-2014Mos

11,854.6Hrs

Ldg

No.235 A/FMC10-13-03110851




18-Dec-2014Mos

11,854.6Hrs

Ldg

Observer35 A/F174326-078UNKNOWN



Life LimitREOxygen Cylinder Assembly

12.8 Years20-Jan-202918020-Jan-2014Mos

11,824.5Hrs

Ldg

Aft35 A/F

Manufactured Date 20-Jan-2014

895-01077281-30300


TsiDUE: 20-Jan-20191. RE 60 MosOxygen Cylinder Assembly • Hydrostatic Test and Functional T...35-CUS-002A/F35

Life LimitREOxygen Cylinder Assembly

12.8 Years20-Jan-202918020-Jan-2014Mos

11,824.5Hrs

Ldg

Fwd35 A/F

Manufactured Date 20-Jan-2014

895-01015282-31610


TsiDUE: 20-Jan-20191. RE 60 MosOxygen Cylinder Assembly • Hydrostatic Test and Functional T...35-CUS-002A/F35

RE (O/C)Oxygen Fill Valve

20-Sep-1983Mos

0Hrs0

0Ldg0

35 A/FNew170080

UNKNOWN

RE (O/C)Oxygen Pressure Gauge

20-Sep-1983Mos

0Hrs0

0Ldg0

No.135 A/FNewG4225-001

UNKNOWN

RE (O/C)Oxygen Pressure Gauge

20-Sep-1983Mos

0Hrs0

0Ldg0

No.235 A/FNew171007

UNKNOWN

RE (O/C)Portable Oxygen Bottle

26-Jan-2011Mos

11,460.7Hrs

0Ldg

35 A/F5900-9CIA-YON937987

Assembly SubDUE:1. RE O/CPortable Oxygen Bottle - Regulator5900-9CIA-YON / 937987A/F35


TsiDUE: 10-Feb-20211. RE 60 MosPortable Oxygen Bottle - Hydrostatic Test35-CUS-003A/F35


Generated: 6-Apr-2016 1:16 PM173/429







RE (O/C)Portable Oxygen Bottle - Regulator

26-Jan-2011Mos

11,460.7Hrs

0Ldg

35 A/F5900-9CIA-YON937987


TsiDUE: 10-Feb-20211. RE 60 MosPortable Oxygen Bottle - Regulator - Functional Test35-CUS-004A/F35

RE (O/C)Regulator, Oxygen Cylinder Assembly

28-Mar-2014Mos

11,824.5Hrs

0Ldg

Aft35 A/F803213-01905

Component Inspection SimpleDUE: 28-Mar-20171. RE 36 MosCabin Oxygen Regulator Functional Check35-CUS-007A/F35

RE (O/C)Regulator, Oxygen Cylinder Assembly

28-Mar-2014Mos

11,824.5Hrs

0Ldg

Fwd35 A/F803213-011981

Component Inspection SimpleDUE: 28-Mar-20171. RE 36 MosCabin Oxygen Regulator Functional Check35-CUS-007A/F35

RE (O/C)Stowage - Oxygen Mask Box

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Stowage - Oxygen Mask Box

20-Sep-1983Mos

0Hrs

0Ldg


MandatoryT (A/R)174080-35-04 Oxygen - Passenger Oxygen System Mask In-Line Flow Indicator Replacement

Mos

Hrs

Ldg

35 A/FEff: 06-Sep-2010

(NOTE: This Service Bulletin applies to all aircraft that use passenger oxygen mask part numbers 174080-XX,174085-XX, 174095-XX, 174097-

XX, 174098-XX, and 174006-XX that were manufactured on or afterJanuary 1, 2002 and before March 1, 2006)

Mandatory (Appliance AD)RE (-)2011-01-09 B/E Aerospace - Oxygen - PBE units having PN 119003-11

08-Jul-2011Mos

11,523.8Hrs

5,970Ldg

35 A/FSB 119003-35-5Eff: 09-Feb-2011 Complied

With

(AVG MAN HRS: 1) (APX COST [USD]: 85) (NOTE: This AD applies to B/E Aerospace protective breathing equipment (PBE) units having part

number (P/N) 119003-11. Ref: BE SB 119003-35-5.)

Mandatory (Appliance AD)T2015-08-07 Paragraph (g) Zodiac Aerotechnics (formerly Intertechnique Aircraft Systems) - Oxygen - Flightcrew Oxygen Mask Regulators - Inspection


Hrs

Ldg

35 A/FEff: 16-Jun-2015

Mandatory (Appliance AD)T2015-08-07 Paragraph (h) Zodiac Aerotechnics (formerly Intertechnique Aircraft Systems) - Oxygen - Flightcrew Oxygen Mask Regulators - Replacement


Hrs

Ldg

35 A/FEff: 16-Jun-2015


Generated: 6-Apr-2016 1:16 PM174/429







Mandatory (Appliance AD)RE (-)2015-23-09 Oxygen - Zodiac Aerotechnics (Formerly Intertechnique Aircraft Systems) Flight Crew Oxygen Mask Regulators - Inspection / Replacement Of Oxygen Mask Regulators

Mos

Hrs

Ldg

35 A/FEff: 28-Dec-2015

Nextdue Share EarliestDUE:1. RE -Oxygen - Inspect Each Flightcrew Oxygen Mask Regulator To Id...2015-23-09 Para (g)A/F35

Nextdue Share EarliestDUE:1. RE -Oxygen - Action For Affected Regulators2015-23-09 Para (h)A/F35

Nextdue Share EarliestDUE: 28-Dec-20161. T 12 Mos | 2. RE -Oxygen - Regulator Replacement2015-23-09 Para (i)A/F35

Mandatory (Appliance AD)RE (-)2015-23-09 Para (g) Oxygen - Inspect Each Flightcrew Oxygen Mask Regulator To Identify The Part Number And Serial Number

Mos

Hrs

Ldg

35 A/FEff: 28-Dec-2015

Mandatory (Appliance AD)RE (-)2015-23-09 Para (h) Oxygen - Action For Affected Regulators

Mos

Hrs

Ldg

35 A/FEff: 28-Dec-2015

Mandatory (Appliance AD)T2015-23-09 Para (i) Oxygen - Regulator Replacement

8.9 Months28-Dec-201612Mos

Hrs

Ldg

35 A/FEff: 28-Dec-2015

MRB ≈03-May-2017RE35-10-00-201 Crew Oxygen System Functional Test

10-Feb-2016Mos

590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs

6,326Ldg

(PKG 600 Hour)

35 A/F


MRBRE35-10-00-205 Crew Oxygen System - Restoration of the Oxygen Regulator Mask Assembly

4.7 Years (+31 Days)18-Dec-2020-/+17218-Dec-2014Mos

Hrs

Ldg

No.135 A/F

Restored Date 18-Dec-2014

MC10-13-032252



4.7 Years (+31 Days)18-Dec-2020-/+17218-Dec-2014Mos

Hrs

Ldg

No.235 A/F


MC10-13-03110851



4.7 Years18-Dec-20207218-Dec-2014Mos

Hrs

Ldg

Observer35 A/F


174326-078UNKNOWN


MRBRE35-10-11-203 Oxygen Cylinder Assembly - Hydrostatic Test and Functional Test of Pressure Regulator

2.8 Years (+31 Days)20-Jan-2019-/+16020-Jan-2014Mos

11,824.5Hrs

Ldg

No.135 A/F895-01077281-7086

Ref.:Section 5-20-05 Para 10 Program Note F (SOURCE: TLMC 05-20-15)


Generated: 6-Apr-2016 1:16 PM175/429







VendorRE35-CUS-002 Oxygen Cylinder Assembly • Hydrostatic Test and Functional Test of pressure regulator

2.8 Years20-Jan-20196020-Jan-2014Mos

Hrs

Ldg

Aft35 A/F


895-01077281-30300

VendorRE35-CUS-002 Oxygen Cylinder Assembly • Hydrostatic Test and Functional Test of pressure regulator

2.8 Years20-Jan-20196020-Jan-2014Mos

Hrs

Ldg

Fwd35 A/F


895-01015282-31610

VendorRE35-CUS-003 Portable Oxygen Bottle - Hydrostatic Test

4.9 Years10-Feb-20216010-Feb-2016Mos

12,041.2Hrs

6,326Ldg

35 A/F

Hydrostatic Tested Date 10-Feb-2016

5900-9CIA-YON937987

VendorRE35-CUS-004 Portable Oxygen Bottle - Regulator - Functional Test

4.9 Years10-Feb-20216010-Feb-2016Mos

12,041.2Hrs

6,326Ldg

35 A/F5900-9CIA-YON937987

RE35-CUS-007 Cabin Oxygen Regulator Functional Check


11,824.5Hrs

Ldg

Aft35 A/F803213-01905

RE35-CUS-007 Cabin Oxygen Regulator Functional Check


11,824.5Hrs

Ldg

Fwd35 A/F803213-011981

RecommendedRE (-)601-0184 Modification - Oxygen Supply Line - Clearances

28-Mar-1989Mos

2,373Hrs

910Ldg


RecommendedT (A/R)601-0614 Special Check/Modification – Crew Oxygen System – Verification and Replacement of Crew Oxygen Mask Inflatable Harness

Mos

Hrs

Ldg

35 A/FEff: 15-Aug-2011

AlertRE (-)A601-0449 Special Check/Modification - Oxygen Cylinder and EROS Pressure Regulator Assembly - Possible Loss of Oxygen Cylinder Pressure

Mos

Hrs

Ldg

35 A/F

Nextdue Share EarliestDUE:1. RE -Special Check/Modification - Oxygen Cylinder and EROS Pressu...A601-0449 Part AA/F35

Nextdue Share EarliestDUE:1. RE -Special Check/Modification - Oxygen Cylinder and EROS Pressu...A601-0449 Part BA/F35

Nextdue Share EarliestDUE:1. T A/R | 2. RE -Special Check/Modification - Oxygen Cylinder and EROS Pressu...A601-0449 Rev 1 Part AA/F35

Nextdue Share EarliestDUE:1. T A/R | 2. RE -Special Check/Modification - Oxygen Cylinder and EROS Pressu...A601-0449 Rev 1 Part BA/F35


Generated: 6-Apr-2016 1:16 PM176/429







AlertRE (-)A601-0449 Part A Special Check/Modification - Oxygen Cylinder and EROS Pressure Regulator Assembly - Possible Loss of Oxygen Cylinder Pressure - Cylinder pressure adjustment

Mos

Hrs

Ldg

35 A/FEff: 14-Jul-1995

AlertRE (-)A601-0449 Part B Special Check/Modification - Oxygen Cylinder and EROS Pressure Regulator Assembly - Possible Loss of Oxygen Cylinder Pressure - frangible disc replacement

Mos

Hrs

Ldg

35 A/FEff: 14-Jul-1995

AlertRE (-)A601-0449 Rev 1 Special Check/Modification - Oxygen Cylinder and EROS Pressure Regulator Assembly - Possible Loss of Oxygen Cylinder Pressure

06-Oct-1995Mos

11,455.7Hrs

5,898Ldg


AlertT (A/R)A601-0449 Rev 1 Part A Special Check/Modification - Oxygen Cylinder and EROS Pressure Regulator Assembly - Possible Loss of Oxygen Cylinder Pressure - Cylinder pressure adjustment

Mos

Hrs

Ldg

35 A/FEff: 15-Aug-1995

AlertT (A/R)A601-0449 Rev 1 Part B Special Check/Modification - Oxygen Cylinder and EROS Pressure Regulator Assembly - Possible Loss of Oxygen Cylinder Pressure - frangible disc replacement

Mos

Hrs

Ldg

35 A/FEff: 15-Aug-1995

▼ 36 - PNEUMATIC

RE (O/C)10 Th Stage Bleed Air Isolation Valve

30-Jul-2002Mos

8,673.7Hrs

4,242Ldg

No.136 A/F979998-1P-185


20-Sep-1983Mos

0Hrs

0Ldg



20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Bleed Air Pressure Indicator

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Bleed Air Shutoff Valve

03-Dec-2015Mos

12,019Hrs

6,308Ldg

Left36 A/F3289590-33419

RE (O/C)Bleed Air Shutoff Valve

04-Aug-2002Mos

8,685.2Hrs

4,252Ldg

Right36 A/F3289590-2P-128


Generated: 6-Apr-2016 1:16 PM177/429







RE (O/C)Check Valve

20-Sep-1983Mos

0Hrs0

0Ldg0


UNKNOWN

RE (O/C)Check Valve

20-Sep-1983Mos

0Hrs0

0Ldg0


UNKNOWN

RE (O/C)Engine Bleed Air Check Valve

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Engine Bleed Air Check Valve

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Engine Bleed Air Controller

20-Sep-1983Mos

0Hrs0

0Ldg0


N/A

RE (O/C)Engine Bleed Air Controller

20-Sep-1983Mos

0Hrs0

0Ldg0


N/A


20-Sep-1983Mos

0Hrs0

0Ldg0


UNKNOWN


01-Apr-2004Mos

10,259.2Hrs

5,182Ldg

Right36 A/F898930-7-2811

RE (O/C)Pressure Transducer

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Pressure Transducer

20-Sep-1983Mos

0Hrs

0Ldg


MRB ≈03-May-2017RE36-10-00-201 Bleed Air Distribution Visual Check - Ducting

10-Feb-2016Mos

590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs

6,326Ldg

(PKG 600 Hour)

36 A/F



Generated: 6-Apr-2016 1:16 PM178/429







RecommendedRE (-)601-0152 Modification - APU Bleed Air Duct - Check Valve Relocation

Mos

Hrs

Ldg

36 A/F

RecommendedRE (-)601-0152 Rev 1 Modification - APU Bleed Air Duct - Check Valve Relocation

Mos

Hrs

Ldg

36 A/F

RecommendedRE (-)601-0152 Rev 2 Modification - APU Bleed Air Duct - Check Valve Relocation

02-May-1988Mos

Hrs

Ldg


RecommendedRE (-)601-0200 Special Check/Modification - Manifold Support Rod Assemblies - Thread-Inspection Holes

22-May-1988Mos

1,995Hrs

756Ldg


RecommendedRE (-)601-0268 Modification - Aircraft Data Plate - Relocation

02-May-1988Mos

1,995Hrs

756Ldg


RecommendedRE (-)601-0288 Special Check/Modification - Bleed Air Distribution - Tenth and Fourteenth Stage Duct Assembly Bleed Hole Location

Mos

Hrs

Ldg

36 A/F

RecommendedRE (-)601-0288 Rev 1 Special Check/Modification - Bleed Air Distribution - Tenth and Fourteenth Stage Duct Assembly Bleed Hole Location

Mos

Hrs

Ldg

36 A/F

RecommendedT (A/R)601-0288 Rev 2 Special Check/Modification - Bleed Air Distribution - Tenth and Fourteenth Stage Duct Assembly Bleed Hole Location

Mos

Hrs

Ldg

36 A/FEff: 30-Aug-1991

RecommendedRE (-)601-0460 Modification - APU Bleed Air Duct - Check Valve Reliability Improvement

18-Nov-1996Mos

5,001Hrs

2,052Ldg


RecommendedRE (-)601-0600 Modification – Bleed-Air Leak Detection System – 10th Stage Bleed-Air Pressure Transducers Relocation

Mos

Hrs

Ldg

36 A/F

RecommendedT (A/R)601-0600 Rev 1 Modification – Bleed-Air Leak Detection System – 10th Stage Bleed-Air Pressure Transducers Relocation

Mos

Hrs

Ldg

36 A/FEff: 12-Sep-2012


Generated: 6-Apr-2016 1:16 PM179/429







▼ 38 - WATER/WASTE

RE (O/C)Galley Drain Mast

20-Sep-1983Mos

0Hrs

0Ldg

Fwd38 A/FUnknownUnknown

OptionalT (A/R)601-0606 Increase Inspection Interval for Lavatory Adjacent Structure

Mos

Hrs

Ldg

38 A/FEff: 14-Dec-2009

▼ 39 - ELECTRICAL - ELECTRONIC PANELS AND MULTIPURPOSE COMPONENTS

RecommendedRE (-)601-0009 Modification - Center Pedestal - Replacement of Landing and Taxi Lights Control Panel

17-Sep-1985Mos

607Hrs

262Ldg


RecommendedRE (-)601-0101 Modification - JB2 and JB3 Connectors - Mating Assurance

Mos

Hrs

Ldg

39 A/F

RecommendedRE (-)601-0101 Rev 1 Modification - JB2 and JB3 Connectors - Mating Assurance

28-Mar-1989Mos

2,373Hrs

910Ldg


RecommendedRE (-)601-0140 Modification - Terminal Block Mounted Component Boards - Isolation

26-Jan-1987Mos

1,267Hrs

480Ldg


RecommendedRE (-)601-0291 Special Check/Modification - Pilot and Copilot Side Consoles- Elimination of Possible Wire Chafing

09-Mar-1989Mos

2,373Hrs

910Ldg


OptionalT (A/R)601-0439 Modification - Center-Pedestal Panel Assemblies - Improved Air Flow

Mos

Hrs

Ldg

39 A/FEff: 15-Jun-1994

▼ 49 - AIRBORNE AUXILIARY POWER

RE (O/C)APU - APU Pneu Surge Valve

20-Sep-1983Mos

0Hrs0

0APUS0

49 APU1New978668-3-1

UNKNOWN

RE (O/C)APU - Bleed Air Check APU Valve

01-Sep-1983Mos

0Hrs

0APUS

49 APU1UnknownUnknown


Generated: 6-Apr-2016 1:16 PM180/429







RE (O/C)APU - Fuel Control Unit APU Fcu

31-Mar-2002Mos

4,756.3Hrs

4,756APUS

49 APU13882600-817679

RE (O/C)APU - Fuel Nozzle

03-Mar-2004Mos

6,114.2Hrs

6,114APUS

49 APU13830061-51VS07084

RE (O/C)APU - Fuel Solenoid Valve

01-Sep-1983Mos

0Hrs0

0APUS0

49 APU1New3888134-4

97-405

RE (O/C)APU - Hourmeter

01-Sep-1983Mos

0Hrs0

0APUS0

49 APU1New3888033-4

UNKNOWN

RE (O/C)APU - Igniter Plug

01-Sep-1983Mos

0Hrs

0APUS


RE (O/C)APU - Immersion Thermocouple

01-Sep-1983Mos

0Hrs0

0APUS0

49 APU1New3876003-1

020219-150

RE (O/C)APU - Low Oil Pressure Switch

03-Mar-2004Mos

6,114.2Hrs

6,114APUS

49 APU13876001-106032

RE (O/C)APU - Low Oil Pressure Switch

01-Sep-1983Mos

0Hrs

0APUS


RE (O/C)APU - Motion Pick Up Transducer

03-Mar-2004Mos

6,114.2Hrs

6,114APUS

49 APU13876000-18-05104-134

RE (O/C)APU - Oil Pressure Regulating Valve

01-Sep-1983Mos

0Hrs0

0APUS0

49 APU1New3880021-2

UNKNOWN

RE (O/C)APU - Oil Temperature High Switch

03-Mar-2004Mos

6,114.2Hrs

6,114APUS

49 APU13888030-10338


Generated: 6-Apr-2016 1:16 PM181/429







RE (O/C)APU - Orifice Fitting

01-Sep-1983Mos

0Hrs

0APUS


RE (O/C)APU - Orifice Fitting

01-Sep-1983Mos

0Hrs

0APUS


RE (O/C)APU - Pneumatic Shutoff Valve

01-Sep-1983Mos

0Hrs0

0APUS0

49 APU1New109776-5

789C

RE (O/C)APU - Rotary Oil Pump

01-Sep-1983Mos

0Hrs0

0APUS0

49 APU1New3880000-2

UNKNOWN

RE (O/C)APU - Unit APU Ignition

01-Sep-1983Mos

0Hrs

0APUS


MRB, Life LimitRE (O/C)APU Bleed Air Supply / Bleed Air Manifold Check Valve

01-Sep-1983Mos

0Hrs

0APUS


TLMC:49-52-00-214, Ref.:Section 5-20-05 Para 10 Program Note E (SOURCE: TLMC 05-20-15)

RE (O/C)APU Control Panel

20-Sep-1983Mos

0Hrs0

0Ldg0

49 A/FNew600-51158-823

UNKNOWN

RE (O/C)APU EGT Indicator

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)APU Fault Indicator

20-Sep-1983Mos

0Hrs0

0Ldg0

49 A/FNew601-53004-5

UNKNOWN

RE (O/C)APU Fuel Booster Pump

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)APU RPM Indicator

20-Sep-1983Mos

0Hrs

0Ldg



Generated: 6-Apr-2016 1:16 PM182/429







RE (O/C)APU Starter Motor

01-Sep-1983Mos

0Hrs

0APUS


Component Inspection SimpleDUE:1. RE N/AAPU Starter Motor (Part Number 519892-3, -4 and -5) - Remove...49-42-01-212APU149

Component Inspection SimpleDUE: 9,862 Hrs1. RE 2100 HrsAPU Starter Motor (Part Number 519892-6) - Remove, inspect a...49-42-01-219APU149

Life Limit ≈15-Aug-2182REAuxiliary Power Unit (APU) Compressor Rotor

22-Apr-2003Mos

92,141 Hrs100,000100,0005,549.2Hrs5,549.2

92,141 APUS100,000100,0005,549APUS5,549

49 APU1Overhauled3822101

001365100738

Life Limit ≈12-Apr-2031REAuxiliary Power Unit (APU) Turbine Rotor

20-Sep-2002Mos

7,355.9 Hrs15,214.910,0005,214.9Hrs0

7,355 APUS15,21410,0005,214APUS0

49 APU1New3615880-1

020134504309

RE (O/C)Electric Control Unit (APU ECU)

20-Sep-1983Mos

0Hrs

0Ldg


MRB ≈03-Apr-2016RE49-10-00-201 APU Power Plant - Remove and inspect combustion chamber, reinstall combustion chamber / Remove, clean, inspect and reinstall fuel nozzle assembly

10-Jan-2008Mos

145 Hrs (+40)8,004-/+404007,604Hrs

APUS

49 APU1


MRBRE (N/A)49-10-00-205 APU Power Plant (Pre - any of the three following combinations of SB’s: GTCP 36-49-6057 and -6052, GTCP 36-49-6057 and -6074, GTCP 36-49-6057 and -6106) - Hot

section inspection and visual check of compressor rotor

Mos

Hrs

APUS

49 APU1

Ref.:PSP 608/608A Chapter 49-21-59 Section 49-20-00 (SOURCE: TLMC 05-20-15)

MRB ≈11-Sep-2016RE49-10-00-206 APU Power Plant (Post - any of the three following combinations of SB’s: GTCP 36-49-6057 and -6052, GTCP 36-49-6057 and -6074, GTCP 36-49-6057 and -6106) - Hot

section inspection and visual check of compressor rotor

03-Mar-2004Mos

355.2 Hrs (+40)8,214.2-/+402,1006,114.2Hrs

APUS

49 APU1


MRB ≈03-Apr-2016RE49-10-00-207 APU Power Plant - Remove, clean and carry out a visual check and reinstall combustor/plenum drain valves/orifice fittings

10-Jan-2008Mos

145 Hrs (+40)8,004-/+404007,604Hrs

APUS

49 APU1


MRB ≈03-Apr-2016RE49-10-10-202 APU Enclosure - Visual check

10-Jan-2008Mos

145 Hrs (+40)8,004-/+404007,604Hrs

APUS

49 APU1


MRB ≈03-Apr-2016RE49-10-60-220 APU Air Intake and Supply/ APU Exhaust Duct - Visual Check of intake and exhaust, paying particular attention to adjacent skin and associated ducting

10-Jan-2008Mos

145 Hrs (+40)8,004-/+404007,604Hrs

APUS

49 APU1



Generated: 6-Apr-2016 1:16 PM183/429







MRB ≈03-Feb-2016RE49-30-10-208 APU Fuel Supply Filter (Post SB 601-0060) Remove, inspect and install new element

25-Jul-2008Mos

0 Hrs (+30.8)12,032-/+4060011,432Hrs

Ldg

49 A/F


MRB ≈03-Apr-2016RE49-31-02-209 APU Fuel Control Unit Fuel Filter - Remove, inspect and install new element

10-Jan-2008Mos

145 Hrs (+40)8,004-/+404007,604Hrs

APUS

49 APU1


MRBRE49-40-00-211 APU Starting and Ignition (Post SB 601-0099 and A/C 3045 to 3099) - Battery requirements - Battery Check

6.6 Months (+31

Days)(21-Oct-2016)1221-Oct-2015Mos

Hrs

Ldg

(PKG 12 Month)

49 A/F

Ref.:PSP 608/608A Section 24-30-03 (SOURCE: TLMC 05-20-15) (NOTE: Applicable to APU Model GTCP 36-100 Only)

MRBRE (N/A)49-42-01-212 APU Starter Motor (Part Number 519892-3, -4 and -5) - Remove, inspect and reinstall

Mos

Hrs

APUS



MRB ≈17-Feb-2020RE49-42-01-219 APU Starter Motor (Part Number 519892-6) - Remove, inspect and reinstall

20-May-2009Mos

2,003 Hrs9,8622,1007,762Hrs

APUS



MRB ≈03-Apr-2016RE49-43-02-213 APU Igniter Plug - Remove, clean, carry out a visual check and reinstall

10-Jan-2008Mos

145 Hrs (+40)8,004-/+404007,604Hrs

APUS

49 APU1


Servicing - OptionalRE (N/A)49-51-00-301 APU General - Restoration (On-Wing Cleaning) of the Auxiliary Power Unit (APU) Load Control Valve Filter

Mos

Hrs

APUS

49 APU1

(ZONE: 311, 312) (ACCESS: 311-BB-BZ) (SOURCE: MPD 3.3) (NOTE: This task applies to filter installed on APU 36-150CL Load Control Valve,

Part No. 3885091-4 only.)

MRB ≈03-Apr-2016RE49-90-00-216 APU Engine Oil System/Auxiliary Power Unit - Drain APU Oil Tank / Fill empty APU Oil Tank

10-Jan-2008Mos

145 Hrs (+40)8,004-/+404007,604Hrs

APUS

49 APU1

(SOURCE: TLMC 05-20-15) (NOTE: Operators participating in the Spectrometric Oil and Filter Analysis Program shall change lubricating oil and

oil filter element as directed in Allied-Signal Aerospace Service Information Letter (SIL) APU-49.)

MRBRE49-90-01-217 APU Magnetic Drain Plug - Remove magnetic element from drain plug, carry out a visual check and reinstall

44 Days (+31)20-May-2016-/+11220-May-2015Mos

400 Hrs (+40)8,259-/+404007,859Hrs

APUS

49 APU1


MRB ≈03-Apr-2016RE49-90-02-218 APU Engine Oil System Oil Filter - Remove, inspect and install new element

10-Jan-2008Mos

145 Hrs (+40)8,004-/+404007,604Hrs

APUS

49 APU1

Ref.:PSP 608/608A Chapter 49-21-59 Section 49-90-47 (SOURCE: TLMC 05-20-15) (NOTE: Operators participating in the Spectrometric Oil and

Filter Analysis Program shall change lubricating oil and oil filter element as directed in Allied-Signal Aerospace Service Information Letter (SIL)

APU-49.)


Generated: 6-Apr-2016 1:16 PM184/429







RecommendedRE (-)601-0017 Modification - APU Inlet Duct Screen - Replacement

Mos

Hrs

Ldg

49 A/FEff: 17-Jan-1984

RecommendedRE (-)601-0054 Modification - APU Exhaust Duct - Addition of Shield

21-Mar-1985Mos

451Hrs

195Ldg


RecommendedRE (-)601-0060 Modification - Auxiliary Power Unit - Fuel Supply

Mos

Hrs

Ldg

49 A/F

RecommendedRE (-)601-0060 Rev 1 Modification - Auxiliary Power Unit - Fuel Supply

Mos

Hrs

Ldg

49 A/F


Mos

Hrs

Ldg

49 A/F


02-May-1988Mos

Hrs

Ldg


RecommendedRE (-)601-0064 Modification - APU Fuel Pump Control - Deletion of Connecting JB3 Wiring

01-Sep-1983Mos

0Hrs

0Ldg


RecommendedRE (-)601-0068 Modification - APU Inler Duct - Damping Tape

Mos

Hrs

Ldg

49 A/FEff: 18-Jun-1984

RecommendedRE (-)601-0076 Special Check/Modification - APU Negative “G” Fuel Shroud - Drain Holes

18-Sep-1985Mos

607Hrs

261Ldg


OptionalRE (-)601-0099 Modification - APU Start - Improvements

Mos

Hrs

Ldg

49 A/F

OptionalT (A/R)601-0099 Rev 1 Modification - APU Start - Improvements

Mos

Hrs

Ldg

49 A/FEff: 23-Sep-1986


Generated: 6-Apr-2016 1:16 PM185/429







OptionalT (A/R)601-0156 Modification - APU Enclosure - Fireproof Lining Improvements and Exhaust Duct Drainage Relocation

Mos

Hrs

Ldg

49 A/FEff: 12-Jan-1987

RecommendedRE (-)601-0172 Modification - APU Control - Introduction of Diodes

Mos

Hrs

Ldg

49 A/F

RecommendedRE (-)601-0172 Rev 1 Modification - APU Control - Introduction of Diodes

16-Jul-1986Mos

952Hrs

403Ldg


RecommendedRE (-)601-0212 Modification - Exhaust Shield Assy - Replacement of Spacers

02-May-1988Mos

1,995Hrs

756Ldg


OptionalT (A/R)601-0254 Modification - APU Installation - Spiral Wrap Addition

Mos

Hrs

Ldg

49 A/FEff: 11-Dec-1987

RecommendedRE (-)601-0290 Modification - Exhaust Shield - Crack Prevention

31-Oct-1993Mos

Hrs

Ldg

49 A/FComplied With

RecommendedRE (-)601-0290 Rev 1 Modification - Exhaust Shield - Crack Prevention

Mos

Hrs

Ldg

49 A/F

RecommendedT (A/R)601-0290 Rev 2 Modification - Exhaust Shield - Crack Prevention

Mos

Hrs

Ldg

49 A/FEff: 15-May-1993

OptionalT (A/R)601-0313 Modification - APU Gearbox - Oil Case Vent Fitting and Drain Adaptor

Mos

Hrs

Ldg

49 A/FEff: 14-Sep-1990

OptionalT (A/R)601-0455 Auxiliary Power Unit (APU) - High Voltage Ignition System (HVIS) - Modification - Fuel Return-Hose and Wire Bundle Clamps

Mos

Hrs

Ldg

49 A/FEff: 15-Aug-1995

OptionalT (A/R)601-0463 Modification - Auxiliary Battery System - HEATER/CHARGER ON/OFF Switch Removal

Mos

Hrs

Ldg

49 A/FEff: 29-Nov-1996


Generated: 6-Apr-2016 1:16 PM186/429







OptionalRE (-)601-0468 Modification - APU Gearbox Vent Line - Routing Improvement

Mos

Hrs

Ldg

49 A/F

OptionalT (A/R)601-0468 Rev 1 Modification - APU Gearbox Vent Line - Routing Improvement

Mos

Hrs

Ldg

49 A/FEff: 28-Nov-1997

RecommendedRE (-)601-0485 Modification - APU Enclosure - Improve Leak Resistance and Drainage

Mos

Hrs

Ldg

49 A/F

RecommendedRE (-)601-0485 Rev 1 Modification - APU Enclosure - Improve Leak Resistance and Drainage

Mos

Hrs

Ldg

49 A/F


Mos

Hrs

Ldg

49 A/F


Mos

Hrs

Ldg

49 A/F

RecommendedT (A/R)601-0485 Rev 4 Modification - APU Enclosure - Improve Leak Resistance and Drainage

Mos

Hrs

Ldg

49 A/FEff: 10-Mar-2010

RecommendedRE (-)601-0504 Modification - APU Exhaust - Replace Drain Tube, Part No. 601-97092-29 with Heat Resistant Tube, Part No. 601-97092-65

05-Nov-1998Mos

5,824Hrs

2,521Ldg


RecommendedRE (-)601-0528 Special Check/Modification - Auxiliary Power Unit (APU) - Prevention of Fuselage Skin Heat Damage Under and Aft of the APU Exhaust Shield

06-Sep-2001Mos

7,694.9Hrs

3,648Ldg


OptionalRE (-)601-0568 Modification - General - Introduction of the 36-150 (CL) Auxiliary Power Unit (APU)

Mos

Hrs

Ldg

49 A/F

OptionalT (A/R)601-0568 Rev 1 Modification - General - Introduction of the 36-150 (CL) Auxiliary Power Unit (APU)

Mos

Hrs

Ldg

49 A/FEff: 16-Apr-2007


Generated: 6-Apr-2016 1:16 PM187/429







RecommendedT (A/R)601-0573 Modification - APU Bleed Air Supply - Installation of the Restrictor in the APU Bleed Air Ducting

Mos

Hrs

Ldg

49 A/FEff: 21-Jul-2005

OptionalRE (-)601-0580 Modification - General - Installation of Provisions for the 36-150 (CL) Auxiliary Power Unit (APU)

Mos

Hrs

Ldg

49 A/F

OptionalRE (-)601-0580 Rev 1 Modification - General - Installation of Provisions for the 36-150 (CL) Auxiliary Power Unit (APU)

Mos

Hrs

Ldg

49 A/FEff: 28-May-2007

OptionalRE (-)601-0581 Modification – General – Activation of the 36-150 (CL) Auxiliary Power Unit (APU)

Mos

Hrs

Ldg

49 A/FEff: 11-Feb-2008

OptionalT (A/R)601-0588 Modification - Exhaust - Introduction of the 36-150 (CL) Auxiliary Power Unit (APU) Stainless Steel Exhaust Extension

Mos

Hrs

Ldg

49 A/FEff: 17-Mar-2008

RecommendedRE (-)601-0615 Special Check/Modification – Auxiliary Power Unit (APU) Engine Oil System – Replacement of the APU Oil Filter Element

Mos

Hrs

Ldg

49 A/F

RecommendedT (A/R)601-0615 Rev 1 Special Check/Modification – Auxiliary Power Unit (APU) Engine Oil System – Replacement of the APU Oil Filter Element

Mos

Hrs

Ldg

49 A/FEff: 14-Nov-2011

AlertRE (-)A601-0074 Special Check/Modification - APU Exhaust - Nozzle

Mos

Hrs

Ldg

49 A/FBY DATE OF MANUFACTUREEff: 16-Nov-1984 Not

Applicable

RE (O/C)APU Auxiliary Power Unit (APU)

20-Sep-1983Mos

0Hrs

0Ldg


RE (-)D200906000072 Airborne Auxiliary Power - Gas Turbine Engine - Standard Storage And Preservation Guidelines

Mos

Hrs

APUS

49 APU1

RE (-)D200906000072 Rev 1 Airborne Auxiliary Power - Gas Turbine Engine - Standard Storage And Preservation Guidelines

Mos

Hrs

APUS

49 APU1


Generated: 6-Apr-2016 1:16 PM188/429








Mos

Hrs

APUS

49 APU1


Mos

Hrs

APUS

49 APU1

T (A/R)D200906000072 Rev 4 Airborne Auxiliary Power - Gas Turbine Engine - Standard Storage And Preservation Guidelines

Mos

Hrs

APUS

49 APU1Eff: 12-Jan-2015

RE (-)D201110000029 Airborne Auxiliary Power Unit (APU) - Oil - General - Approved Oils

Mos

Hrs

APUS

49 APU1

RE (-)D201110000029 Rev 1 Airborne Auxiliary Power Unit (APU) - Oil - General - Approved Oils

Mos

Hrs

APUS

49 APU1


Mos

Hrs

APUS

49 APU1


Mos

Hrs

APUS

49 APU1


Mos

Hrs

APUS

49 APU1

T (A/R)D201110000029 Rev 5 Airborne Auxiliary Power Unit (APU) - Oil - General - Approved Oils

Mos

Hrs

APUS

49 APU1Eff: 23-Oct-2014

Service Information LetterRE (-)SIL No. APU-49 Revision 7 Implementation Of The Honeywell Spectrometric Oil And Filter Analysis Program (SOAP) For Honeywell Auxiliary Power Units (Apu’s)

Mos

Hrs

APUS

49 APU1Eff: 05-May-2003

Service Information LetterRE (-)SIL No. APU-49 Revision 8 Implementation Of The Honeywell Spectrometric Oil And Filter Analysis Program (SOAP) For Honeywell Auxiliary Power Units (Apu’s)

Mos

Hrs

APUS

49 APU1Eff: 11-Apr-2008


Generated: 6-Apr-2016 1:16 PM189/429







Service Information Letter ≈19-Jun-2016RESIL No. APU-49 Revision 9 Implementation Of The Honeywell Spectrometric Oil And Filter Analysis Program (SOAP) For Honeywell Auxiliary Power Units (Apu’s)

10-Jan-2008Mos

245 Hrs8,1045007,604Hrs

APUS

49 APU1Complied With

(NOTE: The SOAP and filter analysis program was initially limited to the operators of the GTCP36-100/-150 Series Auxiliary Power Units

enrolled in the Honeywell Engines, Systems & Services APU Maintenance Service Plan (MSP). The program is now offered to all operators of

the Honeywell GTCP36-100/-150, RE100 and RE220 Series APUs.)

▼ 52 - DOORS

RE (O/C)Gas Passenger Door Spring

25-Jul-2008Mos

11,432Hrs

5,881Ldg

Aft52 A/F601R331911-7UNKNOWN

RE (O/C)Main Door Gas Spring

25-Jul-2008Mos

11,432Hrs

5,881Ldg

Fwd52 A/F601R331911-7UNKNOWN

RE (O/C)Mechanism Baggage Door Latch

20-Sep-1983Mos

0Hrs0

0Ldg0

52 A/FNew600-35025-1

UNKNOWN

MRB ≈18-Sep-2016RE52-00-00-201 Doors Visual Check of passenger/crew entrance door seal

10-Feb-2016Mos

290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs

6,326Ldg

(PKG 300 Hour)

52 A/F


AWL ≈23-Oct-2017RE52-10-00-101 * Passenger Door Hinge - NDT Check

22-Jul-2004Mos

817.1 Hrs12,858.32,40010,458.3Hrs

Ldg

52 A/F

Ref.:PSP 612 Part 6 ET-52-10-01 (SOURCE: TLMC 05-10-30)

MRB ≈18-Sep-2016RE52-10-00-202 Passenger/Crew Entrance Door Visual Check that water drains are clear

10-Feb-2016Mos

290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs

6,326Ldg

(PKG 300 Hour)

52 A/F


MRB ≈03-May-2017RE52-12-00-203 Downward Opening Passenger/Crew Entrance Door Visual Check of hinge, paying particular attention to cracking and corrosion of the lugs (without disassembly of the

hinge)

10-Feb-2016Mos

590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs

6,326Ldg

(PKG 600 Hour)

52 A/F


MRB ≈20-Oct-2017RE (N/A)52-12-00-204 Downward Opening Door (Pre SB 601-0451) Internally Lubricate Passenger/Crew Entrance Door

Mos

812.3 Hrs (+40)(12,853.5)Hrs

Ldg

(PKG 1200 Hour)

52 A/F


MRB ≈20-Oct-2017RE52-12-00-205 Downward Opening Passenger/Crew Entrance Door Visual Check of all structure, paying particular attention to thefollowing: (1) Latch torque tube support brackets

and surrounding structure / (2) Tension rods (3) Underside of stair treads and angles

29-Oct-2012Mos

812.3 Hrs (+40)(12,853.5)-/+401,20011,653.5Hrs

Ldg

(PKG 1200 Hour)

52 A/F



Generated: 6-Apr-2016 1:16 PM190/429







MRB ≈20-Oct-2017RE52-12-00-206 Downward Opening Passenger/Crew Entrance Door Functional Test

29-Oct-2012Mos

812.3 Hrs (+40)(12,853.5)-/+401,20011,653.5Hrs

Ldg

(PKG 1200 Hour)

52 A/F


MRB ≈18-Sep-2016RE52-12-00-212 Downward Opening Passenger/Crew Entrance Door Scheduled Servicing Visual Check (External)- Externally Lubricate Passenger/Crew Entrance Door

10-Feb-2016Mos

290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs

6,326Ldg

(PKG 300 Hour)

52 A/F


MRB ≈18-Sep-2016RE52-12-00-213 Downward Opening Passenger/Crew Entrance Door Cam Latch Mechanism Functional Test

10-Feb-2016Mos

290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs

6,326Ldg

(PKG 300 Hour)

52 A/F


MRB ≈20-Oct-2017RE52-12-00-215 Downward Opening Door (Post SB 601-0451) Internally Lubricate Passenger/Crew Entrance Door

29-Oct-2012Mos

812.3 Hrs (+40)12,853.5-/+401,20011,653.5Hrs

Ldg

52 A/F


AWL ≈10-Jan-2021RE52-20-00-103 * Overwing Emergency Exit - Attachment Fittings - Visual Check

21-Oct-2015Mos

2,359.9 Hrs14,401.12,40012,001.1Hrs

Ldg

52 A/F

Ref.:PSP 612 Part 9 VC-52-20-01 (SOURCE: TLMC 05-10-30)

MRBRE52-20-00-207 Overwing Emergency Exit Operational Test

10 Months (+29

Days)(30-Jan-2017)-/+12430-Jan-2015Mos

Hrs

Ldg

(PKG 24 Month)

52 A/F


MRBRE52-20-00-208 Overwing Emergency Exit Betalight brightness check

10 Months (+29

Days)(30-Jan-2017)-/+12430-Jan-2015Mos

Hrs

Ldg

(PKG 24 Month)

52 A/F


MRBRE52-20-00-209 Overwing Emergency Exit Visual Check of all structure, paying particular attention to the stops, fittings, attachments and to the door seal

5.8 Months (+30

Days)(26-Sep-2016)-/+16024-Oct-2011Mos

Hrs

Ldg

(PKG 60 Month)

52 A/F


Also ConsiderDUE: (26-Sep-2016)1. RE 60 MosOverwing Emergency Exit Door, External - CPCP Check includin...C52-00-801A/F52

Also ConsiderDUE: (26-Sep-2016)1. RE 60 MosOverwing Emergency Exit Door (Internal) - CPCP Check includi...C52-00-806A/F52

MRBRE52-20-00-216 Overwing Emergency Exit Lubricate the Overwing Emergency Exit Door

10 Months (+29

Days)(30-Jan-2017)-/+12430-Jan-2015Mos

Hrs

Ldg

(PKG 24 Month)

52 A/F



Generated: 6-Apr-2016 1:16 PM191/429







MRBRE52-30-00-210 Baggage Compartment Door Visual Check of all structure, paying particular attention to the door alignment crotch fittings, surrounding structure and the door seal

5.8 Months (+30

Days)(26-Sep-2016)-/+16024-Oct-2011Mos

Hrs

Ldg

(PKG 60 Month)

52 A/F


Also ConsiderDUE: (26-Sep-2016)1. RE 60 MosBaggage Compartment Door Structure - CPCP Check including th...C52-00-802A/F52

MRB ≈20-Oct-2017RE52-70-00-211 Door Warning Functional Test - Baggage Door Switches- Functional Test - Passenger/Crew Entrance Door Switches

29-Oct-2012Mos

812.3 Hrs (+40)(12,853.5)-/+401,20011,653.5Hrs

Ldg

(PKG 1200 Hour)

52 A/F


MRB ≈18-Sep-2016RE52-70-00-214 Door Warning - Passenger/Crew Entrance Door Switches Operational Test

10-Feb-2016Mos

290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs

6,326Ldg

(PKG 300 Hour)

52 A/F


AWL ≈03-Feb-2016RE52-80-00-102 * Main Landing Gear Door Hinges - Visual Check

25-Jul-2008Mos

OVD12,03260011,432Hrs

Ldg

52 A/F

Ref.:PSP 612 Part 9 VC-52-10-03 (SOURCE: TLMC 05-10-30) (NOTE: Hinge sector 600-31587-1/2 not installed)

OptionalRE (-)601-0021 Modification - Baggage Compartment Door - Introduction of Interior Handle

Mos

Hrs

Ldg

52 A/F

OptionalRE (-)601-0021 Rev 1 Modification - Baggage Compartment Door - Introduction of Interior Handle

Mos

Hrs

Ldg

52 A/FEff: 27-Apr-1984

RecommendedRE (-)601-0065 Modification - Passenger/Crew Entrance Door - Addition of Strengthening Angles

18-Sep-1985Mos

607Hrs

261Ldg

52 A/FComplied With

RecommendedT (A/R)601-0065 Rev 1 Modification - Passenger/Crew Entrance Door - Addition of Strengthening Angles

Mos

Hrs

Ldg

52 A/FEff: 07-Mar-1985

RecommendedRE (-)601-0192 Modification - Passenger/Crew Entrance Door - Introduction of Improved Cranks and Collar

01-Dec-1990Mos

3,058.6Hrs

1,212Ldg


OptionalT (A/R)601-0207 Modification - Overwing Emergency Exit - Improved Latch Mechanism

Mos

Hrs

Ldg

52 A/FEff: 08-Jun-1988


Generated: 6-Apr-2016 1:16 PM192/429







OptionalRE (-)601-0215 Modification - Baggage Door Proximity Switches - Mounting

Mos

Hrs

Ldg

52 A/F

OptionalT (A/R)601-0215 Rev 1 Modification - Baggage Door Proximity Switches - Mounting

Mos

Hrs

Ldg

52 A/FEff: 10-Jul-1992

OptionalT (A/R)601-0218 Modification - Passenger/Crew Entrance Door - Pull-out Handle

Mos

Hrs

Ldg

52 A/FEff: 12-Jan-1988

OptionalRE (-)601-0236 Modification - Passenger/Crew Entrance Door - Seal Improvement

02-May-1988Mos

1,995Hrs

756Ldg


OptionalT (A/R)601-0270 Modification - Passenger/Crew Entrance Door - Support Mechanism Improvement

Mos

Hrs

Ldg

52 A/FEff: 23-Jan-1989

RecommendedRE (-)601-0335 Special Check/Modification - Passenger Door Stair Counterbalance System - Structure Reinforcement

Mos

Hrs

Ldg

52 A/F

RecommendedT (A/R)601-0335 Rev 1 Special Check/Modification - Passenger Door Stair Counterbalance System - Structure Reinforcement

Mos

Hrs

Ldg

52 A/FEff: 26-Aug-1991

OptionalT (A/R)601-0357 Modification - Downward Opening Door - Introduction of Reinforced Stair Assemblies

Mos

Hrs

Ldg

52 A/FEff: 22-Nov-1993

RecommendedRE (-)601-0395 Special Check/Rework - Passenger/Crew Entrance Door - Latching Mechanism

Mos

Hrs

Ldg

52 A/F

RecommendedRE (-)601-0395 Rev 1 Special Check/Rework - Passenger/Crew Entrance Door - Latching Mechanism

11-Aug-1992Mos

Hrs

Ldg


OptionalT (A/R)601-0417 Modification - Passenger/Crew Entrance Door - Addition of Internal Door-Handle Stop

Mos

Hrs

Ldg

52 A/FEff: 13-Apr-1995


Generated: 6-Apr-2016 1:16 PM193/429







OptionalRE (-)601-0451 Modification - Passenger Door - Introduce Self Lubricating Bushings

17-Dec-2001Mos

7,908.1Hrs

3,787Ldg


OptionalT (A/R)601-0465 Modification - Access Door for Refuel/Defuel Control Panel - Addition of Packer to Aft Latch

Mos

Hrs

Ldg

52 A/FEff: 31-Jan-1996

OptionalT (A/R)601-0483 Modification - Rear Fuselage Equipment Bay Door - Add Liquid Deflector

Mos

Hrs

Ldg

52 A/FEff: 30-Aug-1996

RecommendedRE (-)601-0587 Special Check/Rework - Passenger / Crew Entrance Door - Passenger Door Foot Inspection and Rework

25-Jul-2008Mos

11,432Hrs

5,881Ldg


RecommendedRE (-)601-0604 Modification – Emergency Exit – Installation of New Silicone Rubber Seal to Prevent Water Ingress

Mos

Hrs

Ldg

52 A/F

RecommendedRE (-)601-0604 Rev 1 Modification – Emergency Exit – Installation of New Silicone Rubber Seal to Prevent Water Ingress

Mos

Hrs

Ldg

52 A/F

RecommendedT (A/R)601-0604 Rev 2 Modification – Emergency Exit – Installation of New Silicone Rubber Seal to Prevent Water Ingress

Mos

Hrs

Ldg

52 A/FEff: 06-May-2014

RecommendedRE (-)601-0613 Special Check/Modification – Passenger Door – Epoxy Ramp Removal and Corrosion Prevention

Mos

Hrs

Ldg

52 A/F

RecommendedRE (-)601-0613 Rev 1 Special Check/Modification – Passenger Door – Epoxy Ramp Removal and Corrosion Prevention

Mos

Hrs

Ldg

52 A/F

RecommendedT (A/R)601-0613 Rev 2 Special Check/Modification – Passenger Door – Epoxy Ramp Removal and Corrosion Prevention

Mos

Hrs

Ldg

52 A/FEff: 24-Sep-2013

MandatoryRE (-)82-06-04 Main Entry Door Unlatching System

18-Sep-1985Mos

Hrs

Ldg


Applicable


Generated: 6-Apr-2016 1:16 PM194/429







AlertRE (-)A601-0026 Special Check/Modification - Upper Electronics Equipment Bay Doors - Lightning Protection

Mos

Hrs

Ldg

52 A/F

AlertRE (-)A601-0026 Rev 1 Special Check/Modification - Upper Electronics Equipment Bay Doors - Lightning Protection

Mos

Hrs

Ldg

52 A/FEff: 14-Feb-1984

CPCPREC52-00-801 Overwing Emergency Exit Door, External - CPCP Check including the following items: (1) External stops, fittings, frame and door seal / (2) External skin

5.8 Months (+30

Days)(26-Sep-2016)-/+16026-Sep-2011Mos

Hrs

Ldg

(PKG 60 Month)

52 A/F

(SOURCE: TLMC 05-30-20) (NOTE: This task can be done in conjunction with ScheduledMaintenance Instruction Task 52-20-00-209.)

CPCPREC52-00-802 Baggage Compartment Door Structure - CPCP Check including the following items: (1) Vertical and transverse members / (2) Inner and external skin and frames / (3)

Seal / (4) Fittings and stops

5.8 Months (+30

Days)(26-Sep-2016)-/+16026-Sep-2011Mos

Hrs

Ldg

(PKG 60 Month)

52 A/F

Ref.:PSP 607 51-54-153/3 (SOURCE: TLMC 05-30-20) (NOTE: This task can be done in conjunction with ScheduledMaintenance Instruction Task

52-30-00-210.)

CPCPREC52-00-803 Passenger/Crew Entrance Door Structure (External) - CPCP Check including the following items: (1) External door skins / (2) External door frames / (3) Tension fittings,

rollers, center cam and latches / (4) Hinge and lugs (without removal)


Hrs

Ldg

(PKG 48 Month)

52 A/F


CPCPREC52-00-804 Main Landing Gear Doors - CPCP Check including the following items: (1) Door hinges (without removal) / (2) Door Structure

5.8 Months (+30

Days)(26-Sep-2016)-/+16026-Sep-2011Mos

Hrs

Ldg

(PKG 60 Month)

52 A/F


CPCPREC52-00-805 Passenger/Crew Entrance Door Structure (Internal) - CPCP Check including the following items: (1) Door frames and beams / (2) Backup fittings and support structure /

(3) Inner skin / (4) Torque tubes structure and tension rods

5.8 Months (+30

Days)(26-Sep-2016)-/+16019-Sep-2013Mos

Hrs

Ldg

(PKG 60 Month)

52 A/F

Ref.:PSP 607 51-54-153/3 (SOURCE: TLMC 05-30-20)

CPCPREC52-00-806 Overwing Emergency Exit Door (Internal) - CPCP Check including the following items: (1) Internal Structure

5.8 Months (+30

Days)(26-Sep-2016)-/+16026-Sep-2011Mos

Hrs

Ldg

(PKG 60 Month)

52 A/F

(SOURCE: TLMC 05-30-20) (NOTE: This task can be done in conjunction with Scheduled Maintenance Instruction Task 52-20-00-209.)

IsModSumT (A/R)IS600-52-0001 REV A Installation of Alternate Fasteners for Lower Electronics Bay Access Door, Nose Compartment

Mos

Hrs

Ldg

52 A/F


Generated: 6-Apr-2016 1:16 PM195/429







IsModSumT (A/R)IS600-52-0003 REV A Passenger Door-Rework Hinge Panel Assy 600-31980-1023 to Provide Alternate Part for 600-31980-1011

Mos

Hrs

Ldg

52 A/F

IsModSumT (A/R)IS600-52-0004 REV A Main Passenger Door Seal – Introduction of Drain Holes

Mos

Hrs

Ldg

52 A/F

▼ 53 - FUSELAGE

RE (O/C)Radome Assembly

20-Sep-1983Mos

0Hrs

0Ldg


MRB ≈18-Sep-2016RE53-00-00-201 Fuselage Visual Check (External)

10-Feb-2016Mos

290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs

6,326Ldg

(PKG 300 Hour)

53 A/F


MRB ≈20-Oct-2017RE53-00-00-202 Fuselage Visual Check of the external skin, paying particular attention to the following items for cracks and corrosion: (1) ADG door skin cut-out (zone 112) / (2) All

access panels and skin cut-out areas except windows (zone 240) / (3) Windshield sill installation and skin cut-out area (zone 220) / (4) Side window installation and skin

cut-out area (zone 240) / (5) Cabin window installation and skin cut-out area (zone 240) / (6) Baggage door installation and skin cut-out area (zone 251) / (7)

Equipment bay door installation and skin cut-out area (zone 310)

29-Oct-2012Mos

812.3 Hrs (+40)(12,853.5)-/+401,20011,653.5Hrs

Ldg

(PKG 1200 Hour)

53 A/F


MRBRE53-00-00-203 Fuselage Structure (Internal) - FS169.00 to FS202.75 - Visual Check


Hrs

Ldg

53 A/F

Ref.:PSP 612 Part 9 VC-53-10-57 (SOURCE: TLMC 05-20-15) (NOTE: For aircraft that carried out check 53-00-00-203 at 180M as required prior

to Revision 29 (dated Jan 12/99), the 240M threshold of 53-00-00-203 does not apply and the next due interval should be accomplished 120M

from the completion date of the 180M check 53-00-00-203.)

Also ConsiderDUE: 26-Sep-20161. T 240 Mos | 2. RE 120 MosFuselage Structure (Internal), FS169.00 to FS202.75 - CPCP C...C53-00-803A/F53

MRBRE53-00-00-204 Fuselage Visual Check - External - along rivet lines, paying particular attention for signs of corrosion indicated by pulled rivets, discolored or blistered paint and/or

bulging skins

5.8 Months (+30

Days)(26-Sep-2016)-/+16024-Oct-2011Mos

Hrs

Ldg

(PKG 60 Month)

53 A/F


Also ConsiderDUE: (26-Sep-2016)1. RE 60 MosFuselage Upper External Skin, FS169.00 to FS621.00, above WL...C53-00-801A/F53

Also ConsiderDUE: (26-Sep-2016)1. RE 60 MosFuselage Lower External Skin, FS169.00 to FS621.00 - CPCP Ch...C53-00-802A/F53

MRBRE53-00-00-231 Fuselage Structure (Internal) - FS202.75 to FS621.00, below Floor Visual Check

3.4 Years (+31 Days)18-Aug-2019-/+16018-Aug-2014Mos

Hrs

Ldg

53 A/F


Also ConsiderDUE: 26-Sep-20161. T 180 Mos | 2. RE 60 MosFuselage Structure (Internal), FS202.75 to FS621.00 below Fl...C53-00-819A/F53


Generated: 6-Apr-2016 1:16 PM196/429







MRBRE53-00-00-232 Fuselage Structure (Internal) - FS202.75 to FS621.00, above Floor - Visual Check


Hrs

Ldg

53 A/F

Ref.:PSP 612 Part 9 VC-53-10-58 (SOURCE: TLMC 05-20-15) (NOTE: For aircraft that carried out check 53-00-00-203 at 180M as required prior

to Revision 29 (dated Jan 12/99), the 240M threshold of 53-00-00-203 does not apply and the next due interval should be accomplished 120M

from the completion date of the 180M check 53-00-00-203.)

Also ConsiderDUE: 26-Sep-20161. T 240 Mos | 2. RE 120 MosFuselage Structure (Internal), FS202.75 to FS621.00 above Fl...C53-00-820A/F53

MRBRE53-00-00-233 Fuselage Structure (Internal) - FS621.00 to FS755.00 Visual Check


Hrs

Ldg

53 A/F


Also ConsiderDUE: 26-Sep-20161. T 180 Mos | 2. RE 60 MosFuselage Structure (Internal), FS621.00 to VS67.5% - CPCP Ch...C53-00-821A/F53

AWL ≈20-Oct-2017RE53-10-00-101 * Windshield Upper Sill - FS234.00 and BL2.50 - Visual Check

29-Oct-2012Mos

812.3 Hrs12,853.51,20011,653.5Hrs

Ldg

53 A/F


AWL ≈09-Apr-2022T53-10-00-102 * Underfloor Pressure Bulkhead - FS409.00 - Visual Check (Pre SB 601-0503)

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

53 A/F

(SOURCE: TLMC 05-10-30) (NOTE: NOTE: The Inspection Threshold Interval starts at the incorporation date of SB 601-0503.)

AWL ≈20-Oct-2017RE53-10-00-103 * Keel Longeron - NDT Check

29-Oct-2012Mos

812.3 Hrs12,853.51,20011,653.5Hrs

Ldg

53 A/F


AWL ≈09-Apr-2017T53-10-00-104 * Floor Beam Attachment to Pressure Bulkhead - FS621.00 - Visual Check

Mos

558.8 Hrs12,60012,600Hrs

Ldg

53 A/F


AWL ≈03-Aug-2018RE53-10-00-105 * Windshield Lower Sill - FS209.00 - Visual Check

25-Jul-2008Mos

1,190.8 Hrs13,2321,80011,432Hrs

Ldg

53 A/F


AWL ≈24-Aug-2018RE53-10-00-106 * Rear Pressure Bulkhead Web - Feed-Through Holes and Cut-Outs - FS621.00 - Visual Check

08-Aug-2005Mos

1,218.6 Hrs13,259.82,40010,859.8Hrs

Ldg

53 A/F


AWL ≈10-Jan-2021RE53-10-00-107 * Windshield Lower Sill - FS235.00, FS249.00 and FS264.00 - Visual Check

21-Oct-2015Mos

2,359.9 Hrs14,401.12,40012,001.1Hrs

Ldg

53 A/F


AWL ≈21-Sep-2020RE53-10-00-108 * Forward Fuselage Frame - FS220.00 and WL103.90 - Visual Check

23-Dec-2014Mos

2,214.6 Hrs14,255.82,40011,855.8Hrs

Ldg

53 A/F



Generated: 6-Apr-2016 1:16 PM197/429







AWL ≈09-Apr-2022T53-10-00-109 * Integral Attachment Frame - FS513.00 and BL16.00 - Visual Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

53 A/F


AWL ≈09-Apr-2022T53-10-00-110 * Overwing Emergency Exit and Surround Structure - NDT Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

53 A/F


AWL ≈23-Jul-2021RE53-10-00-112 * Rear Pressure Bulkhead Web - Under the Vertical Stiffeners - Visual Check

10-Aug-2004Mos

2,617.1 Hrs14,658.34,20010,458.3Hrs

Ldg

53 A/F


AWL ≈09-Apr-2022T53-10-00-113 * Rear Pressure Bulkhead, Floor Beams, Fuselage Skin Panels and Associated Structure at FS621.00 - Visual Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

53 A/F

Ref.:PSP 612 Part 9 VC-53-10-37 (SOURCE: TLMC 05-10-30) (NOTE: Post SB 601-0280)

AWL ≈24-Aug-2023RE53-10-00-115 * Forward Pressure Bulkhead Vertical Stiffeners - FS202.75 and BL22.00 - NDT Check

08-Aug-2005Mos

3,618.6 Hrs15,659.84,80010,859.8Hrs

Ldg

53 A/F


AWL ≈22-Sep-2023RE53-10-00-116 * Fuselage Frame Drag Angle - FS755.00 and BL5.28 - NDT Check

26-Sep-2006Mos

3,656.3 Hrs15,697.54,80010,897.5Hrs

Ldg

53 A/F


AWL ≈10-Jan-2041T53-10-00-117 * Longitudinal Floor Beams - FS513.00 and BL18.00 - Visual Check

21-Oct-2015Mos

11,959.9 Hrs24,001.112,00012,001.1Hrs

Ldg

53 A/F


AWL ≈09-Apr-2022T53-10-00-119 * Stiffening Vertical Angles on Forward Face of Engine Support Beam - FS625.30 - Visual Check of stiffening vertical angles on the forward face of the engine support

beam at FS625.30 for cracks or distortion. Pay particular attention to stiffeners 601-35006-41, -75 and -77

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

53 A/F


AWL ≈23-Mar-2026RE53-10-00-121 * Transverse Beam - Aft Pressure Bulkhead - FS621.00 - Visual Check

26-Sep-2006Mos

4,856.3 Hrs16,897.56,00010,897.5Hrs

Ldg

53 A/F


AWL ≈21-Jan-2017RE53-10-00-122 * Forward Pressure Bulkhead Web - FS202.75 - Visual Check

03-Apr-2000Mos

454 Hrs12,495.26,0006,495.2Hrs

Ldg

53 A/F


AWL ≈09-Apr-2022T53-10-00-123 * Longitudinal Floor Beams - FS484.00 - Visual Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

53 A/F



Generated: 6-Apr-2016 1:16 PM198/429







AWL ≈29-Mar-2027RE53-10-00-124 * Intercostals and Clips - FS621.00 to FS625.30 - Visual Check

05-Aug-2003Mos

5,344.4 Hrs17,385.67,8009,585.6Hrs

Ldg

53 A/F


AWL ≈24-Mar-2027RE53-10-00-125 * Pressure Bulkhead Stiffener - FS621.00 - Visual Check

02-Nov-2002Mos

5,338.5 Hrs17,379.78,4008,979.7Hrs

Ldg

53 A/F


AWL ≈29-Dec-2030RE53-10-00-126 * Side Panel End Post - FS280.00 - NDT Check

05-Aug-2003Mos

7,144.4 Hrs19,185.69,6009,585.6Hrs

Ldg

53 A/F


AWL ≈29-Dec-2030RE53-10-00-127 * Overwing Floor Intercostal - FS421.00, FS427.00, FS439.00, FS449.85, FS461.5, FS469.58, FS476.72 and FS484.00 - Visual Check

05-Aug-2003Mos

7,144.4 Hrs19,185.69,6009,585.6Hrs

Ldg

53 A/F


AWL ≈29-Dec-2030RE53-10-00-128 * Cleat - Frame to Longeron - FS439.00, FS461.00, FS484.00, FS499.00, FS529.00 and FS544.00 - Visual Check

05-Aug-2003Mos

7,144.4 Hrs19,185.69,6009,585.6Hrs

Ldg

53 A/F


AWL ≈09-Apr-2022T53-10-00-129 * Floor Structure and Underfloor Longerons - FS513.00 and BL45.00 - Visual Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

53 A/F


AWL ≈09-Jan-2021T53-10-00-130 * Keel Longeron Links and Bolts - Visual Check

Mos

2,358.8 Hrs14,40014,400Hrs

Ldg

53 A/F


AWL ≈09-Apr-2022T53-10-00-132 * Passenger Door and Surrounding Structure - Visual Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

53 A/F


AWL ≈14-Mar-2040T53-10-00-133 * Pressure Floor - Wing Tie Beam - FS460.00 - Visual Check

Mos

Hrs

8,674 Ldg15,00015,000Ldg

53 A/F


AWL ≈09-Apr-2022T53-10-00-134 * Fuselage Frame Cap Angle - FS755.00 - Visual Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

53 A/F


AWL ≈09-Apr-2022T53-10-00-135 * Fuselage Frame at FS755.00 - Vertical Stabilizer Front Spar Attachment - Visual Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

53 A/F



Generated: 6-Apr-2016 1:16 PM199/429







AWL ≈09-Apr-2022T53-10-00-136 * Forward Pressure Bulkhead Vertical Member Near BL22.00 and WL79.50 - WL93.00 - Visual Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

53 A/F


AWL ≈09-Apr-2022T53-10-00-137 * Fuselage Frame at FS235.00 Upper Cap Angle at BL8.00 - Visual Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

53 A/F


AWL ≈09-Apr-2022T53-10-00-138 * Pilot Floor Connection Clips at BL13.00 - Visual Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

53 A/F


AWL ≈09-Apr-2022T53-10-00-139 * Forward Pressure Bulkhead Web at WL79.50 to WL91.70 - Visual Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

53 A/F


AWL ≈09-Apr-2022T53-10-00-140 * NLG Beam Web below Drag Beam - FS210.00 to FS215.00 - Visual Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

53 A/F


AWL ≈09-Apr-2022T53-10-00-141 * NLG Drag Strut at FS213.00 - Visual Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

53 A/F


AWL ≈09-Apr-2022T53-10-00-142 * NLG Beam Vertical Stiffener Clip - FS215.00 - Visual Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

53 A/F


AWL ≈09-Apr-2022T53-10-00-143 * NLG Beam Upper Cap - FS210.00 - Visual Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

53 A/F


AWL ≈09-Apr-2022T53-10-00-144 * NLG Beam Lower Cap at FS224.00 - Visual Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

53 A/F


AWL ≈09-Apr-2022T53-10-00-145 * Overwing Emergency Exit - Surround Structure - Visual Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

53 A/F


AWL ≈09-Apr-2022T53-10-00-146 * Passenger Door Frames - FS310.00 and FS349.00 - Visual Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

53 A/F



Generated: 6-Apr-2016 1:16 PM200/429







AWL ≈09-Apr-2022T53-10-00-147 * Frame Assembly Pressure Bulkhead - Vertical Stiffener - FS621.00 - Visual Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

53 A/F


AWL ≈09-Apr-2022T53-10-00-148 * Rear Pressure Bulkhead - FS621.00 - Frame Cap - Visual Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

53 A/F


AWL ≈09-Apr-2022T53-10-00-149 * Rear Pressure Bulkhead Vertical Stiffener - Visual Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

53 A/F


AWL ≈09-Apr-2022T53-10-00-150 * Outer Flange Cap Splice Angle - FS625.30 - NDT Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

53 A/F


AWL ≈09-Apr-2022T53-10-00-151 * Frame Splice - FS672.20, Stringer 6 - Visual Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

53 A/F


AWL ≈09-Apr-2022T53-10-00-152 * Fuselage Frame FS755.00 Web BL5.50 and WL125.00 to WL131.00 - Visual Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

53 A/F


AWLRE (N/A)53-10-00-153 * Stringers #8 (L/R), 17 (L/R) and 24 (L/R) Between Frames VS55.62% and VS67.5% of the Vertical Stabilizer Chord (Post SB 601-0262) - Visual Check

Mos

Hrs

Ldg

53 A/F


AWL ≈09-Apr-2022T53-10-00-177 * Fuselage to Frame Attachment - FS424.00 and WL73.00 - NDT Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

53 A/F


AWLRE (N/A)53-10-00-187 * Machined Strap - FS409.00 and LBL6.00 to RBL6.00 (Post SB 601-0503) - TBD

Mos

Hrs

Ldg

53 A/F


AWLRE (N/A)53-10-00-188 * Fuselage Frame Cap - FS409.00 and LBL18.00 and RBL18.00 (Post SB 601-0503) - TBD

Mos

Hrs

Ldg

53 A/F


AWL ≈09-Apr-2022T53-10-00-195 * Bonded Doubler Aft of FS617.00 - NDT Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

53 A/F

Ref.:PSP 612 Part 4 UT-53-30-01 (SOURCE: TLMC 05-10-30)


Generated: 6-Apr-2016 1:16 PM201/429







AWL ≈14-Nov-2031T53-10-00-197 * Rear Pressure Bulkhead Web - FS621.00, Fwd Face - NDT Check

Mos

Hrs

5,674 Ldg12,00012,000Ldg

53 A/F

Ref.:PSP 612 Part 6 ET-53-10-15, Ref.:PSP 612 Part 4 UT-53-10-03 (SOURCE: TLMC 05-10-30)

AWL ≈14-Mar-2020T53-10-00-198 * Engine Support Beam - Visual Check

Mos

Hrs

1,474 Ldg7,8007,800Ldg

53 A/F


MRBRE53-10-00-205 Main Frame (Pressure Bulkhead FS202.75) Visual Check of the bulkhead web and doublers around the feed through holes, paying particular attention for cracks

andcorrosion

5.8 Months (+30

Days)(26-Sep-2016)-/+16024-Oct-2011Mos

Hrs

Ldg

(PKG 60 Month)

53 A/F


MRBRE53-10-00-206 Main Frame (FS625.30 and Engine Support Beam Attachment) Visual Check - Internal

5.8 Months (+30

Days)(26-Sep-2016)-/+16024-Oct-2011Mos

Hrs

Ldg

(PKG 60 Month)

53 A/F


MRBRE53-10-00-207 Main Frame (Keel Longerons) Visual Check of the following items, paying particular attentionfor cracks and corrosion: (1) The forward wing box to longeron

attachment links and bolts / (2) The aft wing box to longeron attachment fittings and bolts / (3) The fuselage skin adjacent to the longeron to fuselageattachment area

5.8 Months (+30

Days)(26-Sep-2016)-/+16024-Oct-2011Mos

Hrs

Ldg

(PKG 60 Month)

53 A/F


Also ConsiderDUE: (26-Sep-2016)1. RE 60 MosKeel Longerons and Surround Structure - CPCP Check including...C53-00-804A/F53

MRBRE53-10-00-208 Main Frame (FS755.00) Visual Check, paying particular attention to the machined attachment fittings for the vertical stabilizer front spar and adjacent web

5.8 Months (+30

Days)(26-Sep-2016)-/+16024-Oct-2011Mos

Hrs

Ldg

(PKG 60 Month)

53 A/F


Also ConsiderDUE: (26-Sep-2016)1. RE 60 MosFuselage Frame Attachment at FS755.00 and Skin at FS710.00 t...C53-00-805A/F53

MRBRE53-10-00-209 Main Frame (Floor Beam End Fittings at FS621.00) Visual Check, paying particular attention to: The fasteners and surrounding areas. The pressure bulkhead skin

adjacent to the fitting

5.8 Months (+30

Days)(26-Sep-2016)-/+16024-Oct-2011Mos

Hrs

Ldg

(PKG 60 Month)

53 A/F


MRBRE53-10-00-210 Main Frame (Passenger Door Surround Structure) Visual Check of the following items, paying particular attention for cracks and corrosion: (1) The external fuselage

skin adjacent to the hinges / (2) The internal bonded doubler at the door corners

5.8 Months (+30

Days)(26-Sep-2016)-/+16024-Oct-2011Mos

Hrs

Ldg

(PKG 60 Month)

53 A/F


Also ConsiderDUE: (26-Sep-2016)1. RE 60 MosPassenger Door Surround Structure - CPCP Check including the...C53-00-806A/F53


Generated: 6-Apr-2016 1:16 PM202/429







MRBRE53-10-00-211 Main Frame (Overwing Emergency Exit Surround Structure) Visual Check of the following items, paying particular attention for cracks and corrosion: (1) The external

fuselage skin at the door corners / (2) The internal bonded doubler at the door corners (3) The upper and lower sill members

5.8 Months (+30

Days)(26-Sep-2016)-/+16024-Oct-2011Mos

Hrs

Ldg

(PKG 60 Month)

53 A/F


Also ConsiderDUE: (26-Sep-2016)1. RE 60 MosOverwing Emergency Exit Door Structure - CPCP Check includin...C53-00-807A/F53

MRBRE53-10-00-212 Main Frame (Baggage Door Surround Structure) Visual Check of the following items, paying particular attention for cracks and corrosion: (1) The external fuselage skin

at the door corners / (2) The internal bonded doubler at the door corners / (3) The lower sill members

5.8 Months (+30

Days)(26-Sep-2016)-/+16024-Oct-2011Mos

Hrs

Ldg

(PKG 60 Month)

53 A/F


Also ConsiderDUE: (26-Sep-2016)1. RE 60 MosBaggage Door Surround Structure - CPCP Check including the f...C53-00-808A/F53

MRBRE53-10-00-213 Main Frame (Equipment Bay Door Surround Structure) Visual Check of the following items, paying particular attention for cracks and corrosion: (1) The external

fuselage skin at the door corners / (2) The internal bonded doubler at the door corners / (3) The door hinge support structures

5.8 Months (+30

Days)(26-Sep-2016)-/+16024-Oct-2011Mos

Hrs

Ldg

(PKG 60 Month)

53 A/F


Also ConsiderDUE: (26-Sep-2016)1. RE 60 MosMain Frame (Equipment Bay Door Surround Structure) - CPCP Ch...C53-00-809A/F53

MRBRE53-10-00-214 Main Frame - Fuselage Floor Beam Splices Visual Check

5.8 Months (+30

Days)(26-Sep-2016)-/+16024-Oct-2011Mos

Hrs

Ldg

(PKG 60 Month)

53 A/F


MRBRE53-10-00-215 Main Frame (Frame Assembly FS424.00) Visual Check, paying particular attention to the integral wing attachment lug and the underfloor longeron attachment points

5.8 Months (+30

Days)(26-Sep-2016)-/+16024-Oct-2011Mos

Hrs

Ldg

(PKG 60 Month)

53 A/F


Also ConsiderDUE: (26-Sep-2016)1. RE 60 MosWing to Fuselage Integral Attachment at FS424.00 and BL45.00...C53-00-810A/F53

MRBRE53-10-00-216 Main Frame (Frame Assembly FS473.15) Visual Check, paying particular attention to the integral wing attachment lug and the underfloor longeron attachment points

5.8 Months (+30

Days)(26-Sep-2016)-/+16024-Oct-2011Mos

Hrs

Ldg

(PKG 60 Month)

53 A/F



MRBRE53-10-00-217 Main Frame (Frame Assembly FS513.00) Visual Check, paying particular attention to: (1) The inboard and outboard integral wing attachment lugs / (2) The fuselage to

wing attachment link / (3) The underfloor longeron attachment points

5.8 Months (+30

Days)(26-Sep-2016)-/+16024-Oct-2011Mos

Hrs

Ldg

(PKG 60 Month)

53 A/F




Generated: 6-Apr-2016 1:16 PM203/429







MRBRE53-10-00-218 Main Frame (Frame Assembly FS640.00 and Engine Support Beam Attachment) Visual Check - Internal

5.8 Months (+30

Days)(26-Sep-2016)-/+16024-Oct-2011Mos

Hrs

Ldg

(PKG 60 Month)

53 A/F


MRBRE53-10-00-219 Main Frame (Frame Assembly FS654.50) Visual Check - Internal

5.8 Months (+30

Days)(26-Sep-2016)-/+16024-Oct-2011Mos

Hrs

Ldg

(PKG 60 Month)

53 A/F


MRBRE53-10-00-220 Main Frame (FS672.20 and FS682.20) Visual Check - Internal

5.8 Months (+30

Days)(26-Sep-2016)-/+16024-Oct-2011Mos

Hrs

Ldg

(PKG 60 Month)

53 A/F


AWL - Repair ≈28-May-2034RE53-10-00-406 Repair − Pressure Bulkhead, FS 409 (NDT and Visual Check)

Mos

8,782.8 Hrs20,82420,824Hrs

Ldg

53 A/F

Ref.:PSP 612, Part 4, VT−53−10−02, Ref.:PSP 612, Part 6, ET−53−10−10, Ref.:PSP 612, Part 9, VC−53−30−36 (ZONE: 131,132) (SOURCE: TLMC 5

-10-25)

AWL ≈14-Jul-2023T53-10-01-101 * Upper Latch Pins of the Passenger Door - NDT Check

Mos

Hrs

2,674 Ldg9,0009,000Ldg

53 A/F

Ref.:PSP 612 Part 7 MT-53-40-02 (SOURCE: TLMC 05-10-30)

AWL ≈14-Mar-2040T53-10-01-102 * Splice Strap and Skin at Stringer 20L and 20R Between FS559.00 and FS621.00 - NDT Check

Mos

Hrs

8,674 Ldg15,00015,000Ldg

53 A/F


MRBRE53-10-11-228 Floor Structure Under Toilet and Galley (without removal) carry out a Detailed Inspection of all accessible structure using a Borescope, paying particular attention for

corrosive spillage

6.6 Months (+31

Days)(21-Oct-2016)-/+11221-Oct-2015Mos

Hrs

Ldg

(PKG 12 Month)

53 A/F


MRBRE53-10-11-230 Floor Structure (Pre or Post SB 601-0372) - Remove Toilet, Galley and Floor Boards, carry out a Detailed Inspection of all under-floor structure (including beams),

paying particular attention for corrosive spillage.

5.8 Months (+30

Days)(26-Sep-2016)-/+16024-Oct-2011Mos

Hrs

Ldg

(PKG 60 Month)

53 A/F

Ref.:SRM PSP 607 53-25-07 (SOURCE: TLMC 05-20-15) (NOTE: Remove tape for pre SB 601-0372)

Also ConsiderDUE: (26-Sep-2016)1. RE 60 MosFloor Structure, FS589.00 to FS621.00 - CPCP Check including...C53-00-818A/F53




AWL ≈09-Apr-2022T53-20-00-154 * Pilot’s Floor Web Adjacent to Pressure Bulkhead - FS203.00 and BL16.00 - Visual Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

53 A/F



Generated: 6-Apr-2016 1:16 PM204/429







AWL ≈20-Jul-2031T53-30-00-155 * Cabin Window Cut-Outs - NDT Check

29-Oct-2012Mos

7,412.3 Hrs19,453.57,80011,653.5Hrs

Ldg

53 A/F

Ref.:PSP 612 Part 6 ET-53-30-01 (SOURCE: TLMC 05-10-30) (NOTE: Post SB 601-0280)

AWL ≈09-Apr-2022T53-30-00-157 * Light Fuselage Frames FS220.00 to FS605.00 - Visual Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

53 A/F


AWL ≈09-Apr-2022T53-30-00-159 * Fuselage Skin Panel - FS625.30, Stringer 0.0 - Visual Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

53 A/F


AWL ≈23-Dec-2029T53-30-00-161 * Stringer Splice - FS513.00, Stringer 13 - Visual Check

26-Sep-2006Mos

6,656.3 Hrs18,697.57,80010,897.5Hrs

Ldg

53 A/F


AWL ≈09-Apr-2022T53-30-00-163 * Cabin Window Surround Structures FS364.00 to FS529.00, Stringers 10 to 13 - Visual Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

53 A/F


AWL ≈09-Apr-2022T53-30-00-165 * Skin and Stringer Splice at FS559.00, Stringer 0.0 - Visual Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

53 A/F


AWL ≈29-Dec-2030RE53-30-00-166 * Fuselage Skin at NLG Cut-Out - FS235.00 - Visual Check

05-Aug-2003Mos

7,144.4 Hrs19,185.69,6009,585.6Hrs

Ldg

53 A/F


AWL ≈09-Apr-2022T53-30-00-168 * Wing to Fuselage Attachment Frame - FS513.00 - NDT Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

53 A/F


AWL ≈09-Apr-2022T53-30-00-170 * Stringer Splice at FS473.00, Stringer 3 - Visual Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

53 A/F


AWL ≈09-Apr-2022T53-30-00-171 * Skin Splice at Stringer 0 - FS439.00 - Visual Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

53 A/F


AWL ≈09-Apr-2022T53-30-00-172 * Skin Splice - FS424.00 to FS439.00, Stringer 8 - Visual Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

53 A/F



Generated: 6-Apr-2016 1:16 PM205/429







AWL ≈09-Apr-2022T53-30-00-173 * Stringer Splice - Stringer 1 L&R FS718.00 - Visual Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

53 A/F


AWL ≈09-Apr-2022T53-30-00-174 * Fuselage Stringer Splice at Stringer 0, Forward of FS718.00 - Visual Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

53 A/F


AWL ≈09-Apr-2022T53-30-00-175 * Baggage Door and Surround Structure - NDT Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

53 A/F


AWL ≈09-Apr-2022T53-30-00-176 * Pressure Skin/Floor Angle at WL73.00 Between FS409.00 and FS559.00 - NDT Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

53 A/F


AWL ≈09-Apr-2022T53-30-00-178 * Fuselage Frame Ref VS55.625%, Stringer 5 - Visual Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

53 A/F


AWLRE (N/A)53-30-00-179 * Drag Angle at Frame 67.5% of the Vertical Stabilizer Chord (Post SB 601-0262) - NDT Check

Mos

Hrs

Ldg

53 A/F


AWLRE (N/A)53-30-00-180 * Skin Over Drag Angle and Frame at 67.5% and Over Stringers #8 (L/R), 17 (L/R) and 24 (L/R) Between Frames 55.62% and 67.5% of Vertical Stabilizer Chord (Post SB

601-0262) - Visual Check

Mos

Hrs

Ldg

53 A/F


AWL ≈20-Feb-2016RE53-30-00-185 * Structures Adjacent to Overboard Lavatory Services (External) - Visual Check

22-Mar-2013Mos

14.1 Hrs12,055.330011,755.3Hrs

Ldg

53 A/F

Ref.:PSP 612 Part 9 VC-53-30-01 (SOURCE: TLMC 05-10-30) (NOTE: This check is not required if you have done the internal visual check, 53-30

-00-186, every 3600 hours. If you have not done 53-30-00-185 but now want to, you must do both 53-30-00-185 and 53-30-00-186 before

you change to 53-30-00-185.)

AWLRE (N/A)53-30-00-186 * Structures Adjacent to Overboard Lavatory Services (Internal) - Visual Check

Mos

Hrs

Ldg

53 A/F


MRBRE53-30-00-221 Cabin Window Cut-Outs NDT Check

5.8 Months (+30

Days)(26-Sep-2016)-/+16024-Oct-2011Mos

Hrs

Ldg

(PKG 60 Month)

53 A/F


Also ConsiderDUE: (26-Sep-2016)1. RE 60 MosCabin Window Cut-Outs and Surround Structure FS364.00 to FS5...C53-00-813A/F53


Generated: 6-Apr-2016 1:16 PM206/429







MRBRE53-30-00-222 Plates/Skins (Side Skin Panel FS409.00 and WL73.50) Visual Check, paying particular attention to the external corner area at the wing cut-out

5.8 Months (+30

Days)(26-Sep-2016)-/+16024-Oct-2011Mos

Hrs

Ldg

(PKG 60 Month)

53 A/F


MRBRE53-30-00-224 Lower Fuselage Skins (External) NDT Check

OVD(11-Dec-2015)-/+19611-Dec-2007Mos

Hrs

Ldg

(PKG 96 Month)

53 A/F


MRB ≈17-Nov-2016RE53-30-00-229 Intercostals and Door Surround Structure (Pre SB 601-0335) Visual Check

11-Nov-2015Mos

Hrs

277 Ldg (+40)6,603-/+403006,303Ldg

53 A/F


AWL - Repair ≈06-Apr-2022RE53-30-00-401 Repair − Fuselage Skin FS 235.0, BL 6.0 (NDT and Visual Check)

03-May-2002Mos

2,955.3 Hrs14,996.56,6008,396.5Hrs

Ldg

53 A/F

Ref.:PSP 612, Part 6, ET−53−30−09, Ref.:PSP 612, Part 9, VC−53−30−25 (ZONE: 114,115,121,122) (SOURCE: TLMC 5-10-25)

AWL - Repair ≈06-Apr-2022RE53-30-00-401 Repair − Fuselage Skin FS 235.0, BL 6.0 (NDT and Visual Check)

03-May-2002Mos

2,955.3 Hrs14,996.56,6008,396.5Hrs

Ldg

53 A/F

Ref.:PSP 612, Part 6, ET−53−30−09, Ref.:PSP 612, Part 9, VC−53−30−25 (ZONE: 114,115,121,122,) (SOURCE: TLMC 5-10-25)

AWL ≈09-Apr-2022T53-40-00-181 * Integral Frame Attachment Lugs - FS424.00 and BL45.00 - Visual Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

53 A/F


AWLRE (N/A)53-40-00-182 * Tail Tank Attachment Bolts (Post SB 601-0262) - NDT Check

Mos

Hrs

Ldg

53 A/F

Ref.:PSP 612 Part 7 MT-53-40-01 (SOURCE: TLMC 05-10-30)

AWL ≈09-Apr-2022T53-40-00-183 * Integral Frame Attachment Lugs - FS473.00 and BL45.00 - Visual Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

53 A/F


AWL ≈09-Apr-2022T53-40-00-184 * Integral Frame Attachment Lugs - FS513.00 and BL45.00 and BL13.50 - Visual Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

53 A/F


AWL ≈09-Apr-2022T53-40-00-189 * Integral Frame Attachment Bolts - FS424.00 and BL45.00 - NDT Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

53 A/F


AWL ≈09-Apr-2022T53-40-00-190 * Integral Frame Attachment Bolts - FS473.00 and BL45.00 - NDT Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

53 A/F



Generated: 6-Apr-2016 1:16 PM207/429







AWL ≈09-Apr-2022T53-40-00-191 * Integral Frame Attachment Bolts - FS513.00 and BL45.00 and BL13.50 - NDT Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

53 A/F


AWL ≈10-Jan-2021RE53-40-00-192 * Overwing Emergency Exit - Surround Structure and Attachment Fittings - Visual Check

21-Oct-2015Mos

2,359.9 Hrs14,401.12,40012,001.1Hrs

Ldg

53 A/F


MRBRE53-40-00-225 Attachment Fittings (Nose Gear Trunnion Assembly) Visual Check, paying particular attention to: (1) The drag brace and the nose gear trunnion fitting for cracks / (2)

The web of the trunnion box assembly adjacent to trunnion fitting assembly for evidence of cracking or buckling

6.6 Months (+31

Days)(21-Oct-2016)-/+11221-Oct-2015Mos

Hrs

Ldg

(PKG 12 Month)

53 A/F


Also ConsiderDUE: (21-Oct-2016)1. RE 48 MosNose Landing Gear Wheel Well Structure - CPCP Check includin...C53-00-815A/F53

MRB ≈29-Dec-2030RE53-50-00-226 Tail Cone Visual Check of interior surface, frames, access door, door surrounding structure and fasteners

05-Aug-2003Mos

7,144.4 Hrs (+40)(19,185.6)-/+409,6009,585.6Hrs

Ldg

(PKG 9600 Hour)

53 A/F


MRBRE53-50-11-227 Nose Radome Visual Check, paying particular attention to interior surface and attachments

5.8 Months (+30

Days)(26-Sep-2016)-/+16024-Oct-2011Mos

Hrs

Ldg

(PKG 60 Month)

53 A/F


Also ConsiderDUE: (26-Sep-2016)1. RE 60 MosNose Radome - CPCP Check including the following items: (1) ...C53-00-817A/F53

RecommendedRE (-)601-0078 Special Check/Modification - Upper Mid-Fuselage (Left Side) - Stringers

Mos

Hrs

Ldg

53 A/FEff: 22-Oct-1984

RecommendedRE (-)601-0094 Special Check/Rework - Fuselage Frame Station 394.00 - Missing Rivets

26-Jan-1987Mos

1,267Hrs

480Ldg

53 A/FComplied With

RecommendedT (A/R)601-0094 Rev 1 Special Check/Rework - Fuselage Frame Station 394.00 - Missing Rivets

Mos

Hrs

Ldg

53 A/FEff: 10-Dec-1984

RecommendedRE (-)601-0161 Special Check/Rework - Mid Fuselage - Undersize Hi-Lok Fasteners and Missing Gusset

Mos

Hrs

Ldg

53 A/F

RecommendedRE (-)601-0161 Rev 1 Special Check/Rework - Mid Fuselage - Undersize Hi-Lok Fasteners and Missing Gusset

27-Jan-1987Mos

1,267Hrs

470Ldg



Generated: 6-Apr-2016 1:16 PM208/429







RecommendedRE (-)601-0164 Modification - Seat Tracks - Primary Stop

Mos

Hrs

Ldg

53 A/F

RecommendedRE (-)601-0164 Rev 1 Modification - Seat Tracks - Primary Stop

28-Mar-1989Mos

2,373Hrs

910Ldg


OptionalRE (-)601-0169 Special Check/Rework - Floor Beam - Clearance for Access to Vent Valve on Forward Fuselage Fuel Tank

Mos

Hrs

Ldg

53 A/FEff: 02-May-1986

OptionalRE (-)601-0173 Modification - Tail Cone - Static Discharger

Mos

Hrs

Ldg

53 A/F

OptionalT (A/R)601-0173 Rev 1 Modification - Tail Cone - Static Discharger

Mos

Hrs

Ldg

53 A/FEff: 18-Jun-1990

RecommendedRE (-)601-0178 Modification - Front Wing-to-Fuselage Fairings - Center Splice Joint Fasteners

27-Jan-1987Mos

1,267Hrs

470Ldg


OptionalRE (-)601-0179 Passenger Door Frame - Addition of Drain Holes and Tubes

Mos

Hrs

Ldg

53 A/F

OptionalT (A/R)601-0179 Rev 1 Passenger Door Frame - Addition of Drain Holes and Tubes

Mos

Hrs

Ldg

53 A/FEff: 14-Oct-1988

RecommendedRE (-)601-0194 Modification - Main Frame - Main Landing Gear Support Structure

Mos

Hrs

Ldg

53 A/FEff: 03-Apr-1987

RecommendedRE (-)601-0201 Modification - Rear Pressure Bulkhead - Introduction of Doublers

12-Nov-1992Mos

3,754Hrs

1,519Ldg


OptionalT (A/R)601-0214 Modification - Rear Fuselage Equipment Bay - Installation of Tow Bar

Mos

Hrs

Ldg

53 A/FEff: 09-Mar-1988


Generated: 6-Apr-2016 1:16 PM209/429







RecommendedRE (-)601-0372 Modification - Cabin Fuselage Floor Structure - Improved Isolation Between Floor Beams and Floor Panels

Mos

Hrs

Ldg

53 A/F

RecommendedRE (-)601-0372 Rev 1 Modification - Cabin Fuselage Floor Structure - Improved Isolation Between Floor Beams and Floor Panels

Mos

Hrs

Ldg

53 A/F

RecommendedRE (-)601-0372 Rev 2 Modification - Cabin Fuselage Floor Structure - Improved Isolation Between Floor Beams and Floor Panels

26-Jan-1996Mos

4,785Hrs

1,932Ldg


OptionalT (A/R)601-0412 Modification - Wheel Bin Brushes - Introduction of Three-Piece Wheel-Bin Brush

Mos

Hrs

Ldg

53 A/FEff: 15-Sep-1994

OptionalT (A/R)601-0452 Modification - Right Main Wheel Bin - Replacement of Fasteners on the Inboard Access Panel 144-BZ

Mos

Hrs

Ldg

53 A/FEff: 31-Aug-1995

OptionalT (A/R)601-0459 Modification - Rear Fuselage Frame Assembly Install Doublers for APU Hoist

Mos

Hrs

Ldg

53 A/FEff: 30-Nov-1995

OptionalT (A/R)601-0487 Modification - Tail Cone Fuel Tank Assembly - Increase Strobe Light Reliability

Mos

Hrs

Ldg

53 A/FEff: 30-Apr-1998

OptionalRE (-)601-0488 Modification - Main Landing Gear Fairing - Installation of Removable Fasteners

08-Nov-1998Mos

5,824Hrs

2,521Ldg


RecommendedRE (-)601-0501 Special Check - Inspection of Underfloor Pressure Bulkhead at FS409.00

04-May-2004Mos

10,325.2Hrs

5,223Ldg


RecommendedRE (-)601-0503 Special Check/Modification - Middle Fuselage - FS409.00 Pressure Bulkhead Reinforcement

Mos

Hrs

Ldg

53 A/F

RecommendedT (A/R)601-0503 Rev 1 Special Check/Modification - Middle Fuselage - FS409.00 Pressure Bulkhead Reinforcement

Mos

Hrs

Ldg

53 A/FEff: 17-Mar-2008


Generated: 6-Apr-2016 1:16 PM210/429







RecommendedRE (-)601-0507 Modification - Main Landing Gear Bay Fairing - Add a Protection Shield Against Ice Build-up on Aileron Cables

05-Nov-1998Mos

Hrs

Ldg


RecommendedRE (-)601-0537 Modification - Main Frame - Addition of a Liquid Deflector Around Aft Equipment Compartment Door

15-Sep-2007Mos

11,184.3Hrs

5,748Ldg

53 A/FComplied With

RecommendedT (A/R)601-0537 Rev 1 Modification - Main Frame - Addition of a Liquid Deflector Around Aft Equipment Compartment Door

Mos

Hrs

Ldg

53 A/FEff: 30-Jan-2004

RecommendedT (A/R)601-0565 Modification - Aerodynamic Fairings - Installation of Decals on the Tail Cone Assembly

Mos

Hrs

Ldg

53 A/FEff: 05-Oct-2006

RecommendedRE (-)601-0586 Special Check/Modification – Floor – Addition of Seat Track Extensions

Mos

Hrs

Ldg

53 A/F

Nextdue Share EarliestDUE:1. RE -Special Check/Modification – Floor – Addition of Seat Track ...601-0586 Part AA/F53

Nextdue Share EarliestDUE:1. RE -Special Check/Modification – Floor – Addition of Seat Track ...601-0586 Part BA/F53

RecommendedRE (-)601-0586 Part A Special Check/Modification – Floor – Addition of Seat Track Extensions - Verify Applicability

Mos

Hrs

Ldg

53 A/FEff: 24-Sep-2007

RecommendedRE (-)601-0586 Part B Special Check/Modification – Floor – Addition of Seat Track Extensions - Modification

Mos

Hrs

Ldg

53 A/FEff: 24-Sep-2007

RecommendedRE (-)601-0586 Rev 1 Special Check/Modification – Floor – Addition of Seat Track Extensions

Mos

Hrs

Ldg

53 A/F

Nextdue Share EarliestDUE:1. RE -Special Check/Modification – Floor – Addition of Seat Track ...601-0586 Rev 1 Part AA/F53

Nextdue Share EarliestDUE:1. RE -Special Check/Modification – Floor – Addition of Seat Track ...601-0586 Rev 1 Part BA/F53

RecommendedRE (-)601-0586 Rev 1 Part A Special Check/Modification – Floor – Addition of Seat Track Extensions - Verify Applicability

Mos

Hrs

Ldg

53 A/FEff: 09-Oct-2007

RecommendedRE (-)601-0586 Rev 1 Part B Special Check/Modification – Floor – Addition of Seat Track Extensions - Modification

Mos

Hrs

Ldg

53 A/FEff: 09-Oct-2007


Generated: 6-Apr-2016 1:16 PM211/429







RecommendedRE (-)601-0586 Rev 2 Special Check/Modification – Floor – Addition of Seat Track Extensions

25-Jul-2008Mos

11,432Hrs

5,881Ldg

53 A/FComplied With

Nextdue Share EarliestDUE:1. RE -Special Check/Modification – Floor – Addition of Seat Track ...601-0586 Rev 2 Part AA/F53

Nextdue Share EarliestDUE:1. RE -Special Check/Modification – Floor – Addition of Seat Track ...601-0586 Rev 2 Part BA/F53

RecommendedRE (-)601-0586 Rev 2 Part A Special Check/Modification – Floor – Addition of Seat Track Extensions - Verify Applicability

Mos

Hrs

Ldg

53 A/FEff: 28-Apr-2008

RecommendedRE (-)601-0586 Rev 2 Part B Special Check/Modification – Floor – Addition of Seat Track Extensions - Modification

Mos

Hrs

Ldg

53 A/FEff: 28-Apr-2008

RecommendedT (A/R)601-0586 Rev 3 Special Check/Modification – Floor – Addition of Seat Track Extensions

Mos

Hrs

Ldg

53 A/FEff: 21-Jul-2008

Nextdue Share EarliestDUE:1. T A/R | 2. RE -Special Check/Modification – Floor – Addition of Seat Track ...601-0586 Rev 3 Part AA/F53

Nextdue Share EarliestDUE:1. T A/R | 2. RE -Special Check/Modification – Floor – Addition of Seat Track ...601-0586 Rev 3 Part BA/F53

RecommendedT (A/R)601-0586 Rev 3 Part A Special Check/Modification – Floor – Addition of Seat Track Extensions - Verify Applicability

Mos

Hrs

Ldg

53 A/FEff: 21-Jul-2008

RecommendedT (A/R)601-0586 Rev 3 Part B Special Check/Modification – Floor – Addition of Seat Track Extensions - Modification

Mos

Hrs

Ldg

53 A/FEff: 21-Jul-2008

RecommendedT (A/R)601-0596 Special Check/Rework – Floor – Inspect the Under Floor Support Channel for FOD and Clean the Area

Mos

Hrs

Ldg

53 A/FEff: 21-Jul-2008

RecommendedT601-0612 Special Check – Floor Structure – Inspection and Torque, if Required, of the Bolts Attaching the Floor Beam Assembly Installed Over the Fwd and Aft Auxiliary Fuel

Tanks

3.2 Years05-Jul-201996Mos

Hrs

Ldg

53 A/FEff: 05-Jul-2011

MandatoryRE (-)97-24-02 R1 Pressure bulkhead

18-Mar-2009Mos

11,458.6Hrs

5,902Ldg

53 A/FAMOCEff: 13-Feb-2004 Complied

With

Compliance Share DoubleDUE:1. T A/R | 2. RE -Special Check - Inspection of Underfloor Pressure Bulkhead a...601-0501A/F53


Generated: 6-Apr-2016 1:16 PM212/429







CPCPREC53-00-801 Fuselage Upper External Skin, FS169.00 to FS621.00, above WL73.50 - CPCP Check including the following items: (1) Skin splices of main frame, FS513.00 Stringers 11

to 13 / (2) Skin splice at FS450.00 and WL73.00 / (3) Skin splice at FS439.00 Stringer 0.0 / (4) Skin at FS559.00 Stringer 0.0 / (5) Skin splice at FS424.00 to FS439.00

Stringer 8 / (6) Frame splice at FS424.00 and WL73.00 / (7) Splice at FS473.00 Stringer 3 / (8) Skin panel at light frames / (9) Antenna cut-outs (without removal) / (10)

Skin around cabin windows, doors and cockpit windows

5.8 Months (+30

Days)(26-Sep-2016)-/+16026-Sep-2011Mos

Hrs

Ldg

(PKG 60 Month)

53 A/F


CPCPREC53-00-802 Fuselage Lower External Skin, FS169.00 to FS621.00 - CPCP Check including the following items: (1) Nose landing gear cut-out at FS235.00 / (2) Fuselage skin including

area covered by fairings / (3) Fuselage skin as viewed from MLG bay / (4) Antenna cut-outs (without removal) and access doors

5.8 Months (+30

Days)(26-Sep-2016)-/+16026-Sep-2011Mos

Hrs

Ldg

(PKG 60 Month)

53 A/F


CPCPREC53-00-803 Fuselage Structure (Internal), FS169.00 to FS202.75 - CPCP Check including the following items: (1) Aft face of bulkhead FS169.00 / (2) Forward web of bulkhead

FS202.75 / (3) Vertical stiffeners of bulkhead FS202.75 / (4) Internal skins, frames and stringers / (5) Floor beams

5.8 Months (+30

Days)26-Sep-2016-/+112026-Sep-2006Mos

Hrs

Ldg

53 A/F

(SOURCE: TLMC 05-30-20) (NOTE: [1] Remove insulation blankets, do not removeself-adhesive panels. [2] This task can be done in conjunction

with Scheduled Maintenance Instruction Task 53-00-00-203.)

CPCPREC53-00-804 Keel Longerons and Surround Structure - CPCP Check including the following items: (1) Forward wing box to longeron attachment links and bolts / (2) Aft wing box to

longeron attachment fittings and bolts / (3) Fuselage skin adjacent to the longerons

5.8 Months (+30

Days)(26-Sep-2016)-/+16026-Sep-2011Mos

Hrs

Ldg

(PKG 60 Month)

53 A/F

Ref.:PSP 607 51-54-153/3 (SOURCE: TLMC 05-30-20) (NOTE: This task can be done in conjunction with Scheduled Maintenance Instruction Task

53-10-00-207.)

CPCPREC53-00-805 Fuselage Frame Attachment at FS755.00 and Skin at FS710.00 to FS718.00, Stringers 1L to 1R - CPCP Check including the following items: (1) Fuselage frame and drag

angle / (2) Attachment fitting for the vertical stabilizer / (3) Adjacent Web / (4) Skin area at FS718.00, stringers 1L to 1R

5.8 Months (+30

Days)(26-Sep-2016)-/+16026-Sep-2011Mos

Hrs

Ldg

(PKG 60 Month)

53 A/F


CPCPREC53-00-806 Passenger Door Surround Structure - CPCP Check including the following items: (1) The external fuselage skin adjacent to the hinges / (2) The internal bonded doubler

at the four corners / (3) Upper sill, lower cap and plate / (4) Lower sill, butt strap and sill longeron / (5) Frame at FS310.00 and FS349.00 / (6) Fittings and Latches

5.8 Months (+30

Days)(26-Sep-2016)-/+16026-Sep-2011Mos

Hrs

Ldg

(PKG 60 Month)

53 A/F


CPCPREC53-00-807 Overwing Emergency Exit Door Structure - CPCP Check including the following items: (1) External skin at the door structure four corners / (2) Internal doubler at the

door structure four corners / (3) Upper and lower sill members / (4) Latch fittings, frame stop fittings and hinge support fittings

5.8 Months (+30

Days)(26-Sep-2016)-/+16026-Sep-2011Mos

Hrs

Ldg

(PKG 60 Month)

53 A/F


CPCPREC53-00-808 Baggage Door Surround Structure - CPCP Check including the following items: (1) External fuselage skin at the four corners / (2) Internal bonded doubler at the four

corners / (3) Lower sill members

5.8 Months (+30

Days)(26-Sep-2016)-/+16026-Sep-2011Mos

Hrs

Ldg

(PKG 60 Month)

53 A/F



Generated: 6-Apr-2016 1:16 PM213/429







CPCPREC53-00-809 Main Frame (Equipment Bay Door Surround Structure) - CPCP Check including the following items: (1) The external fuselage skin at the door corners / (2) The internal

bonded doubler at the door corners / (3) The door hinge support structures

5.8 Months (+30

Days)(26-Sep-2016)-/+16026-Sep-2011Mos

Hrs

Ldg

(PKG 60 Month)

53 A/F


CPCPREC53-00-810 Wing to Fuselage Integral Attachment at FS424.00 and BL45.00 - CPCP Check including the following items: (1) Wing to fuselage integral bolts / (2) Bolts, nuts and

safety pins (without removal of bolts)

5.8 Months (+30

Days)(26-Sep-2016)-/+16026-Sep-2011Mos

Hrs

Ldg

(PKG 60 Month)

53 A/F


CPCPREC53-00-811 Wing to Fuselage Integral Attachment at FS473.15 and BL45.00 - CPCP Check including the following items: (1) Wing to fuselage integral bolts / (2) Bolts, nuts and

safety pins (without removal of bolts)

5.8 Months (+30

Days)(26-Sep-2016)-/+16026-Sep-2011Mos

Hrs

Ldg

(PKG 60 Month)

53 A/F


CPCPREC53-00-812 Wing to Fuselage Integral Attachment at FS513.00 and BL13.00 and BL45.00 - CPCP Check including the following items: (1) Attachment frame at FS513.00 and BL13.00

/ (2) Frame flanges, webs / (3) Dragbrace fitting of the floor support beam / (4) Wing to fuselage lugs at BL45.00 / (5) Bolts, nuts and safety pins (without removal of

bolts)

5.8 Months (+30

Days)(26-Sep-2016)-/+16026-Sep-2011Mos

Hrs

Ldg

(PKG 60 Month)

53 A/F


CPCPREC53-00-813 Cabin Window Cut-Outs and Surround Structure FS364.00 to FS529.00 (FS364.00 to FS559.00 Post SB 601-0006) - CPCP Check including the following items: (1)

External skin around the window cut-outs (9 inches lateraland 20 inches vertical) / (2) Stringer runouts

5.8 Months (+30

Days)(26-Sep-2016)6026-Sep-2011Mos

Hrs

Ldg

(PKG 60 Month)

53 A/F


CPCPREC53-00-814 Fuselage External Skin Panels, FS621.00 to VS67.5% - CPCP Check including the following items: (1) Area Corresponding to Stringer 5 at VS55.62% / (2) Area

Corresponding to Stringer 0 at FS630.00 and (1) NLG drag strut / (2) NLG beam vertical stiffener clip / (3) NLG beam upper and lower caps / (4) Web and internal skin

of the wheel well


Hrs

Ldg

(PKG 48 Month)

53 A/F


CPCPREC53-00-815 Nose Landing Gear Wheel Well Structure - CPCP Check including the following items: (1) NLG drag strut / (2) NLG beam vertical stiffener clip / (3) NLG beam upper and

lower caps / (4) Web and internal skin of the wheel well


Hrs

Ldg

(PKG 48 Month)

53 A/F

(ZONE: 110, 240) (ACCESS: 711-AL-AR) (SOURCE: TLMC 05-30-20) (NOTE: This task can be done in conjunction with ScheduledMaintenance

Instruction Task 53−40−00−225.)

CPCPREC53-00-816 Tail Cone Assembly (Pre SB 601-0262) - CPCP Check including the following items: (1) Exterior surfaces and surrounding structure / (2) Interior surfaces / (3) Frames

and access doors

5.8 Months (+30

Days)(26-Sep-2016)-/+16026-Sep-2011Mos

Hrs

Ldg

(PKG 60 Month)

53 A/F



Generated: 6-Apr-2016 1:16 PM214/429







CPCPREC53-00-817 Nose Radome - CPCP Check including the following items: (1) Interior surface / (2) Attachments and (1) Floor beams, channels and joint channels / (2) Floor support

fittings and intercostals / (3) Floor plates, splices and doublers / (4) Profile plates floor attachment at bulkhead FS621.00

5.8 Months (+30

Days)(26-Sep-2016)-/+16026-Sep-2011Mos

Hrs

Ldg

(PKG 60 Month)

53 A/F

Ref.:PSP 607 51-54-153/3 (SOURCE: TLMC 05-30-20) (NOTE: [1] Remove insulation blankets. [2] Check for fluid spillage under galley and

lavatory. [3]This task can be done in conjunction with Scheduled Maintenance Instruction Task 53-50-11-227 and Task 53-10-11-230.)

CPCPREC53-00-818 Floor Structure, FS589.00 to FS621.00 - CPCP Check including the following items: (1) Floor beams, channels and joint channels / (2) Floor support fittings and

intercostals / (3) Floor plates, splices and doublers / (4) Profile plates floor attachment at bulkhead FS621.00

5.8 Months (+30

Days)(26-Sep-2016)-/+16026-Sep-2011Mos

Hrs

Ldg

(PKG 60 Month)

53 A/F

Ref.:PSP 607 51-54-153/3 (ZONE: 251, 252) (ACCESS: 151-DZ-EZ-FZ, 152-CZ-DZ) (SOURCE: TLMC 05-30-20) (NOTE: [1] Remove insulation

blankets.[2] Check for fluid spillage under galley and lavatory.[3] This task can be done in conjunction with ScheduledMaintenance Instruction

Task 53−10−11−230.)

CPCPREC53-00-819 Fuselage Structure (Internal), FS202.75 to FS621.00 below Floor - CPCP Check including the following items: (1) Aft face of web of bulkhead at FS202.75 / (2) Bulkhead

at FS280.00 / (3) Internal skins, frames, splices / (4) Stringers, longerons, brackets, cleats / (5) Forward face of bulkhead at FS621.00 / (6) Forward face of bulkhead at

FS409.00 / (7) Aft face of bulkhead at FS559.00

5.8 Months (+30

Days)26-Sep-2016-/+16026-Sep-2011Mos

Hrs

Ldg

53 A/F

Ref.:PSP 607 51-54-153/3 (SOURCE: TLMC 05-30-20) (NOTE: [1] Remove insulation blankets, do not remove lavatory. [2]This task can be done

in conjunction with Scheduled Maintenance Instruction Task 53-00-00-231.)

CPCPREC53-00-820 Fuselage Structure (Internal), FS202.75 to FS621.00 above Floor - CPCP Check including the following items: (1) Aft face of web of bulkhead FS202.75 / (2) Bulkhead

FS280.00 / (3) Internal skins, frames, splices / (4) Stringers, longerons, brackets, cleats / (5) Forward face of bulkhead FS621.00 / (6) Internal cabin windows surround

structure / (7) Internal overwing exit structure / (8) Passenger door internal surround structure / (9) Internal baggage door surround structure / (10) Internal antenna

cut-outs / (11) Area around sound dampening panels

5.8 Months (+30

Days)26-Sep-2016-/+112026-Sep-2006Mos

Hrs

Ldg

53 A/F

Ref.:PSP 607 51-54-153/3 (SOURCE: TLMC 05-30-20) (NOTE: [1] Do not remove self-adhesive sound damping. [2] This task can be done in

conjunction with Scheduled Maintenance Instruction Task 53-00-00-232. [3] Removal of furnishings and equipment may be required to

complete the check.)

CPCPREC53-00-821 Fuselage Structure (Internal), FS621.00 to VS67.5% - CPCP Check including the following items: (1) Aft face of web of bulkhead FS621.00 / (2) Bulkhead FS755.00 / (3)

Frame VS55.0%, forward face of frame VS67.5% / (4) Internal skins, frames, splices / (5) Stringers, longerons, brackets, cleats / (6) Aft equipment door internal

structure / (7) Engine support beam / (8) Transverse beam / (9) Intercostal / (10) Internal antenna cut-outs

5.8 Months (+30

Days)26-Sep-2016-/+16026-Sep-2011Mos

Hrs

Ldg

53 A/F

(SOURCE: TLMC 05-30-20) (NOTE: [1] Do not remove self-adhesive sound damping, [2] This task can be done in conjunction with Scheduled

Maintenance Instruction Task 53-00-00-233.)

CPCPREC53-00-822 Tail Cone (Post SB 601-0262) - CPCP Check including the following items: (1) Aft face of VS67.5% / (2) Forward bulkhead of tail tank / (3) Exterior skins and doors

5.8 Months (+30

Days)(26-Sep-2016)6026-Sep-2011Mos

Hrs

Ldg

(PKG 60 Month)

53 A/F

(SOURCE: TLMC 05-30-20) (NOTE: Use a borescope and monitor)

CPCPREC53-00-823 Floor Structure, FS169.00 to FS280.00 - CPCP Check including the following items: (1) Floor beams, channels and joint channels / (2) Floor support fittings, intercostals,

brackets and splices / (3) Flight compartment floor structure and central walkway

5.8 Months (+30

Days)(26-Sep-2016)-/+16026-Sep-2011Mos

Hrs

Ldg

(PKG 60 Month)

53 A/F

(SOURCE: TLMC 05-30-20) (NOTE: [1] Remove insulation blankets, carpets and seats. [2] Check for spillage under forward galley. [3] This task

can be done in conjunction with Scheduled Maintenance Instruction Task 53-10-11-230.)


Generated: 6-Apr-2016 1:16 PM215/429







CPCPREC53-00-824 Floor Structure, FS280.00 to FS424.00 - CPCP Check including the following items: (1) Floor beams, channels, beam plates and angles(2) Floor support fittings,

intercostals, struts and brackets(3) Floor sill structure (webs)(4) Pressure floor skin panels

5.8 Months (+30

Days)(26-Sep-2016)-/+16026-Sep-2011Mos

Hrs

Ldg

(PKG 60 Month)

53 A/F

Ref.:PSP 607 51-54-153/3 (SOURCE: TLMC 05-30-20) (NOTE: [1] Check for fluid spillage under forward galley. [2] This task can be done in

conjunction with ScheduledMaintenance Instruction Task 53-10-11-230.)

CPCPREC53-00-825 Floor Structure, FS424.00 to FS589.00 - CPCP Check including the following items: (1) Floor beams, channels and joint channels / (2) Floor support fittings and

intercostals / (3) Pressurized floor skin panel and flanged panels / (4) Pressure floor wing tie beam and longerons

5.8 Months (+30

Days)(26-Sep-2016)-/+16026-Sep-2011Mos

Hrs

Ldg

(PKG 60 Month)

53 A/F

Ref.:PSP 607 51-54-153/3 (SOURCE: TLMC 05-30-20) (NOTE: [1] Remove insulation blankets [2] Check for fluid spillage. If spillage is found,

removepanels 152-AZ/BZ [3] This task can be done in conjunction with Scheduled Maintenance Instruction Task 53-10-11-230)

CPCPREC53-00-826 Structure Adjacent to Overboard Lavatory Services (External) - CPCP Check including the following items: (1) Fuselage skin doubler (by looking through the splash

guard) / (2) Fuselage skin for 2 inches around the edge of the doubler

5.8 Months (+30

Days)(26-Sep-2016)-/+16026-Sep-2011Mos

Hrs

Ldg

(PKG 60 Month)

53 A/F


CPCPREC53-00-827 Fuselage Frame FS409.00, Aft Face, External - CPCP Check including the following items: (1) Bulkhead Web / (2) Frame Cap Members / (3) Machined Strap (Post SB 601-

0503)

5.8 Months (+30

Days)(26-Sep-2016)-/+16026-Sep-2011Mos

Hrs

Ldg

(PKG 60 Month)

53 A/F


MandatoryRE (-)CF-1997-16R2 Paragraph 1 Bombardier CL-600 "Challenger" - FS409 Bulkhead Fatigue Cracks, Detailed Visual Inspection

Mos

Hrs

Ldg

53 A/FEff: 15-Oct-1997

IsModSumT (A/R)IS600-53-0002 REV A Alternative CRES Fasteners for Door Assy Fwd Fuselage

Mos

Hrs

Ldg

53 A/F

▼ 54 - NACELLES/PYLONS

MRB ≈18-Sep-2016RE54-00-00-201 Nacelles/Pylons Visual Check - External

10-Feb-2016Mos

290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs

6,326Ldg

(PKG 300 Hour)

54 A/F


MRBRE54-00-00-202 Nacelles/Pylons (Pylon Structure) Visual Check - Internal

5.8 Months (+30

Days)(26-Sep-2016)-/+16024-Oct-2011Mos

Hrs

Ldg

(PKG 60 Month)

54 A/F


Also ConsiderDUE: (26-Sep-2016)1. RE 60 MosNacelles/Pylons, Internal (Pylon Structure) - CPCP CheckC54-00-802A/F54

AWL ≈09-Apr-2022T54-10-00-101 * Engine Supporting Beam Upper Cap - FS625.30 and BL38.00 - Visual Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

54 A/F



Generated: 6-Apr-2016 1:16 PM216/429







AWL ≈09-Apr-2022T54-10-00-102 * Pylon Spar/Fuselage Frame Attachment - FS672.20 - NDT Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

54 A/F


AWL ≈09-Apr-2022T54-10-00-103 * Pylon Spar Upper Cap - FS625.30 - NDT Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

54 A/F


AWL ≈09-Apr-2022T54-10-00-104 * Pylon Canted Rib - Upper Splice at FS672.20 - Visual Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

54 A/F


AWL ≈14-Mar-2040T54-10-00-106 * Rib Upper Cap, Skin and Doubler from FS672.20 to FS682.00 - NDT Check

Mos

Hrs

8,674 Ldg15,00015,000Ldg

54 A/F


AWL ≈09-Apr-2022T54-30-00-105 * Pylon Upper Skin - FS682.00 - Visual Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

54 A/F


RecommendedRE (-)601-0073 Modification - Pylon Structure - Panel Fasteners

Mos

Hrs

Ldg

54 A/FEff: 21-Jan-1986

RecommendedRE (-)601-0087 Modification - Pylon Firewall - Addition of Doubler

Mos

Hrs

Ldg

54 A/F

RecommendedT (A/R)601-0087 Rev 1 Modification - Pylon Firewall - Addition of Doubler

Mos

Hrs

Ldg

54 A/FEff: 30-Nov-1984

RecommendedRE (-)601-0462 Special Check/Rework – Aft Engine Mount Support Rib Fasteners

Mos

Hrs

Ldg

54 A/F

Nextdue Share EarliestDUE:1. RE -Special Check/Rework – Aft Engine Mount Support Rib Fastener...601-0462 Part AA/F54

Nextdue Share EarliestDUE:1. RE -Special Check/Rework – Aft Engine Mount Support Rib Fastener...601-0462 Part BA/F54

RecommendedRE (-)601-0462 Part A Special Check/Rework – Aft Engine Mount Support Rib Fasteners - Left Engine

Mos

Hrs

Ldg

54 A/FEff: 31-Oct-1995


Generated: 6-Apr-2016 1:16 PM217/429







RecommendedRE (-)601-0462 Part B Special Check/Rework – Aft Engine Mount Support Rib Fasteners - Right Engine

Mos

Hrs

Ldg

54 A/FEff: 31-Oct-1995

RecommendedRE (-)601-0462 Rev 1 Special Check/Rework – Aft Engine Mount Support Rib Fasteners

18-Nov-1996Mos

5,001Hrs

2,052Ldg


Nextdue Share EarliestDUE:1. T A/R | 2. RE -Special Check/Rework – Aft Engine Mount Support Rib Fastener...601-0462 Rev 1 Part AA/F54

Nextdue Share EarliestDUE:1. T A/R | 2. RE -Special Check/Rework – Aft Engine Mount Support Rib Fastener...601-0462 Rev 1 Part BA/F54

RecommendedT (A/R)601-0462 Rev 1 Part A Special Check/Rework – Aft Engine Mount Support Rib Fasteners - Left Engine

Mos

Hrs

Ldg

54 A/FEff: 14-Jun-1996

RecommendedT (A/R)601-0462 Rev 1 Part B Special Check/Rework – Aft Engine Mount Support Rib Fasteners - Right Engine

Mos

Hrs

Ldg

54 A/FEff: 14-Jun-1996

CPCPREC54-00-801 Nacelles/Pylons, External - CPCP Check

10 Months (+29

Days)(30-Jan-2017)-/+12430-Jan-2015Mos

Hrs

Ldg

(PKG 24 Month)

54 A/F


CPCPREC54-00-802 Nacelles/Pylons, Internal (Pylon Structure) - CPCP Check

5.8 Months (+30

Days)(26-Sep-2016)-/+16026-Sep-2011Mos

Hrs

Ldg

(PKG 60 Month)

54 A/F


MandatoryRE (-)CF-2015-09R1 Nacelle/Pylon – Non-conforming Bushing Holes on the Engine Mount Rib

Mos

Hrs

Ldg

54 A/FEff: 13-Jul-2015

IsModSumT (A/R)IS600-54-0001 REV A Pylon Trailing Edge Attachment Modification

Mos

Hrs

Ldg

54 A/F

▼ 55 - STABILIZERS

RE (O/C)Elevator Assy

20-Sep-1983Mos

0Hrs0

0Ldg0

Left55 A/FNew600-24025-1007

UNKNOWN

RE (O/C)Elevator Assy

20-Sep-1983Mos

0Hrs0

0Ldg0

Right55 A/FNew600-24025-1008

UNKNOWN


Generated: 6-Apr-2016 1:16 PM218/429







RE (O/C)Horizontal Assy Stabilizer

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Rudder Assy

20-Sep-1983Mos

0Hrs0

0Ldg0

55 A/FNew600-22000-1001

UNKNOWN

AWL ≈19-Apr-2025RE55-00-00-127 * Pitch Trim Actuator - Visual Check

11-Mar-2000Mos

4,411.7 Hrs16,452.910,0006,452.9Hrs

Ldg

55 A/F


MRB ≈18-Sep-2016RE55-00-00-201 Stabilizers Visual Check - External

10-Feb-2016Mos

290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs

6,326Ldg

(PKG 300 Hour)

55 A/F


AWL ≈09-Apr-2022T55-10-00-101 * Horizontal Stabilizer Rear Spar - Centerline Splice - Visual Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

55 A/F


AWL ≈23-Jul-2021RE55-10-00-102 * Horizontal Stabilizer Rear Spar Upper Cap at Rib 1, BL6.00 - NDT Check

19-Jul-2004Mos

2,617.1 Hrs14,658.34,20010,458.3Hrs

Ldg

55 A/F


AWL ≈09-Apr-2022T55-10-00-103 * Horizontal Stabilizer - Rear Spar Upper Cap and Splice - Visual Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

55 A/F


AWL ≈09-Apr-2022T55-10-00-104 * Horizontal Stabilizer Front Spar Upper Cap Splice - BL6.00 - NDT Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

55 A/F


AWL ≈09-Apr-2022T55-10-00-105 * Horizontal Stabilizer - Upper Stringer 1 - BL6.00 - Visual Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

55 A/F


AWL ≈09-Apr-2022T55-10-00-106 * Horizontal Stabilizer - Centerline Rib - Visual Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

55 A/F



Generated: 6-Apr-2016 1:16 PM219/429







MRBRE55-10-00-202 Horizontal Stabilizer Visual Check of the following items paying particular attention for cracks, and corrosion: (1) The rear spar splice on the left and right side

specifically,theweb attachments and the cap splice fittins / (2) The front spar splice on the left and right side specifically - the web in the area of the screw jack fitting -

the front and back faces of the web splice - the spar splice fittings and the attachment fitting which joins the web to the machined rib at BL6.00 (3) The visor fittings

10 Months (+29

Days)(30-Jan-2017)-/+12430-Jan-2015Mos

Hrs

Ldg

(PKG 24 Month)

55 A/F


Also ConsiderDUE: (30-Jan-2017)1. RE 48 MosHorizontal Stabilizer Front Spar - CPCP Check including the ...C55-00-806A/F55

MRBRE55-10-00-203 Horizontal Stabilizer Visual Check of the following items, paying particular attention for cracks and corrosion: (1) The rear spar web adjacent to the elevator hinge

fittings / (2) PCU support structure

5.8 Months (+30

Days)(26-Sep-2016)-/+16024-Oct-2011Mos

Hrs

Ldg

(PKG 60 Month)

55 A/F


Also ConsiderDUE: (26-Sep-2016)1. RE 60 MosHorizontal Stabilizer Rear Spar - CPCP Check including the f...C55-00-807A/F55

MRBRE55-10-00-204 Horizontal Stabilizer Visual Check - Internal - Structure at BL10.00L to BL10.00R

5.8 Months (+30

Days)(26-Sep-2016)-/+16024-Oct-2011Mos

Hrs

Ldg

(PKG 60 Month)

55 A/F


Also ConsiderDUE: (26-Sep-2016)1. RE 60 MosHorizontal Stabilizer Internal Structure - CPCP Check includ...C55-00-808A/F55

MRBRE55-10-00-205 Horizontal Stabilizer Visual Check of internal structure, complete


Hrs

Ldg

55 A/F


MRBRE55-10-11-206 Horizontal Stabilizer Visual Check (Upon removal of the inner pivot pin only) of the inner and outer pivot pins. Reinstall inner pivot pin

10 Months (+29

Days)(30-Jan-2017)-/+12430-Jan-2015Mos

Hrs

Ldg

(PKG 24 Month)

55 A/F


AWL ≈17-Oct-2020RE55-20-00-107 * Elevator/Horizontal Stabilizer PCU and Supporting Hinges - NDT Check

17-Nov-2000Mos

2,248.7 Hrs14,289.97,2007,089.9Hrs

Ldg

55 A/F


AWL ≈09-Apr-2022T55-20-00-108 * Elevator, Skin and Front Spar - Visual Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

55 A/F


MRB ≈18-Sep-2016RE55-20-00-207 Elevators and Rudder Visual Check - External

10-Feb-2016Mos

290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs

6,326Ldg

(PKG 300 Hour)

55 A/F


AWL ≈09-Apr-2022T55-30-00-109 * Vertical Stabilizer - Mid Spar Cap at Rib 1 - Visual Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

55 A/F



Generated: 6-Apr-2016 1:16 PM220/429







AWL ≈09-Apr-2022T55-30-00-110 * Vertical Stabilizer - Front Spar - Visual Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

55 A/F


AWL ≈09-Apr-2022T55-30-00-111 * Vertical Stabilizer - Front Spar Cap FS755.00 and WL137.50 - Visual Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

55 A/F


AWL ≈09-Apr-2022T55-30-00-112 * Vertical Stabilizer - Stringer Splice - Visual Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

55 A/F


AWL ≈09-Apr-2022T55-30-00-113 * Vertical Stabilizer - Stringer Splice - VS31.875% at Rib 2 and VS55.625% at Rib 3 - Visual Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

55 A/F


AWL ≈09-Apr-2022T55-30-00-114 * Vertical Stabilizer - Rear Spar - NDT Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

55 A/F

Ref.:PSP 612 Part 6 ET-55-30-03 Pre SB 601-0262, Ref.:PSP 612 Part TBD Post SB 601-0262 (SOURCE: TLMC 05-10-30)

AWL ≈09-Apr-2022T55-30-00-115 * Vertical Stabilizer - Front Spar Cap at Rib 1 - NDT Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

55 A/F


AWL ≈09-Apr-2022T55-30-00-116 * Vertical Stabilizer - Rear Spar Web at Rib 7 - Visual Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

55 A/F


AWL ≈09-Apr-2022T55-30-00-117 * Vertical Stabilizer - Front Spar Cap Splice Strap - NDT Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

55 A/F


AWL ≈09-Apr-2022T55-30-00-118 * Vertical Stabilizer - Access Hole - Skin Cut-Out - Visual Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

55 A/F


MRBRE55-30-00-209 Vertical Stabilizer Visual Check of the Canted Top Rib for cracks and corrosion, paying particular attention to: (1) the front spar attachment / (2) the mid spar

attachment / (3) the rear spar attachment / (4) the upper rear spar splice to the canted rib.

10 Months (+29

Days)(30-Jan-2017)-/+12430-Jan-2015Mos

Hrs

Ldg

(PKG 24 Month)

55 A/F



Generated: 6-Apr-2016 1:16 PM221/429







MRBRE55-30-00-210 Vertical Stabilizer Visual Check of the following items, paying particular attention for cracks and corrosion: (1) The rear spar frame assembly at FS815.00, specifically-

the web adjacent to the spar attachment - the spar caps - the fuselage skin adjacent to the spar caps. / (2) The front spar, specifically - the machined cruciform

attachment fittings at the sparbase - the spar web adjacent to the fitting - the splice with the vertical stabilizer cap rib the fuselage skin adjacent to the cruciform

fittin. / (3) Mid spar, specificall - the machined caps at the spar base - the spar web at the spar base, adjacent to the machined caps - the splice to the machined cap rib.

/ (4) Rear spar lower, specifically, the web and caps adjacent to the rudder hinge fittings / (5) The mid spar frame assembly at FS785.00, specifically - the web adjacent

to the rear attachment - the spar caps and the adjacent fuselage skin.

5.8 Months (+30

Days)(26-Sep-2016)-/+16024-Oct-2011Mos

Hrs

Ldg

(PKG 60 Month)

55 A/F


Also ConsiderDUE: (26-Sep-2016)1. RE 60 MosVertical Stabilizer Front Spar - CPCP Check including the fo...C55-00-802A/F55

Also ConsiderDUE: (26-Sep-2016)1. RE 60 MosVertical Stabilizer Internal Structure - CPCP Check includin...C55-00-803A/F55

AWL ≈22-Apr-2023RE55-40-00-119 * Rudder/Vertical Stabilizer Support and PCU Hinge Fittings - NDT Check

10-Sep-2001Mos

3,456.2 Hrs15,497.47,8007,697.4Hrs

Ldg

55 A/F


AWL ≈09-Apr-2022T55-40-00-120 * Rudder, Skin and Front Spar - Visual Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

55 A/F


AWL ≈09-Apr-2022T55-50-00-121 * Vertical Stabilizer Pitch Trim Actuator Pivot Lugs - NDT Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

55 A/F


AWL ≈09-Apr-2022T55-50-00-122 * Vertical Stabilizer/Horizontal Stabilizer Pivot Fitting - NDT Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

55 A/F


AWL ≈09-Apr-2022T55-50-00-123 * Horizontal Stabilizer - Pivot Fitting Lugs - Visual Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

55 A/F


AWL ≈09-Apr-2022T55-50-00-124 * Horizontal Stabilizer Bathtub Fittings - Visual Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

55 A/F


AWL ≈29-Dec-2030RE55-50-00-125 * Rudder - Hinge Bolts - Visual Check

05-Aug-2003Mos

7,144.4 Hrs19,185.69,6009,585.6Hrs

Ldg

55 A/F


AWL ≈29-Dec-2030RE55-50-00-126 * Elevator - Hinge Bolts - Visual Check

05-Aug-2003Mos

7,144.4 Hrs19,185.69,6009,585.6Hrs

Ldg

55 A/F



Generated: 6-Apr-2016 1:16 PM222/429







MRBRE55-50-00-211 Attachment Fittings Visual Check of Horizontal Stabilizer Pivot Fittings, paying particular attention between the fasteners on either side of the lugs

10 Months (+29

Days)(30-Jan-2017)-/+12430-Jan-2015Mos

Hrs

Ldg

(PKG 24 Month)

55 A/F


Also ConsiderDUE: (30-Jan-2017)1. RE 48 MosHorizontal and Vertical Stabilizer - CPCP Check including th...C55-00-809A/F55

MRBRE55-50-00-212 Attachment Fittings Visual Check of the vertical stabilizer pivot fittings, paying particular attention to: (1) The fitting lugs / (2) Integrity of the attachments / (3) The

adjacent web and cap of the vertical stabilizer top rib

10 Months (+29

Days)(30-Jan-2017)-/+12430-Jan-2015Mos

Hrs

Ldg

(PKG 24 Month)

55 A/F


Also ConsiderDUE: (30-Jan-2017)1. RE 48 MosHorizontal and Vertical Stabilizer - CPCP Check including th...C55-00-809A/F55

MRBRE55-50-00-213 Attachment Fittings Visual Check of Horizontal Stabilizer - Pitch Trim Actuator Fittings, paying particular attention to: (1) The ballscrew yoke, attachment / (2) The

fitting lugs / (3) Integrity of the fasteners / (4) Front spar web splice and backup fittings attached to theupper and lower horizontal stabilizer skins

10 Months (+29

Days)(30-Jan-2017)-/+12430-Jan-2015Mos

Hrs

Ldg

(PKG 24 Month)

55 A/F


Also ConsiderDUE: (30-Jan-2017)1. RE 48 MosVertical Stabilizer, Pitch Trim Actuator Attachment Structur...C55-00-804A/F55

Also ConsiderDUE: (30-Jan-2017)1. RE 48 MosHorizontal Stabilizer, Pitch Trim Actuator Attachment - CPCP...C55-00-810A/F55

MRBRE55-50-00-214 Attachment Fittings Visual Check of the vertical stabilizer to rudder center hinge fitting, paying particular attention to: (1) The lugs for elongation and wear / (2) The

integrity of the fitting attachments on both sides of the rear spar

11.9 Months (+31

Days)(28-Mar-2017)-/+13628-Mar-2014Mos

Hrs

Ldg

(PKG 36 Month)

55 A/F


Also ConsiderDUE: (28-Mar-2017)1. RE 36 MosVertical Stabilizer Rear Spar Structure - CPCP Check includi...C55-00-805A/F55

MRBRE55-50-00-215 Attachment Fittings Visual Check of the rudder actuator/hinge fitting, paying particular attention to: (1) The lugs for elongation and wear / (2) The integrity of the

fitting attachments on both sides of the rear spar

11.9 Months (+31

Days)(28-Mar-2017)-/+13628-Mar-2014Mos

Hrs

Ldg

(PKG 36 Month)

55 A/F


MRBRE55-50-00-216 Attachment Fittings Visual Check of the rudder attachment fittings, paying particular attention to: (1) The integral attachment fork end of each machined fitting / (2)

The stabilizer skin mounting support brackets and the adjacent skin

11.9 Months (+31

Days)(28-Mar-2017)-/+13628-Mar-2014Mos

Hrs

Ldg

(PKG 36 Month)

55 A/F


Also ConsiderDUE: (28-Mar-2017)1. RE 36 MosRudder External Skin, Structure and Attachments - CPCP Check...C55-00-812A/F55

MRBRE55-50-00-217 Attachment Fittings Visual Check of Hinge Fitting on Horizontal Stabilizer BL15.25, paying particular attention to: (1) The adjacent spar web / (2) The internal backup

fittings / (3) The fitting lugs for elongation and wear

11.9 Months (+31

Days)(28-Mar-2017)-/+13628-Mar-2014Mos

Hrs

Ldg

(PKG 36 Month)

55 A/F



Generated: 6-Apr-2016 1:16 PM223/429







MRBRE55-50-00-218 Attachment Fittings Visual Check of PCU Fittings, Horizontal Stabilizer, paying particular attention to the lugs of the elevator PCU

11.9 Months (+31

Days)(28-Mar-2017)-/+13628-Mar-2014Mos

Hrs

Ldg

(PKG 36 Month)

55 A/F


MRBRE55-50-00-219 Attachment Fittings Visual Check of PCU and Elevator, paying particular attention to the integritiy of fasteners, fitting lugs and the adjacent spar web

11.9 Months (+31

Days)(28-Mar-2017)-/+13628-Mar-2014Mos

Hrs

Ldg

(PKG 36 Month)

55 A/F


Also ConsiderDUE: (28-Mar-2017)1. RE 36 MosElevator External Skin, Structure and Attachments - CPCP Che...C55-00-813A/F55

MRB ≈24-Aug-2023RE55-50-00-220 Stabilizers Structure NDT Check of the vertical stabilizer to rudder hinge bolts for cracks

08-Aug-2005Mos

3,618.6 Hrs (+40)(15,659.8)-/+404,80010,859.8Hrs

Ldg

(PKG 4800 Hour)

55 A/F

Ref.:PSP 612 Part 8 PT-55-50-02 (SOURCE: TLMC 05-20-15) (NOTE: This check may be traded - off for bolt replacement if economically

justifiable or convenient.)

MRB ≈24-Aug-2023RE55-50-00-221 Stabilizers Structure NDT Check of the horizontal stabilizer to elevator hinge bolts for cracks

08-Aug-2005Mos

3,618.6 Hrs (+40)(15,659.8)-/+404,80010,859.8Hrs

Ldg

(PKG 4800 Hour)

55 A/F

Ref.:PSP 612 Part 8 PT-55-50-01 (SOURCE: TLMC 05-20-15) (NOTE: This check may be traded - off for bolt replacement if economically

justifiable or convenient.)

RecommendedRE (-)601-0116 Modification - Horiz/Stab to Vert/Stab Fairing - Drainage Provision and Corrosion Prevention

26-Jan-1987Mos

1,267Hrs

480Ldg

55 A/FComplied With

RecommendedT (A/R)601-0116 Rev 1 Modification - Horiz/Stab to Vert/Stab Fairing - Drainage Provision and Corrosion Prevention

Mos

Hrs

Ldg

55 A/FEff: 14-Jul-1986

RecommendedRE (-)601-0185 Special Check/Rework - Vertical Stabilizer - Missing Rivets

28-Mar-1989Mos

2,373Hrs

910Ldg

55 A/FComplied With

RecommendedT (A/R)601-0185 Rev 1 Special Check/Rework - Vertical Stabilizer - Missing Rivets

Mos

Hrs

Ldg

55 A/FEff: 21-May-1987

CPCPREC55-00-801 Vertical Stabilizer External Surfaces - CPCP Check including the following items: (1) Vertical Stabilizer External Surfaces


Hrs

Ldg

(PKG 48 Month)

55 A/F



Generated: 6-Apr-2016 1:16 PM224/429







CPCPREC55-00-802 Vertical Stabilizer Front Spar - CPCP Check including the following items: (1) Forward face of the front spar / (2) Front spar to fuselage attachment fittings / (3) Splice

straps / (4) Fuselage skin adjacent to spar caps

5.8 Months (+30

Days)(26-Sep-2016)-/+16026-Sep-2011Mos

Hrs

Ldg

(PKG 60 Month)

55 A/F


CPCPREC55-00-803 Vertical Stabilizer Internal Structure - CPCP Check including the following items: (1) Front, mid and rear spar / (2) Skins (internal), ribs and stringers / (3) Rudder PCU

support (backup) structure / (4) Stringer splices at VS31.87% and VS55.62%

5.8 Months (+30

Days)(26-Sep-2016)-/+16026-Sep-2011Mos

Hrs

Ldg

(PKG 60 Month)

55 A/F


CPCPREC55-00-804 Vertical Stabilizer, Pitch Trim Actuator Attachment Structure - CPCP Check including the following items: (1) Attachment lugs and fittings to vertical stabilizer / (2)

Vertical stabilizer skin around fittings / (3) Pitch trim actuator attachment bolts (without removal) / (4) Top canted rib


Hrs

Ldg

(PKG 48 Month)

55 A/F


CPCPREC55-00-805 Vertical Stabilizer Rear Spar Structure - CPCP Check including the following items: (1) Aft face of rear spar / (2) Hinge fittings and lugs / (3) Spar cap area at attachment

to fuselage / (4) Web at rib 1 area

11.9 Months (+31

Days)(28-Mar-2017)-/+13628-Mar-2014Mos

Hrs

Ldg

(PKG 36 Month)

55 A/F

(SOURCE: TLMC 05-30-20) (NOTE: [1] Deflect and secure rudder. [2] This task can be done in conjunction with Scheduled Maintenance

Instruction Task 55-50-00-214.)

CPCPREC55-00-806 Horizontal Stabilizer Front Spar - CPCP Check including the following items: (1) Front spar upper and lower cap and web / (2) Front spar splices / (3) Attachment

fittings of web to machined ribs / (4) Front spar covered by skin


Hrs

Ldg

(PKG 48 Month)

55 A/F


CPCPREC55-00-807 Horizontal Stabilizer Rear Spar - CPCP Check including the following items: (1) Rear spar upper and lower cap and web / (2) Rear spar splices / (3) Hinge fittings and

lugs

5.8 Months (+30

Days)(26-Sep-2016)-/+16026-Jan-2011Mos

Hrs

Ldg

(PKG 60 Month)

55 A/F


CPCPREC55-00-808 Horizontal Stabilizer Internal Structure - CPCP Check including the following items: (1) Upper and lower internal skins / (2) Internal upper and lower skin splices / (3)

Ribs and stringers / (4) Internal PCU support attachment fittings / (5) Backup fittings / (6) Centerline structure assembly

5.8 Months (+30

Days)(26-Sep-2016)-/+16026-Jan-2011Mos

Hrs

Ldg

(PKG 60 Month)

55 A/F


CPCPREC55-00-809 Horizontal and Vertical Stabilizer - CPCP Check including the following items: (1) Horizontal Stabilizer pivot fittings / (2) Vertical Stabilizer pivot fittings / (3) Vertical

Stabilizer skin around pivot fittings / (4) Pivot pins (without removal)


Hrs

Ldg

(PKG 48 Month)

55 A/F

(SOURCE: TLMC 05-30-20) (NOTE: This task can be done in conjunction with Scheduled Maintenance Instruction Task 55-50-00-211 and 55-50

-00-212.)


Generated: 6-Apr-2016 1:16 PM225/429







CPCPREC55-00-810 Horizontal Stabilizer, Pitch Trim Actuator Attachment - CPCP Check including the following items: (1) Attachment lugs and fittings / (2) Bathtub fittings / (3) Upper and

lower horizontal stabilizer skin splices


Hrs

Ldg

(PKG 48 Month)

55 A/F


CPCPREC55-00-811 Horizontal Stabilizer, External Surfaces - CPCP Check including the following items: (1) Upper and lower skin panels


Hrs

Ldg

(PKG 48 Month)

55 A/F


CPCPREC55-00-812 Rudder External Skin, Structure and Attachments - CPCP Check including the following items: (1) Rudder front spar assembly / (2) Hinge fittings and PCU attachments /

(3) Hinge attachment bolts (without removal)

11.9 Months (+31

Days)(28-Mar-2017)-/+13628-Mar-2014Mos

Hrs

Ldg

(PKG 36 Month)

55 A/F


CPCPREC55-00-813 Elevator External Skin, Structure and Attachments - CPCP Check including the following items: (1) Elevator front spar assembly / (2) Hinge and PCU attachment fittings

/ (3) Attachment bolts (without removal)

11.9 Months (+31

Days)(28-Mar-2017)-/+13628-Mar-2014Mos

Hrs

Ldg

(PKG 36 Month)

55 A/F

(SOURCE: TLMC 05-30-20) (NOTE: [1] Deflect and secure rudder [2] This task can be done in conjunction with Scheduled Maintenance

Instruction Task and 55-50-00-219.)

▼ 56 - WINDOWS

RE (O/C)Cabin Window

20-Sep-1983Mos

0Hrs

0Ldg



20-Sep-1983Mos

0Hrs

0Ldg



20-Sep-1983Mos

0Hrs

0Ldg



20-Sep-1983Mos

0Hrs

0Ldg



20-Sep-1983Mos

0Hrs

0Ldg



20-Sep-1983Mos

0Hrs

0Ldg



Generated: 6-Apr-2016 1:16 PM226/429








20-Sep-1983Mos

0Hrs

0Ldg



20-Sep-1983Mos

0Hrs

0Ldg



20-Sep-1983Mos

0Hrs

0Ldg



20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Cockpit Side Window

17-Jan-2004Mos

10,047.9Hrs

5,053Ldg

Left56 A/F600-33030-217867

RE (O/C)Cockpit Side Window

17-Jan-2004Mos

10,047.9Hrs

5,053Ldg

Right56 A/F600-33030-227800

RE (O/C)Windshield

07-Sep-2005Mos

10,813.8Hrs

5,509Ldg

Left56 A/F600-33030-259415

Component Inspection SimpleDUE: 12,262.7 Hrs1. RE 400 HrsWindshield - Functional Test of the windshield rain repellan...30-40-00-213A/F30

RE (O/C)Windshield

18-Dec-2014Mos

11,854.6Hrs363.5

Ldg


11030 REPAIR

Component Inspection SimpleDUE: 12,262.7 Hrs1. RE 400 HrsWindshield - Functional Test of the windshield rain repellan...30-40-00-213A/F30

AWL ≈03-May-2017RE56-10-00-101 * Side Window Glazings - Prism Checks - Visual Check

10-Feb-2016Mos

590.8 Hrs12,63260012,041.2Hrs

6,326Ldg

56 A/F

Ref.:PSP 612 Part 9 VC-56-10-01 (Tol. Adjustment: -9.2 Hrs) (SOURCE: TLMC 05-10-30)

AWL ≈20-Oct-2017RE56-10-00-102 * Windshield and Side Window Glazings - Prism Checks - Visual Check

29-Oct-2012Mos

812.3 Hrs12,853.51,20011,653.5Hrs

Ldg

56 A/F



Generated: 6-Apr-2016 1:16 PM227/429







AWL ≈24-Aug-2018RE56-10-00-104 * Windshield and Side Window ’T’ Plate Fasteners - NDT Check

08-Aug-2005Mos

1,218.6 Hrs13,259.82,40010,859.8Hrs

Ldg

56 A/F

Ref.:PSP 612 Part 8 PT-56-10-01 (SOURCE: TLMC 05-10-30) (NOTE: It is acceptable to replace the fasteners with new fasteners in lieu of this

inspection.)

AWL ≈24-Aug-2018RE56-10-00-105 * Windshield and Side Window Lower T-Caps - Visual Check

08-Aug-2005Mos

1,218.6 Hrs13,259.82,40010,859.8Hrs

Ldg

56 A/F


AWL ≈29-Dec-2030RE56-10-00-106 * Windshield and Side Window Glazing - All Fasteners - NDT Check of the fasteners for cracks. Pay particular attention to the first thread and directly underneath the

countersink head. NDT Check all fasteners attaching glazings to sill, centre post, side strap and end post

05-Aug-2003Mos

7,144.4 Hrs19,185.69,6009,585.6Hrs

Ldg

56 A/F

Ref.:PSP 612 Part 8 PT-56-10-02 (SOURCE: TLMC 05-10-30) (NOTE: It is acceptable to replace the fasteners with new fasteners in lieu of this

inspection.)

MRB ≈18-Sep-2016RE56-10-00-201 Flight Compartment Windows Visual Check - Internal and External, paying particular attention to the aerodynamic seal

10-Feb-2016Mos

290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs

6,326Ldg

(PKG 300 Hour)

56 A/F


OptionalRE (-)601-0006 Modification - Cabin Windows - Additional Installation

Mos

Hrs

Ldg

56 A/F

OptionalRE (-)601-0006 Rev 1 Modification - Cabin Windows - Additional Installation

Mos

Hrs

Ldg

56 A/F


Mos

Hrs

Ldg

56 A/F


Mos

Hrs

Ldg

56 A/F


Mos

Hrs

Ldg

56 A/F


Mos

Hrs

Ldg

56 A/F

OptionalT (A/R)601-0006 Rev 6 Modification - Cabin Windows - Additional Installation

Mos

Hrs

Ldg

56 A/FEff: 29-Apr-2013


Generated: 6-Apr-2016 1:16 PM228/429







RecommendedRE (-)601-0027 Modification - Terminal Block - Hardware Replacement

26-Jan-1987Mos

1,267Hrs

470Ldg

56 A/FComplied With

RecommendedT (A/R)601-0027 Rev 1 Modification - Terminal Block - Hardware Replacement

Mos

Hrs

Ldg

56 A/FEff: 03-Feb-1984

RecommendedRE (-)601-0030 Modification - Windshields/Side Windows - Warning Placard

Mos

Hrs

Ldg

56 A/F

RecommendedRE (-)601-0030 Rev 1 Modification - Windshields/Side Windows - Warning Placard

Mos

Hrs

Ldg

56 A/FEff: 15-Jan-1985

OptionalT (A/R)601-0059 Modification - Flight Compartment - Improved Access for Windshield Replacement

Mos

Hrs

Ldg

56 A/FEff: 15-Aug-1985

OptionalT (A/R)601-0572 Modification - Flight Compartment Windows - Installation of the Center Post Strip Assemblies

Mos

Hrs

Ldg

56 A/FEff: 13-Mar-2006

▼ 57 - WINGS

AWL - Life Limit ≈24-Apr-2026REAileron Anti-Float Spring

20-Sep-1983Mos

0Hrs0

3,674 Ldg10,00010,0000Ldg0

Left57 A/FNew600-10057-5

UNKNOWN

AWL - Life Limit ≈24-Apr-2026REAileron Anti-Float Spring

20-Sep-1983Mos

0Hrs0

3,674 Ldg10,00010,0000Ldg0


UNKNOWN

RE (O/C)Aileron Assy

20-Sep-1983Mos

0Hrs0

0Ldg0

Left57 A/FNew600-13000-811

UNKNOWN

RE (O/C)Aileron Assy

20-Sep-1983Mos

0Hrs0

0Ldg0

Right57 A/FNew600-13000-812

UNKNOWN

RE (O/C)Flap Inboard Vane Assy

20-Sep-1983Mos

0Hrs0

0Ldg0

Left57 A/FNew600-14302-3

UNKNOWN


Generated: 6-Apr-2016 1:16 PM229/429







RE (O/C)Flap Inboard Vane Assy

20-Sep-1983Mos

0Hrs0

0Ldg0


UNKNOWN

RE (O/C)Flight Spoiler

20-Sep-1983Mos

0Hrs0

0Ldg0

Left57 A/FNew600-10602-35

UNKNOWN

RE (O/C)Flight Spoiler

20-Sep-1983Mos

0Hrs0

0Ldg0

Right57 A/FNew600-10602-36

UNKNOWN

RE (O/C)Ground Spoiler

20-Sep-1983Mos

0Hrs0

0Ldg0

Left57 A/FNew600-10502-1

UNKNOWN

RE (O/C)Ground Spoiler

20-Sep-1983Mos

0Hrs0

0Ldg0


UNKNOWN

RE (O/C)Inboard Flap Assy

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Inboard Flap Assy

20-Sep-1983Mos

0Hrs

0Ldg


AWL - Life Limit ≈14-Mar-2025REInboard Flap Vane Support Beam

20-Sep-1983Mos

0Hrs0

3,274 Ldg9,6009,6000Ldg0

Left No.157 A/FNew600-14250-15

UNKNOWN


20-Sep-1983Mos

0Hrs0

3,274 Ldg9,6009,6000Ldg0

Left No.257 A/FNew600-14250-15

UNKNOWN


20-Sep-1983Mos

0Hrs0

3,274 Ldg9,6009,6000Ldg0

Left No.357 A/FNew600-14250-15

UNKNOWN


20-Sep-1983Mos

0Hrs0

3,274 Ldg9,6009,6000Ldg0

Right No.157 A/FNew600-14250-15

UNKNOWN


Generated: 6-Apr-2016 1:16 PM230/429








20-Sep-1983Mos

0Hrs0

3,274 Ldg9,6009,6000Ldg0

Right No.257 A/FNew600-14250-15

UNKNOWN


20-Sep-1983Mos

0Hrs0

3,274 Ldg9,6009,6000Ldg0

Right No.357 A/FNew600-14250-15

UNKNOWN

RE (O/C)Outboard Flap Assy

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Outboard Flap Assy

20-Sep-1983Mos

0Hrs

0Ldg


MandatoryRE (-)2014-03-17 Wings - fractured fastener heads found on the inboard flap hinge-box forward fitting at wing station (WS) 76.50

28-Mar-2014Mos

11,824.5Hrs

6,169Ldg

57 A/FBY INSPECTIONEff: 06-Mar-2014 Complied

With

Mandatory ≈29-Apr-2016RE2015-02-23 Wings

13-Nov-2015Mos

12,014.3Hrs

79 Ldg6,4051006,305Ldg

57 A/FBY INSPECTIONComplied With

Compliance Share DoubleDUE:1. T A/R | 2. RE -Special Check/Modification – Attachment Fittings – Inboard F...A601-0627 Rev 2A/F57

Mandatory ≈04-Oct-2020RE (-)2015-07-02 Wings

Mos

Hrs

1,674 Ldg[8,000]Ldg

57 A/FEff: 04-Jun-2015

Nextdue Share EarliestDUE:1. T 60 Days | 2. RE -Wings - Maintenance or Inspection Program Revision2015-07-02 Paragraph (g)A/F57

Nextdue Share EarliestDUE: 04-Jun-2019, 14,169 Ldg1. T 48 Mos, 7900 Ldg | 2. RE -Wings - Lug Edge Measurement and Inspection2015-07-02 Paragraph (h)(Inbd)A/F57

Nextdue Share EarliestDUE: 04-Jun-2019, 14,269 Ldg1. T 48 Mos, 8000 Ldg | 2. RE -Wings - Lug Edge Measurement and Inspection2015-07-02 Paragraph (h)(Outb)A/F57

Nextdue Share EarliestDUE:1. T A/R | 2. RE -Wings - Corrective Actions2015-07-02 Paragraph (i)A/F57

MandatoryRE (-)2015-07-02 Paragraph (g) Wings - Maintenance or Inspection Program Revision

21-Oct-2015Mos

12,001.1Hrs

6,291Ldg

57 A/FREVISED AMMEff: 04-Jun-2015 Complied

With

MandatoryT2015-07-02 Paragraph (h)

(Inbd)

Wings - Lug Edge Measurement and Inspection


Hrs

7,843 Ldg≈14,1697,900Ldg

57 A/FEff: 04-Jun-2015

(NOTE: Inboard Flaps having less than or equal to 7400 total flight cycles as of the effective date of this AD.)

Compliance Share DoubleDUE: 26-Sep-2017, 7,900 Ldg1. T 48 Mos | 2. RE -Special Check – Flap Hinge Box – Forward Lugs Edge to Edge D...601-0631A/F57


Generated: 6-Apr-2016 1:16 PM231/429







MandatoryT2015-07-02 Paragraph (h)

(Outb)

Wings - Lug Edge Measurement and Inspection


Hrs

7,943 Ldg≈14,2698,000Ldg

57 A/FEff: 04-Jun-2015

(NOTE: Outboard Flaps having equal to or less than 7500 total flight cycles as of the effective date of this AD.)

Compliance Share DoubleDUE: 26-Sep-2017, 7,900 Ldg1. T 48 Mos | 2. RE -Special Check – Flap Hinge Box – Forward Lugs Edge to Edge D...601-0631A/F57

MandatoryT (A/R)2015-07-02 Paragraph (i) Wings - Corrective Actions

Mos

Hrs

Ldg

57 A/FEff: 04-Jun-2015

MRB ≈30-Dec-2016RE57-00-00-202 Wing Structure Visual Check of leading edge external surface

05-Feb-2004Mos

426.1 Hrs (+40)12,467.3-/+402,40010,067.3Hrs

Ldg

(PKG 2400 Hour)

57 A/F


MRBRE57-00-00-203 Wing Structure Visual Check of the following areas: (1) Wing leading edges for Piccolo tube failure or evidence of internal structural damage (hot spots, discoloration,

distortion and loose rivets) / (2) Lower Plank external surface between wing stations WS148.00 and WS196.00 / (3) Lower Plank external surface between wing stations

WS247.00 and WS288.00 / (4) Outboard of wing station WS324.00 / (5) Wing trailing edge

6.6 Months (+31

Days)(21-Oct-2016)-/+11221-Oct-2015Mos

Hrs

Ldg

(PKG 12 Month)

57 A/F


Also ConsiderDUE: (21-Oct-2016)1. RE 24 MosWing Lower External Surface, BL0.00 to WS353.00 - CPCP Check...C57-00-802A/F57

MRBRE57-00-00-204 Wing Structure - Wing Box Visual Check of the following items, paying particular attention for cracks and corrosion: (1) Upper wing box skin in the area between the

front and rear spars and span wise from BL0.00 to WS148.00 / (2) Upper skin splice at BL0.00 and the adjacent skin / (3) The upper two span wise lap splices on either

side of the center wing plank / (4) The upper fasteners and adjacent areas / (5) Lower wing box skin in the area between the front and rear spars and span wise from

BL0.00 to WS148.00 / (6) Lower skin splice at BL0.00 and the adjacent skin / (7) The lower two span wise lap splices on either side of the center wing plank / (8) The

lower skin around inspection panels and water drains / (9) The lower fasteners and the adjacent areas

5.8 Months (+30

Days)(26-Sep-2016)-/+16024-Oct-2011Mos

Hrs

Ldg

(PKG 60 Month)

57 A/F


Also ConsiderDUE: (26-Sep-2016)1. RE 60 MosWing Upper Surface, BL0.00 to BL50.00 - CPCP Check: (1) Wing...C57-00-803A/F57

AWL ≈09-Apr-2022T57-10-00-101 * Lower Wing Plank and Rear Spar - WS45.00 and WS47.00 - NDT Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

57 A/F

Ref.:PSP 612 Part 2 RT-57-10-01 (SOURCE: TLMC 05-10-30)

AWL ≈20-Oct-2017RE57-10-00-102 * Lower Wing Plank - Rear Spar WS178.00 and WS189.00 - NDT Check

29-Oct-2012Mos

812.3 Hrs12,853.51,20011,653.5Hrs

Ldg

57 A/F


AWL ≈20-Oct-2017RE57-10-00-103 * Lower Wing Plank - Rear Spar at WS166.00 - NDT Check

29-Oct-2012Mos

812.3 Hrs12,853.51,20011,653.5Hrs

Ldg

57 A/F



Generated: 6-Apr-2016 1:16 PM232/429







AWL ≈09-Apr-2022T57-10-00-104 * Front Spar Web at Lower Wing Plank - WS45.00 - Visual Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

57 A/F


AWL ≈09-Apr-2022T57-10-00-106 * Front Spar Splice at the Lower Wing Plank - WS29.42 - Visual Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

57 A/F


AWL ≈24-Aug-2023T57-10-00-108 * Lower Wing Plank and Rear Spar at WS148.00 - Visual Check

29-Jun-2006Mos

3,618.6 Hrs15,659.84,80010,859.8Hrs

Ldg

57 A/F


AWL ≈29-Dec-2030RE57-10-00-109 * Wing Box - Internal Structure - Visual Check

05-Aug-2003Mos

7,144.4 Hrs19,185.69,6009,585.6Hrs

Ldg

57 A/F


AWL ≈09-Apr-2022T57-10-00-110 * Lower Wing Plank - Rear Spar - WS242.00 - Visual Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

57 A/F


AWL ≈09-Apr-2022T57-10-00-111 * Lower Wing Plank - Rear Spar at WS260.00 - NDT Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

57 A/F


AWL ≈09-Apr-2022T57-10-00-112 * Lower Wing Plank - Rear Spar at WS217.00 and WS222.00 - NDT Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

57 A/F


AWL ≈09-Apr-2022T57-10-00-113 * Rear Spar/Lower Wing Plank at WS219.00 - NDT Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

57 A/F

Ref.:PSP 612 Part 2 RT-57-10-02 (SOURCE: TLMC 05-10-30)

AWL ≈09-Apr-2022T57-10-00-114 * Lower Wing Plank - WS314.50, Butt Strap and Front Spar - Visual Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

57 A/F


AWL ≈09-Apr-2022T57-10-00-115 * Lower Wing Plank - WS315.00, Butt Strap and Rear Spar - Visual Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

57 A/F



Generated: 6-Apr-2016 1:16 PM233/429







MRBRE57-10-00-205 Main Frame (Wing Center Section Internal Structure) Visual Check

5.8 Months (+30

Days)(26-Sep-2016)-/+16024-Oct-2011Mos

Hrs

Ldg

(PKG 60 Month)

57 A/F


Also ConsiderDUE: (26-Sep-2016)1. RE 60 MosWing Structure Between the Front Spar and Rear Spar, BL0.00 ...C57-00-804A/F57

MRBRE57-10-00-206 Main Frame (Front Spar Splice WS29.42) Visual Check (Internal and External) of the area around the front spar splice, paying particular attention to the webs, caps,

splices, rib and fastener surround area

5.8 Months (+30

Days)(26-Sep-2016)-/+16024-Oct-2011Mos

Hrs

Ldg

(PKG 60 Month)

57 A/F


Also ConsiderDUE: (26-Sep-2016)1. RE 60 MosWing Front Spar, BL0.00 to WS50.00 - CPCP Check of the follo...C57-00-805A/F57

MRBRE57-10-00-207 Main Frame (Wing Inboard Box Internal Structure WS45.00 to WS65.70 and WS85.50 to WS106.00) Visual Check

5.8 Months (+30

Days)(26-Sep-2016)-/+16024-Oct-2011Mos

Hrs

Ldg

(PKG 60 Month)

57 A/F

(SOURCE: TLMC 05-20-15) (NOTE: If evidence of corrosion or other defects are found, progressively check the adjacent outboard tank cavity,

until a defect free area is located.)

Also ConsiderDUE: (26-Sep-2016)1. RE 60 MosWing Structure Between the Front Spar and Rear Spar, WS45.00...C57-00-806A/F57

MRBRE57-10-00-208 Main Frame (Wing Outboard Box Internal Structure WS148.00 to WS163.00 and WS199.00 to WS220.00) Visual Check

5.8 Months (+30

Days)(26-Sep-2016)-/+16024-Oct-2011Mos

Hrs

Ldg

(PKG 60 Month)

57 A/F

(SOURCE: TLMC 05-20-15) (NOTE: If evidence of corrossion or other defects are found, progressively check the adjacent outboard tank cavity,

until a defect free area is located)

MRBRE57-10-00-209 Main Frame (Rear Spar Splice at WS45.00) Visual Check (Internal and External) of the area around the rear spar splice, paying particular attention to the webs, caps,

splices,rib and fastener surround area

5.8 Months (+30

Days)(26-Sep-2016)-/+16024-Oct-2011Mos

Hrs

Ldg

(PKG 60 Month)

57 A/F


Also ConsiderDUE: (26-Sep-2016)1. RE 60 MosWing Rear Spar, BL0.00 to WS66.00 (External) - CPCP Check in...C57-00-807A/F57

AWL ≈10-Jan-2021RE57-20-00-116 * Wing Tip - External Surface - Visual Check

21-Oct-2015Mos

2,359.9 Hrs14,401.12,40012,001.1Hrs

Ldg

57 A/F


MRBRE57-20-00-210 Auxiliary Structure (Winglet) Visual Check (Internal and External), paying particular attention to front/rear spars and attachment to the wing

5.8 Months (+30

Days)(26-Sep-2016)-/+16024-Oct-2011Mos

Hrs

Ldg

(PKG 60 Month)

57 A/F


Also ConsiderDUE: (26-Sep-2016)1. RE 60 MosWingtip/Winglet Assembly (Internal/External) - CPCP Check in...C57-00-808A/F57


Generated: 6-Apr-2016 1:16 PM234/429







MRBRE57-20-00-211 Auxiliary Structure Visual Check of Wing Trailing Edge and Wing Leading Edge internal structure

5.8 Months (+30

Days)(26-Sep-2016)-/+16024-Oct-2011Mos

Hrs

Ldg

(PKG 60 Month)

57 A/F


Also ConsiderDUE: (26-Sep-2016)1. RE 60 MosWing Rear Spar and Auxiliary Spar, WS50.00 to WS353.00 - CPC...C57-00-809A/F57

Also ConsiderDUE: (26-Sep-2016)1. RE 60 MosWing Rear Spar and Auxiliary Spar, WS66.00 to WS148.00 - CPC...C57-00-811A/F57

AWL ≈20-Jan-2024T57-30-00-117 * Lower Center Wing Plank - WS65.00, Stringers 14 and 15 - NDT Check

29-Oct-2012Mos

3,812.3 Hrs15,853.54,20011,653.5Hrs

Ldg

57 A/F


AWL ≈20-Oct-2017RE57-30-00-118 * Lower Wing Plank Near Main Landing Gear Trunnion - WS65.75 - NDT Check

29-Oct-2012Mos

812.3 Hrs12,853.51,20011,653.5Hrs

Ldg

57 A/F


AWL ≈20-Oct-2017RE57-30-00-119 * Lower Wing Plank - Auxiliary Spar Access Hole at WS85.00 - NDT Check

29-Oct-2012Mos

812.3 Hrs12,853.51,20011,653.5Hrs

Ldg

57 A/F


AWL ≈03-May-2017RE57-30-00-120 * Lower Wing Plank - WS88.00, Between Stringers 14 and 15 - Visual Check

25-Jul-2008Mos

590.8 Hrs12,6321,20011,432Hrs

Ldg

57 A/F


AWL ≈20-Oct-2017RE57-30-00-121 * Lower Center Wing Plank at WS45.00 - Stringers 14 and 15, Center and Forward Splice - NDT Check

29-Oct-2012Mos

812.3 Hrs12,853.51,20011,653.5Hrs

Ldg

57 A/F


AWL ≈20-Jan-2024T57-30-00-122 * Lower Center Wing Plank - WS65.00, Stringer 10 - NDT Check

29-Oct-2012Mos

3,812.3 Hrs15,853.54,20011,653.5Hrs

Ldg

57 A/F


AWL ≈03-May-2017RE57-30-00-124 * Lower Center Wing Plank - WS45.00, Stringer 10 - NDT Check

25-Jul-2008Mos

590.8 Hrs12,6321,20011,432Hrs

Ldg

57 A/F


AWL ≈20-Oct-2032T57-30-00-125 * Lower Wing Planks - WS45.00, Stringers 15 and 16 - NDT Check

29-Oct-2012Mos

8,012.3 Hrs20,053.58,40011,653.5Hrs

Ldg

57 A/F


AWL ≈20-Oct-2017RE57-30-00-126 * Wing Upper Cover - Visual Check

29-Oct-2012Mos

812.3 Hrs12,853.51,20011,653.5Hrs

Ldg

57 A/F



Generated: 6-Apr-2016 1:16 PM235/429







AWL ≈20-Oct-2017RE57-30-00-127 * Lower Wing Plank - Aft Edge - WS163.00 to WS170.50 - NDT Check

29-Oct-2012Mos

812.3 Hrs12,853.51,20011,653.5Hrs

Ldg

57 A/F


AWL ≈20-Oct-2017RE57-30-00-128 * Lower Wing Planks - WS86.00, Stringers 14 to 17 - NDT Check

29-Oct-2012Mos

812.3 Hrs12,853.51,20011,653.5Hrs

Ldg

57 A/F


AWL ≈09-Apr-2022T57-30-00-129 * Lower Wing Planks - WS163.00, Stringer 15 - NDT Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

57 A/F


AWL ≈09-Apr-2022T57-30-00-130 * Lower Wing Plank - WS148.00, Stringer 19 - NDT Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

57 A/F

Ref.:PSP 612 Part 2 RT-57-30-01 (SOURCE: TLMC 05-10-30) (NOTE: Post SB 601-0280)

AWL ≈09-Apr-2022T57-30-00-131 * Lower Wing Plank - Centerline Splice, Stringers 15 and 16 - Visual Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

57 A/F


AWL ≈09-Apr-2022T57-30-00-132 * Lower Wing Plank - WS94.00, Stringer 23 - Visual Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

57 A/F



Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

57 A/F


AWL ≈09-Apr-2022T57-30-00-134 * Lower Wing Plank - WS106.40, Stringers 15 and 16 - Visual Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

57 A/F



Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

57 A/F



Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

57 A/F



Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

57 A/F



Generated: 6-Apr-2016 1:16 PM236/429








Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

57 A/F


AWL ≈03-Feb-2021T57-30-00-139 * Lower Wing Plank - WS148.00, Stringers 8 and 9 - NDT Check

25-Jul-2008Mos

2,390.8 Hrs14,4323,00011,432Hrs

Ldg

57 A/F


AWL ≈03-Feb-2021T57-30-00-140 * Lower Center Wing Plank - WS148.00, Stringer 15 - NDT Check

25-Jul-2008Mos

2,390.8 Hrs14,4323,00011,432Hrs

Ldg

57 A/F


AWL ≈03-Aug-2018RE57-30-00-141 * Lower Center Wing Panel - Access Hole, WS112.00, Stringer 10 - NDT Check

25-Jul-2008Mos

1,190.8 Hrs13,2321,80011,432Hrs

Ldg

57 A/F


AWL ≈24-May-2017RE57-30-00-142 * Fuel Tank Water Drain Port - WS48.00, Stringer 17 - Visual Check

08-Aug-2005Mos

618.6 Hrs12,659.81,80010,859.8Hrs

Ldg

57 A/F


AWL ≈03-Aug-2018RE57-30-00-143 * Lower Center Wing Plank - Access Hole, WS220.00,Stringer 10 - NDT Check

25-Jul-2008Mos

1,190.8 Hrs13,2321,80011,432Hrs

Ldg

57 A/F



Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

57 A/F


AWL ≈10-Jan-2036T57-30-00-150 * Lower Forward Wing Plank - WS65.75, Stringer 17 - NDT Check

21-Oct-2015Mos

9,559.9 Hrs21,601.19,60012,001.1Hrs

Ldg

57 A/F


AWL ≈09-Apr-2022T57-30-00-153 * Lower Aft Wing Plank at the Rear Spar Between WS59.00 and WS65.75 - NDT Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

57 A/F



Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

57 A/F


AWL ≈09-Apr-2022T57-30-00-156 * Lower Wing Plank - WS242.00 Inboard/Outboard and WS238.00, Stringer 16 - Visual Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

57 A/F



Generated: 6-Apr-2016 1:16 PM237/429








Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

57 A/F


AWL ≈09-Apr-2022T57-30-00-160 * Lower Wing Plank Centerline Splice Between Stringer 8 and Stringer 9 - Visual Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

57 A/F



Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

57 A/F


MRB ≈30-Dec-2016RE57-30-00-212 Plates/Skins (Upper Wing Box) Visual Check - External

05-Feb-2004Mos

426.1 Hrs (+40)12,467.3-/+402,40010,067.3Hrs

Ldg

(PKG 2400 Hour)

57 A/F


MRBRE57-30-00-213 Plates/Skins (Wing Box Lower Skin BL0.00 to WS148.00) Visual Check - External

6.6 Months (+31

Days)(21-Oct-2016)-/+11221-Oct-2015Mos

Hrs

Ldg

(PKG 12 Month)

57 A/F


Also ConsiderDUE: (21-Oct-2016)1. RE 60 MosWing Upper External Surface, WS50.00 to WS353.00 - CPCP Chec...C57-00-819A/F57

AWL - Repair ≈14-Feb-2017RE57-30-00-401 Wing Fuel Access Holes (NDT and Visual Check)

25-Jul-2008Mos

485.8 Hrs12,5271,09511,432Hrs

Ldg

57 A/F

Ref.:PSP 612 Part 6 ET-57-30-20, Ref.:PSP 612 Part 9 VC-57-30-45 (ZONE: 500) (ACCESS: 140-DL,550-GB) (SOURCE: TLMC 5-10-25)

AWL - Repair ≈20-Sep-2017RE57-30-00-401 Wing Fuel Access Holes (NDT and Visual Check)

25-Jul-2008Mos

773.8 Hrs12,8151,38311,432Hrs

Ldg

57 A/F

Ref.:PSP 612 Part 6 ET-57-30-20, Ref.:PSP 612 Part 9 VC-57-30-45 (ZONE: 500,600,) (ACCESS: 540-BB-CB-DB-EB-FB-GB,550-AB-BB-DB-EB-

FB,140-DR-ER) (SOURCE: TLMC 5-10-25) (NOTE: Additional Aceess Panel: 640-AB-FB-GB,650-AB-CB-FB-GB-HB)

AWL - Repair ≈13-Apr-2016RE57-30-00-401 Wing Fuel Access Holes (NDT and Visual Check)

26-Dec-2007Mos

84.1 Hrs12,125.394111,184.3Hrs

Ldg

57 A/F

Ref.:PSP 612 Part 6 ET-57-30-20, Ref.:PSP 612 Part 9 VC-57-30-45 (ZONE: 500,600) (ACCESS: 550-CB,650-BB-DB-EB) (SOURCE: TLMC 5-10-25)

AWL - Repair ≈16-Nov-2016RE57-30-00-401 Wing Fuel Access Holes (NDT and Visual Check)

02-Apr-2005Mos

367.8 Hrs12,4091,69110,718Hrs

Ldg

57 A/F

Ref.:PSP 612 Part 6 ET-57-30-20, Ref.:PSP 612 Part 9 VC-57-30-45 (ZONE: 600,) (ACCESS: 650-CB) (SOURCE: TLMC 5-10-25)

AWL - Repair ≈04-Dec-2016RE57-30-00-402 Fuel Tank Water Drain Holes (Visual Check) Wing Station: 244.0

25-Jul-2008Mos

391.8 Hrs12,4331,00111,432Hrs

Ldg

57 A/F

Ref.:PSP 612 Part 9 VC-57-30-41 (ZONE: 500) (ACCESS: 550-DB) (SOURCE: TLMC 5-10-25)


Generated: 6-Apr-2016 1:16 PM238/429







AWL - Repair ≈08-Jun-2017RE57-30-00-402 Fuel Tank Water Drain Holes (Visual Check)Wing Station: 48.0,68.7,88.5,151.0

25-Jul-2008Mos

637.8 Hrs12,6791,24711,432Hrs

Ldg

57 A/F

Ref.:PSP 612 Part 9 VC-57-30-41 (ZONE: 500,600) (ACCESS: 640-BB,540-DB,540-EB,550-AB) (SOURCE: TLMC 5-10-25)

≈10-Nov-2016RE57-30-00-407 Wing Lower Plank/Rear Spar, LBL42.5-38

Mos

359.8 Hrs12,40112,401Hrs

Ldg

57 A/F

AWL ≈14-Mar-2040T57-40-00-163 * Inboard Flap - Forward Attachment Fittings - Visual Check

Mos

Hrs

8,674 Ldg15,00015,000Ldg

57 A/F

Ref.:PSP 612 Part 9 VC-57-40-01 (SOURCE: TLMC 05-10-30) (NOTE: Post SB A601-0135)

AWL ≈14-Mar-2040T57-40-00-165 * Outboard Flap Arm - Forward Upper Lugs, WS220.00 - NDT Check

Mos

Hrs

8,674 Ldg15,00015,000Ldg

57 A/F


AWL ≈14-Mar-2040T57-40-00-166 * Inboard Flap - Flap Arm Lower Lugs - NDT Check

Mos

Hrs

8,674 Ldg15,00015,000Ldg

57 A/F


AWL ≈14-Mar-2040T57-40-00-167 * Outboard Flap Wing/Hinge Box Forward Fitting - NDT Check

Mos

Hrs

8,674 Ldg15,00015,000Ldg

57 A/F


AWL ≈14-Mar-2040T57-40-00-168 * Outboard Flap-Vane Support Fittings - Flap Stations 189.57, 235.84 and 280.66 - Visual Check

Mos

Hrs

8,674 Ldg15,00015,000Ldg

57 A/F


AWL ≈22-Jan-2022RE57-40-00-171 * Flight Spoilers Wing/Hinge Attachment Points - NDT Check

08-Apr-2015Mos

2,855.9 Hrs14,897.13,00011,897.1Hrs

Ldg

57 A/F


AWL ≈14-Mar-2040T57-40-00-172 * Outboard Flap - Hinge Box Lower Flange Supports - NDT Check

Mos

Hrs

8,674 Ldg15,00015,000Ldg

57 A/F


AWL ≈14-Mar-2040T57-40-00-173 * Inboard Flap - Forward Attachment Lugs - NDT Check

Mos

Hrs

8,674 Ldg15,00015,000Ldg

57 A/F


AWL ≈29-Jun-2018RE57-40-00-174 * Inboard Flap - Hinge Supports Part Numbers 600-10116-13 and 600-10117-13 - NDT Check

24-Oct-2011Mos

Hrs

859 Ldg7,1851,2005,985Ldg

57 A/F



Generated: 6-Apr-2016 1:16 PM239/429







AWL ≈04-Oct-2020T57-40-00-175 * Outboard Flap - Hinge Box Forward Attachment Lugs - NDT Check

Mos

Hrs

1,674 Ldg8,0008,000Ldg

57 A/F

Ref.:PSP 612 Part 6 ET-57-40-10 Part B (SOURCE: TLMC 05-10-30)

AWL ≈24-Dec-2017T57-40-00-178 * Inboard Flap - WS127.25 Wing Rib Backup Fitting - NDT Check

Mos

Hrs

674 Ldg7,0007,000Ldg

57 A/F


AWL ≈10-Apr-2032RE57-40-00-179 * Wing to Fuselage Attachment Fitting Lugs FS424.00 and BL45.00 - Visual Check

21-Oct-2015Mos

7,759.9 Hrs19,801.17,80012,001.1Hrs

Ldg

57 A/F


AWL ≈14-Mar-2040T57-40-00-180 * Inboard Flap - Vane Carriages - NDT Check

Mos

Hrs

8,674 Ldg15,00015,000Ldg

57 A/F


AWL ≈09-Apr-2022T57-40-00-183 * Wing/Fuselage Attachment Fitting Lugs, FS473.00 and BL45.00, FS513.00 and BL45.00, FS513.00 and BL13.50 - Visual Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

57 A/F


AWL ≈29-Dec-2030RE57-40-00-189 * Aileron - Hinge Bolts - Visual Check

05-Aug-2003Mos

7,144.4 Hrs19,185.69,6009,585.6Hrs

Ldg

57 A/F


AWL ≈14-Mar-2040T57-40-00-198 * Flap Hinge Bolt Attachments - NDT Check

Mos

Hrs

8,674 Ldg15,00015,000Ldg

57 A/F

Ref.:PSP 612 Part 8 PT-57-40-01 (SOURCE: TLMC 05-10-30)

AWL ≈29-Dec-2030RE57-40-00-199 * Flight Spoiler - Hinge Bolts - Visual Check

05-Aug-2003Mos

7,144.4 Hrs19,185.69,6009,585.6Hrs

Ldg

57 A/F


MRB ≈30-Dec-2016RE57-40-00-214 Attachment Fittings - Main Gear Side Brace (MLG Actuator Pickup) Visual Check of structure, paying particular attention to the following items: (1) The wing upper aft

panel and intercostal for deterioration of protective treatments / (2) The wing to fuselage attachment lug / (3) The area surrounding actuator bolt holes / (4) The

fasteners for looseness / (5) The area adjacent to the fasteners / (6) The adjacent spar web and the upper wing skin

05-Feb-2004Mos

426.1 Hrs (+40)12,467.3-/+402,40010,067.3Hrs

Ldg

(PKG 2400 Hour)

57 A/F


MRB ≈24-Aug-2023RE57-40-00-215 Wing Structure NDT Check of wing to aileron hinge bolts for cracks

05-Aug-2005Mos

3,618.6 Hrs (+40)(15,659.8)-/+404,80010,859.8Hrs

Ldg

(PKG 4800 Hour)

57 A/F

Ref.:PSP 612 Part 8 PT-57-40-02 (SOURCE: TLMC 05-20-15) (NOTE: This check may be traded-off for bolt replacement ifeconomically justifiable

or convenient.)


Generated: 6-Apr-2016 1:16 PM240/429







MRB ≈24-Aug-2023RE57-40-00-216 Wing to Flap Hinge Bolts NDT Check

08-Aug-2005Mos

3,618.6 Hrs (+40)(15,659.8)-/+404,80010,859.8Hrs

Ldg

(PKG 4800 Hour)

57 A/F

Ref.:PSP 612 Part 8 PT-57-40-03 (SOURCE: TLMC 05-20-15) (NOTE: This check may be traded-off for bolt replacement ifeconomically justifiable

or convenient.)

MRBRE57-40-00-217 Attachment Fittings (Main Gear Trunnion) Visual Check (as externally visible) by gaining access through the MLG bay and trailing edge structure with the flaps

extended, paying particular attention to the following items: (1) Integrity of the area surrounding fastener holes / (2) Auxiliary and rear spar splices to the trunnion

fitting (looking for distortion in the spars) / (3) The area surrounding the bushing

5.8 Months (+30

Days)(26-Sep-2016)-/+16024-Oct-2011Mos

Hrs

Ldg

(PKG 60 Month)

57 A/F


MRBRE57-40-00-218 Attachment Fittings (Wing to Fuselage Attach Assembly FS424.00, FWD) Visual Check assembly as visible, paying particular attention to the following items: (1)

Deterioration of protective treatments / (2) The area surrounding the fastener holes / (3) The wing to fuselage attachment lug

5.8 Months (+30

Days)(26-Sep-2016)-/+16024-Oct-2011Mos

Hrs

Ldg

(PKG 60 Month)

57 A/F


Also ConsiderDUE: (26-Sep-2016)1. RE 60 MosWing to Fuselage Attachment Fitting, FS424.00 and BL45.00 - ...C57-00-812A/F57

MRBRE57-40-00-219 Attachment Fittings (Wing to Fuselage Attachment Fitting FS473.15, Center) Visual Check assembly as visible, paying particular attention tothe following items: (1)

Deterioration of protective treatments / (2) Integrity of bolt hole surround areas / (3) Wing to fuselage attachment lug

5.8 Months (+30

Days)(26-Sep-2016)-/+16024-Oct-2011Mos

Hrs

Ldg

(PKG 60 Month)

57 A/F


Also ConsiderDUE: (26-Sep-2016)1. RE 60 MosWing to Fuselage Attachment Fitting, FS473.15 and BL45.00 - ...C57-00-813A/F57

MRBRE57-40-00-220 Attachment Fittings (Hinge/Actuator Aileron) Visual Check (Upon removal of the upper and lower aerodynamic seals), paying particular attention to the following

items: (1) Deterioration of protective treatments / (2) The area of the hinge and actuator bolt holes / (3) Wear in the hinge and actuator attachment fitting bolt holes

5.8 Months (+30

Days)(26-Sep-2016)-/+16024-Oct-2011Mos

Hrs

Ldg

(PKG 60 Month)

57 A/F


MRBRE57-40-00-221 Attachment Fittings (Flap Hinges) Visual Check (Upon extension of the flaps) of the hinge arm assembly, paying particular attention to the following items: (1) The

hinge arm attachment point on the flap surface / (2) The area surrounding the clevis pin / (3) The area adjacent to the fasteners on the machined plates ofthe hinge

arm / (4) Wear of the clevis pin and bolt holes of the flap hinge arm attachment points

5.8 Months (+30

Days)(26-Sep-2016)-/+16024-Oct-2011Mos

Hrs

Ldg

(PKG 60 Month)

57 A/F


Also ConsiderDUE: (26-Sep-2016)1. RE 60 MosOutboard Flap (External) - CPCP Check including the followin...C57-00-814A/F57

AWL ≈24-Jun-2020T57-40-01-101 * Inboard Flap - Hinge Box Forward Lugs - NDT Check

Mos

Hrs

1,574 Ldg7,9007,900Ldg

57 A/F

Ref.:PSP 612 Part 6 ET-57-40-10 Part A (SOURCE: TLMC 05-10-30)


Generated: 6-Apr-2016 1:16 PM241/429







MRBRE57-50-00-222 Flight Control Surfaces (Ailerons, Spoilers and Flaps) Visual Check of the external surfaces of Ailerons, Spoilers, Inboard Flaps and Outboard Flaps. Inspect for condition

of external surfaces as well as externally visible flaws indicating damage in the internal structure

5.8 Months (+30

Days)(26-Sep-2016)-/+16024-Oct-2011Mos

Hrs

Ldg

(PKG 60 Month)

57 A/F


Also ConsiderDUE: (26-Sep-2016)1. RE 60 MosInboard Flap (External) - CPCP Check including the following...C57-00-815A/F57

Also ConsiderDUE: (26-Sep-2016)1. RE 60 MosAileron (External) - CPCP Check including the following item...C57-00-817A/F57

Also ConsiderDUE: (26-Sep-2016)1. RE 60 MosFlight Spoiler (External) - CPCP Check including the followi...C57-00-818A/F57

AWL ≈23-Apr-2020RE57-51-00-186 * Ailerons - Visual Check

10-Aug-2004Mos

2,017.1 Hrs14,058.33,60010,458.3Hrs

Ldg

57 A/F


AWL ≈09-Apr-2022T57-51-00-187 * Ailerons - Upper and Lower Skin and Front Spar - Visual Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

57 A/F


AWL ≈14-Jul-2023T57-53-00-161 * Outboard Flap-Vane Support Struts - Flap Stations 171.94 and 296.00 - NDT Check

Mos

Hrs

2,674 Ldg9,0009,000Ldg

57 A/F


AWL ≈14-Mar-2040T57-53-00-164 * Outboard Flap-Vane Intermediate Support - Flap Stations 209.39 and 254.96 - NDT Check

Mos

Hrs

8,674 Ldg15,00015,000Ldg

57 A/F

Ref.:PSP 612 Part 4 UT-57-53-01, Ref.:PSP 612 Part 6 ET-57-53-09 (SOURCE: TLMC 05-10-30)

AWL ≈14-Mar-2040T57-53-00-176 * Outboard Flap-Vane Intermediate Support Fittings - Flap Stations 209.39 and 254.96 - NDT Check

Mos

Hrs

8,674 Ldg15,00015,000Ldg

57 A/F


AWL ≈14-Mar-2040T57-53-00-181 * Outboard Flap-Vane End Ramps - Flap Stations 171.94 and 296 - NDT Check

Mos

Hrs

8,674 Ldg15,00015,000Ldg

57 A/F


AWL ≈14-Mar-2040T57-53-00-182 * Outboard Flap - Forward Lugs - NDT Check

Mos

Hrs

8,674 Ldg15,00015,000Ldg

57 A/F


AWL ≈04-Feb-2029T57-53-00-190 * Inboard Flap - Front Spar - Visual Check

Mos

Hrs

4,674 Ldg11,00011,000Ldg

57 A/F


AWL ≈21-Apr-2031T57-53-00-191 * Inboard Flap - Vane Support Attachment Brackets - NDT Check

05-Aug-2003Mos

Hrs

5,471 Ldg11,7977,0004,797Ldg

57 A/F

Ref.:PSP 612 Part 6 ET-57-53-01 (SOURCE: TLMC 05-10-30) (NOTE: Post SB A601-0532 with: (1) No gaps/cracks at original bracket)


Generated: 6-Apr-2016 1:16 PM242/429







AWL ≈24-Apr-2026T57-53-00-192 * Outboard Flap-Vane Tangs (End Support) - Flap Stations 189.57, 235.84 and 280.66 - NDT Check

Mos

Hrs

3,674 Ldg10,00010,000Ldg

57 A/F


AWL ≈24-Apr-2026T57-53-00-194 * Outboard Flap - Front Spar - NDT Check

Mos

Hrs

3,674 Ldg10,00010,000Ldg

57 A/F


MRB ≈30-Dec-2016RE57-53-00-224 Flaps (Inboard Flap Vane Assembly) Visual Check (Upon removal of the lower access panels) of each of the vane actuating assemblies. Reinstall lower access panels.

05-Feb-2004Mos

426.1 Hrs (+40)12,467.3-/+402,40010,067.3Hrs

Ldg

(PKG 2400 Hour)

57 A/F


AWL ≈09-Apr-2022T57-55-00-197 Flight Spoiler - Upper and Lower Skin - Visual Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

57 A/F


RecommendedRE (-)601-0013 Modification - Rear Spar Bute Door Area - Fastener Substitution

Mos

Hrs

Ldg

57 A/F

RecommendedRE (-)601-0013 Rev 1 Modification - Rear Spar Bute Door Area - Fastener Substitution

Mos

Hrs

Ldg

57 A/FEff: 24-Oct-1984

RecommendedRE (-)601-0025 Special Check/Modification - Outboard Flap - CAM Follower Engagement

17-Sep-1985Mos

607Hrs

262Ldg


RecommendedRE (-)601-0029 Modification - Wing Trailing Edge and Outboard Flap Vane - Rubbing Strip Addition

28-Mar-1989Mos

Hrs

Ldg

57 A/FComplied With

RecommendedT (A/R)601-0029 Rev 1 Modification - Wing Trailing Edge and Outboard Flap Vane - Rubbing Strip Addition

Mos

Hrs

Ldg

57 A/FEff: 24-May-1985

RecommendedRE (-)601-0134 Modification - Inboard Flap Hinge Forward Fairings - Upper Edge Strengthening

Mos

Hrs

Ldg

57 A/F

RecommendedRE (-)601-0134 Rev 1 Modification - Inboard Flap Hinge Forward Fairings - Upper Edge Strengthening

Mos

Hrs

Ldg

57 A/F


Generated: 6-Apr-2016 1:16 PM243/429







RecommendedRE (-)601-0134 Rev 2 Modification - Inboard Flap Hinge Forward Fairings - Upper Edge Strengthening

26-Jan-1987Mos

1,267Hrs

480Ldg


OptionalT (A/R)601-0202 Modification - Auxiliary Spar Assemblies and Access Panels - Deflector Plates and Drain Holes

Mos

Hrs

Ldg

57 A/FEff: 31-Aug-1987

RecommendedRE (-)601-0221 Modification - Leading Edge Bleed Air Access Panels - Ground Stud Relocation

28-Mar-1989Mos

2,373Hrs

910Ldg


OptionalRE (-)601-0260 Modification - Inboard Trailing Edge - Gusset ReplacementInboard Trailing Edge - Gusset Replacement

Mos

Hrs

Ldg

57 A/F

OptionalT (A/R)601-0260 Rev 1 Modification - Inboard Trailing Edge - Gusset ReplacementInboard Trailing Edge - Gusset Replacement

Mos

Hrs

Ldg

57 A/FEff: 30-Nov-1989

RecommendedRE (-)601-0610 Special Check – Inboard Flaps – Forward Lugs

Mos

Hrs

Ldg

57 A/F

Recommended ≈14-Mar-2040T (A/R)601-0610 Rev 1 Special Check – Inboard Flaps – Forward Lugs

Mos

Hrs

8,674 Ldg[15,000]Ldg

57 A/FEff: 27-Apr-2011

RecommendedT (A/R)601-0611 Rework/Modification – Ailerons – Addition of Drain Holes on Aileron PCU Access Panels

Mos

Hrs

Ldg

57 A/FEff: 19-Mar-2012

RecommendedRE (-)601-0624 Special Check/Modification – Attachment Fittings – Wings Box Main Landing Gear (MLG) Side Brace Fittings

8.5 Months[18-Dec-2016]18-Dec-2014Mos

11,854.6Hrs

Ldg

57 A/FPART AEff: 01-Oct-2012 Complied

With

RecommendedT601-0631 Special Check – Flap Hinge Box – Forward Lugs Edge to Edge Distance

1.5 Years[26-Sep-2017]48Mos

Hrs

1,574 Ldg[7,900]Ldg

57 A/FEff: 26-Sep-2013

RecommendedT (A/R)601-0636 Special Check/Rework – Attachment Fittings – Serialization of Main Landing Gear (MLG) Side-Brace Fitting-Shaft Part No. 600-10237-3

Mos

Hrs

Ldg

57 A/FEff: 09-Sep-2014


Generated: 6-Apr-2016 1:16 PM244/429







Mandatory ≈28-Feb-2017RE84-13-03 R1 Flap Vane Support Straps

13-Nov-2015Mos

12,014.3Hrs

379 Ldg6,7054006,305Ldg

57 A/FSI A601-004.R3Eff: 26-Jul-1985 Complied

With

AlertRE (-)A601-0096 Special Check/Modification - Aileron - Hinge/Actuator Fitting

Mos

Hrs

Ldg

57 A/F

AlertRE (-)A601-0096 Rev 1 Special Check/Modification - Aileron - Hinge/Actuator Fitting

27-Feb-1999Mos

5,912Hrs

2,584Ldg


AlertRE (-)A601-0135 Modification - Inboard Flap Hinge Arm Forward Fittings - Fastener Replacement

Mos

Hrs

Ldg

57 A/F

AlertRE (-)A601-0135 Rev 1 Modification - Inboard Flap Hinge Arm Forward Fittings - Fastener Replacement

26-Jan-1987Mos

Hrs

Ldg


AlertRE (-)A601-0554 Special Check - Plates/Skins - Possible Development of Crack(s) on Lower Wing Plank at WS148.02 (Rear Spar)

Mos

Hrs

Ldg

57 A/F

AlertRE (-)A601-0554 Rev 1 Special Check - Plates/Skins - Possible Development of Crack(s) on Lower Wing Plank at WS148.02 (Rear Spar)

24-Mar-2003Mos

9,346.7Hrs

4,655Ldg


AlertRE (-)A601-0627 Special Check/Modification – Attachment Fittings – Inboard Flap Hinge Box Forward Attachment Fittings Fasteners

OVD[26-Sep-2015]Mos

Hrs

Ldg

57 A/F

Nextdue Share EarliestDUE:1. RE -Special Check/Modification – Attachment Fittings – Inboard F...A601-0627 Part AA/F57

Nextdue Share EarliestDUE:1. RE -Special Check/Modification – Attachment Fittings – Inboard F...A601-0627 Part BA/F57

Nextdue Share EarliestDUE:1. RE -Special Check/Modification – Attachment Fittings – Inboard F...A601-0627 Part CA/F57

AlertRE (-)A601-0627 Part A Special Check/Modification – Attachment Fittings – Inboard Flap Hinge Box Forward Attachment Fittings Fasteners - Inspection

Mos

Hrs

Ldg

57 A/FEff: 26-Sep-2013

AlertRE (-)A601-0627 Part B Special Check/Modification – Attachment Fittings – Inboard Flap Hinge Box Forward Attachment Fittings Fasteners - Removal / Re-Installation

Mos

Hrs

Ldg

57 A/FEff: 26-Sep-2013


Generated: 6-Apr-2016 1:16 PM245/429







AlertRE (-)A601-0627 Part C Special Check/Modification – Attachment Fittings – Inboard Flap Hinge Box Forward Attachment Fittings Fasteners - Fwd Fasteners Heads correctly oriented.

Mos

Hrs

Ldg

57 A/FEff: 26-Sep-2013

AlertRE (-)A601-0627 Rev 1 Special Check/Modification – Attachment Fittings – Inboard Flap Hinge Box Forward Attachment Fittings Fasteners

Mos

Hrs

Ldg

57 A/F

Nextdue Share EarliestDUE:1. RE -Special Check/Modification – Attachment Fittings – Inboard F...A601-0627 Rev 1 Part AA/F57

Nextdue Share EarliestDUE:1. RE -Special Check/Modification – Attachment Fittings – Inboard F...A601-0627 Rev 1 Part BA/F57

Nextdue Share EarliestDUE:1. RE -Special Check/Modification – Attachment Fittings – Inboard F...A601-0627 Rev 1 Part CA/F57

AlertRE (-)A601-0627 Rev 1 Part A Special Check/Modification – Attachment Fittings – Inboard Flap Hinge Box Forward Attachment Fittings Fasteners - Inspection

Mos

Hrs

Ldg

57 A/FEff: 26-Feb-2014

AlertRE (-)A601-0627 Rev 1 Part B Special Check/Modification – Attachment Fittings – Inboard Flap Hinge Box Forward Attachment Fittings Fasteners - Removal / Re-Installation

Mos

Hrs

Ldg

57 A/FEff: 26-Feb-2014

AlertRE (-)A601-0627 Rev 1 Part C Special Check/Modification – Attachment Fittings – Inboard Flap Hinge Box Forward Attachment Fittings Fasteners - Fwd Fasteners Heads correctly oriented.

Mos

Hrs

Ldg

57 A/FEff: 26-Feb-2014

AlertT (A/R)A601-0627 Rev 2 Special Check/Modification – Attachment Fittings – Inboard Flap Hinge Box Forward Attachment Fittings Fasteners

Mos

Hrs

Ldg

57 A/FEff: 09-Dec-2014

Nextdue Share EarliestDUE:1. RE -Special Check/Modification – Attachment Fittings – Inboard F...A601-0627 Rev 2 Part AA/F57

Nextdue Share EarliestDUE: 26-Sep-20171. T 24 Mos | 2. RE -Special Check/Modification – Attachment Fittings – Inboard F...A601-0627 Rev 2 Part BA/F57

Nextdue Share EarliestDUE:1. T A/R | 2. RE -Special Check/Modification – Attachment Fittings – Inboard F...A601-0627 Rev 2 Part CA/F57

AlertRE (-)A601-0627 Rev 2 Part A Special Check/Modification – Attachment Fittings – Inboard Flap Hinge Box Forward Attachment Fittings Fasteners - Inspection

13-Nov-2015Mos

12,014.3Hrs

6,305Ldg


AlertTA601-0627 Rev 2 Part B Special Check/Modification – Attachment Fittings – Inboard Flap Hinge Box Forward Attachment Fittings Fasteners - Removal / Re-Installation

1.5 Years[26-Sep-2017]24Mos

Hrs

Ldg

57 A/FEff: 09-Dec-2014

AlertT (A/R)A601-0627 Rev 2 Part C Special Check/Modification – Attachment Fittings – Inboard Flap Hinge Box Forward Attachment Fittings Fasteners - Fwd Fasteners Heads correctly oriented.

Mos

Hrs

Ldg

57 A/FEff: 09-Dec-2014


Generated: 6-Apr-2016 1:16 PM246/429







CPCPREC57-00-801 Wing Front Spar and Leading Edge WS50.00 to WS353.00 - CPCP Check of the following items: (1) Forward face of the front spar / (2) Leading edge structure (internal

and external) / (3) Wing anti-ice installations / (4) Piccolo installations

5.8 Months (+30

Days)(26-Sep-2016)-/+16026-Sep-2011Mos

Hrs

Ldg

(PKG 60 Month)

57 A/F


CPCPREC57-00-802 Wing Lower External Surface, BL0.00 to WS353.00 - CPCP Check including the following items: (1) Wing lower skins / (2) Skin splices / (3) Splice plates

10 Months (+29

Days)(30-Jan-2017)-/+12430-Jan-2015Mos

Hrs

Ldg

(PKG 24 Month)

57 A/F

(SOURCE: TLMC 05-30-20) (NOTE: [1] With fuselage fairings installed [2] This task can be done in conjunction with Scheduled Maintenance

Instruction Task 57-00-00-203.)

CPCPREC57-00-803 Wing Upper Surface, BL0.00 to BL50.00 - CPCP Check: (1) Wing upper external surface / (2) Wing upper skin splice

5.8 Months (+30

Days)(26-Sep-2016)-/+16026-Sep-2011Mos

Hrs

Ldg

(PKG 60 Month)

57 A/F

Ref.:PSP 607 51-54-153/3 (SOURCE: TLMC 05-30-20) (NOTE: This task can be done in conjunction with Scheduled Maintenance Instruction

Task 57-00-00-204.)

CPCPREC57-00-804 Wing Structure Between the Front Spar and Rear Spar, BL0.00 to BL45.00 - CPCP Check including the following items: (1) Wing structure (2) Area around all access

panel openings, internal and external.

5.8 Months (+30

Days)(26-Sep-2016)-/+16026-Sep-2011Mos

Hrs

Ldg

(PKG 60 Month)

57 A/F


CPCPREC57-00-805 Wing Front Spar, BL0.00 to WS50.00 - CPCP Check of the following items: (1) Forward face of the front spar, wing center section / (2) Splices, web, caps and machined

fittings

5.8 Months (+30

Days)(26-Sep-2016)-/+16026-Sep-2011Mos

Hrs

Ldg

(PKG 60 Month)

57 A/F


Task 57-10-00-206.)

CPCPREC57-00-806 Wing Structure Between the Front Spar and Rear Spar, WS45.00 to WS353.00 (Internal) - CPCP Check including the following items: (1) Wing structure / (2) Machined

backup fittings / (3) Area around access panel openings (internal and external)

5.8 Months (+30

Days)(26-Sep-2016)-/+16026-Sep-2011Mos

Hrs

Ldg

(PKG 60 Month)

57 A/F


CPCPREC57-00-807 Wing Rear Spar, BL0.00 to WS66.00 (External) - CPCP Check including the following items: (1) Aft face of the rear spar / (2) All attachments / (3) MLG trunnion and

MLG door attachment

5.8 Months (+30

Days)(26-Sep-2016)-/+16026-Sep-2011Mos

Hrs

Ldg

(PKG 60 Month)

57 A/F


Task 57-10-00-209.)

CPCPREC57-00-808 Wingtip/Winglet Assembly (Internal/External) - CPCP Check including the following items: (1) Wingtip/winglet assembly / (2) Attachment to the wing

5.8 Months (+30

Days)(26-Sep-2016)-/+16026-Sep-2011Mos

Hrs

Ldg

(PKG 60 Month)

57 A/F



Generated: 6-Apr-2016 1:16 PM247/429







CPCPREC57-00-809 Wing Rear Spar and Auxiliary Spar, WS50.00 to WS353.00 - CPCP Check including the following items: (1) Attachment fittings and hinges / (2) Auxiliary spar aft face

WS50.00 to WS148.00 / (3) Web / (4) Rear spar aft face WS148.00 to WS353.00

5.8 Months (+30

Days)(26-Sep-2016)-/+16026-Sep-2011Mos

Hrs

Ldg

(PKG 60 Month)

57 A/F

(SOURCE: TLMC 05-30-20) (NOTE: [1] Lower and secure flaps. [2] This task can be done in conjunction with Scheduled Maintenance Instruction

Task 57-20-00-211.)

CPCPREC57-00-810 Main Landing Gear Actuator Fitting at Wing Box FS513.00 and BL13.50 - CPCP Check including the following items: (1) Actuator fitting(2) Wing upper aft panel(3)

Intercostal and spar web(4) Bolt (without removal)


Hrs

Ldg

(PKG 48 Month)

57 A/F


CPCPREC57-00-811 Wing Rear Spar and Auxiliary Spar, WS66.00 to WS148.00 - CPCP Check of all internal structure between and including: (1) Rear spar / (2) Auxiliary spar / (3) Wing

planks

5.8 Months (+30

Days)(26-Sep-2016)-/+16026-Sep-2011Mos

Hrs

Ldg

(PKG 60 Month)

57 A/F


CPCPREC57-00-812 Wing to Fuselage Attachment Fitting, FS424.00 and BL45.00 - CPCP Check including the following items: (1) Adjacent wing plank / (2) Lugs and attachment fittings

5.8 Months (+30

Days)(26-Sep-2016)-/+16026-Sep-2011Mos

Hrs

Ldg

(PKG 60 Month)

57 A/F


CPCPREC57-00-813 Wing to Fuselage Attachment Fitting, FS473.15 and BL45.00 - CPCP Check including the following items: (1) Attachment lugs and fittings / (2) Adjacent wing plank

5.8 Months (+30

Days)(26-Sep-2016)-/+16026-Sep-2011Mos

Hrs

Ldg

(PKG 60 Month)

57 A/F


CPCPREC57-00-814 Outboard Flap (External) - CPCP Check including the following items: (1) External surfaces / (2) Hinge arm assemblies and attachment fittings / (3) Hinge bolts

(without removal) / (4) Vanes and vane support structures / (5) Flap front spar / (6) Wing plank under the fairings

5.8 Months (+30

Days)(26-Sep-2016)-/+16026-Sep-2011Mos

Hrs

Ldg

(PKG 60 Month)

57 A/F


CPCPREC57-00-815 Inboard Flap (External) - CPCP Check including the following items: (1) External surfaces / (2) Vane and vane attachment brackets / (3) Front spar / (4) Hinge arm

assemblies, hinge bolts (without removal) andattachment fittings / (5) Attachment points on the flap and wing surfaces / (6) Backup fittings in the wing / (7) Wing

plank under fairings

5.8 Months (+30

Days)(26-Sep-2016)-/+16026-Sep-2011Mos

Hrs

Ldg

(PKG 60 Month)

57 A/F


CPCPREC57-00-816 Inboard Flap Vane Actuating Assemblies - CPCP Check including the following: (1) Vane actuating assemblies

5.8 Months (+30

Days)(26-Sep-2016)-/+16026-Sep-2011Mos

Hrs

Ldg

(PKG 60 Month)

57 A/F



Generated: 6-Apr-2016 1:16 PM248/429







CPCPREC57-00-817 Aileron (External) - CPCP Check including the following items: (1) External surfaces / (2) Hinge fittings and lugs / (3) Hinge bolts (without removal)

5.8 Months (+30

Days)(26-Sep-2016)-/+16026-Sep-2011Mos

Hrs

Ldg

(PKG 60 Month)

57 A/F


CPCPREC57-00-818 Flight Spoiler (External) - CPCP Check including the following items: (1) External surfaces / (2) Hinge fittings and lugs / (3) Hinge bolts (without removal)

5.8 Months (+30

Days)(26-Sep-2016)-/+16026-Sep-2011Mos

Hrs

Ldg

(PKG 60 Month)

57 A/F

(SOURCE: TLMC 05-30-20) (NOTE: [1] Extend spoliers. [2] This task can be done in conjunction with Scheduled Maintenance Instruction Task

57-50-00-222.)

CPCPREC57-00-819 Wing Upper External Surface, WS50.00 to WS353.00 - CPCP Check including the following items: (1) Upper surface

5.8 Months (+30

Days)(26-Sep-2016)-/+16026-Sep-2011Mos

Hrs

Ldg

(PKG 60 Month)

57 A/F


CPCPREC57-00-820 Wing to Fuselage Attachment Fitting, WS513.00 and BL45.00 - CPCP Check including the following items: (1) Adjacent wing plank / (2) Lower link bolt (without

removal) / (3) Link

5.8 Months (+30

Days)(26-Sep-2016)-/+16026-Sep-2011Mos

Hrs

Ldg

(PKG 60 Month)

57 A/F


Mandatory ≈02-Mar-2016TCF-2014-01 Paragraph C2, C3

Inboard

Flap Hinge Box – Non-Conforming Forward Lugs Edge Distance, Special Check Inboard

Mos

Hrs

22 Ldg≈6,348250Ldg

57 A/FEff: 17-Jan-2014

Mandatory ≈27-Aug-2016TCF-2014-01 Paragraph C2, C3

Outboard

Flap Hinge Box – Non-Conforming Forward Lugs Edge Distance, Special Check Outboard

Mos

Hrs

196 Ldg≈6,522250Ldg

57 A/FEff: 26-Sep-2013

IsModSumT (A/R)IS600-57-0001 REV A Kit-Flap Box Hinge Bushings Instl – Improved Corrosion Protection

Mos

Hrs

Ldg

57 A/F

▼ 71 - POWER PLANT

RE (O/C)Engine Aft Mount

20-Sep-1983Mos

0Hrs0

0Ldg0

Left71 A/FNew601-37002-1

UNKNOWN

RE (O/C)Engine Aft Mount

20-Sep-1983Mos

0Hrs0

0Ldg0


UNKNOWN


Generated: 6-Apr-2016 1:16 PM249/429







RE (O/C)Engine Forward Mount

20-Sep-1983Mos

0Hrs0

0Ldg0

Left71 A/FNew601-37001-1

UNKNOWN

RE (O/C)Engine Forward Mount

20-Sep-1983Mos

0Hrs0

0Ldg0


UNKNOWN

MandatoryT2013-05-06 Modification of the left-hand engine thrust control mechanism

18 Days[24-Apr-2016]36Mos

5,725.9 Hrs[17,767.1]6,000Hrs

Ldg

71 A/FEff: 24-Apr-2013

Compliance Share DoubleDUE:1. T A/R | 2. RE -Modification – Core Cowl Doors – Installation of a Hold Open...601-0609A/F71

RecommendedRE (-)601-0014 Special Check/Modification - Forward Engine Mount - Bushings

Mos

Hrs

Ldg

71 A/FEff: 08-Feb-1984

RecommendedT (A/R)601-0153 Modification - Forward Engine Mount - Retention Bolts

Mos

Hrs

Ldg

71 A/FEff: 08-Oct-1985

RecommendedRE (-)601-0181 Modification - Flight Control Systems and Engine Sensors - E.M.I. Protection

Mos

Hrs

Ldg

71 A/F

RecommendedRE (-)601-0181 Rev 1 Modification - Flight Control Systems and Engine Sensors - E.M.I. Protection

Mos

Hrs

Ldg

71 A/FEff: 23-Apr-1986

RecommendedRE (-)601-0474 Special Check/Modification - Forward Engine Mount - Replacement of Nuts and Damaged Bolts

18-Nov-1996Mos

5,001Hrs

2,052Ldg


Nextdue Share EarliestDUE:1. T A/R | 2. RE -Special Check/Modification - Forward Engine Mount - Replacem...601-0474 Part AA/F71

Nextdue Share EarliestDUE:1. T A/R | 2. RE -Special Check/Modification - Forward Engine Mount - Replacem...601-0474 Part BA/F71

RecommendedT (A/R)601-0474 Part A Special Check/Modification - Forward Engine Mount - Replacement of Nuts and Damaged Bolts - Left Engine

Mos

Hrs

Ldg

71 A/FEff: 14-Jun-1996

RecommendedT (A/R)601-0474 Part B Special Check/Modification - Forward Engine Mount - Replacement of Nuts and Damaged Bolts - Right Engine

Mos

Hrs

Ldg

71 A/FEff: 14-Jun-1996


Generated: 6-Apr-2016 1:16 PM250/429







RecommendedT (A/R)601-0522 Special Check/Rework - Engine Mounts - Serialization of Engine Mounts and Yoke Fitting Assembly

Mos

Hrs

Ldg

71 A/FEff: 30-Sep-2003

RecommendedT (A/R)601-0599 Modification – Cowlings – Addition of Warning Placards to Correctly Install Fasteners

Mos

Hrs

Ldg

71 A/FEff: 18-Aug-2008

RecommendedT (A/R)601-0609 Modification – Core Cowl Doors – Installation of a Hold Open Rod Bracket to Prevent Malfunction of the L/H Engine Fuel Control Unit

Mos

Hrs

Ldg

71 A/FEff: 31-Aug-2011

OptionalT (A/R)601-1003 Modification - Core Cowl Assemblies - Interchangeability

Mos

Hrs

Ldg

71 A/FEff: 01-May-1985

RecommendedRE (-)601-1004 Modification - Upper and Lower Core Cowl Doors - Strut Stay Brace

02-May-1988Mos

1,995Hrs

756Ldg


RecommendedRE (-)601-1027 Modification - Service Pylon - IDG Hose Restraints

02-May-1988Mos

1,995Hrs

756Ldg


RecommendedT (A/R)601-1028 Special Check/Modification - Left Lower Core Cowl Stay Brace - Clearance Between Stow Bracket and Power Lever

Mos

Hrs

Ldg

71 A/FEff: 10-Apr-1984

RecommendedT (A/R)601-1031 Special Check/Modification - Nose Cowl Fixed Side Panel - Forward Engine Mount Aperture

Mos

Hrs

Ldg

71 A/FEff: 25-Feb-1987

RecommendedRE (-)601-1032 Modification - Nose Cowl Assembly - Drain Hole Relocation

18-Sep-1985Mos

607Hrs

261Ldg


RecommendedRE (-)601-1035 Modification - Wiring Harness - Clamping

02-May-1988Mos

1,995Hrs

756Ldg


RecommendedRE (-)601-1036 Modification - Drain and Vent System - Combustor Drain Line Support

18-Sep-1985Mos

607Hrs

261Ldg



Generated: 6-Apr-2016 1:16 PM251/429







RecommendedRE (-)601-1051 Special Check/Modification - Fixed Nose Cowls - Electrical Connectors

02-May-1988Mos

1,995Hrs

756Ldg


RecommendedRE (-)601-1052 Modification - Lower Core Cowl Door - Alignment

Mos

Hrs

Ldg

71 A/F

RecommendedRE (-)601-1052 Rev 1 Modification - Lower Core Cowl Door - Alignment

02-May-1988Mos

1,995Hrs

756Ldg


RecommendedRE (-)601-1053 Special Check and Modification - Upper Access Cowl - Clearances

Mos

Hrs

Ldg

71 A/F

RecommendedRE (-)601-1053 Rev 1 Special Check and Modification - Upper Access Cowl - Clearances

Mos

Hrs

Ldg

71 A/F

RecommendedRE (-)601-1053 Rev 2 Special Check and Modification - Upper Access Cowl - Clearances

25-Oct-1988Mos

Hrs

Ldg


RecommendedRE (-)601-1055 Special Check/Rework - Core Cowl Doors - Undersize Exhaust Port

02-May-1988Mos

1,995Hrs

756Ldg


RecommendedRE (-)601-1062 Modification - Oil Scavenge Tube - Reorientation of Clamp

02-May-1988Mos

1,995Hrs

756Ldg


OptionalRE (-)601-1072 Modification - Exhaust Nozzle Fairing - Prevention of Heat Shield Delamination

27-Feb-1999Mos

5,912Hrs

2,584Ldg


RecommendedRE (-)601-1078 Special Check/Modification - Upper Access Cowl - Clearance with Ballscrew Actuators

21-Feb-1991Mos

3,142Hrs

1,250Ldg


RecommendedRE (-)601-1083 Modification - Core Cowl Doors - Improved Fire Resistance and Containment

26-Jan-1996Mos

4,785Hrs

1,932Ldg



Generated: 6-Apr-2016 1:16 PM252/429







RecommendedT (A/R)601-1090 Modification - Core Cowl Doors - Larger Vent Holes in Aft Frame

Mos

Hrs

Ldg

71 A/FEff: 16-Jan-1995

RecommendedT (A/R)601-1091 Modification - Upper Access Cowl Install Shorter Screws

Mos

Hrs

Ldg

71 A/FEff: 31-Jan-1995

AWL ≈23-Feb-2016RE71-10-00-101 * (Left) Nose Cowl Actuator Support Fitting - Forward Attachment Lugs - NDT Check

08-Aug-2005Mos

18.6 Hrs12,059.81,20010,859.8Hrs

Ldg

71 A/F


AWL ≈23-Feb-2016RE71-10-00-101 * (Right) Nose Cowl Actuator Support Fitting - Forward Attachment Lugs - NDT Check

08-Aug-2005Mos

18.6 Hrs12,059.81,20010,859.8Hrs

Ldg

71 A/F


AWL ≈09-Oct-2019T71-10-00-102 * Forward Nacelle Structure at the Engine Nacelle Joint - NDT Check

Mos

1,758.8 Hrs13,80013,800Hrs

Ldg

71 A/F


MRB ≈18-Sep-2016RE71-10-11-209 Nose Cowl Assembly Visual Check

10-Feb-2016Mos

290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs

6,326Ldg

(PKG 300 Hour)

71 A/F


MRB ≈18-Sep-2016RE71-10-16-201 Translating Cowl Doors Visual Check, paying particular attention to the trailing edge upper and lower doors

10-Feb-2016Mos

290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs

6,326Ldg

(PKG 300 Hour)

71 A/F


MRB ≈18-Sep-2016RE71-12-01-202 Core Cowl Doors Check Core Cowl

10-Feb-2016Mos

290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs

6,326Ldg

(PKG 300 Hour)

71 A/F


MRB ≈09-Mar-2019RE71-13-01-206 Core Cowl Fixed Side Panel Visual Check of the pylon installation and casting including oil cooler installation

30-Dec-2004Mos

1,478.4 Hrs (+40)13,519.6-/+403,00010,519.6Hrs

Ldg

71 A/F


AWL ≈09-Apr-2022T71-20-00-103 * Aft Engine Mount - Thrust Fitting - NDT Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

71 A/F


AWL ≈29-Mar-2042RE71-20-00-104 * Engine Mount Yoke - Lower Lug - NDT Check

05-Aug-2003Mos

12,544.4 Hrs24,585.615,0009,585.6Hrs

Ldg

71 A/F



Generated: 6-Apr-2016 1:16 PM253/429







AWL ≈09-Apr-2022T71-20-00-105 * Forward Engine Mount Upper Link - NDT Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

71 A/F


AWL ≈09-Apr-2022T71-20-00-106 * Forward Engine Mount Upper Bolts - NDT Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

71 A/F

Ref.:PSP 612 Part 4 UT-71-20-02, Ref.:PSP 612 Part 6 ET-71-20-03, Ref.:PSP 612 Part 8 PT-71-20-01 (SOURCE: TLMC 05-10-30)

AlertT (A/R)A601-1010 Special Check/Replacement - Throttle Control - Gearbox

Mos

Hrs

Ldg

71 A/FEff: 24-Aug-1983

CPCPREC71-00-801 Forward Engine Mount - CPCP Check including the following items: (without removal of engine) (1) Yoke assembly / (2) Link assembly / (3) Attachment bolts

5.8 Months (+30

Days)(26-Sep-2016)-/+16026-Sep-2011Mos

Hrs

Ldg

(PKG 60 Month)

71 A/F


CPCPREC71-00-802 Aft Engine Mount - CPCP Check including the following items: (without removal of engine) (1) Thrust fitting

5.8 Months (+30

Days)(26-Sep-2016)-/+16026-Sep-2011Mos

Hrs

Ldg

(PKG 60 Month)

71 A/F


CPCPREC71-00-803 Forward Nacelle and Nose Cowl Actuator Support Fitting - CPCP Check (without removal of engine)

5.8 Months (+30

Days)(26-Sep-2016)-/+16026-Sep-2011Mos

Hrs

Ldg

(PKG 60 Month)

71 A/F


RE (O/C)Engine - No.1 Powerplant

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Engine - No.2 Powerplant

20-Sep-1983Mos

0Hrs

0Ldg


▼ 72 - ENGINE

RE (O/C)Accessory Gearbox

27-Jun-2005Mos

10,839Hrs

5,949Enc

72 ENG26014T81G24HCP00906

RE (O/C)Accessory Gearbox

31-May-2005Mos

10,956Hrs

5,990Enc

72 ENG16014T81G24HPC00814


Generated: 6-Apr-2016 1:16 PM254/429







RE (O/C)Balance Piston Stationary Air Seal

20-Sep-1983Mos

0Hrs

0Enc

72 ENG1UnknownUnknown

RE (O/C)Balance Piston Stationary Air Seal

20-Sep-1983Mos

0Hrs

0Enc


RE (O/C)Ball Bearing

20-Sep-1983Mos

0Hrs

0Enc

No.172 ENG1UnknownUnknown


20-Sep-1983Mos

0Hrs

0Enc



20-Sep-1983Mos

0Hrs

0Enc



20-Sep-1983Mos

0Hrs

0Enc



20-Sep-1983Mos

0Hrs

0Enc



20-Sep-1983Mos

0Hrs

0Enc


RE (O/C)Ball Duplex Bearing

20-Sep-1983Mos

0Hrs

0Enc


RE (O/C)Ball Duplex Bearing

20-Sep-1983Mos

0Hrs

0Enc


RE (O/C)Combustion Frame

20-Sep-1983Mos

0Hrs

0Enc



Generated: 6-Apr-2016 1:16 PM255/429







RE (O/C)Combustion Frame

20-Sep-1983Mos

0Hrs

0Enc


≈01-Jul-2069RECompressor Rotor Disk (Stage 9)

27-Jun-2005Mos

10,839Hrs0

19,221 Enc25,94920,0005,949Enc0

72 ENG2New6087T01P03

NCE337AC

Ref:EMM 5-11-02 (SOURCE: EMM - Life Limit) (NOTE: Subject to inspection by Airworthiness Directive 99-22-10 and AMOC dated March 24,

2004.)

≈01-Jul-2069RECompressor Rotor Disk (Stage 9)

31-May-2005Mos

10,956Hrs0

19,221 Enc25,99020,0005,990Enc0


NCE671AC


2004.)

≈21-Jul-2046RECompressor Rotor Forward Shaft

27-Jun-2005Mos

10,839Hrs0

10,961 Enc17,68911,7405,949Enc0


GATS9134

Ref:EMM 5-11-02 (SOURCE: EMM - Life Limit)

≈01-Dec-2029RECompressor Rotor Forward Shaft

31-May-2005Mos

10,956Hrs10,956

4,971 Enc11,74011,7405,990Enc5,990

72 ENG1Overhauled5037T01P03

GATR1090


≈11-Aug-2030RECompressor Rotor Forward Spool (3 - 8 Stage)

27-Jun-2005Mos

10,839Hrs0

5,221 Enc11,9496,0005,949Enc0


GATHF97K

Ref:EMM 5-11-02 (SOURCE: EMM - Life Limit) (NOTE: For forward HPC spools, part number (P/N) 6078T56P01 (Subject to inspection by

Airworthiness Directive 99-22-10), , which have accumulated fewer than 6,000 cycles since new (CSN) on the effective date of this AD, remove

prior to accumulating 6,000 CSN.)

≈11-Aug-2030RECompressor Rotor Forward Spool (3 - 8 Stage)

31-May-2005Mos

10,956Hrs0

5,221 Enc11,9906,0005,990Enc0


GWN07DE5

Ref:EMM 5-11-02 (SOURCE: EMM - Life Limit) (NOTE: For forward HPC spools, part number (P/N) 6078T56P01 (Subject to inspection by

Airworthiness Directive 99-22-10), , which have accumulated fewer than 6,000 cycles since new (CSN) on the effective date of this AD, remove

prior to accumulating 6,000 CSN.)

≈01-Nov-2077RECompressor Rotor Rear Shaft

27-Jun-2005Mos

10,839Hrs0

22,221 Enc28,94923,0005,949Enc0


GWN0943K


≈01-Nov-2077RECompressor Rotor Rear Shaft

31-May-2005Mos

10,956Hrs0

22,221 Enc28,99023,0005,990Enc0


GEE1FRFN



Generated: 6-Apr-2016 1:16 PM256/429







≈09-Dec-2037RECompressor Rotor Rear Shaft CDP Seal

27-Jun-2005Mos

10,839Hrs10,839

7,859 Enc14,58714,4005,949Enc5,762


APV15195


≈21-Apr-2037RECompressor Rotor Rear Shaft CDP Seal

31-May-2005Mos

10,956Hrs10,956

7,631 Enc14,40014,4005,990Enc5,990


APV12114


≈02-Mar-2061RECompressor Rotor Rear Spool (Stage 10 - 14)

27-Jun-2005Mos

10,839Hrs0

16,221 Enc22,94917,0005,949Enc0


GATHFDL2


2004.)

≈02-Mar-2061RECompressor Rotor Rear Spool (Stage 10 - 14)

31-May-2005Mos

10,956Hrs0

16,221 Enc22,99017,0005,990Enc0


GATHFE9G


2004.)

RE (O/C)Engine Combustion Liner

27-Jun-2005Mos

10,839Hrs3,043

5,949Enc1,792

72 ENG2Overhauled5021T51G02

GGMUW068

RE (O/C)Engine Combustion Liner

31-May-2005Mos

10,956Hrs

5,990Enc

72 ENG15021T51G02GGMVC780

RE (O/C)Fan Blade

20-Sep-1983Mos

0Hrs

0Enc


RE (O/C)Fan Blade

20-Sep-1983Mos

0Hrs

0Enc


RE (O/C)Fan Blade

20-Sep-1983Mos

0Hrs

0Enc


RE (O/C)Fan Blade

20-Sep-1983Mos

0Hrs

0Enc



Generated: 6-Apr-2016 1:16 PM257/429







RE (O/C)Fan Blade

20-Sep-1983Mos

0Hrs

0Enc


RE (O/C)Fan Blade

20-Sep-1983Mos

0Hrs

0Enc


RE (O/C)Fan Blade

20-Sep-1983Mos

0Hrs

0Enc


RE (O/C)Fan Blade

20-Sep-1983Mos

0Hrs

0Enc


RE (O/C)Fan Blade

20-Sep-1983Mos

0Hrs

0Enc


RE (O/C)Fan Blade

20-Sep-1983Mos

0Hrs

0Enc


RE (O/C)Fan Blade

20-Sep-1983Mos

0Hrs

0Enc


RE (O/C)Fan Blade

20-Sep-1983Mos

0Hrs

0Enc


RE (O/C)Fan Blade

20-Sep-1983Mos

0Hrs

0Enc


RE (O/C)Fan Blade

20-Sep-1983Mos

0Hrs

0Enc


RE (O/C)Fan Blade

20-Sep-1983Mos

0Hrs

0Enc



Generated: 6-Apr-2016 1:16 PM258/429







RE (O/C)Fan Blade

20-Sep-1983Mos

0Hrs

0Enc


RE (O/C)Fan Blade

20-Sep-1983Mos

0Hrs

0Enc


RE (O/C)Fan Blade

20-Sep-1983Mos

0Hrs

0Enc


RE (O/C)Fan Blade

20-Sep-1983Mos

0Hrs

0Enc


RE (O/C)Fan Blade

20-Sep-1983Mos

0Hrs

0Enc


RE (O/C)Fan Blade

20-Sep-1983Mos

0Hrs

0Enc


RE (O/C)Fan Blade

20-Sep-1983Mos

0Hrs

0Enc


RE (O/C)Fan Blade

20-Sep-1983Mos

0Hrs

0Enc


RE (O/C)Fan Blade

20-Sep-1983Mos

0Hrs

0Enc


RE (O/C)Fan Blade

20-Sep-1983Mos

0Hrs

0Enc


RE (O/C)Fan Blade

20-Sep-1983Mos

0Hrs

0Enc



Generated: 6-Apr-2016 1:16 PM259/429







RE (O/C)Fan Blade

20-Sep-1983Mos

0Hrs

0Enc


RE (O/C)Fan Blade

20-Sep-1983Mos

0Hrs

0Enc


RE (O/C)Fan Blade

20-Sep-1983Mos

0Hrs

0Enc


RE (O/C)Fan Blade

20-Sep-1983Mos

0Hrs

0Enc


RE (O/C)Fan Blade

20-Sep-1983Mos

0Hrs

0Enc


RE (O/C)Fan Blade

20-Sep-1983Mos

0Hrs

0Enc


RE (O/C)Fan Blade

20-Sep-1983Mos

0Hrs

0Enc


RE (O/C)Fan Blade

20-Sep-1983Mos

0Hrs

0Enc


RE (O/C)Fan Blade

20-Sep-1983Mos

0Hrs

0Enc


RE (O/C)Fan Blade

20-Sep-1983Mos

0Hrs

0Enc


RE (O/C)Fan Blade

20-Sep-1983Mos

0Hrs

0Enc



Generated: 6-Apr-2016 1:16 PM260/429







RE (O/C)Fan Blade

20-Sep-1983Mos

0Hrs

0Enc


RE (O/C)Fan Blade

20-Sep-1983Mos

0Hrs

0Enc


RE (O/C)Fan Blade

20-Sep-1983Mos

0Hrs

0Enc


RE (O/C)Fan Blade

20-Sep-1983Mos

0Hrs

0Enc


RE (O/C)Fan Blade

20-Sep-1983Mos

0Hrs

0Enc


RE (O/C)Fan Blade

20-Sep-1983Mos

0Hrs

0Enc


RE (O/C)Fan Blade

20-Sep-1983Mos

0Hrs

0Enc


RE (O/C)Fan Blade

20-Sep-1983Mos

0Hrs

0Enc


RE (O/C)Fan Blade

20-Sep-1983Mos

0Hrs

0Enc


RE (O/C)Fan Blade

20-Sep-1983Mos

0Hrs

0Enc


RE (O/C)Fan Blade

20-Sep-1983Mos

0Hrs

0Enc



Generated: 6-Apr-2016 1:16 PM261/429







RE (O/C)Fan Blade

20-Sep-1983Mos

0Hrs

0Enc


RE (O/C)Fan Blade

20-Sep-1983Mos

0Hrs

0Enc


RE (O/C)Fan Blade

20-Sep-1983Mos

0Hrs

0Enc


RE (O/C)Fan Blade

20-Sep-1983Mos

0Hrs

0Enc


RE (O/C)Fan Blade

20-Sep-1983Mos

0Hrs

0Enc


RE (O/C)Fan Blade

20-Sep-1983Mos

0Hrs

0Enc


RE (O/C)Fan Blade

20-Sep-1983Mos

0Hrs

0Enc


RE (O/C)Fan Blade

20-Sep-1983Mos

0Hrs

0Enc


RE (O/C)Fan case Assy

20-Sep-1983Mos

0Hrs

0Enc

Aft72 ENG1UnknownUnknown


20-Sep-1983Mos

0Hrs

0Enc

Aft72 ENG2UnknownUnknown


20-Sep-1983Mos

0Hrs

0Enc

Fwd72 ENG1UnknownUnknown


Generated: 6-Apr-2016 1:16 PM262/429








20-Sep-1983Mos

0Hrs

0Enc

Fwd72 ENG2UnknownUnknown

≈16-Jun-2082REFan Disk

05-Jul-2009Mos

11,437.8Hrs0

23,886 Enc30,61424,3006,314Enc0

72 ENG2New6078T57G06

GEE1GPLT


≈11-Dec-2038REFan Disk

31-May-2005Mos

10,956Hrs0

8,221 Enc14,9909,0005,990Enc0


GEE1FR6L


≈21-Dec-2038REFan Drive Shaft

31-May-2005Mos

10,956Hrs10,956

8,231 Enc15,00015,0005,990Enc5,990


REA0976H


≈02-Feb-2039REFan Drive Shaft

20-Sep-1983Mos

0Hrs0

8,272 Enc15,00015,0000Enc0


UNKNOWN


≈13-Feb-2109REFan Forward Shaft

27-Jul-2005Mos

10,839Hrs6,418

33,483 Enc40,21138,2805,949Enc4,018


GATWF998


≈21-Aug-2103REFan Forward Shaft

31-May-2005Mos

10,956Hrs10,956

31,511 Enc38,28038,2805,990Enc5,990


GATP8695


RE (O/C)Fan Rotor Assy

20-Sep-1983Mos

0Hrs

0Enc


RE (O/C)Fan Rotor Assy

20-Sep-1983Mos

0Hrs

0Enc


RE (O/C)Fan Speed Sensor

20-Sep-1983Mos

0Hrs

0Enc



Generated: 6-Apr-2016 1:16 PM263/429







RE (O/C)Fan Speed Sensor

20-Sep-1983Mos

0Hrs

0Enc


RE (O/C)HPT Assembly Stator

20-Sep-1983Mos

0Hrs

0Enc


RE (O/C)HPT Assembly Stator

20-Sep-1983Mos

0Hrs

0Enc


RE (O/C)HPT Rotor Assy

20-Sep-1983Mos

0Hrs

0Enc


RE (O/C)HPT Rotor Assy

20-Sep-1983Mos

0Hrs

0Enc


≈11-Aug-2030REHPT Rotor Balance Piston Air Seal

27-Jun-2005Mos

10,839Hrs0

5,221 Enc11,9496,0005,949Enc0


NCE5484AF


≈11-Aug-2030REHPT Rotor Balance Piston Air Seal

31-May-2005Mos

10,956Hrs0

5,221 Enc11,9906,0005,990Enc0


NCE0564Y


≈11-Aug-2030REHPT Rotor Inner Torque Coupling

27-Jun-2005Mos

10,839Hrs0

5,221 Enc11,9496,0005,949Enc0


GATHF3HJ


≈11-Aug-2030REHPT Rotor Inner Torque Coupling

31-May-2005Mos

10,956Hrs0

5,221 Enc11,9906,0005,990Enc0


GATP8672


≈11-Aug-2030REHPT Rotor Outer Torque Coupling

27-Jun-2005Mos

10,839Hrs0

5,221 Enc11,9496,0005,949Enc0


GATHEF3E



Generated: 6-Apr-2016 1:16 PM264/429







≈11-Aug-2030REHPT Rotor Outer Torque Coupling

31-May-2005Mos

10,956Hrs0

5,221 Enc11,9906,0005,990Enc0


GATHEF39


≈11-Aug-2030REHPT Rotor Shaft

27-Jun-2005Mos

10,839Hrs0

5,221 Enc11,9496,0005,949Enc0


GEE1FRNE


≈11-Aug-2030REHPT Rotor Shaft

31-May-2005Mos

10,956Hrs0

5,221 Enc11,9906,0005,990Enc0


GEE1FRNG


≈11-Aug-2030REHPT Rotor Stage 1 Cooling Aft Plate

27-Jun-2005Mos

10,839Hrs0

5,221 Enc11,9496,0005,949Enc0


GATCWHJ2


≈11-Aug-2030REHPT Rotor Stage 1 Cooling Aft Plate

31-May-2005Mos

10,956Hrs0

5,221 Enc11,9906,0005,990Enc0


NCE4602Y


≈11-Aug-2030REHPT Rotor Stage 1 Front Cooling Plate

27-Jun-2005Mos

Hrs0

5,221 Enc11,9496,0005,949Enc0


NCE155AA


≈11-Aug-2030REHPT Rotor Stage 1 Front Cooling Plate

31-May-2005Mos

Hrs0

5,221 Enc11,9906,0005,990Enc0


NCE150AA


≈11-Aug-2030REHPT Rotor Stage 1 Turbine Disk

27-Jun-2005Mos

10,839Hrs0

5,221 Enc11,9496,0005,949Enc0


GATHWA3W1



31-May-2005Mos

10,956Hrs0

5,221 Enc11,9906,0005,990Enc0


GATHD55D



Generated: 6-Apr-2016 1:16 PM265/429







≈04-Aug-2020REHPT Rotor Stage 2 Rear Cooling Plate

27-Jun-2005Mos

Hrs

1,614 Enc8,3426,0005,949Enc3,607


GATADJ07


≈11-Aug-2030REHPT Rotor Stage 2 Rear Cooling Plate

31-May-2005Mos

Hrs0

5,221 Enc11,9906,0005,990Enc0


NCE847AC



27-Jun-2005Mos

10,839Hrs0

5,221 Enc11,9496,0005,949Enc0


GATHE4TT



31-May-2005Mos

10,956Hrs0

5,221 Enc11,9906,0005,990Enc0


GATHE4TP


≈22-Feb-2021REHPT Stage 2 Nozzle Ring

05-Jun-2009Mos

2,417.4 Hrs14,554.83,00011,554.8Hrs0

6,355Enc

72 ENG14019T91P03UNKNOWN

≈24-Nov-2019REHPT Stage 2 Nozzle Ring

28-Jul-2005Mos

1,818.6 Hrs13,8393,00010,839Hrs0

5,949Enc

72 ENG2UNKNOWNUNKNOWN

≈23-May-2027REHPT Stage 2 Studs

05-Jun-2009Mos

5,417.4 Hrs17,554.86,00011,554.8Hrs0

6,355Enc


≈23-Feb-2026REHPT Stage 2 Studs

27-Jun-2005Mos

4,818.6 Hrs16,8396,00010,839Hrs0

5,949Enc


RE (O/C)LPT Rotor Assy

20-Sep-1983Mos

0Hrs

0Enc


RE (O/C)LPT Rotor Assy

20-Sep-1983Mos

0Hrs

0Enc



Generated: 6-Apr-2016 1:16 PM266/429







≈02-Feb-2039RELPT Rotor Drive Cone

27-Jun-2005Mos

10,839Hrs10,839

8,272 Enc15,00015,0005,949Enc5,949


GATP7954


≈21-Dec-2038RELPT Rotor Drive Cone

31-May-2005Mos

10,956Hrs10,956

8,231 Enc15,00015,0005,990Enc5,990


GATP7964


≈22-Mar-2093RELPT Rotor Rear Shaft

27-Jun-2005Mos

10,839Hrs10,739

27,762 Enc34,49034,4905,949Enc5,949


GAT51376


≈11-Feb-2093RELPT Rotor Rear Shaft

31-May-2005Mos

10,956Hrs10,956

27,721 Enc34,49034,4905,990Enc5,990


GATR19P01


≈11-Aug-2055RELPT Rotor Stage 3 Disk

27-Jun-2005Mos

10,839Hrs0

14,221 Enc20,94915,0005,949Enc0


GATHFM4C



31-May-2005Mos

10,956Hrs0

14,221 Enc20,99015,0005,990Enc0


GATHF0E3


≈02-Mar-2061RELPT Rotor Stage 4 Disk

27-Jun-2005Mos

10,839Hrs0

16,221 Enc22,94917,0005,949Enc0


GATHE2TK


≈02-Mar-2061RELPT Rotor Stage 4 Disk

31-May-2005Mos

10,956Hrs0

16,221 Enc22,99017,0005,990Enc0


GATHE57H


≈02-Feb-2039RELPT Rotor Stage 5 Disk

27-Jun-2005Mos

10,839Hrs10,839

8,272 Enc15,00015,0005,949Enc5,949


GATHF6KF



Generated: 6-Apr-2016 1:16 PM267/429








31-May-2005Mos

10,956Hrs0

14,221 Enc20,99015,0005,990Enc0


GATHELWF


≈22-Jun-2019RELPT Rotor Stage 6 Disk

27-Jun-2005Mos

10,839Hrs10,839

1,212 Enc7,9407,9405,949Enc5,949


GATT0117


≈11-May-2019RELPT Rotor Stage 6 Disk

31-May-2005Mos

10,956Hrs10,956

1,171 Enc7,9407,9405,990Enc5,990


GATP3216


≈02-Jan-2080RELPT Rotor Stage Turbine Seal (3 - 4)

27-Jun-2005Mos

10,839Hrs10,839

23,002 Enc29,73029,7305,949Enc5,949


ABIA0784


≈21-Nov-2079RELPT Rotor Stage Turbine Seal (3 - 4)

31-May-2005Mos

10,956Hrs10,956

22,961 Enc29,73029,7305,990Enc5,990


ABIA2176



27-Jun-2005Mos

10,839Hrs10,839

23,002 Enc29,73029,7305,949Enc5,949


HAAB0694


≈21-Dec-2088RELPT Rotor Stage Turbine Seal (4 - 5)

31-May-2005Mos

10,956Hrs10,956

26,231 Enc33,00033,0005,990Enc5,990


HAAB2843



27-Jun-2005Mos

10,839Hrs10,839

23,002 Enc29,73029,7305,949Enc5,949


ABIA0719


≈21-Nov-2079RELPT Rotor Stage Turbine Seal (5 - 6)

31-May-2005Mos

10,956Hrs10,956

22,961 Enc29,73029,7305,990Enc5,990


HAAB1278


RE (O/C)LPT Stator Assy

20-Sep-1983Mos

0Hrs

0Enc



Generated: 6-Apr-2016 1:16 PM268/429







RE (O/C)LPT Stator Assy

20-Sep-1983Mos

0Hrs

0Enc


RE (O/C)LPT Transition Turbine Outer Liner

20-Sep-1983Mos

0Hrs

0Enc


RE (O/C)LPT Transition Turbine Outer Liner

20-Sep-1983Mos

0Hrs

0Enc


RE (O/C)Power Take Off Assembly Drive

27-Jun-2005Mos

10,839Hrs10,839

5,949Enc5,949


HCP01212

RE (O/C)Power Take Off Assembly Drive

31-May-2005Mos

10,956Hrs

5,990Enc

72 ENG16037T72G19HPC01002

RE (O/C)Roller Bearing

20-Sep-1983Mos

0Hrs

0Enc



20-Sep-1983Mos

0Hrs

0Enc



20-Sep-1983Mos

0Hrs

0Enc



20-Sep-1983Mos

0Hrs

0Enc



20-Sep-1983Mos

0Hrs

0Enc



20-Sep-1983Mos

0Hrs

0Enc



Generated: 6-Apr-2016 1:16 PM269/429








20-Sep-1983Mos

0Hrs

0Enc



20-Sep-1983Mos

0Hrs

0Enc


≈11-Aug-2055REStage 1 Compressor Rotor Disk

27-Jun-2005Mos

10,839Hrs0

14,221 Enc20,94915,0005,949Enc0


GATFHEAW



31-May-2005Mos

10,956Hrs0

14,221 Enc20,99015,0005,990Enc0


GATHF3G0


RE (O/C)Stage 1 HPT Blades

27-Jun-2005Mos

10,839Hrs

5,949Enc

72 ENG26078T19P10UNKNOWN

RE (O/C)Stage 1 HPT Blades

31-May-2005Mos

10,956Hrs10,956

5,990Enc5,990


UNKNOWN


27-Jun-2005Mos

10,839Hrs

8,459 Enc15,18715,0005,949Enc5,762

72 ENG26036T91P01GATR6493


≈21-Dec-2038REStage 2 Compressor Rotor Disk

31-May-2005Mos

10,956Hrs10,956

8,231 Enc15,00015,0005,990Enc5,990


GATM2467


EMM - Life Limit ≈11-Aug-2030REStage 2 Front Cooling Plate

27-Jun-2005Mos

Hrs0

5,221 Enc11,9496,0005,949Enc0


NCE027AA

EMM - Life Limit ≈11-Aug-2030REStage 2 Front Cooling Plate

31-May-2005Mos

Hrs0

5,221 Enc11,9906,0005,990Enc0


NCE026AA


Generated: 6-Apr-2016 1:16 PM270/429







RE (O/C)Stage 2 HPT Blade

20-Sep-1983Mos

0Hrs

0Enc


RE (O/C)Stage 2 HPT Blade

20-Sep-1983Mos

0Hrs

0Enc


RE (O/C)Thermocouple Assy

27-Jun-2005Mos

10,839Hrs10,839

5,949Enc5,949

Left72 ENG2Overhauled6040T41P01

GDB04982


31-May-2005Mos

10,956Hrs10,956

5,990Enc5,990

Left72 ENG1Overhauled6040T41P01

GDB05018


27-Jun-2005Mos

10,839Hrs

5,949Enc

Right72 ENG26030T40P01GDB07353


31-May-2005Mos

10,956Hrs10,956

5,990Enc5,990

Right72 ENG1Overhauled6040T41P01

GDB05209

RE (O/C)Transition Turbine Case

20-Sep-1983Mos

0Hrs

0Enc


RE (O/C)Transition Turbine Case

20-Sep-1983Mos

0Hrs

0Enc


RE (O/C)Turbine High Pressure Inner Casing

20-Sep-1983Mos

0Hrs

0Enc


RE (O/C)Turbine High Pressure Inner Casing

20-Sep-1983Mos

0Hrs

0Enc


RE (O/C)Turbine High Pressure Outer Casing

20-Sep-1983Mos

0Hrs

0Enc



Generated: 6-Apr-2016 1:16 PM271/429







RE (O/C)Turbine High Pressure Outer Casing

20-Sep-1983Mos

0Hrs

0Enc


RE (O/C)Turbine Low Pressure Casing

20-Sep-1983Mos

0Hrs

0Enc


RE (O/C)Turbine Low Pressure Casing

20-Sep-1983Mos

0Hrs

0Enc


MandatoryRE (-)2001-10-03 Rupture of Fan Disk (Superseded By FAA AD 2006-05-04)

31-May-2001Mos

Hrs

Enc

72 ENG1NEW PART INSTALLEDEff: 31-May-2001 Not

Applicable

MandatoryRE (-)2001-10-03 Rupture of Fan Disk (Superseded By FAA AD 2006-05-04)

31-May-2001Mos

Hrs

Enc

72 ENG2Eff: 31-May-2001 Complied With

MandatoryRE (-)2001-12-06 General Electric Company - Lubrication System for the Engine Bearings

Mos

Hrs

Enc

72 ENG1Eff: 20-Jul-2001

MandatoryRE (-)2001-12-06 General Electric Company - Lubrication System for the Engine Bearings

Mos

Hrs

Enc

72 ENG2Eff: 20-Jul-2001

MandatoryRE (-)2001-12-06 Paragraph (a) General Electric Company - Lubrication System for the Engine Bearings - Magnetic Chip Detector Indicator check

22-Mar-2013Mos

11,734.5Hrs

6,520Enc

72 ENG2Eff: 20-Jul-2001 Complied With

MandatoryRE (-)2001-12-06 Paragraph (a) General Electric Company - Lubrication System for the Engine Bearings - Magnetic Chip Detector Indicator check

20-Jul-2001Mos

Hrs

Enc

72 ENG1FOUND P/C/WEff: 20-Jul-2001 Complied

With

MandatoryRE (-)2001-12-06 Paragraph (d) General Electric Company - Lubrication System for the Engine Bearings - Replacement of Air Seal

08-Mar-2002Mos

Hrs

Enc

72 ENG2Eff: 20-Jul-2001 Complied With

MandatoryRE (-)2001-12-06 Paragraph (d) General Electric Company - Lubrication System for the Engine Bearings - Replacement of Air Seal

20-Jul-2001Mos

Hrs

Enc

72 ENG1FOUND P/C/WEff: 20-Jul-2001 Complied

With


Generated: 6-Apr-2016 1:16 PM272/429







MandatoryRE (-)2004-26-02 Certain high pressure compressor (HPC)

11-Jul-2008Mos

11,411.2Hrs

6,293Enc

72 ENG2Eff: 26-Jan-2005 Not Applicable

MandatoryRE (-)2004-26-02 Certain high pressure compressor (HPC)

26-Jan-2005Mos

Hrs

Enc

72 ENG1Eff: 26-Jan-2005 Not Applicable

Mandatory ≈05-Jan-2024RE2006-04-12 General Electric Company - Stage 5 low pressure turbine (LPT) disks

26-Dec-2012Mos

11,775.4Hrs

2,845 Enc9,6143,1006,514Enc

72 ENG1

Nextdue Share EarliestDUE:1. RE -General Electric Company - Stage 5 low pressure turbine (LPT...2006-04-12 Paragraph (f)(2)(h)(1)ENG172

Nextdue Share EarliestDUE:1. RE -General Electric Company - Stage 5 low pressure turbine (LPT...2006-04-12 Paragraph (m)ENG172

Nextdue Share LatestDUE:1. T 2469 Days | 2. RE -General Electric Company - Stage 5 low pressure turbine (LPT...2006-04-12 Paragraph (n)ENG172

Mandatory ≈05-Jan-2024RE2006-04-12 General Electric Company - Stage 5 low pressure turbine (LPT) disks

26-Dec-2012Mos

11,658.4Hrs

2,845 Enc9,5733,1006,473Enc

72 ENG2

Nextdue Share EarliestDUE:1. RE -General Electric Company - Stage 5 low pressure turbine (LPT...2006-04-12 Paragraph (f)(2)(h)(1)ENG272

Nextdue Share EarliestDUE:1. RE -General Electric Company - Stage 5 low pressure turbine (LPT...2006-04-12 Paragraph (m)ENG272

Nextdue Share LatestDUE:1. T 2469 Days | 2. RE -General Electric Company - Stage 5 low pressure turbine (LPT...2006-04-12 Paragraph (n)ENG272

MandatoryRE (-)2006-04-12 Paragraph (f)(2)(h)

(1)

General Electric Company - Stage 5 low pressure turbine (LPT) disks - For engines installed in Bombardier Canadair BJ airplanes, perform an initial visual inspection

and ECI of stage 5 LPT disks and stage 6 LPT disks

Mos

Hrs

Enc

72 ENG1Eff: 30-Mar-2006

Compliance Share DoubleDUE:1. RE -ENGINE - Low Pressure Turbine (LPT) Rotor (72-53-00) - Repl...72-A0148 R02ENG172

MandatoryRE (-)2006-04-12 Paragraph (f)(2)(h)

(1)

General Electric Company - Stage 5 low pressure turbine (LPT) disks - For engines installed in Bombardier Canadair BJ airplanes, perform an initial visual inspection

and ECI of stage 5 LPT disks and stage 6 LPT disks

Mos

Hrs

Enc

72 ENG2Eff: 30-Mar-2006

Compliance Share DoubleDUE:1. RE -ENGINE - Low Pressure Turbine (LPT) Rotor (72-53-00) - Repl...72-A0148 R02ENG272

MandatoryRE (-)2006-04-12 Paragraph (m) General Electric Company - Stage 5 low pressure turbine (LPT) disks - Optional Terminating Action

Mos

Hrs

Enc

72 ENG1Eff: 30-Mar-2006

MandatoryRE (-)2006-04-12 Paragraph (m) General Electric Company - Stage 5 low pressure turbine (LPT) disks - Optional Terminating Action

Mos

Hrs

Enc

72 ENG2Eff: 30-Mar-2006


Generated: 6-Apr-2016 1:16 PM273/429







MandatoryRE (-)2006-04-12 Paragraph (n) General Electric Company - Stage 5 low pressure turbine (LPT) disks - Terminating Action

Days

Hrs

Enc

72 ENG1Eff: 30-Mar-2006

MandatoryRE (-)2006-04-12 Paragraph (n) General Electric Company - Stage 5 low pressure turbine (LPT) disks - Terminating Action

Days

Hrs

Enc

72 ENG2Eff: 30-Mar-2006

MandatoryRE (-)2006-05-04 Fan Disk

Mos

Hrs

Enc

72 ENG1Eff: 07-Apr-2006

(NOTE: SUPERSEDED BY FAA AD 2007-07-07)


Mos

Hrs

Enc

72 ENG2Eff: 07-Apr-2006


MandatoryRE (-)2007-07-07 Fan Disk Inspection

Mos

Hrs

Enc

72 ENG1Eff: 30-Mar-2007


MandatoryRE (-)2007-07-07 Fan Disk Inspection

Mos

Hrs

Enc

72 ENG2Eff: 30-Mar-2007


MandatoryRE (-)2007-07-07R1 Fan disk inspection

25-Jul-2008Mos

11,528.2Hrs

6,334Enc

72 ENG1Eff: 12-Sep-2007 Not Applicable


MandatoryRE (-)2007-07-07R1 Fan disk inspection

25-Jul-2008Mos

11,411.2Hrs

6,293Enc

72 ENG2Eff: 12-Sep-2007 Complied With


Mandatory ≈22-Feb-2021T (A/R)2009-07-12 General Electric Company - High-pressure (HP) - Remove the 4-step seals, P/Ns 4923T54G01, 6019T90G03, 6037T99G01, 6037T99G02, and 6037T99G03. Incorporate an

8-step seal, either by modifying the existing 4-step seal to an 8-step seal, or by replacing it with an 8-step seal.

Mos

2,417.4 Hrs[14,554.8]Hrs

Enc

72 ENG1Eff: 07-May-2009

Compliance Share DoubleDUE:1. RE -ENGINE - (72-42-00) - Rework of the Air Balance Piston Stati...72-0217 R00ENG172

Mandatory ≈24-Nov-2019T (A/R)2009-07-12 General Electric Company - High-pressure (HP) - Remove the 4-step seals, P/Ns 4923T54G01, 6019T90G03, 6037T99G01, 6037T99G02, and 6037T99G03. Incorporate an

8-step seal, either by modifying the existing 4-step seal to an 8-step seal, or by replacing it with an 8-step seal.

Mos

1,818.6 Hrs[13,839]Hrs

Enc

72 ENG2Eff: 07-May-2009

Compliance Share DoubleDUE:1. T A/R | 2. RE -ENGINE - (72-42-00) - Rework of the Air Balance Piston Stati...72-0217 R00ENG272


Generated: 6-Apr-2016 1:16 PM274/429







MandatoryRE (-)2009-24-11 Fan blade and aft actuator head hoses (SUPERSEDED BY FAA AD 2010-01-04)

Mos

Hrs

Enc

72 ENG1Eff: 04-Jan-2010


Nextdue Share EarliestDUE:1. RE -Fan blade and aft actuator head hoses CF34-1A, CF34-3A, CF34...2009-24-11 Paragraph (l)(1)(2)ENG172

Nextdue Share EarliestDUE:1. RE -Fan blade and aft actuator head hoses CF34-1A, CF34-3A, CF34...2009-24-11 Paragraph (l)(3)(4)(6)ENG172


MandatoryRE (-)2009-24-11 Fan blade and aft actuator head hoses (SUPERSEDED BY FAA AD 2010-01-04)

Mos

Hrs

Enc

72 ENG2Eff: 04-Jan-2010


Nextdue Share EarliestDUE:1. RE -Fan blade and aft actuator head hoses CF34-1A, CF34-3A, CF34...2009-24-11 Paragraph (l)(1)(2)ENG272



MandatoryRE (-)2009-24-11 Paragraph (l)(1)(2) Fan blade and aft actuator head hoses CF34-1A, CF34-3A, CF34-3A2, CF34-3B and CF34-3A1- Remove fan blades from service.(SUPERSEDED BY FAA AD 2010-01-04)

Mos

Hrs

Enc

72 ENG1Eff: 04-Jan-2010

MandatoryRE (-)2009-24-11 Paragraph (l)(1)(2) Fan blade and aft actuator head hoses CF34-1A, CF34-3A, CF34-3A2, CF34-3B and CF34-3A1- Remove fan blades from service.(SUPERSEDED BY FAA AD 2010-01-04)

Mos

Hrs

Enc

72 ENG2Eff: 04-Jan-2010

MandatoryRE (-)2009-24-11 Paragraph (l)(3)(4)

(6)

Fan blade and aft actuator head hoses CF34-1A, CF34-3A, CF34-3A2, CF34-3B and CF34-3A1- Initial / Repetitive Eddy Current Inspection (ECI) of the fan blades.

(SUPERSEDED BY FAA AD 2010-01-04)

Mos

Hrs

Enc

72 ENG1Eff: 04-Jan-2010


(6)

Fan blade and aft actuator head hoses CF34-1A, CF34-3A, CF34-3A2, CF34-3B and CF34-3A1- Initial / Repetitive Eddy Current Inspection (ECI) of the fan blades.

(SUPERSEDED BY FAA AD 2010-01-04)

Mos

Hrs

Enc

72 ENG2Eff: 04-Jan-2010


(10)

Fan blade and aft actuator head hoses CF34-1A, CF34-3A, CF34-3A2, CF34-3B and CF34-3A1- Initial / Repetitive Inspection of the Fan Blade Abradable Rub Strip for

Wear.(SUPERSEDED BY FAA AD 2010-01-04)

Mos

Hrs

Enc

72 ENG1Eff: 04-Jan-2010


(10)

Fan blade and aft actuator head hoses CF34-1A, CF34-3A, CF34-3A2, CF34-3B and CF34-3A1- Initial / Repetitive Inspection of the Fan Blade Abradable Rub Strip for

Wear.(SUPERSEDED BY FAA AD 2010-01-04)

Mos

Hrs

Enc

72 ENG2Eff: 04-Jan-2010


Generated: 6-Apr-2016 1:16 PM275/429







MandatoryRE (-)2009-26-09 General Electric Company - Fan disks

Mos

Hrs

Enc

72 ENG1Eff: 11-Feb-2010

Nextdue Share EarliestDUE:1. T A/R | 2. RE -General Electric Company - Fan disks - Removing Certain Fan ...2009-26-09 Paragraph (f)(g)ENG172

MandatoryRE (-)2009-26-09 General Electric Company - Fan disks

Mos

Hrs

Enc

72 ENG2Eff: 11-Feb-2010

Nextdue Share EarliestDUE:1. T A/R | 2. RE -General Electric Company - Fan disks - Removing Certain Fan ...2009-26-09 Paragraph (f)(g)ENG272

MandatoryT (A/R)2009-26-09 Paragraph (f)(g) General Electric Company - Fan disks - Removing Certain Fan Disks From Service

Mos

Hrs

Enc

72 ENG1Eff: 11-Feb-2010

Not SetDUE:1. RE -ENGINE - Fan Rotor Assembly (72-21-00) - Shop Level Inspecti...72-A0212 R04ENG172

MandatoryT (A/R)2009-26-09 Paragraph (f)(g) General Electric Company - Fan disks - Removing Certain Fan Disks From Service

Mos

Hrs

Enc

72 ENG2Eff: 11-Feb-2010

Not SetDUE:1. RE -ENGINE - Fan Rotor Assembly (72-21-00) - Shop Level Inspecti...72-A0212 R04ENG272

Mandatory ≈18-Jul-2023RE2009-26-09 Paragraph (k) General Electric Company - Fan disks - For CF34-3A1, CF34-1A, CF34-3A, CF34-3A2 and CF34-3B, Inspections of Tier 1 Fan Disks

22-Mar-2012Mos

11,674.8Hrs

2,678 Enc9,4473,0006,447Enc

72 ENG1SB 72-A0212Eff: 11-Feb-2010 Complied

With

Compliance Share DoubleDUE:1. RE -ENGINE - Fan Rotor Assembly (72-21-00) - Shop Level Inspecti...72-A0212 R04 (Tier 1)ENG172

Compliance Share DoubleDUE:1. RE -ENGINE - Fan Rotor Assembly (72-21-00) - Shop Level Eddy Cur...72-A0234 R00ENG172

Compliance Share DoubleDUE:1. RE -ENGINE - Fan Rotor Assembly (72-21-00) - On Wing Repetitive ...72-A0235 R00ENG172

Mandatory ≈18-Jul-2023RE2009-26-09 Paragraph (k) General Electric Company - Fan disks - For CF34-3A1, CF34-1A, CF34-3A, CF34-3A2 and CF34-3B, Inspections of Tier 1 Fan Disks

19-Mar-2012Mos

Hrs

2,678 Enc9,4063,0006,406Enc

72 ENG2Eff: 11-Feb-2010




Mandatory ≈18-Jul-2023RE2009-26-09 Paragraph (l) General Electric Company - Fan disks - For CF34-3A1, CF34-1A, CF34-3A, CF34-3A2 and CF34-3B, Inspections of Tier 2 Fan Disks

22-Mar-2012Mos

11,674.8Hrs

2,678 Enc9,4473,0006,447Enc

72 ENG1SB 72-A0233Eff: 11-Feb-2010 Complied

With





Generated: 6-Apr-2016 1:16 PM276/429







Mandatory ≈18-Jul-2023RE2009-26-09 Paragraph (l) General Electric Company - Fan disks - For CF34-3A1, CF34-1A, CF34-3A, CF34-3A2 and CF34-3B, Inspections of Tier 2 Fan Disks

19-Mar-2012Mos

11,557.8Hrs

2,678 Enc9,4063,0006,406Enc

72 ENG2Eff: 11-Feb-2010




MandatoryRE (-)2009-26-09 Paragraph (m) General Electric Company - Fan disks - For CF34-3A1, CF34-1A, CF34-3A, CF34-3A2 and CF34-3B, Inspections of Tier 3 Fan Disks

Mos

Hrs

Enc

72 ENG1Eff: 11-Feb-2010



MandatoryRE (-)2009-26-09 Paragraph (m) General Electric Company - Fan disks - For CF34-3A1, CF34-1A, CF34-3A, CF34-3A2 and CF34-3B, Inspections of Tier 3 Fan Disks

Mos

Hrs

Enc

72 ENG2Eff: 11-Feb-2010



MandatoryRE (-)2009-26-09 Paragraph (o) General Electric Company - Fan Disks - Mandatory Terminating Action

Mos

Hrs

Enc

72 ENG1Eff: 11-Feb-2010

Compliance Share DoubleDUE:1. RE -ENGINE - Fan Rotor Assembly (72-21-00) - Shop Level Inspecti...72-A0212 R04ENG172

MandatoryRE (-)2009-26-09 Paragraph (o) General Electric Company - Fan Disks - Mandatory Terminating Action

Mos

Hrs

Enc

72 ENG2Eff: 11-Feb-2010

Compliance Share DoubleDUE:1. RE -ENGINE - Fan Rotor Assembly (72-21-00) - Shop Level Inspecti...72-A0212 R04ENG272

MandatoryRE (-)2010-01-04 General Electric Company - Fan blade

Mos

Hrs

Enc

72 ENG1Eff: 30-Apr-2010

Nextdue Share EarliestDUE: 7,645 Enc1. T 1200 Enc | 2. RE -General Electric Company - Fan blade - For CF34-1A, CF34-3A,...2010-01-04 Paragraph (l)(1)(2)ENG172

Nextdue Share EarliestDUE: 6,795 Enc1. T 350 Enc | 2. RE 600 EncGeneral Electric Company - Fan blade - For CF34-1A, CF34-3A,...2010-01-04 Paragraph (l)(3)(4)(6)ENG172

Nextdue Share EarliestDUE: 12,215.2 Hrs, 6,826 Enc1. T 1220 Enc | 2. RE 100 Hrs, 75 Enc (later)General Electric Company - Fan blade - For CF34-1A, CF34-3A,...2010-01-04 Paragraph (l)(8)(9)(10)ENG172

MandatoryRE (-)2010-01-04 General Electric Company - Fan blade

Mos

Hrs

Enc

72 ENG2Eff: 30-Apr-2010

Nextdue Share EarliestDUE: 7,604 Enc1. T 1200 Enc | 2. RE -General Electric Company - Fan blade - For CF34-1A, CF34-3A,...2010-01-04 Paragraph (l)(1)(2)ENG272

Nextdue Share EarliestDUE: 6,754 Enc1. T 350 Enc | 2. RE 600 EncGeneral Electric Company - Fan blade - For CF34-1A, CF34-3A,...2010-01-04 Paragraph (l)(3)(4)(6)ENG272

Nextdue Share EarliestDUE: 12,098.2 Hrs, 6,785 Enc1. T 1220 Enc | 2. RE 100 Hrs, 75 Enc (later)General Electric Company - Fan blade - For CF34-1A, CF34-3A,...2010-01-04 Paragraph (l)(8)(9)(10)ENG272


Generated: 6-Apr-2016 1:16 PM277/429







Mandatory ≈16-Jul-2018T2010-01-04 Paragraph (l)(1)(2) General Electric Company - Fan blade - For CF34-1A, CF34-3A, CF34-3A2, CF34-3B and CF34-3A1 - Remove fan blades from service.

Mos

Hrs

876 Enc[7,645]1,200Enc

72 ENG1Eff: 25-Jan-2010

Mandatory ≈16-Jul-2018T2010-01-04 Paragraph (l)(1)(2) General Electric Company - Fan blade - For CF34-1A, CF34-3A, CF34-3A2, CF34-3B and CF34-3A1 - Remove fan blades from service.

Mos

Hrs

876 Enc[7,604]1,200Enc

72 ENG2Eff: 25-Jan-2010

Mandatory ≈06-Mar-2016T2010-01-04 Paragraph (l)(3)(4)

(6)

General Electric Company - Fan blade - For CF34-1A, CF34-3A, CF34-3A2, CF34-3B and CF34-3A1, Initial / Repetitive Eddy Current Inspection of the Fan Blades

Mos

Hrs

26 Enc[6,795]350Enc

72 ENG1Eff: 25-Jan-2010

Compliance Share DoubleDUE:1. RE -ENGINE - Fan Rotor (72-21-00) - Field Management Program of ...72-0229 R01ENG172

Mandatory ≈06-Mar-2016T2010-01-04 Paragraph (l)(3)(4)

(6)

General Electric Company - Fan blade - For CF34-1A, CF34-3A, CF34-3A2, CF34-3B and CF34-3A1, Initial / Repetitive Eddy Current Inspection of the Fan Blades

Mos

Hrs

26 Enc[6,754]350Enc

72 ENG2Eff: 25-Jan-2010

Compliance Share DoubleDUE: 6,914 Enc1. T 350 Enc | 2. RE 600 EncENGINE - Fan Rotor (72-21-00) - Field Management Program of ...72-0229 R01ENG272

Mandatory ≈08-Apr-2016RE2010-01-04 Paragraph (l)(8)(9)

(10)

General Electric Company - Fan blade - For CF34-1A, CF34-3A, CF34-3A2, CF34-3B and CF34-3A1, Initial / Repetitive Visual Inspection of the Fan Blade Abradable Rub

Strip for Wear

03-Dec-2015Mos

77.8 Hrs12,215.210012,115.2Hrs

57 Enc6,826756,751Enc

72 ENG1SB 72-0250Complied With

Compliance Share DoubleDUE:1. RE -ENGINE - Fan Stator (72-23-00) - Visual Inspection of Fan Ca...72-0231 R02ENG172

Mandatory ≈08-Apr-2016RE2010-01-04 Paragraph (l)(8)(9)

(10)

General Electric Company - Fan blade - For CF34-1A, CF34-3A, CF34-3A2, CF34-3B and CF34-3A1, Initial / Repetitive Visual Inspection of the Fan Blade Abradable Rub

Strip for Wear

03-Dec-2015Mos

77.8 Hrs12,098.210011,998.2Hrs

57 Enc6,785756,710Enc

72 ENG2SB 72-0250Complied With

Compliance Share DoubleDUE:1. RE -ENGINE - Fan Stator (72-23-00) - Visual Inspection of Fan Ca...72-0231 R02ENG272

MRB ≈25-Sep-2016RE72-00-00-201 Engine - General - Visual Check of Fan Stator for the following: (1) Flowpath Aluminum skin for dents and cracks / (2) Abradable Rub Strip for rubbing

10-Feb-2016Mos

300 Hrs (+40)(12,320.4)-/+4030012,020.4Hrs

6,728Enc

(PKG 300 Eng Hour)

72 ENG2

Ref.:G.E. MM SEI-580 Section 5-21-00 (SOURCE: TLMC 05-20-15)

MRB ≈25-Sep-2016RE72-00-00-201 Engine - General - Visual Check of Fan Stator for the following: (1) Flowpath Aluminum skin for dents and cracks / (2) Abradable Rub Strip for rubbing

10-Feb-2016Mos

300 Hrs (+40)(12,437.4)-/+4030012,137.4Hrs

6,769Enc

(PKG 300 Eng Hour)

72 ENG1


MRB ≈25-Sep-2016RE72-00-00-203 Engine - General - Carry out a visual check of the following: (1) Engine Mounts / (2) Fan Rotor / (3) Fan Stator / (4) Compressor Case / (5) Front Frame, paying particular

attention around AGB Mount Pads / (6) Accessory Gearbox

10-Feb-2016Mos

300 Hrs (+40)(12,437.4)-/+4030012,137.4Hrs

6,769Enc

(PKG 300 Eng Hour)

72 ENG1



Generated: 6-Apr-2016 1:16 PM278/429







MRB ≈25-Sep-2016RE72-00-00-203 Engine - General - Carry out a visual check of the following: (1) Engine Mounts / (2) Fan Rotor / (3) Fan Stator / (4) Compressor Case / (5) Front Frame, paying particular

attention around AGB Mount Pads / (6) Accessory Gearbox

10-Feb-2016Mos

300 Hrs (+40)(12,320.4)-/+4030012,020.4Hrs

6,728Enc

(PKG 300 Eng Hour)

72 ENG2


MRB ≈25-Sep-2016RE72-00-00-206 Engine - General - Visual Check of engine external lines, ports, flanges, clamps, brackets, electrical connectors, engine surface and accessories

10-Feb-2016Mos

300 Hrs (+40)(12,320.4)-/+4030012,020.4Hrs

6,728Enc

(PKG 300 Eng Hour)

72 ENG2


MRB ≈25-Sep-2016RE72-00-00-206 Engine - General - Visual Check of engine external lines, ports, flanges, clamps, brackets, electrical connectors, engine surface and accessories

10-Feb-2016Mos

300 Hrs (+40)(12,437.4)-/+4030012,137.4Hrs

6,769Enc

(PKG 300 Eng Hour)

72 ENG1


MRB ≈25-Sep-2016RE72-00-00-208 Engine - General - Visual check of high pressure turbine section casing, paying particular attention for cracks, bulges, hot spots and security of centre body

10-Feb-2016Mos

300 Hrs (+40)(12,437.4)-/+4030012,137.4Hrs

6,769Enc

(PKG 300 Eng Hour)

72 ENG1


MRB ≈25-Sep-2016RE72-00-00-208 Engine - General - Visual check of high pressure turbine section casing, paying particular attention for cracks, bulges, hot spots and security of centre body

10-Feb-2016Mos

300 Hrs (+40)(12,320.4)-/+4030012,020.4Hrs

6,728Enc

(PKG 300 Eng Hour)

72 ENG2


MRB ≈10-May-2017RE72-00-00-209 Engine - General - Carry out a visual check of the following: (1) Compressor assembly for missing lock tabs on visible Variable Vane Outer Shanknuts / (2) Fan Rotor

Blade Removal Port, Water Drain for blockage / Borescope inspection of outer transition liner. This inspection applies to Engine 350489 and below as instructed in G.E.

SB 72-32 that have not been modified to SB 72-38

10-Feb-2016Mos

600 Hrs (+40)(12,737.4)-/+4060012,137.4Hrs

6,769Enc

(PKG 600 Eng Hour)

72 ENG1


MRB ≈03-May-2017RE72-00-00-209 Engine - General - Carry out a visual check of the following: (1) Compressor assembly for missing lock tabs on visible Variable Vane Outer Shanknuts / (2) Fan Rotor

Blade Removal Port, Water Drain for blockage / Borescope inspection of outer transition liner. This inspection applies to Engine 350489 and below as instructed in G.E.

SB 72-32 that have not been modified to SB 72-38

10-Feb-2016Mos

590.8 Hrs (+40)(12,611.2)-/+4060012,020.4Hrs

6,728Enc

(PKG 600 Eng Hour)

72 ENG2

Ref.:G.E. MM SEI-580 Section 5-21-00 (Tol. Adjustment: -9.2 Hrs) (SOURCE: TLMC 05-20-15)

MRB ≈20-Oct-2017RE72-00-00-210 Engine - General - Borescope inspection of combustion liner / Visual Check for cracks in combustion chamber frame / Borescope inspection of fuel injectors, paying

particular attention to centering in swirlers / Borescope inspection of outer transition liner. This inspection applies to Engine 350489 and below as instructed in G.E. SB

72-32 that have not been modified to SB 72-38

29-Oct-2012Mos

812.3 Hrs (+40)(12,949.7)-/+401,20011,749.7Hrs

Enc

(PKG 1200 Eng Hour)

72 ENG1


MRB ≈20-Oct-2017RE72-00-00-210 Engine - General - Borescope inspection of combustion liner / Visual Check for cracks in combustion chamber frame / Borescope inspection of fuel injectors, paying

particular attention to centering in swirlers / Borescope inspection of outer transition liner. This inspection applies to Engine 350489 and below as instructed in G.E. SB

72-32 that have not been modified to SB 72-38

29-Oct-2012Mos

812.3 Hrs (+40)(12,832.7)-/+401,20011,632.7Hrs

Enc

(PKG 1200 Eng Hour)

72 ENG2



Generated: 6-Apr-2016 1:16 PM279/429







MRB ≈20-Oct-2017RE72-00-00-211 Engine - General - Borescope inspection of turbine section, stage 1 nozzle and HPT stage 1 blades

29-Oct-2012Mos

812.3 Hrs (+40)(12,949.7)-/+401,20011,749.7Hrs

Enc

(PKG 1200 Eng Hour)

72 ENG1


MRB ≈20-Oct-2017RE72-00-00-211 Engine - General - Borescope inspection of turbine section, stage 1 nozzle and HPT stage 1 blades

29-Oct-2012Mos

812.3 Hrs (+40)(12,832.7)-/+401,20011,632.7Hrs

Enc

(PKG 1200 Eng Hour)

72 ENG2


MRB ≈20-Oct-2017RE72-00-00-212 Engine - General (Pre G.E. SB (CF34) 72-11) - Borescope inspection of Power Take-Off (PTO) Part Number 6037T72G01 or 6037T72G06 for forward movement of Carbon

Sleeve

29-Oct-2012Mos

812.3 Hrs (+40)(12,949.7)-/+401,20011,749.7Hrs

Enc

(PKG 1200 Eng Hour)

72 ENG1


MRB ≈20-Oct-2017RE72-00-00-212 Engine - General (Pre G.E. SB (CF34) 72-11) - Borescope inspection of Power Take-Off (PTO) Part Number 6037T72G01 or 6037T72G06 for forward movement of Carbon

Sleeve

29-Oct-2012Mos

812.3 Hrs (+40)(12,832.7)-/+401,20011,632.7Hrs

Enc

(PKG 1200 Eng Hour)

72 ENG2


MRB ≈22-Feb-2021RE72-00-00-213 Engine - General - Mid point inspection

05-Jun-2009Mos

2,417.4 Hrs (+40)(14,554.8)-/+403,00011,554.8Hrs

Enc

(PKG 3000 Eng Hour)

72 ENG1


Compliance Share SingleDUE: 05-Jun-20191. RE 120 MosEngine - General - Borescope Inspection of Engine72-00-00-217 (10 Yrs)ENG172

MRB ≈24-Nov-2019RE72-00-00-213 Engine - General - Mid point inspection

28-Jul-2005Mos

1,818.6 Hrs (+40)(13,839)-/+403,00010,839Hrs

Enc

(PKG 3000 Eng Hour)

72 ENG2


Compliance Share SingleDUE: 27-Jul-20251. RE 120 MosEngine - General - Borescope Inspection of Engine72-00-00-217 (10 Yrs)ENG272

MRB ≈22-Feb-2021RE72-00-00-215 Engine - General - Borescope Compressor / Visual Check of visible areas of compressor casings / Visual Check of variable vanes, paying particular attention for nicks,

dents, cracks and excessive movement

05-Jun-2009Mos

2,417.4 Hrs (+40)(14,554.8)-/+403,00011,554.8Hrs

Enc

(PKG 3000 Eng Hour)

72 ENG1


MRB ≈24-Nov-2019RE72-00-00-215 Engine - General - Borescope Compressor / Visual Check of visible areas of compressor casings / Visual Check of variable vanes, paying particular attention for nicks,

dents, cracks and excessive movement

28-Jul-2005Mos

1,818.6 Hrs (+40)(13,839)-/+403,00010,839Hrs

Enc

(PKG 3000 Eng Hour)

72 ENG2


MRB ≈23-May-2027RE72-00-00-217 Engine - General - Overhaul

05-Jun-2009Mos

5,417.4 Hrs (+40)17,554.8-/+406,00011,554.8Hrs

Enc

72 ENG1

Ref.:G.E. MM SEI-580 Section 5-21-00 (SOURCE: TLMC 05-20-15) (NOTE: If an engine does not reach 3000 hours TSN/TBO before 10 years

since engine installation, a complete borescope inspection of engine must be accomplished.)

Compliance Share SingleDUE: 05-Jun-20191. RE 120 MosEngine - General - Borescope Inspection of Engine72-00-00-217 (10 Yrs)ENG172


Generated: 6-Apr-2016 1:16 PM280/429







MRB ≈23-Feb-2026RE72-00-00-217 Engine - General - Overhaul

28-Jul-2005Mos

4,818.6 Hrs (+40)16,839-/+406,00010,839Hrs

Enc

72 ENG2

Ref.:G.E. MM SEI-580 Section 5-21-00 (SOURCE: TLMC 05-20-15) (NOTE: If an engine does not reach 3000 hours TSN/TBO before 10 years

since engine installation, a complete borescope inspection of engine must be accomplished.)

Compliance Share SingleDUE: 27-Jul-20251. RE 120 MosEngine - General - Borescope Inspection of Engine72-00-00-217 (10 Yrs)ENG272

MRBRE72-00-00-217 (10 Yrs) Engine - General - Borescope Inspection of Engine

9.3 Years (+31 Days)27-Jul-2025-/+112010-Feb-2016Mos

12,020.4Hrs

6,728Enc

72 ENG2

Ref.:G.E. MM SEI-580 Section 5-21-00 (Tol. Adjustment: -193d) (SOURCE: TLMC 05-20-15)

MRBRE72-00-00-217 (10 Yrs) Engine - General - Borescope Inspection of Engine

3.2 Years (+30 Days)05-Jun-2019-/+112005-Jun-2009Mos

Hrs

Enc

72 ENG1


MRB ≈22-Feb-2021RE72-00-00-218 Engine - General - Detailed Inspection of engine accessory gearbox mounts

05-Jun-2009Mos

2,417.4 Hrs (+40)(14,554.8)-/+403,00011,554.8Hrs

Enc

(PKG 3000 Eng Hour)

72 ENG1


MRB ≈24-Nov-2019RE72-00-00-218 Engine - General - Detailed Inspection of engine accessory gearbox mounts

28-Jul-2005Mos

1,818.6 Hrs (+40)(13,839)-/+403,00010,839Hrs

Enc

(PKG 3000 Eng Hour)

72 ENG2


MRB ≈03-May-2017RE72-00-00-219 Engine - General - Oil Sample Check

10-Feb-2016Mos

590.8 Hrs (+40)(12,611.2)-/+4060012,020.4Hrs

6,728Enc

(PKG 600 Eng Hour)

72 ENG2


MRB ≈10-May-2017RE72-00-00-219 Engine - General - Oil Sample Check

10-Feb-2016Mos

600 Hrs (+40)(12,737.4)-/+4060012,137.4Hrs

6,769Enc

(PKG 600 Eng Hour)

72 ENG1


MRB ≈20-Oct-2017RE72-00-00-220 Engine - General (Pre SB 75-2) - B-Sump pressure measurement check

29-Oct-2012Mos

812.3 Hrs (+40)(12,949.7)-/+401,20011,749.7Hrs

Enc

(PKG 1200 Eng Hour)

72 ENG1


MRB ≈20-Oct-2017RE72-00-00-220 Engine - General (Pre SB 75-2) - B-Sump pressure measurement check

29-Oct-2012Mos

812.3 Hrs (+40)(12,832.7)-/+401,20011,632.7Hrs

Enc

(PKG 1200 Eng Hour)

72 ENG2


MRB ≈22-Feb-2021RE72-00-00-221 Engine - General - Visual Check of 6 o’clock c-sump scavenge tube and groove for internal coking

05-Jun-2009Mos

2,417.4 Hrs (+40)(14,554.8)-/+403,00011,554.8Hrs

Enc

(PKG 3000 Eng Hour)

72 ENG1


MRB ≈24-Nov-2019RE72-00-00-221 Engine - General - Visual Check of 6 o’clock c-sump scavenge tube and groove for internal coking

28-Jul-2005Mos

1,818.6 Hrs (+40)(13,839)-/+403,00010,839Hrs

Enc

(PKG 3000 Eng Hour)

72 ENG2



Generated: 6-Apr-2016 1:16 PM281/429







MRB ≈22-Feb-2021RE72-00-00-222 Engine - General - Visual Check of LPT stator assembly P/N 6020T15G14 for tack welding of the pin and clip assemblies. Rework and re-identify if required

05-Jun-2009Mos

2,417.4 Hrs (+40)(14,554.8)3,00011,554.8Hrs

Enc

(PKG 3000 Eng Hour)

72 ENG1


MRB ≈24-Nov-2019RE72-00-00-222 Engine - General - Visual Check of LPT stator assembly P/N 6020T15G14 for tack welding of the pin and clip assemblies. Rework and re-identify if required

28-Jul-2005Mos

1,818.6 Hrs (+40)(13,839)3,00010,839Hrs

Enc

(PKG 3000 Eng Hour)

72 ENG2


MRB ≈22-Feb-2021RE72-00-00-223 Engine - General - Visual Check of HPT stage 1 and stage 2 shrouds

05-Jun-2009Mos

2,417.4 Hrs (+40)(14,554.8)-/+403,00011,554.8Hrs

Enc

(PKG 3000 Eng Hour)

72 ENG1


MRB ≈24-Nov-2019RE72-00-00-223 Engine - General - Visual Check of HPT stage 1 and stage 2 shrouds

28-Jul-2005Mos

1,818.6 Hrs (+40)(13,839)-/+403,00010,839Hrs

Enc

(PKG 3000 Eng Hour)

72 ENG2


MRB ≈22-Feb-2021RE72-00-00-224 Engine - General - Inspect/Check turbine thermocouple harness

05-Jun-2009Mos

2,417.4 Hrs (+40)(14,554.8)-/+403,00011,554.8Hrs

Enc

(PKG 3000 Eng Hour)

72 ENG1


MRB ≈24-Nov-2019RE72-00-00-224 Engine - General - Inspect/Check turbine thermocouple harness

28-Jul-2005Mos

1,818.6 Hrs (+40)(13,839)-/+403,00010,839Hrs

Enc

(PKG 3000 Eng Hour)

72 ENG2


MRB ≈22-Feb-2021RE72-00-00-225 Engine - General - Visual Check of turbine nozzles

05-Jun-2009Mos

2,417.4 Hrs (+40)(14,554.8)-/+403,00011,554.8Hrs

Enc

(PKG 3000 Eng Hour)

72 ENG1


MRB ≈24-Nov-2019RE72-00-00-225 Engine - General - Visual Check of turbine nozzles

28-Jul-2005Mos

1,818.6 Hrs (+40)(13,839)-/+403,00010,839Hrs

Enc

(PKG 3000 Eng Hour)

72 ENG2


MRB ≈22-Feb-2021RE72-00-00-226 Engine - General - Detailed visual inspection of the swirlers after removal of the injectors

05-Jun-2009Mos

2,417.4 Hrs (+40)(14,554.8)-/+403,00011,554.8Hrs

Enc

(PKG 3000 Eng Hour)

72 ENG1


MRB ≈24-Nov-2019RE72-00-00-226 Engine - General - Detailed visual inspection of the swirlers after removal of the injectors

28-Jul-2005Mos

1,818.6 Hrs (+40)(13,839)-/+403,00010,839Hrs

Enc

(PKG 3000 Eng Hour)

72 ENG2


MRB ≈22-Feb-2021RE72-00-00-227 Engine - General - Visual Check of primary swirlers, paying particular attention for wear

05-Jun-2009Mos

2,417.4 Hrs (+40)(14,554.8)-/+403,00011,554.8Hrs

Enc

(PKG 3000 Eng Hour)

72 ENG1



Generated: 6-Apr-2016 1:16 PM282/429







MRB ≈24-Nov-2019RE72-00-00-227 Engine - General - Visual Check of primary swirlers, paying particular attention for wear

28-Jul-2005Mos

1,818.6 Hrs (+40)(13,839)-/+403,00010,839Hrs

Enc

(PKG 3000 Eng Hour)

72 ENG2


MRB ≈22-Feb-2021RE72-00-00-228 Engine - General - Visual Check of stage 1 and stage 2 nozzle assemblies

05-Jun-2009Mos

2,417.4 Hrs (+40)(14,554.8)-/+403,00011,554.8Hrs

Enc

(PKG 3000 Eng Hour)

72 ENG1


MRB ≈24-Nov-2019RE72-00-00-228 Engine - General - Visual Check of stage 1 and stage 2 nozzle assemblies

28-Jul-2005Mos

1,818.6 Hrs (+40)(13,839)-/+403,00010,839Hrs

Enc

(PKG 3000 Eng Hour)

72 ENG2


MRB ≈22-Feb-2021RE72-00-00-229 Engine - General - Visual Check of combustion liner after disassembly

Mos

2,417.4 Hrs (+40)(14,554.8)-/+403,000Hrs

Enc

(PKG 3000 Eng Hour)

72 ENG1


MRB ≈24-Nov-2019RE72-00-00-229 Engine - General - Visual Check of combustion liner after disassembly

Mos

1,818.6 Hrs (+40)(13,839)-/+403,000Hrs

Enc

(PKG 3000 Eng Hour)

72 ENG2


MRB ≈22-Feb-2021RE72-00-00-230 Engine - General - Check combustion section fuel injector heat shields for looseness

05-Jun-2009Mos

2,417.4 Hrs (+40)(14,554.8)-/+403,00011,554.8Hrs

Enc

(PKG 3000 Eng Hour)

72 ENG1


MRB ≈24-Nov-2019RE72-00-00-230 Engine - General - Check combustion section fuel injector heat shields for looseness

28-Jul-2005Mos

1,818.6 Hrs (+40)(13,839)-/+403,00010,839Hrs

Enc

(PKG 3000 Eng Hour)

72 ENG2


MRB ≈22-Feb-2021RE72-00-00-231 Engine - General - Visual Check of fan disk to ensure bushings are not protruding

05-Jun-2009Mos

2,417.4 Hrs (+40)(14,554.8)-/+403,00011,554.8Hrs

Enc

(PKG 3000 Eng Hour)

72 ENG1


MRB ≈24-Nov-2019RE72-00-00-231 Engine - General - Visual Check of fan disk to ensure bushings are not protruding

28-Jul-2005Mos

1,818.6 Hrs (+40)(13,839)-/+403,00010,839Hrs

Enc

(PKG 3000 Eng Hour)

72 ENG2


Servicing - Optional ≈25-Sep-2016RE72-00-00-301 Engine - General - Compressor Waterwash

10-Feb-2016Mos

300 Hrs (+40)(12,437.4)-/+4030012,137.4Hrs

6,769Enc

(PKG 300 Eng Hour)

72 ENG1

Ref.:G.E. M.M. SEI-580 Section 5-21-00, Ref.:G.E. M.M. SEI-780 (ZONE: 410, 420) (ACCESS: 412-AT, 414-AT, 422-AT, 424-AT) (SOURCE: MPD 3.3)

(NOTE: For engine model CF34-1A/-3A/-3A2, it is recommended that this task be done prior to the Power Assurance Check.)


Generated: 6-Apr-2016 1:16 PM283/429







Servicing - Optional ≈25-Sep-2016RE72-00-00-301 Engine - General - Compressor Waterwash

10-Feb-2016Mos

300 Hrs (+40)(12,320.4)-/+4030012,020.4Hrs

6,728Enc

(PKG 300 Eng Hour)

72 ENG2

Ref.:G.E. M.M. SEI-580 Section 5-21-00, Ref.:G.E. M.M. SEI-780 (ZONE: 410, 420) (ACCESS: 412-AT, 414-AT, 422-AT, 424-AT) (SOURCE: MPD 3.3)

(NOTE: For engine model CF34-1A/-3A/-3A2, it is recommended that this task be done prior to the Power Assurance Check.)

Servicing - Optional ≈25-Sep-2016RE72-00-00-302 Engine - General (Engine model CF34-1A/-3A/-3A2 only) - Power Assurance Check

10-Feb-2016Mos

300 Hrs (+40)(12,320.4)-/+4030012,020.4Hrs

6,728Enc

(PKG 300 Eng Hour)

72 ENG2

Ref.:G.E. M.M. SEI-580 Section 5-21-00 (ZONE: 220, 410, 420) (SOURCE: MPD 3.3) (NOTE: It is recommended that this task be done following

the Compressor Waterwash Check.)

Servicing - Optional ≈25-Sep-2016RE72-00-00-302 Engine - General (Engine model CF34-1A/-3A/-3A2 only) - Power Assurance Check

10-Feb-2016Mos

300 Hrs (+40)(12,437.4)-/+4030012,137.4Hrs

6,769Enc

(PKG 300 Eng Hour)

72 ENG1

Ref.:G.E. M.M. SEI-580 Section 5-21-00 (ZONE: 220, 410, 420) (SOURCE: MPD 3.3) (NOTE: It is recommended that this task be done following

the Compressor Waterwash Check.)

Recommended ≈20-Dec-1989T72-0005 R06 ENGINE - Life Improvement of Certain High-Pressure and Low-Pressure Turbine Parts by Rework

Mos

OVD3,0003,000Hrs

Enc

72 ENG1

Recommended ≈20-Dec-1989T72-0005 R06 ENGINE - Life Improvement of Certain High-Pressure and Low-Pressure Turbine Parts by Rework

Mos

OVD3,0003,000Hrs

Enc

72 ENG2

RecommendedRE (-)72-0008 R02 ENGINE Modification of CF341A Engines to CF343A Engines

Mos

Hrs

Enc

72 ENG1Eff: 04-Oct-1989

RecommendedRE (-)72-0008 R02 ENGINE Modification of CF341A Engines to CF343A Engines

Mos

Hrs

Enc

72 ENG2Eff: 04-Oct-1989

RecommendedRE (-)72-0010 R02 ENGINE - Power Takeoff (PTO) Drive Assembly: Replacement of Duplex Ball Bearing

Mos

Hrs

Enc

72 ENG1Eff: 25-Apr-1991

Also ConsiderDUE:1. RE -ENGINE - Power Takeoff (PTO) Drive Assembly: Rework of PTO D...72-0011 R03ENG172

Also ConsiderDUE:1. RE -ENGINE - Power Take off (PTO) Drive Assembly: Increased Torq...72-0013 R00ENG172

RecommendedRE (-)72-0010 R02 ENGINE - Power Takeoff (PTO) Drive Assembly: Replacement of Duplex Ball Bearing

Mos

Hrs

Enc

72 ENG2Eff: 25-Apr-1991




Generated: 6-Apr-2016 1:16 PM284/429







RecommendedRE (-)72-0011 R00 ENGINE Power Takeoff (PTO) Drive Assembly: Rework of PTO Drive Assembly

Mos

Hrs

Enc

72 ENG1Eff: 09-Jun-1989


Mos

Hrs

Enc

72 ENG2Eff: 09-Jun-1989


Mos

Hrs

Enc

72 ENG1Eff: 31-Aug-1989


Mos

Hrs

Enc

72 ENG2Eff: 31-Aug-1989


Mos

Hrs

Enc

72 ENG1Eff: 25-Apr-1991


Mos

Hrs

Enc

72 ENG2Eff: 25-Apr-1991

RecommendedRE (-)72-0011 R03 ENGINE - Power Takeoff (PTO) Drive Assembly: Rework of PTO Drive Assembly

Mos

Hrs

Enc

72 ENG1Eff: 27-Apr-2005

RecommendedRE (-)72-0011 R03 ENGINE - Power Takeoff (PTO) Drive Assembly: Rework of PTO Drive Assembly

Mos

Hrs

Enc

72 ENG2Eff: 27-Apr-2005

RecommendedRE (-)72-0013 R00 ENGINE - Power Take off (PTO) Drive Assembly: Increased Torque on Horizontal and Vertical Axis Locknuts

Mos

Hrs

Enc

72 ENG1Eff: 25-Apr-1991


Also ConsiderDUE:1. T A/R | 2. RE -ENGINE - General (72-00-00) - Change of CF34-3A and CF34-3A2...72-0263 R00ENG172

RecommendedRE (-)72-0013 R00 ENGINE - Power Take off (PTO) Drive Assembly: Increased Torque on Horizontal and Vertical Axis Locknuts

Mos

Hrs

Enc

72 ENG2Eff: 25-Apr-1991




Generated: 6-Apr-2016 1:16 PM285/429







RecommendedRE (-)72-0014 R00 ENGINE - Accessory Drive Gearbox (AGB): Replacement of Axis-A Duplex Bearing and Axis-BB Ball Bearing

Mos

Hrs

Enc

72 ENG1Eff: 07-May-1991


Mos

Hrs

Enc

72 ENG2Eff: 07-May-1991


Mos

Hrs

Enc

72 ENG1Eff: 16-Dec-1991


Mos

Hrs

Enc

72 ENG2Eff: 16-Dec-1991


Mos

Hrs

Enc

72 ENG1Eff: 07-Jan-1992

Also ConsiderDUE:1. RE -ENGINE - Accessory Gearbox Assembly (72-62-00) - Introductio...72-0260 R03ENG172


Mos

Hrs

Enc

72 ENG2Eff: 07-Jan-1992


RecommendedT (A/R)72-0014 R03 ENGINE - Accessory Drive Gearbox (AGB): Replacement of Axis-A Duplex Bearing and Axis-BB Ball Bearing

Mos

Hrs

Enc

72 ENG1Eff: 30-Jun-2015

(NOTE: Effectivity: Engines which do not have AGB PN 6014T81G24)

RecommendedT (A/R)72-0014 R03 ENGINE - Accessory Drive Gearbox (AGB): Replacement of Axis-A Duplex Bearing and Axis-BB Ball Bearing

Mos

Hrs

Enc

72 ENG2Eff: 30-Jun-2015

(NOTE: Effectivity: Engines which do not have AGB PN 6014T81G24)

RecommendedRE (-)72-0015 R02 ENGINE - On-Wing Replacement of Accessory Drive Gearbox (AGB) Axis-BB Ball Bearing

Mos

Hrs

Enc

72 ENG1Eff: 03-Aug-1995

RecommendedRE (-)72-0015 R02 ENGINE - On-Wing Replacement of Accessory Drive Gearbox (AGB) Axis-BB Ball Bearing

Mos

Hrs

Enc

72 ENG2Eff: 03-Aug-1995


Generated: 6-Apr-2016 1:16 PM286/429







RecommendedRE (-)72-0016 R00 ENGINE Rework of the Forward Fan Shaft

Mos

Hrs

Enc

72 ENG1Eff: 01-May-1991


Mos

Hrs

Enc

72 ENG2Eff: 01-May-1991


Mos

Hrs

Enc

72 ENG1Eff: 12-Feb-1993


Mos

Hrs

Enc

72 ENG2Eff: 12-Feb-1993

RecommendedRE (-)72-0016 R02 ENGINE - Rework of the Forward Fan Shaft

Mos

Hrs

Enc

72 ENG1Eff: 17-Aug-2007

Also ConsiderDUE:1. RE -ENGINE - General (72-00-00) - Upgrade of CF34-1A and CF34-3A...72-0195 R08ENG172


RecommendedRE (-)72-0016 R02 ENGINE - Rework of the Forward Fan Shaft

Mos

Hrs

Enc

72 ENG2Eff: 17-Aug-2007



RecommendedRE (-)72-0017 R02 ENGINE - Rework of Fan Disk PN 6020T62G04 Using Enlarged Bushings

Mos

Hrs

Enc

72 ENG1Eff: 21-Apr-1993

RecommendedRE (-)72-0017 R02 ENGINE - Rework of Fan Disk PN 6020T62G04 Using Enlarged Bushings

Mos

Hrs

Enc

72 ENG2Eff: 21-Apr-1993

RecommendedT (A/R)72-0019 R02 ENGINE - Improved Coating for Compressor Stator Casing and Compressor Rotor Front and Rear Spools

Mos

Hrs

Enc

72 ENG1Eff: 21-Apr-1993



Generated: 6-Apr-2016 1:16 PM287/429







RecommendedT (A/R)72-0019 R02 ENGINE - Improved Coating for Compressor Stator Casing and Compressor Rotor Front and Rear Spools

Mos

Hrs

Enc

72 ENG2Eff: 21-Apr-1993


RecommendedRE (-)72-0021 R00 ENGINE - Power Takeoff (PTO) Drive Assembly: Replacement of Radial Duplex Bearing

Mos

Hrs

Enc

72 ENG1Eff: 01-May-1991


Mos

Hrs

Enc

72 ENG2Eff: 01-May-1991


Mos

Hrs

Enc

72 ENG1Eff: 17-Dec-1991


Mos

Hrs

Enc

72 ENG2Eff: 17-Dec-1991


Mos

Hrs

Enc

72 ENG1Eff: 21-Apr-1993




Mos

Hrs

Enc

72 ENG2Eff: 21-Apr-1993



RecommendedRE (-)72-0022 R01 ENGINE - Replacement of Combustion Liner Primary Swirlers

Mos

Hrs

Enc

72 ENG1Eff: 05-Dec-1991

RecommendedRE (-)72-0022 R01 ENGINE - Replacement of Combustion Liner Primary Swirlers

Mos

Hrs

Enc

72 ENG2Eff: 05-Dec-1991

RecommendedRE (-)72-0023 R03 ENGINE - Replacement of CF34-3A/-3A2 Stage 1 High-Pressure Turbine (HPT) Blades, and Stages 1 and 2 Wire Seals

Mos

Hrs

Enc

72 ENG1


Generated: 6-Apr-2016 1:16 PM288/429







RecommendedRE (-)72-0023 R03 ENGINE - Replacement of CF34-3A/-3A2 Stage 1 High-Pressure Turbine (HPT) Blades, and Stages 1 and 2 Wire Seals

Mos

Hrs

Enc

72 ENG2

RecommendedRE (-)72-0027 R01 ENGINE - Inspection of Low-Pressure Turbine (LPT) Borescope Plugs PN 5071T39G02 and Installation of LPT Borescope Plug Covers PN 3904T92P01

Mos

Hrs

Enc

72 ENG1Eff: 24-Jan-1994

Also ConsiderDUE:1. RE -ENGINE - Rework of the Borescope Plug Bosses on the Low-Pres...72-0037 R01ENG172

RecommendedRE (-)72-0027 R01 ENGINE - Inspection of Low-Pressure Turbine (LPT) Borescope Plugs PN 5071T39G02 and Installation of LPT Borescope Plug Covers PN 3904T92P01

Mos

Hrs

Enc

72 ENG2Eff: 24-Jan-1994

Also ConsiderDUE:1. RE -ENGINE - Rework of the Borescope Plug Bosses on the Low-Pres...72-0037 R01ENG272

RecommendedRE (-)72-0028 R00 ENGINE - Accessory Drive Gearbox (AGB): Improved Axis-BB Rear Ball Bearing

Mos

Hrs

Enc

72 ENG1Eff: 21-Oct-1992



Mos

Hrs

Enc

72 ENG2Eff: 21-Oct-1992



Mos

Hrs

Enc

72 ENG1Eff: 08-Jul-2015


Mos

Hrs

Enc

72 ENG2Eff: 08-Jul-2015

RecommendedRE (-)72-0030 R00 ENGINE Asbestos Elimination

Mos

Hrs

Enc

72 ENG1Eff: 30-Jul-1993


Mos

Hrs

Enc

72 ENG2Eff: 30-Jul-1993


Mos

Hrs

Enc

72 ENG1Eff: 08-Mar-1995


Generated: 6-Apr-2016 1:16 PM289/429








Mos

Hrs

Enc

72 ENG2Eff: 08-Mar-1995

RecommendedRE (-)72-0030 R02 ENGINE - Asbestos Elimination

Mos

Hrs

Enc

72 ENG1Eff: 22-Jan-2008

RecommendedRE (-)72-0030 R02 ENGINE - Asbestos Elimination

Mos

Hrs

Enc

72 ENG2Eff: 22-Jan-2008

RecommendedT (A/R)72-0030 R03 ENGINE - Asbestos Elimination

Mos

Hrs

Enc

72 ENG1Eff: 18-Jul-2008

RecommendedT (A/R)72-0030 R03 ENGINE - Asbestos Elimination

Mos

Hrs

Enc

72 ENG2Eff: 18-Jul-2008

OptionalT (A/R)72-0031 R01 ENGINE - Replacement of CF34-1A/-3A/-3A2 Stage 1 High-Pressure Turbine (HPT) Blades, Stage 1 High-Pressure Turbine (HPT) Baffles, and Stages 1 and 2 Wire Seals

Mos

Hrs

Enc

72 ENG1Eff: 15-Jul-1993


OptionalT (A/R)72-0031 R01 ENGINE - Replacement of CF34-1A/-3A/-3A2 Stage 1 High-Pressure Turbine (HPT) Blades, Stage 1 High-Pressure Turbine (HPT) Baffles, and Stages 1 and 2 Wire Seals

Mos

Hrs

Enc

72 ENG2Eff: 15-Jul-1993


RecommendedRE (-)72-0032 R01 ENGINE - Borescope Inspection of the Turbine Transition Assembly Outer Liner

Mos

Hrs

Enc

72 ENG1Eff: 20-Oct-1993

(NOTE: For engines over 1,200 hours, inspect within the next 300 hours. For engines below 1,200 hours, inspect at first scheduled 1,200 hour

borescope inspection.)

RecommendedRE (-)72-0032 R01 ENGINE - Borescope Inspection of the Turbine Transition Assembly Outer Liner

Mos

Hrs

Enc

72 ENG2Eff: 20-Oct-1993

(NOTE: For engines over 1,200 hours, inspect within the next 300 hours. For engines below 1,200 hours, inspect at first scheduled 1,200 hour

borescope inspection.)

RecommendedRE (-)72-0034 R01 ENGINE - Replacement of CF34-1A Stage 1 High-Pressure Turbine (HPT) Blades, and Stages 1 and 2 Wire Seals

Mos

Hrs

Enc

72 ENG1Eff: 20-Oct-1993


Generated: 6-Apr-2016 1:16 PM290/429







RecommendedRE (-)72-0034 R01 ENGINE - Replacement of CF34-1A Stage 1 High-Pressure Turbine (HPT) Blades, and Stages 1 and 2 Wire Seals

Mos

Hrs

Enc

72 ENG2Eff: 20-Oct-1993

Category 7RE (-)72-0035 R00 ENGINE Rear Main Mount: Rework of Additional Hole for Fire Detection System Harness

Mos

Hrs

Enc

72 ENG1Eff: 17-Jan-2003

Category 7RE (-)72-0035 R00 ENGINE Rear Main Mount: Rework of Additional Hole for Fire Detection System Harness

Mos

Hrs

Enc

72 ENG2Eff: 17-Jan-2003

Cat. 7 - OptionalT (A/R)72-0035 R01 ENGINE - Rear Main Mount: Rework of Additional Hole for Fire Detection System Harness

Mos

Hrs

Enc

72 ENG1Eff: 17-Jan-2003


Cat. 7 - OptionalT (A/R)72-0035 R01 ENGINE - Rear Main Mount: Rework of Additional Hole for Fire Detection System Harness

Mos

Hrs

Enc

72 ENG2Eff: 17-Jan-2003


Cat. 3 - RecommendedRE (-)72-0037 R01 ENGINE - Rework of the Borescope Plug Bosses on the Low-Pressure Turbine Casing

Mos

Hrs

Enc

72 ENG1Eff: 28-Jun-2000

Cat. 3 - RecommendedRE (-)72-0037 R01 ENGINE - Rework of the Borescope Plug Bosses on the Low-Pressure Turbine Casing

Mos

Hrs

Enc

72 ENG2Eff: 28-Jun-2000

RecommendedRE (-)72-0038 R02 ENGINE - Replacement of Forward Transition Liner Seal and Turbine Transition Outer Liner

Mos

Hrs

Enc

72 ENG1

(NOTE: It is recommended that this Service Bulletin be accomplished within the next 300 hours for those operators that have completed the

3000 hour hot section inspection and retained the original liner and seal in their unmodified condition (not hardcoated).It is recommended for

those operators that have not completed the 3000 hours hot section inspection that this Service Bulletin be accomplished at the 3000 hour hot

section inspection.)

RecommendedRE (-)72-0038 R02 ENGINE - Replacement of Forward Transition Liner Seal and Turbine Transition Outer Liner

Mos

Hrs

Enc

72 ENG2

(NOTE: It is recommended that this Service Bulletin be accomplished within the next 300 hours for those operators that have completed the

3000 hour hot section inspection and retained the original liner and seal in their unmodified condition (not hardcoated).It is recommended for

those operators that have not completed the 3000 hours hot section inspection that this Service Bulletin be accomplished at the 3000 hour hot

section inspection.)

OptionalT (A/R)72-0039 R00 ENGINE - Rework of Rear C-Sump Cover: Vent Tube Screen

Mos

Hrs

Enc

72 ENG1Eff: 26-Jan-1994


Generated: 6-Apr-2016 1:16 PM291/429







OptionalT (A/R)72-0039 R00 ENGINE - Rework of Rear C-Sump Cover: Vent Tube Screen

Mos

Hrs

Enc

72 ENG2Eff: 26-Jan-1994

Category 4RE (-)72-0040 R00 ENGINE Rework of the Compressor Rotor Assembly

Mos

Hrs

Enc

72 ENG1Eff: 18-Feb-1994

Category 4RE (-)72-0040 R00 ENGINE Rework of the Compressor Rotor Assembly

Mos

Hrs

Enc

72 ENG2Eff: 18-Feb-1994

Cat. 4 - RecommendedT (A/R)72-0040 R01 ENGINE - Rework of the Compressor Rotor Assembly

Mos

Hrs

Enc

72 ENG1Eff: 30-Aug-2006


Cat. 4 - RecommendedT (A/R)72-0040 R01 ENGINE - Rework of the Compressor Rotor Assembly

Mos

Hrs

Enc

72 ENG2Eff: 30-Aug-2006


RecommendedRE (-)72-0041 R00 ENGINE - Replacement of the Borescope Plug in the High-Pressure Turbine Casing

Mos

Hrs

Enc

72 ENG1Eff: 05-May-1994

RecommendedRE (-)72-0041 R00 ENGINE - Replacement of the Borescope Plug in the High-Pressure Turbine Casing

Mos

Hrs

Enc

72 ENG2Eff: 05-May-1994

RecommendedRE (-)72-0043 R00 ENGINE - Replacement of the Engine Identification Plate

Mos

Hrs

Enc

72 ENG1Eff: 10-Jun-1994

RecommendedRE (-)72-0043 R00 ENGINE - Replacement of the Engine Identification Plate

Mos

Hrs

Enc

72 ENG2Eff: 10-Jun-1994

RecommendedRE (-)72-0046 R00 ENGINE - One-Time Visual and Torque Inspection of the Total Temperature and Pressure Boss Cap

Mos

Hrs

Enc

72 ENG1Eff: 08-Dec-1994


Generated: 6-Apr-2016 1:16 PM292/429







RecommendedRE (-)72-0046 R00 ENGINE - One-Time Visual and Torque Inspection of the Total Temperature and Pressure Boss Cap

Mos

Hrs

Enc

72 ENG2Eff: 08-Dec-1994

Category 9RE (-)72-0048 R00 ENGINE General Hardware Exposed to Abnormal Operating Events

Mos

Hrs

Enc

72 ENG1Eff: 26-Jan-1995


Mos

Hrs

Enc

72 ENG2Eff: 26-Jan-1995


Mos

Hrs

Enc

72 ENG1Eff: 08-Sep-1995


Mos

Hrs

Enc

72 ENG2Eff: 08-Sep-1995


Mos

Hrs

Enc

72 ENG1Eff: 26-Apr-1999


Mos

Hrs

Enc

72 ENG2Eff: 26-Apr-1999


Mos

Hrs

Enc

72 ENG1Eff: 29-Jun-2001


Mos

Hrs

Enc

72 ENG2Eff: 29-Jun-2001


Mos

Hrs

Enc

72 ENG1Eff: 28-Aug-2001


Mos

Hrs

Enc

72 ENG2Eff: 28-Aug-2001


Generated: 6-Apr-2016 1:16 PM293/429







Cat. 9 - InformationalRE (-)72-0048 R05 ENGINE - General - Hardware Exposed to Abnormal Operating Events

Mos

Hrs

Enc

72 ENG1Eff: 21-Apr-2005


Mos

Hrs

Enc

72 ENG2Eff: 21-Apr-2005


Mos

Hrs

Enc

72 ENG1Eff: 18-May-2006


Mos

Hrs

Enc

72 ENG2Eff: 18-May-2006


Mos

Hrs

Enc

72 ENG1Eff: 23-Apr-2012


Mos

Hrs

Enc

72 ENG2Eff: 23-Apr-2012


Mos

Hrs

Enc

72 ENG1Eff: 05-Nov-2013


Mos

Hrs

Enc

72 ENG2Eff: 05-Nov-2013

RecommendedRE (-)72-0049 R01 ENGINE - Introduction of Kalrez Preformed Packing PN J1400P044

Mos

Hrs

Enc

72 ENG1Eff: 04-Dec-1995


RecommendedRE (-)72-0049 R01 ENGINE - Introduction of Kalrez Preformed Packing PN J1400P044

Mos

Hrs

Enc

72 ENG2Eff: 04-Dec-1995



Generated: 6-Apr-2016 1:16 PM294/429







Category 1RE (-)72-0051 R00 ENGINE General (720000) Compliance and Interchangeability Statements Used in CF34BJ Service Bulletins

Mos

Hrs

Enc

72 ENG1Eff: 15-Jun-1995

Category 1RE (-)72-0051 R00 ENGINE General (720000) Compliance and Interchangeability Statements Used in CF34BJ Service Bulletins

Mos

Hrs

Enc

72 ENG2Eff: 15-Jun-1995

Cat. 9 - InformationalT (A/R)72-0051 R01 ENGINE - General (72-00-00) - Compliance and Interchangeability Statements Used in CF34-BJ Service Bulletins

Mos

Hrs

Enc

72 ENG1Eff: 11-May-2012

Cat. 9 - InformationalT (A/R)72-0051 R01 ENGINE - General (72-00-00) - Compliance and Interchangeability Statements Used in CF34-BJ Service Bulletins

Mos

Hrs

Enc

72 ENG2Eff: 11-May-2012

OptionalT (A/R)72-0052 R00 ENGINE - Alternate Parts for Upgrade of Compressor Rotor Assemblies During LCF Changes

Mos

Hrs

Enc

72 ENG1Eff: 25-Jan-1996

OptionalT (A/R)72-0052 R00 ENGINE - Alternate Parts for Upgrade of Compressor Rotor Assemblies During LCF Changes

Mos

Hrs

Enc

72 ENG2Eff: 25-Jan-1996

RecommendedRE (-)72-0053 R00 ENGINE - Recommended Upgrade Program to Reduce Unscheduled Engine Removals for CF34-1A/-3A/-3A2 Model Engines

Mos

+500Hrs

Enc

72 ENG1Eff: 27-Sep-1996

(NOTE: Compliance Operators of affected CF34-1A/-3A/-3A2 model engines will receive GE financial participation, if they comply with this

Service Bulletin prior to or concurrent with hot section inspection, between 2000-2500 hours TSN.)

RecommendedRE (-)72-0053 R00 ENGINE - Recommended Upgrade Program to Reduce Unscheduled Engine Removals for CF34-1A/-3A/-3A2 Model Engines

Mos

+500Hrs

Enc

72 ENG2Eff: 27-Sep-1996

(NOTE: Compliance Operators of affected CF34-1A/-3A/-3A2 model engines will receive GE financial participation, if they comply with this

Service Bulletin prior to or concurrent with hot section inspection, between 2000-2500 hours TSN.)

Category 3RE (-)72-0054 R00 ENGINE Rework of the HighPressure Turbine Stator Borescope Plugs to Threaded Configuration

Mos

Hrs

Enc

72 ENG1Eff: 04-Dec-1995


Mos

Hrs

Enc

72 ENG2Eff: 04-Dec-1995


Generated: 6-Apr-2016 1:16 PM295/429








Mos

Hrs

Enc

72 ENG1


Mos

Hrs

Enc

72 ENG2


Mos

Hrs

Enc

72 ENG1Eff: 08-Jun-2000


Mos

Hrs

Enc

72 ENG2Eff: 08-Jun-2000

Cat. 3 - RecommendedRE (-)72-0054 R03 ENGINE - Rework of the High-Pressure Turbine Stator Borescope Plugs to Threaded Configuration

Mos

Hrs

Enc

72 ENG1Eff: 14-Mar-2007

Cat. 3 - RecommendedRE (-)72-0054 R03 ENGINE - Rework of the High-Pressure Turbine Stator Borescope Plugs to Threaded Configuration

Mos

Hrs

Enc

72 ENG2Eff: 14-Mar-2007

RecommendedRE (-)72-0055 R00 ENGINE Fan Rotor Introduction of Improved LCF Fan Disks

Mos

Hrs

Enc

72 ENG1Eff: 17-Jan-2003

RecommendedRE (-)72-0055 R00 ENGINE Fan Rotor Introduction of Improved LCF Fan Disks

Mos

Hrs

Enc

72 ENG2Eff: 17-Jan-2003

RecommendedRE (-)72-0055 R01 ENGINE - Fan Rotor - Introduction of Improved LCF Fan Disks

Mos

Hrs

Enc

72 ENG1Eff: 17-Jan-2003

RecommendedRE (-)72-0055 R01 ENGINE - Fan Rotor - Introduction of Improved LCF Fan Disks

Mos

Hrs

Enc

72 ENG2Eff: 17-Jan-2003

RecommendedRE (-)72-0056 R00 ENGINE - Engine Waterwash at 300-Hours

Mos

Hrs

Enc

72 ENG1Eff: 22-Jul-1996


Generated: 6-Apr-2016 1:16 PM296/429







RecommendedRE (-)72-0056 R00 ENGINE - Engine Waterwash at 300-Hours

Mos

Hrs

Enc

72 ENG2Eff: 22-Jul-1996

RecommendedRE (-)72-0057 R00 FUEL SYSTEM - Accessory Drive Gearbox (AGB) - Replacement of Axis-J Ball Bearing PN 4017T02P01/P03 with New Roller Bearing PN 4017T12P03/P04

Mos

Hrs

Enc

72 ENG1Eff: 18-Mar-1997


Mos

Hrs

Enc

72 ENG2Eff: 18-Mar-1997


Mos

Hrs

Enc

72 ENG1Eff: 01-Jan-1998


Mos

Hrs

Enc

72 ENG2Eff: 01-Jan-1998


Mos

Hrs

Enc

72 ENG1Eff: 06-Jun-1999


Mos

Hrs

Enc

72 ENG2Eff: 06-Jun-1999


Mos

Hrs

Enc

72 ENG1Eff: 11-Feb-1999





Mos

Hrs

Enc

72 ENG2Eff: 11-Feb-1999





Generated: 6-Apr-2016 1:16 PM297/429







RecommendedRE (-)72-0058 R00 ENGINE Compressor VanetoBlade Axial Clearance Increase

Mos

Hrs

Enc

72 ENG1Eff: 08-Apr-1997


Mos

Hrs

Enc

72 ENG2Eff: 08-Apr-1997


Mos

Hrs

Enc

72 ENG1Eff: 12-Nov-1999


Mos

Hrs

Enc

72 ENG2Eff: 12-Nov-1999

RecommendedRE (-)72-0058 R02 ENGINE - Compressor Vane-to-Blade Axial Clearance Increase

Mos

Hrs

Enc

72 ENG1Eff: 13-Jan-2004

RecommendedRE (-)72-0058 R02 ENGINE - Compressor Vane-to-Blade Axial Clearance Increase

Mos

Hrs

Enc

72 ENG2Eff: 13-Jan-2004

RecommendedT (A/R)72-0058 R03 ENGINE - Compressor Vane-to-Blade Axial Clearance Increase

Mos

Hrs

Enc

72 ENG1Eff: 27-Apr-2006

RecommendedT (A/R)72-0058 R03 ENGINE - Compressor Vane-to-Blade Axial Clearance Increase

Mos

Hrs

Enc

72 ENG2Eff: 27-Apr-2006

Category 3RE (-)72-0060 R00 ENGINE Rework of the Power Takeoff (PTO) Assemblies PN 6037T72G12/G16/G17 and Introduction of PTO Assembly PN 6037T72G18

Mos

Hrs

Enc

72 ENG1Eff: 16-Apr-1997


Mos

Hrs

Enc

72 ENG2Eff: 16-Apr-1997


Mos

Hrs

Enc

72 ENG1


Generated: 6-Apr-2016 1:16 PM298/429








Mos

Hrs

Enc

72 ENG2


Mos

Hrs

Enc

72 ENG1


Mos

Hrs

Enc

72 ENG2

Cat. 3 - RecommendedT (A/R)72-0060 R03 ENGINE - Rework of the Power Takeoff (PTO) Assemblies PN 6037T72G12/G16/G17 and Introduction of PTO Assembly PN 6037T72G18

Mos

Hrs

Enc

72 ENG1Eff: 11-Mar-2003

Cat. 3 - RecommendedT (A/R)72-0060 R03 ENGINE - Rework of the Power Takeoff (PTO) Assemblies PN 6037T72G12/G16/G17 and Introduction of PTO Assembly PN 6037T72G18

Mos

Hrs

Enc

72 ENG2Eff: 11-Mar-2003

RecommendedRE (-)72-0061 R00 ENGINE - Stage 1 Compressor Rotor Disk PN 6087T00G02 Broach Spacing

Mos

Hrs

Enc

72 ENG1Eff: 19-May-1997

RecommendedRE (-)72-0061 R00 ENGINE - Stage 1 Compressor Rotor Disk PN 6087T00G02 Broach Spacing

Mos

Hrs

Enc

72 ENG2Eff: 19-May-1997

RecommendedT (A/R)72-0062 R00 ENGINE - Introduction of Improved High-Pressure Turbine (HPT) Stage 1 Blades with Internal Coating

Mos

Hrs

Enc

72 ENG1Eff: 18-Jul-1997

RecommendedT (A/R)72-0062 R00 ENGINE - Introduction of Improved High-Pressure Turbine (HPT) Stage 1 Blades with Internal Coating

Mos

Hrs

Enc

72 ENG2Eff: 18-Jul-1997

RecommendedRE (-)72-0063 R00 ENGINE - Rework of Compressor Forward Shaft PN 5037T01P03 to PN 5037T01P04 and Introduction of New Compressor Forward Shaft PN 5037T01P04

Mos

Hrs

Enc

72 ENG1Eff: 17-Jan-2003


Mos

Hrs

Enc

72 ENG2Eff: 17-Jan-2003


Generated: 6-Apr-2016 1:16 PM299/429








Mos

Hrs

Enc

72 ENG1Eff: 17-Jan-2003


Mos

Hrs

Enc

72 ENG2Eff: 17-Jan-2003

RecommendedT (A/R)72-0064 R00 ENGINE - Compressor Stator - Elimination of Splitline Pins from Compressor Inner Shrouds

Mos

Hrs

Enc

72 ENG1Eff: 23-Oct-1997

RecommendedT (A/R)72-0064 R00 ENGINE - Compressor Stator - Elimination of Splitline Pins from Compressor Inner Shrouds

Mos

Hrs

Enc

72 ENG2Eff: 23-Oct-1997

Cat. 7 - OptionalRE (-)72-0065 R00 ENGINE - Interchangeability of CF34-3B and CF34-3B1 Engine Models

Mos

Hrs

Enc

72 ENG1Eff: 10-Jun-2003


Mos

Hrs

Enc

72 ENG2Eff: 10-Jun-2003


Mos

Hrs

Enc

72 ENG1Eff: 10-Jun-2003


Mos

Hrs

Enc

72 ENG2Eff: 10-Jun-2003

RecommendedRE (-)72-0066 R00 ENGINE - Fan Rotor - Forward Fan Shaft Design Change

Mos

Hrs

Enc

72 ENG1Eff: 19-Feb-1998

RecommendedRE (-)72-0066 R00 ENGINE - Fan Rotor - Forward Fan Shaft Design Change

Mos

Hrs

Enc

72 ENG2Eff: 19-Feb-1998

RecommendedRE (-)72-0067 R02 ENGINE - CF34-3B Fleet Leader Sampling Program

Mos

Hrs

Enc

72 ENG1Eff: 11-Dec-1998

(NOTE: A CF34-3B turbofan engine which is identified as a "Fleet Leader" (a fleet leader is an engine that has accumulated more hours and/or

more cycles than other engines).)


Generated: 6-Apr-2016 1:16 PM300/429







RecommendedRE (-)72-0067 R02 ENGINE - CF34-3B Fleet Leader Sampling Program

Mos

Hrs

Enc

72 ENG2Eff: 11-Dec-1998

(NOTE: A CF34-3B turbofan engine which is identified as a "Fleet Leader" (a fleet leader is an engine that has accumulated more hours and/or

more cycles than other engines).)

RecommendedRE (-)72-0068 R00 ENGINE - General - Engine Service Record (Logbook) Entry for the CF34-3B HPT Balance Piston Seal

Mos

Hrs

Enc

72 ENG1Eff: 23-Apr-1998


RecommendedRE (-)72-0068 R00 ENGINE - General - Engine Service Record (Logbook) Entry for the CF34-3B HPT Balance Piston Seal

Mos

Hrs

Enc

72 ENG2Eff: 23-Apr-1998


RecommendedT (A/R)72-0069 R01 ENGINE - Turbine Transition Assembly - Replacement of the Self-Locking Nuts on the Thermocouple Probes and on the PT5 Pressure Probe or Plug

Mos

Hrs

Enc

72 ENG1Eff: 04-Mar-1999

RecommendedT (A/R)72-0069 R01 ENGINE - Turbine Transition Assembly - Replacement of the Self-Locking Nuts on the Thermocouple Probes and on the PT5 Pressure Probe or Plug

Mos

Hrs

Enc

72 ENG2Eff: 04-Mar-1999

RecommendedRE (-)72-0070 R00 ENGINE - Compressor Stator - Inspection and Rework of VG Actuator Bellcrank Clevis

Mos

Hrs

Enc

72 ENG1Eff: 01-Oct-1998


Mos

Hrs

Enc

72 ENG2Eff: 01-Oct-1998


Mos

Hrs

Enc

72 ENG1Eff: 06-Apr-1999


Mos

Hrs

Enc

72 ENG2Eff: 06-Apr-1999


Mos

Hrs

Enc

72 ENG1Eff: 09-Jun-1999


Generated: 6-Apr-2016 1:16 PM301/429








Mos

Hrs

Enc

72 ENG2Eff: 09-Jun-1999


Mos

Hrs

Enc

72 ENG1Eff: 05-Jan-2011


Mos

Hrs

Enc

72 ENG2Eff: 05-Jan-2011

RecommendedT (-)72-0070 R04 ENGINE - Compressor Stator - Inspection and Rework of VG Actuator Bellcrank and Clevis Bushing

Mos

Hrs

Enc

72 ENG1

(NOTE: For engines with less than 5,000 hours time-since-new (TSN), or for engines with less than 5,000 hours time-since-repair (TSR) (refer to

step 1.D.(7)), it is recommended that an initial clevis bushing inspection be performed at the next opportunity, but not to exceed 5,000 hours

TSN or TSR. All four bushings (for each engine) should be inspected.)

RecommendedT (-)72-0070 R04 ENGINE - Compressor Stator - Inspection and Rework of VG Actuator Bellcrank and Clevis Bushing

Mos

Hrs

Enc

72 ENG2




RecommendedRE (-)72-0070 R05 ENGINE - Compressor Stator - Inspection and Rework of VG Actuator Bellcrank and Clevis Bushing

Mos

Hrs

Enc

72 ENG1




RecommendedRE (-)72-0070 R05 ENGINE - Compressor Stator - Inspection and Rework of VG Actuator Bellcrank and Clevis Bushing

Mos

Hrs

Enc

72 ENG2




RecommendedT (A/R)72-0071 R00 ENGINE - Compressor Rotor - Introduction of Stages 5 through 9 Compressor Rotor Blades with Improved Wear-Resistant Dovetail Coating

Mos

Hrs

Enc

72 ENG1Eff: 09-Nov-1998

RecommendedT (A/R)72-0071 R00 ENGINE - Compressor Rotor - Introduction of Stages 5 through 9 Compressor Rotor Blades with Improved Wear-Resistant Dovetail Coating

Mos

Hrs

Enc

72 ENG2Eff: 09-Nov-1998

RecommendedRE (-)72-0072 R00 ENGINE - Compressor Stator - Introduction of Improved VG Actuator Rings

Mos

Hrs

Enc

72 ENG1Eff: 19-Nov-1998


Generated: 6-Apr-2016 1:16 PM302/429








Mos

Hrs

Enc

72 ENG2Eff: 19-Nov-1998


Mos

Hrs

Enc

72 ENG1Eff: 03-Mar-1999


Mos

Hrs

Enc

72 ENG2Eff: 03-Mar-1999

RecommendedT (A/R)72-0072 R02 ENGINE - Compressor Stator - Introduction of Improved VG Actuator Rings

Mos

Hrs

Enc

72 ENG1Eff: 30-Mar-2004

RecommendedT (A/R)72-0072 R02 ENGINE - Compressor Stator - Introduction of Improved VG Actuator Rings

Mos

Hrs

Enc

72 ENG2Eff: 30-Mar-2004

Category 5RE (-)72-0073 R00 ENGINE Eddy Current and Ultrasonic Inspections of the Fan Disk and Compressor Forward Spool

Mos

Hrs

Enc

72 ENG1Eff: 11-Dec-1998


Mos

Hrs

Enc

72 ENG2Eff: 11-Dec-1998


Mos

Hrs

Enc

72 ENG1Eff: 03-Mar-1999


Mos

Hrs

Enc

72 ENG2Eff: 03-Mar-1999


Mos

Hrs

Enc

72 ENG1Eff: 04-May-1999


Mos

Hrs

Enc

72 ENG2Eff: 04-May-1999


Generated: 6-Apr-2016 1:16 PM303/429







Cat. 5 - RecommendedRE (-)72-0073 R03 ENGINE - Eddy Current and Ultrasonic Inspections of the Fan Disk and Compressor Forward Spool

Mos

Hrs

Enc

72 ENG1Eff: 18-Feb-2009

Cat. 5 - RecommendedRE (-)72-0073 R03 ENGINE - Eddy Current and Ultrasonic Inspections of the Fan Disk and Compressor Forward Spool

Mos

Hrs

Enc

72 ENG2Eff: 18-Feb-2009

RecommendedRE (-)72-0074 R00 ENGINE - Compressor (72-30-00) - Introduction of Improved VG Actuator Shaft and Bellcrank Assembly

Mos

Hrs

Enc

72 ENG1Eff: 24-Nov-1998


Mos

Hrs

Enc

72 ENG2Eff: 24-Nov-1998


Mos

Hrs

Enc

72 ENG1Eff: 06-Apr-1999


Mos

Hrs

Enc

72 ENG2Eff: 06-Apr-1999


Mos

Hrs

Enc

72 ENG1Eff: 30-Sep-1999


Mos

Hrs

Enc

72 ENG2Eff: 30-Sep-1999


Mos

Hrs

Enc

72 ENG1Eff: 02-Aug-2006


Mos

Hrs

Enc

72 ENG2Eff: 02-Aug-2006

RecommendedT (A/R)72-0074 R04 ENGINE - Compressor (72-30-00) - Introduction of Improved VG Actuator Shaft and Bellcrank Assembly

Mos

Hrs

Enc

72 ENG1Eff: 14-Aug-2006


Generated: 6-Apr-2016 1:16 PM304/429








Mos

Hrs

Enc

72 ENG2Eff: 14-Aug-2006


Mos

Hrs

Enc

72 ENG1


Mos

Hrs

Enc

72 ENG2

Cat. 3 - RecommendedRE (-)72-0075 R00 ENGINE - Combustion Section - Improved Rear Main Mount Firewall Seals

Mos

Hrs

Enc

72 ENG1Eff: 14-Jan-1999


Mos

Hrs

Enc

72 ENG2Eff: 14-Jan-1999


Mos

Hrs

Enc

72 ENG1Eff: 19-Feb-1999


Mos

Hrs

Enc

72 ENG2Eff: 19-Feb-1999


Mos

Hrs

Enc

72 ENG1Eff: 14-Mar-2003


Mos

Hrs

Enc

72 ENG2Eff: 14-Mar-2003

Cat. 5 - RecommendedT (A/R)72-0075 R03 ENGINE - Combustion Section - Improved Rear Main Mount Firewall Seals

Mos

Hrs

Enc

72 ENG1Eff: 05-May-2008



Generated: 6-Apr-2016 1:16 PM305/429







Cat. 5 - RecommendedT (A/R)72-0075 R03 ENGINE - Combustion Section - Improved Rear Main Mount Firewall Seals

Mos

Hrs

Enc

72 ENG2Eff: 05-May-2008


Category 3RE (-)72-0077 R00 ENGINE HPT Stator Assembly (724500) Rework of Interstage Turbine Seal, and Introduction of Improved Seal Pin and Retaining Ring Sector

Mos

Hrs

Enc

72 ENG1Eff: 31-Mar-1999


Mos

Hrs

Enc

72 ENG2Eff: 31-Mar-1999


Mos

Hrs

Enc

72 ENG1Eff: 06-May-1999


Mos

Hrs

Enc

72 ENG2Eff: 06-May-1999


Mos

Hrs

Enc

72 ENG1Eff: 21-Jan-2000


Mos

Hrs

Enc

72 ENG2Eff: 21-Jan-2000


Mos

Hrs

Enc

72 ENG1Eff: 08-Jun-2000


Mos

Hrs

Enc

72 ENG2Eff: 08-Jun-2000

Cat. 3 - RecommendedRE (-)72-0077 R04 ENGINE - HPT Stator Assembly (72-45-00) - Rework of Interstage Turbine Seal and Introduction of Improved Seal Pin and Retaining Ring Sector

Mos

Hrs

Enc

72 ENG1Eff: 12-May-2006

Cat. 3 - RecommendedRE (-)72-0077 R04 ENGINE - HPT Stator Assembly (72-45-00) - Rework of Interstage Turbine Seal and Introduction of Improved Seal Pin and Retaining Ring Sector

Mos

Hrs

Enc

72 ENG2Eff: 12-May-2006


Generated: 6-Apr-2016 1:16 PM306/429







Cat. 3 - RecommendedT (A/R)72-0077 R05 ENGINE - HPT Stator Assembly (72-45-00) - Rework of Interstage Turbine Seal and Introduction of Improved Seal Pin and Retaining Ring Sector

Mos

Hrs

Enc

72 ENG1Eff: 30-Oct-2006


Cat. 3 - RecommendedT (A/R)72-0077 R05 ENGINE - HPT Stator Assembly (72-45-00) - Rework of Interstage Turbine Seal and Introduction of Improved Seal Pin and Retaining Ring Sector

Mos

Hrs

Enc

72 ENG2Eff: 30-Oct-2006


RecommendedRE (-)72-0078 R00 ENGINE - Turbine Section - Improved LPT Rotor Assemblies

Mos

Hrs

Enc

72 ENG1Eff: 03-Feb-1999

RecommendedRE (-)72-0078 R00 ENGINE - Turbine Section - Improved LPT Rotor Assemblies

Mos

Hrs

Enc

72 ENG2Eff: 03-Feb-1999

Cat. 6 - RecommendedRE (-)72-0079 R01 ENGINE - Turbine Section - Improved HPT Stator Assembly and Turbine Transition Assembly

Mos

Hrs

Enc

72 ENG1Eff: 08-Jun-2000

Cat. 6 - RecommendedRE (-)72-0079 R01 ENGINE - Turbine Section - Improved HPT Stator Assembly and Turbine Transition Assembly

Mos

Hrs

Enc

72 ENG2Eff: 08-Jun-2000

RecommendedRE (-)72-0080 R01 ENGINE - Fan Rotor - Replacement of No. 1 Ball bearing Manufacturing Lot

Mos

Hrs

Enc

72 ENG1Eff: 09-Jun-1999

RecommendedRE (-)72-0080 R01 ENGINE - Fan Rotor - Replacement of No. 1 Ball bearing Manufacturing Lot

Mos

Hrs

Enc

72 ENG2Eff: 09-Jun-1999

Cat. 3 - RecommendedRE (-)72-0081 R00 ENGINE - Combustion Liner and Stage 1 Nozzle (72-42-00) - CF34 Combustion Liner Shell and Dome Part Number and Serial Number Tracking

Mos

Hrs

Enc

72 ENG1Eff: 07-Jul-1999

Also ConsiderDUE:1. RE -ENGINE - Combustion Liner and Stage 1 Nozzle (72-42-00) - In...72-0087 R02ENG172

Cat. 3 - RecommendedRE (-)72-0081 R00 ENGINE - Combustion Liner and Stage 1 Nozzle (72-42-00) - CF34 Combustion Liner Shell and Dome Part Number and Serial Number Tracking

Mos

Hrs

Enc

72 ENG2Eff: 07-Jul-1999

Also ConsiderDUE:1. RE -ENGINE - Combustion Liner and Stage 1 Nozzle (72-42-00) - In...72-0087 R02ENG272


Generated: 6-Apr-2016 1:16 PM307/429







Cat. 2 - RecommendedRE (-)72-0082 R02 ENGINE - Compressor Stator Assembly (72-32-00) - CF34 Compressor Variable Vane Actuating Arm Wear at the Compressor Splitline

12-Nov-1999Mos

Hrs

Enc

72 ENG1BY PART S/N INSTALLEDEff: 12-Nov-1999 Not

Applicable

Also ConsiderDUE:1. RE -ENGINE - Compressor Stator Assembly (72-32-00) - CF34 Compre...72-0134 R01ENG172


Mos

Hrs

Enc

72 ENG2Eff: 12-Nov-1999

Also ConsiderDUE:1. RE -ENGINE - Compressor Stator Assembly (72-32-00) - CF34 Compre...72-0134 R01ENG272

Cat. 7 - OptionalRE (-)72-0083 R01 ENGINE - High Pressure Turbine Stator (72-45-00) - Rework of HPT Stator Assembly and Introduction of Improved Durability Stage 2 HPT Nozzle and HPT Inner Case

and Spline Seals

Mos

Hrs

Enc

72 ENG1Eff: 27-Apr-2005

Cat. 7 - OptionalRE (-)72-0083 R01 ENGINE - High Pressure Turbine Stator (72-45-00) - Rework of HPT Stator Assembly and Introduction of Improved Durability Stage 2 HPT Nozzle and HPT Inner Case

and Spline Seals

Mos

Hrs

Enc

72 ENG2Eff: 27-Apr-2005

Cat. 5 - RecommendedRE (-)72-0084 R01 ENGINE - Compressor Rotor Assembly (72-33-00) - Re-identification of Compressor Rotor Assemblies

Mos

Hrs

Enc

72 ENG1Eff: 08-Jun-2000

Cat. 5 - RecommendedRE (-)72-0084 R01 ENGINE - Compressor Rotor Assembly (72-33-00) - Re-identification of Compressor Rotor Assemblies

Mos

Hrs

Enc

72 ENG2Eff: 08-Jun-2000

Cat. 7 - OptionalRE (-)72-0087 R01 ENGINE - Combustion Liner and Stage 1 Nozzle (72-42-00) - Introduction of Improved Combustion Liner

Mos

Hrs

Enc

72 ENG1Eff: 21-Oct-2004


Mos

Hrs

Enc

72 ENG2Eff: 21-Oct-2004


Mos

Hrs

Enc

72 ENG1Eff: 02-Jan-2007

Also ConsiderDUE:1. T A/R | 2. RE -ENGINE - Combustion Liner Assembly (72-42-00) - Introduction...72-0240 R00ENG172


Generated: 6-Apr-2016 1:16 PM308/429








Mos

Hrs

Enc

72 ENG2Eff: 02-Jan-2007

Also ConsiderDUE:1. T A/R | 2. RE -ENGINE - Combustion Liner Assembly (72-42-00) - Introduction...72-0240 R00ENG272

Cat. 7 - OptionalT (A/R)72-0089 R00 ENGINE - HPT Rotor (72-46-00) - Introduction of Improved Stage 2 HPT Blades

Mos

Hrs

Enc

72 ENG1Eff: 03-Nov-2000

Cat. 7 - OptionalT (A/R)72-0089 R00 ENGINE - HPT Rotor (72-46-00) - Introduction of Improved Stage 2 HPT Blades

Mos

Hrs

Enc

72 ENG2Eff: 03-Nov-2000

Cat. 3 - RecommendedT (A/R)72-0090 R00 ENGINE - Add Safety Wire at the Total Temperature and Pressure Boss Cap

Mos

Hrs

Enc

72 ENG1Eff: 28-Feb-2001

Cat. 3 - RecommendedT (A/R)72-0090 R00 ENGINE - Add Safety Wire at the Total Temperature and Pressure Boss Cap

Mos

Hrs

Enc

72 ENG2Eff: 28-Feb-2001

Cat. 2 - RecommendedRE (-)72-0091 R00 ENGINE - Fan Section Module (72-21-00) - Fan Blade Pin Hole Inspection

Mos

Hrs

Enc

72 ENG1Eff: 16-Nov-2001


Mos

Hrs

Enc

72 ENG2Eff: 16-Nov-2001


Mos

Hrs

Enc

72 ENG1Eff: 09-Oct-2002

(NOTE: If it is recorded in the engine log book that the fan blade pin holes were inspected while in an overhaul shop in accordance with one of

the documents listed below, the intent of the 18,000 CSN requirement of this Service Bulletin has been met. • IFM 20 (dated 04-28-00) •

IFM 20 Revision 1 (dated 05-05-00) • IFM 20 Revision 2 (dated 05-08-00)GE recommends subsequent re-inspection of the affected fan

blades, in compliance with this Service Bulletin, at 3,000 cycle intervals until fan blades with reworked pin holes are available and installed on

the engine.)


Mos

Hrs

Enc

72 ENG2Eff: 09-Oct-2002





the engine.)


Generated: 6-Apr-2016 1:16 PM309/429








Mos

Hrs

Enc

72 ENG1Eff: 14-Jan-2005





the engine.)


Mos

Hrs

Enc

72 ENG2Eff: 14-Jan-2005





the engine.)


Mos

Hrs

Enc

72 ENG1Eff: 29-Jul-2010





the engine.)


Mos

Hrs

Enc

72 ENG2Eff: 29-Jul-2010





the engine.)


Mos

Hrs

Enc

72 ENG1Eff: 16-Sep-2010





the engine.)


Mos

Hrs

Enc

72 ENG2Eff: 16-Sep-2010





the engine.)


Generated: 6-Apr-2016 1:16 PM310/429








Mos

Hrs

Enc

72 ENG1Eff: 08-Nov-2010





the engine.)


Mos

Hrs

Enc

72 ENG2Eff: 08-Nov-2010





the engine.)

Cat. 2 - Recommended ≈21-Apr-2047RE (-)72-0091 R06 ENGINE - Fan Section Module (72-21-00) - Fan Blade Pin Hole Inspection

Mos

Hrs

11,231 Enc[18,000]0Enc

72 ENG1Eff: 01-Jun-2011


Mos

Hrs

Enc

72 ENG2Eff: 01-Jun-2011

Category 2 ≈21-Apr-2047RE (-)72-0091 R07 ENGINE - Fan Section Module (72-21-00) - Fan Blade Pin Hole Inspection

Mos

Hrs

11,231 Enc[18,000]Enc

72 ENG1Eff: 13-Apr-2015

Also ConsiderDUE:1. RE -ENGINE - Fan Rotor (72-21-00) - Field Management Program of ...72-0229 R01ENG172

Category 2RE (-)72-0091 R07 ENGINE - Fan Section Module (72-21-00) - Fan Blade Pin Hole Inspection

Mos

Hrs

Enc

72 ENG2Eff: 13-Apr-2015

Also ConsiderDUE: 6,914 Enc1. T 350 Enc | 2. RE 600 EncENGINE - Fan Rotor (72-21-00) - Field Management Program of ...72-0229 R01ENG272

Cat. 5 - RecommendedRE (-)72-0092 R01 HPT Stator Assembly - Introduction of Improved Borescope Plug

Mos

Hrs

Enc

72 ENG1Eff: 14-Dec-2001

Cat. 5 - RecommendedRE (-)72-0092 R01 HPT Stator Assembly - Introduction of Improved Borescope Plug

Mos

Hrs

Enc

72 ENG2Eff: 14-Dec-2001

Cat. 4 - RecommendedRE (-)72-0093 R00 HPT Rotor Assembly (72-46-00) - Introduction of Improved No. 5 Bearing Rotating Air Seal

Mos

Hrs

Enc

72 ENG1Eff: 23-Jul-2001


Generated: 6-Apr-2016 1:16 PM311/429







Cat. 4 - RecommendedRE (-)72-0093 R00 HPT Rotor Assembly (72-46-00) - Introduction of Improved No. 5 Bearing Rotating Air Seal

Mos

Hrs

Enc

72 ENG2Eff: 23-Jul-2001

Cat. 4 - RecommendedT (-)72-0093 R01 HPT Rotor Assembly (72-46-00) - Introduction of Improved No. 5 Bearing Rotating Air Seal

Mos

Hrs

Enc

72 ENG1Eff: 23-Jul-2001


Cat. 4 - RecommendedT (-)72-0093 R01 HPT Rotor Assembly (72-46-00) - Introduction of Improved No. 5 Bearing Rotating Air Seal

Mos

Hrs

Enc

72 ENG2Eff: 23-Jul-2001


Cat. 4 - RecommendedT (A/R)72-0093 R02 HPT Rotor Assembly (72-46-00) - Introduction of Improved No. 5 Bearing Rotating Air Seal

Mos

Hrs

Enc

72 ENG1Eff: 27-Apr-2015

Cat. 4 - RecommendedT (A/R)72-0093 R02 HPT Rotor Assembly (72-46-00) - Introduction of Improved No. 5 Bearing Rotating Air Seal

Mos

Hrs

Enc

72 ENG2Eff: 27-Apr-2015

Cat. 7 - OptionalRE (-)72-0095 R00 ENGINE - Combustion Liner and Stage 1 Nozzle (72-42-00) - Introduction of Improved-Durability Stage 1 Turbine Nozzle

Mos

Hrs

Enc

72 ENG1Eff: 20-Mar-2001

Cat. 7 - OptionalRE (-)72-0095 R00 ENGINE - Combustion Liner and Stage 1 Nozzle (72-42-00) - Introduction of Improved-Durability Stage 1 Turbine Nozzle

Mos

Hrs

Enc

72 ENG2Eff: 20-Mar-2001

Cat. 7 - OptionalT (A/R)72-0095 R01 ENGINE - Combustion Liner and Stage 1 Nozzle (72-42-00) - Introduction of Improved-Durability Stage 1 Turbine Nozzle

Mos

Hrs

Enc

72 ENG1Eff: 08-Dec-2008

Cat. 7 - OptionalT (A/R)72-0095 R01 ENGINE - Combustion Liner and Stage 1 Nozzle (72-42-00) - Introduction of Improved-Durability Stage 1 Turbine Nozzle

Mos

Hrs

Enc

72 ENG2Eff: 08-Dec-2008

Cat. 2 - RecommendedRE (-)72-0096 R00 ENGINE - Compressor Section (72-30-00) - Inspection of Compressor Casings and Spools

Mos

Hrs

Enc

72 ENG1Eff: 02-Jul-2002


Generated: 6-Apr-2016 1:16 PM312/429







Cat. 2 - RecommendedRE (-)72-0096 R00 ENGINE - Compressor Section (72-30-00) - Inspection of Compressor Casings and Spools

Mos

Hrs

Enc

72 ENG2Eff: 02-Jul-2002

Cat. 2 - RecommendedRE (-)72-0098 R02 (LPT Stage 6

Disk)

ENGINE - Low-Pressure Turbine Rotor (72-53-00) - Replacement of Selected CF34 Low-Pressure Turbine Stage 6 Disks.

Mos

Hrs

Enc

72 ENG1Eff: 16-Nov-2004

Cat. 2 - RecommendedRE (-)72-0098 R02 (LPT Stage 6

Disk)

ENGINE - Low-Pressure Turbine Rotor (72-53-00) - Replacement of Selected CF34 Low-Pressure Turbine Stage 6 Disks.

Mos

Hrs

Enc

72 ENG2Eff: 16-Nov-2004

InformationalT (A/R)72-0099 R00 ENGINE - General - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Turbofan Engines

Mos

Hrs

Enc

72 ENG1Eff: 24-Jun-2001

InformationalT (A/R)72-0099 R00 ENGINE - General - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Turbofan Engines

Mos

Hrs

Enc

72 ENG2Eff: 24-Jun-2001

InformationalRE (-)72-0101 R00 ENGINE - General - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Turbofan Engines

Mos

Hrs

Enc

72 ENG1Eff: 29-Jul-2001

InformationalRE (-)72-0101 R00 ENGINE - General - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Turbofan Engines

Mos

Hrs

Enc

72 ENG2Eff: 29-Jul-2001

Cat. 4 - RecommendedT (A/R)72-0102 R00 ENGINE - Accessory Gearbox Assembly (72-62-00) - Introduction of Improved Ball Bearing Design for Axes -P, -J, and -K Bearings

Mos

Hrs

Enc

72 ENG1Eff: 07-Sep-2001

(NOTE: This Service Bulletin is not applicable to the CF34 turbofan engines affected that have accessory gearbox assemblies with AGB bearings

PN 5071T20P01 installed)


Cat. 4 - RecommendedT (A/R)72-0102 R00 ENGINE - Accessory Gearbox Assembly (72-62-00) - Introduction of Improved Ball Bearing Design for Axes -P, -J, and -K Bearings

Mos

Hrs

Enc

72 ENG2Eff: 07-Sep-2001

(NOTE: This Service Bulletin is not applicable to the CF34 turbofan engines affected that have accessory gearbox assemblies with AGB bearings

PN 5071T20P01 installed)


Category 7RE (-)72-0104 R00 ENGINE - High-Pressure Turbine Rotor (72-46-00) Introduction of Improved HPT Stage 1 Blades PN 6078T19P10 and PN 6078T19P11

Mos

Hrs

Enc

72 ENG1Eff: 01-Oct-2001


Generated: 6-Apr-2016 1:16 PM313/429







Category 7RE (-)72-0104 R00 ENGINE - High-Pressure Turbine Rotor (72-46-00) Introduction of Improved HPT Stage 1 Blades PN 6078T19P10 and PN 6078T19P11

Mos

Hrs

Enc

72 ENG2Eff: 01-Oct-2001

Cat. 7 - OptionalRE (-)72-0104 R01 ENGINE - High-Pressure Turbine Rotor (72-46-00) - Introduction of Improved HPT Stage 1 Blades PN 6078T19P10 and PN 6078T19P11

Mos

Hrs

Enc

72 ENG1Eff: 23-Feb-2005

Cat. 7 - OptionalRE (-)72-0104 R01 ENGINE - High-Pressure Turbine Rotor (72-46-00) - Introduction of Improved HPT Stage 1 Blades PN 6078T19P10 and PN 6078T19P11

Mos

Hrs

Enc

72 ENG2Eff: 23-Feb-2005

Cat. 7 - OptionalT (A/R)72-0104 R02 ENGINE - High-Pressure Turbine Rotor (72-46-00) - Introduction of Improved HPT Stage 1 Blades PN 6078T19P10 and PN 6078T19P11

Mos

Hrs

Enc

72 ENG1Eff: 05-Nov-2013

Cat. 7 - OptionalT (A/R)72-0104 R02 ENGINE - High-Pressure Turbine Rotor (72-46-00) - Introduction of Improved HPT Stage 1 Blades PN 6078T19P10 and PN 6078T19P11

Mos

Hrs

Enc

72 ENG2Eff: 05-Nov-2013

Cat. 6 - RecommendedRE (-)72-0105 R00 ENGINE - Accessory Gearbox Assembly (72-62-00) - Introduction of AGB Assembly PN 6014T81G32 with Metal Peening on Axes L, P, and K Gears

Mos

Hrs

Enc

72 ENG1Eff: 13-Dec-2001


Mos

Hrs

Enc

72 ENG2Eff: 13-Dec-2001


Mos

Hrs

Enc

72 ENG1Eff: 22-Sep-2014


Mos

Hrs

Enc

72 ENG2Eff: 22-Sep-2014


Mos

Hrs

Enc

72 ENG1Eff: 29-Sep-2014


Mos

Hrs

Enc

72 ENG2Eff: 29-Sep-2014


Generated: 6-Apr-2016 1:16 PM314/429







Cat. 7 - OptionalRE (-)72-0106 R00 ENGINE - Compressor Rotor Assembly (72-33-00) - Stage 9 Compressor Rotor Blade Replacement

Mos

Hrs

Enc

72 ENG1Eff: 01-Mar-2002


Mos

Hrs

Enc

72 ENG2Eff: 01-Mar-2002


Mos

Hrs

Enc

72 ENG1Eff: 07-Nov-2002


Mos

Hrs

Enc

72 ENG2Eff: 07-Nov-2002

Cat. 4 - RecommendedRE (-)72-0106 R02 ENGINE - Compressor Rotor Assembly (72-33-00) - Stage 9 Compressor Rotor Blade Replacement

Mos

Hrs

Enc

72 ENG1Eff: 17-Jun-2003


Mos

Hrs

Enc

72 ENG2Eff: 17-Jun-2003


Mos

Hrs

Enc

72 ENG1Eff: 16-Sep-2003


Mos

Hrs

Enc

72 ENG2Eff: 16-Sep-2003

Cat. 4 - RecommendedRE (-)72-0106 R04 ENGINE - Compressor Rotor Assembly (72-33-00) - Stage 9 CompressorRotor Blade Replacement

Mos

Hrs

Enc

72 ENG1Eff: 21-Jan-2004

Cat. 4 - RecommendedRE (-)72-0106 R04 ENGINE - Compressor Rotor Assembly (72-33-00) - Stage 9 CompressorRotor Blade Replacement

Mos

Hrs

Enc

72 ENG2Eff: 21-Jan-2004


Mos

Hrs

Enc

72 ENG1Eff: 26-Feb-2004


Generated: 6-Apr-2016 1:16 PM315/429








Mos

Hrs

Enc

72 ENG2Eff: 26-Feb-2004


Mos

Hrs

Enc

72 ENG1Eff: 09-Jun-2005


Mos

Hrs

Enc

72 ENG2Eff: 09-Jun-2005

Cat. 4 - RecommendedT (A/R)72-0106 R07 ENGINE - Compressor Rotor Assembly (72-33-00) - Stage 9 Compressor Rotor Blade Replacement

Mos

Hrs

Enc

72 ENG1Eff: 07-Nov-2005

Cat. 4 - RecommendedT (A/R)72-0106 R07 ENGINE - Compressor Rotor Assembly (72-33-00) - Stage 9 Compressor Rotor Blade Replacement

Mos

Hrs

Enc

72 ENG2Eff: 07-Nov-2005

Cat. 8 - InformationalRE (-)72-0107 R00 ENGINE - General - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Turbofan Engines

Mos

Hrs

Enc

72 ENG1Eff: 10-May-2002


Mos

Hrs

Enc

72 ENG2Eff: 10-May-2002


Mos

Hrs

Enc

72 ENG1Eff: 10-May-2002


Mos

Hrs

Enc

72 ENG2Eff: 10-May-2002

Cat. 7 - OptionalRE (-)72-0108 R00 ENGINE - High Pressure Turbine Rotor (72-46-00) or High Pressure Turbine Rotor (72-52-00) - Improved Durability Stage 2 HPT Blade with Airfoil Cavity Coating

Mos

Hrs

Enc

72 ENG1Eff: 01-Mar-2002

Cat. 7 - OptionalRE (-)72-0108 R00 ENGINE - High Pressure Turbine Rotor (72-46-00) or High Pressure Turbine Rotor (72-52-00) - Improved Durability Stage 2 HPT Blade with Airfoil Cavity Coating

Mos

Hrs

Enc

72 ENG2Eff: 01-Mar-2002


Generated: 6-Apr-2016 1:16 PM316/429







Cat. 4 - RecommendedRE (-)72-0108 R01 ENGINE - High Pressure Turbine Rotor (72-46-00) or High Pressure Turbine Rotor (72-52-00) - Improved Durability Stage 2 HPT Blade with Airfoil Cavity Coating

Mos

Hrs

Enc

72 ENG1Eff: 21-Oct-2003


Mos

Hrs

Enc

72 ENG2Eff: 21-Oct-2003


Mos

Hrs

Enc

72 ENG1Eff: 16-Nov-2004


Mos

Hrs

Enc

72 ENG2Eff: 16-Nov-2004


Mos

Hrs

Enc

72 ENG1Eff: 23-Feb-2005


Mos

Hrs

Enc

72 ENG2Eff: 23-Feb-2005

Cat. 4 - RecommendedT (A/R)72-0108 R04 ENGINE - High Pressure Turbine Rotor (72-46-00) or High Pressure Turbine Rotor (72-52-00) - Improved Durability Stage 2 HPT Blade with Airfoil Cavity Coating

Mos

Hrs

Enc

72 ENG1Eff: 23-Feb-2006

Cat. 4 - RecommendedT (A/R)72-0108 R04 ENGINE - High Pressure Turbine Rotor (72-46-00) or High Pressure Turbine Rotor (72-52-00) - Improved Durability Stage 2 HPT Blade with Airfoil Cavity Coating

Mos

Hrs

Enc

72 ENG2Eff: 23-Feb-2006

Cat. 2 - RecommendedRE (-)72-0109 R00 ENGINE - Compressor Stator (72-32-00) - Inspection and Rework of VG Shaft Aft Bearing Support

25-Jul-2008Mos

11,528.2Hrs

6,334Enc

72 ENG1BY PART S/N INSTALLEDEff: 21-May-2002 Not

Applicable

(NOTE: This Service Bulletin is not applicable to CF34 turbofan engines with VG actuator shaft aft bearing support PN 5024T65G03 identified

with supplier code 56946 if the support has been identified with the "R" marking.)


25-Jul-2008Mos

11,411.2Hrs

6,293Enc


Applicable




Generated: 6-Apr-2016 1:16 PM317/429








Mos

Hrs

Enc

72 ENG1Eff: 03-Mar-2003



Also ConsiderDUE:1. T A/R | 2. RE -ENGINE - Compressor Stator (72-32-00) - Replacement of VG Sh...72-0110 R01ENG172


Mos

Hrs

Enc

72 ENG2Eff: 03-Mar-2003




Cat. 3 - RecommendedRE (-)72-0110 R00 ENGINE - Compressor Stator (72-32-00) - Replacement of VG Shaft Aft Bearing Support

Mos

Hrs

Enc

72 ENG1Eff: 21-May-2002


with supplier code 56946 if the support has been identified with the rework "R" marking.

For each of the affected engines it is recommended that both VG shaft aft supports be removed and replaced at the next shop visit after

receipt of this Service Bulletin.)

Cat. 3 - RecommendedRE (-)72-0110 R00 ENGINE - Compressor Stator (72-32-00) - Replacement of VG Shaft Aft Bearing Support

Mos

Hrs

Enc

72 ENG2Eff: 21-May-2002





Cat. 3 - RecommendedT (A/R)72-0110 R01 ENGINE - Compressor Stator (72-32-00) - Replacement of VG Shaft Aft Bearing Support

Mos

Hrs

Enc

72 ENG1Eff: 27-Feb-2003





Cat. 3 - RecommendedT (A/R)72-0110 R01 ENGINE - Compressor Stator (72-32-00) - Replacement of VG Shaft Aft Bearing Support

Mos

Hrs

Enc

72 ENG2Eff: 27-Feb-2003





Cat. 2 - RecommendedRE (-)72-0111 R00 ENGINE - Compressor Stator (72-32-00) - Inspection and Temporary Loctite Rework of VG Shaft Aft Bearing Support

Mos

Hrs

Enc

72 ENG1Eff: 02-Apr-2002


with supplier code 56946 if the supports at both the 2:00 and 8:00 VG shaft locations have been identified with the rework "R" marking.)


Mos

Hrs

Enc

72 ENG2Eff: 02-Apr-2002




Generated: 6-Apr-2016 1:16 PM318/429








Mos

Hrs

Enc

72 ENG1Eff: 03-Mar-2003




Mos

Hrs

Enc

72 ENG2Eff: 03-Mar-2003




Mos

Hrs

Enc

72 ENG1Eff: 06-May-2003





Mos

Hrs

Enc

72 ENG2Eff: 06-May-2003





Mos

Hrs

Enc

72 ENG1Eff: 28-Mar-2002


Mos

Hrs

Enc

72 ENG2Eff: 28-Mar-2002

Cat. 8 - InformationalT (A/R)72-0112 R01 ENGINE - General - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Turbofan Engines

Mos

Hrs

Enc

72 ENG1Eff: 29-Apr-2002


Mos

Hrs

Enc

72 ENG2Eff: 29-Apr-2002


Mos

Hrs

Enc

72 ENG1Eff: 12-Jun-2002


Mos

Hrs

Enc

72 ENG2Eff: 12-Jun-2002


Generated: 6-Apr-2016 1:16 PM319/429








Mos

Hrs

Enc

72 ENG1Eff: 23-Sep-2002


Mos

Hrs

Enc

72 ENG2Eff: 23-Sep-2002

Cat. 7 - OptionalT (A/R)72-0120 R00 ENGINE - Compressor Rotor Components (72-33-00) - Introduction of Improved Stages 3 and 5 Compressor Rotor Locking Nut Halves

Mos

Hrs

Enc

72 ENG1Eff: 29-Jul-2002

Cat. 7 - OptionalT (A/R)72-0120 R00 ENGINE - Compressor Rotor Components (72-33-00) - Introduction of Improved Stages 3 and 5 Compressor Rotor Locking Nut Halves

Mos

Hrs

Enc

72 ENG2Eff: 29-Jul-2002


Mos

Hrs

Enc

72 ENG1Eff: 14-Aug-2002


Mos

Hrs

Enc

72 ENG2Eff: 14-Aug-2002

Cat. 8 - InformationalRE (-)72-0123 R00 ENGINE - General (72-00-00) - Introduction of Fan Blade Bushing Repair

Mos

Hrs

Enc

72 ENG1Eff: 13-Dec-2002

Cat. 8 - InformationalRE (-)72-0123 R00 ENGINE - General (72-00-00) - Introduction of Fan Blade Bushing Repair

Mos

Hrs

Enc

72 ENG2Eff: 13-Dec-2002

Cat. 7 - OptionalRE (-)72-0123 R01 ENGINE - General (72-00-00) - Introduction of Fan Blade Bushing Repair

Mos

Hrs

Enc

72 ENG1Eff: 11-Aug-2008

Cat. 7 - OptionalRE (-)72-0123 R01 ENGINE - General (72-00-00) - Introduction of Fan Blade Bushing Repair

Mos

Hrs

Enc

72 ENG2Eff: 11-Aug-2008

Cat. 7 - OptionalT (-)72-0123 R02 ENGINE - General (72-00-00) - Introduction of Fan Blade Bushing Repair

Mos

Hrs

Enc

72 ENG1Eff: 05-Aug-2013


Generated: 6-Apr-2016 1:16 PM320/429







Cat. 7 - OptionalT (-)72-0123 R02 ENGINE - General (72-00-00) - Introduction of Fan Blade Bushing Repair

Mos

Hrs

Enc

72 ENG2Eff: 05-Aug-2013

Category 7T (-)72-0123 R03 ENGINE - General (72-00-00) - Introduction of Fan Blade Bushing Repair

Mos

Hrs

Enc

72 ENG1Eff: 09-Apr-2015


Category 7T (-)72-0123 R03 ENGINE - General (72-00-00) - Introduction of Fan Blade Bushing Repair

Mos

Hrs

Enc

72 ENG2Eff: 09-Apr-2015


Category 7T (A/R)72-0123 R04 ENGINE - General (72-00-00) - Introduction of Fan Blade Bushing Repair

Mos

Hrs

Enc

72 ENG1Eff: 21-Oct-2015


Category 7T (A/R)72-0123 R04 ENGINE - General (72-00-00) - Introduction of Fan Blade Bushing Repair

Mos

Hrs

Enc

72 ENG2Eff: 21-Oct-2015



Mos

Hrs

Enc

72 ENG1Eff: 07-Nov-2002


Mos

Hrs

Enc

72 ENG2Eff: 07-Nov-2002

Cat. 7 - OptionalRE (-)72-0125 R00 ENGINE - Fan Rotor Assembly (72-33-00) - Rework of Fan Blades PN 6018T30P06 and PN 6018T30P13

Mos

Hrs

Enc

72 ENG1Eff: 03-Feb-2003

Cat. 7 - OptionalRE (-)72-0125 R00 ENGINE - Fan Rotor Assembly (72-33-00) - Rework of Fan Blades PN 6018T30P06 and PN 6018T30P13

Mos

Hrs

Enc

72 ENG2Eff: 03-Feb-2003

Cat. 7 - OptionalRE (-)72-0125 R01 ENGINE - Fan Rotor Assembly (72-33-00) - Rework of Fan Blades PN 6018T30P03 PN 6018T30P05 PN 6018T30P06 PN 6018T30P07 PN 6018T30P13 and PN

5922T34P01

Mos

Hrs

Enc

72 ENG1Eff: 19-Jun-2003


Generated: 6-Apr-2016 1:16 PM321/429







Cat. 7 - OptionalRE (-)72-0125 R01 ENGINE - Fan Rotor Assembly (72-33-00) - Rework of Fan Blades PN 6018T30P03 PN 6018T30P05 PN 6018T30P06 PN 6018T30P07 PN 6018T30P13 and PN

5922T34P01

Mos

Hrs

Enc

72 ENG2Eff: 19-Jun-2003

Cat. 7 - OptionalT (A/R)72-0125 R02 ENGINE - Fan Rotor Assembly (72-21-00) - Rework of Fan Blades P/N 4923T56G02 P/N 4923T56G05 P/N 4923T56G07 P/N 4923T56G09 P/N 5922T34P01 P/N

6018T30P03 P/N 6018T30P06 and P/N 6018T30P13

Mos

Hrs

Enc

72 ENG1Eff: 09-Jan-2008

Cat. 7 - OptionalT (A/R)72-0125 R02 ENGINE - Fan Rotor Assembly (72-21-00) - Rework of Fan Blades P/N 4923T56G02 P/N 4923T56G05 P/N 4923T56G07 P/N 4923T56G09 P/N 5922T34P01 P/N

6018T30P03 P/N 6018T30P06 and P/N 6018T30P13

Mos

Hrs

Enc

72 ENG2Eff: 09-Jan-2008

Cat. 9 - InformationalRE (-)72-0126 R00 ENGINE - Fan Stator Assembly (72-23-00) - Rework of Fan Case Outer Spacers and Introduction of a New Aft Fan Case

Mos

Hrs

Enc

72 ENG1Eff: 03-Feb-2003

Cat. 9 - InformationalRE (-)72-0126 R00 ENGINE - Fan Stator Assembly (72-23-00) - Rework of Fan Case Outer Spacers and Introduction of a New Aft Fan Case

Mos

Hrs

Enc

72 ENG2Eff: 03-Feb-2003

Cat. 7 - OptionalT (A/R)72-0126 R01 ENGINE - Fan Stator Assembly (72-23-00) - Rework of Fan Case Outer Spacers and Introduction of a New Aft Fan Case

Mos

Hrs

Enc

72 ENG1Eff: 11-Mar-2003

Cat. 7 - OptionalT (A/R)72-0126 R01 ENGINE - Fan Stator Assembly (72-23-00) - Rework of Fan Case Outer Spacers and Introduction of a New Aft Fan Case

Mos

Hrs

Enc

72 ENG2Eff: 11-Mar-2003


Mos

Hrs

Enc

72 ENG1Eff: 02-Dec-2002


Mos

Hrs

Enc

72 ENG2Eff: 02-Dec-2002


Mos

Hrs

Enc

72 ENG1Eff: 10-Dec-2002


Generated: 6-Apr-2016 1:16 PM322/429








Mos

Hrs

Enc

72 ENG2Eff: 10-Dec-2002

Cat. 7 - OptionalRE (-)72-0128 R00 ENGINE - Compressor Stator Assembly (72-32-00) - Introduction of New Stage 1 and Stage 2 Compressor Shroud Seals PN 5026T64G14 PN 5026T64G13 and PN

5026T62G11

Mos

Hrs

Enc

72 ENG1Eff: 17-Jan-2003

Cat. 7 - OptionalRE (-)72-0128 R00 ENGINE - Compressor Stator Assembly (72-32-00) - Introduction of New Stage 1 and Stage 2 Compressor Shroud Seals PN 5026T64G14 PN 5026T64G13 and PN

5026T62G11

Mos

Hrs

Enc

72 ENG2Eff: 17-Jan-2003

Cat. 7 - OptionalT (A/R)72-0128 R01 ENGINE - Compressor Stator Assembly (72-32-00) - Introduction of New Stage 1 and Stage 2 Compressor Shroud Seals PN 5026T64G14 PN 5026T64G13 and PN

5026T62G11

Mos

Hrs

Enc

72 ENG1Eff: 05-Feb-2007

Cat. 7 - OptionalT (A/R)72-0128 R01 ENGINE - Compressor Stator Assembly (72-32-00) - Introduction of New Stage 1 and Stage 2 Compressor Shroud Seals PN 5026T64G14 PN 5026T64G13 and PN

5026T62G11

Mos

Hrs

Enc

72 ENG2Eff: 05-Feb-2007


Mos

Hrs

Enc

72 ENG1Eff: 22-Dec-2002


Mos

Hrs

Enc

72 ENG2Eff: 22-Dec-2002


Mos

Hrs

Enc

72 ENG1Eff: 05-Apr-2006


Mos

Hrs

Enc

72 ENG2Eff: 05-Apr-2006


Mos

Hrs

Enc

72 ENG1Eff: 22-Jan-2008


Generated: 6-Apr-2016 1:16 PM323/429








Mos

Hrs

Enc

72 ENG2Eff: 22-Jan-2008

Cat. 9 - InformationalT (A/R)72-0130 R00 ENGINE - General - Spare Parts Release for CF34 Turbofan Engines

Mos

Hrs

Enc

72 ENG1Eff: 06-Feb-2003

Cat. 9 - InformationalT (A/R)72-0130 R00 ENGINE - General - Spare Parts Release for CF34 Turbofan Engines

Mos

Hrs

Enc

72 ENG2Eff: 06-Feb-2003


Mos

Hrs

Enc

72 ENG1Eff: 23-Feb-2003


Mos

Hrs

Enc

72 ENG2Eff: 23-Feb-2003


Mos

Hrs

Enc

72 ENG1Eff: 27-Apr-2004


Mos

Hrs

Enc

72 ENG2Eff: 27-Apr-2004


Mos

Hrs

Enc

72 ENG1Eff: 27-Jul-2003


Mos

Hrs

Enc

72 ENG2Eff: 27-Jul-2003


Mos

Hrs

Enc

72 ENG1Eff: 02-Sep-2003


Mos

Hrs

Enc

72 ENG2Eff: 02-Sep-2003


Generated: 6-Apr-2016 1:16 PM324/429








Mos

Hrs

Enc

72 ENG1Eff: 30-Sep-2003


Mos

Hrs

Enc

72 ENG2Eff: 30-Sep-2003

Cat. 8 - InformationalRE (-)72-0141 R00 ENGINE - General - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3BTurbofan Engines

Mos

Hrs

Enc

72 ENG1Eff: 26-Oct-2003

Cat. 8 - InformationalRE (-)72-0141 R00 ENGINE - General - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3BTurbofan Engines

Mos

Hrs

Enc

72 ENG2Eff: 26-Oct-2003


Mos

Hrs

Enc

72 ENG1Eff: 20-Jan-2004


Mos

Hrs

Enc

72 ENG2Eff: 20-Jan-2004

Cat. 9 - InformationalRE (-)72-0142 R00 ENGINE - Compressor Rotor (72-33-00) - Life Limited Stages 3 thru 8Compressor Rotor Spool PN 6078T56P05 Part Introduction

Mos

Hrs

Enc

72 ENG1Eff: 24-Nov-2003


Mos

Hrs

Enc

72 ENG2Eff: 24-Nov-2003


Mos

Hrs

Enc

72 ENG1Eff: 20-Jan-2004


Mos

Hrs

Enc

72 ENG2Eff: 20-Jan-2004

Cat. 9 - InformationalT (A/R)72-0142 R02 ENGINE - Compressor Rotor (72-33-00) - Life Limited Stages 3 thru 8 Compressor Rotor Spool PN 6078T56P05 Part Introduction

Mos

Hrs

Enc

72 ENG1Eff: 11-May-2004


Generated: 6-Apr-2016 1:16 PM325/429







Cat. 9 - InformationalT (A/R)72-0142 R02 ENGINE - Compressor Rotor (72-33-00) - Life Limited Stages 3 thru 8 Compressor Rotor Spool PN 6078T56P05 Part Introduction

Mos

Hrs

Enc

72 ENG2Eff: 11-May-2004


Mos

Hrs

Enc

72 ENG1Eff: 03-Dec-2003


Mos

Hrs

Enc

72 ENG2Eff: 03-Dec-2003


Mos

Hrs

Enc

72 ENG1Eff: 21-Dec-2003


Mos

Hrs

Enc

72 ENG2Eff: 21-Dec-2003


Mos

Hrs

Enc

72 ENG1Eff: 25-Jan-2004


Mos

Hrs

Enc

72 ENG2Eff: 25-Jan-2004


Mos

Hrs

Enc

72 ENG1Eff: 24-Feb-2004


Mos

Hrs

Enc

72 ENG2Eff: 24-Feb-2004

Cat. 5 - RecommendedRE (-)72-0147 R00 ENGINE - Compressor Stator (72-32-00) - Removal of Inlet Guide Vane (IGV) and Stages 1 through 5 Self-Locking Nut PN 4037T84P03 (No Longer Valid)

Mos

Hrs

Enc

72 ENG1Eff: 30-Mar-2004

(NOTE: GE is requesting operators not to comply with this service bulletin)

Cat. 5 - RecommendedRE (-)72-0147 R00 ENGINE - Compressor Stator (72-32-00) - Removal of Inlet Guide Vane (IGV) and Stages 1 through 5 Self-Locking Nut PN 4037T84P03 (No Longer Valid)

Mos

Hrs

Enc

72 ENG2Eff: 30-Mar-2004



Generated: 6-Apr-2016 1:16 PM326/429







Cat. 9 - InformationalT (A/R)72-0147 R01 ENGINE - Compressor Stator (72-32-00) - Removal of Inlet Guide Vane (IGV) and Stages 1 through 5 Self-Locking Nut PN 4037T84P03 (No Longer Valid)

Mos

Hrs

Enc

72 ENG1Eff: 01-Jun-2005


Cat. 9 - InformationalT (A/R)72-0147 R01 ENGINE - Compressor Stator (72-32-00) - Removal of Inlet Guide Vane (IGV) and Stages 1 through 5 Self-Locking Nut PN 4037T84P03 (No Longer Valid)

Mos

Hrs

Enc

72 ENG2Eff: 01-Jun-2005



Mos

Hrs

Enc

72 ENG1Eff: 07-Apr-2004


Mos

Hrs

Enc

72 ENG2Eff: 07-Apr-2004


Mos

Hrs

Enc

72 ENG1Eff: 25-Apr-2004


Mos

Hrs

Enc

72 ENG2Eff: 25-Apr-2004

Cat. 2 - RecommendedRE (-)72-0157 R00 ENGINE - Compressor Stator (72-32-00) - Stages IGV thru 5 Self-Locking Nut Field Inspection

Mos

Hrs

Enc

72 ENG1Eff: 02-Jun-2004


Mos

Hrs

Enc

72 ENG2Eff: 02-Jun-2004


Mos

Hrs

Enc

72 ENG1Eff: 18-Mar-2005


Mos

Hrs

Enc

72 ENG2Eff: 18-Mar-2005


Mos

Hrs

Enc

72 ENG1

(NOTE: GE recommends that all engines that have reused stages IGV thru 5 self-locking nuts, with a single tab engaged on the tab washer be

inspected within 4,000 flight hours time since overhaul (TSO).)


Generated: 6-Apr-2016 1:16 PM327/429








Mos

Hrs

Enc

72 ENG2

(NOTE: GE recommends that all engines that have reused stages IGV thru 5 self-locking nuts, with a single tab engaged on the tab washer be

inspected within 4,000 flight hours time since overhaul (TSO).)

Cat. 7 - OptionalRE (-)72-0160 R00 ENGINE ~ Low Pressure Turbine Rotor (72-53-00) - Life Limited Low Pressure Turbine Disks Stages 3 Thru 6 PN 6078T91P02 PN 6078T02P04 PN 6078T92P02 and PN

6078T89P03 Parts Introduction.

Mos

Hrs

Enc

72 ENG1Eff: 08-Sep-2004

Cat. 7 - OptionalRE (-)72-0160 R00 ENGINE ~ Low Pressure Turbine Rotor (72-53-00) - Life Limited Low Pressure Turbine Disks Stages 3 Thru 6 PN 6078T91P02 PN 6078T02P04 PN 6078T92P02 and PN


Mos

Hrs

Enc

72 ENG2Eff: 08-Sep-2004

Cat. 7 - OptionalT (A/R)72-0160 R01 ENGINE - Low Pressure Turbine Rotor (72-53-00) - Life Limited Low Pressure Turbine Disks Stages 3 Thru 6 PN 6078T91P02 PN 6078T02P04 PN 6078T92P02 and PN


Mos

Hrs

Enc

72 ENG1Eff: 21-Nov-2011

Cat. 7 - OptionalT (A/R)72-0160 R01 ENGINE - Low Pressure Turbine Rotor (72-53-00) - Life Limited Low Pressure Turbine Disks Stages 3 Thru 6 PN 6078T91P02 PN 6078T02P04 PN 6078T92P02 and PN


Mos

Hrs

Enc

72 ENG2Eff: 21-Nov-2011

Cat. 7 - OptionalT (A/R)72-0161 R00 ENGINE - High Pressure Turbine Stator (72-45-00) - Introduction of Reworked Stage 2 High Pressure Turbine Seal Shroud Segments PN 5902T33G01

Mos

Hrs

Enc

72 ENG1Eff: 09-Dec-2004


Mos

Hrs

Enc

72 ENG2Eff: 09-Dec-2004


Mos

Hrs

Enc

72 ENG1Eff: 09-Dec-2004


Mos

Hrs

Enc

72 ENG2Eff: 09-Dec-2004

Cat. 5 - RecommendedRE (-)72-0163 R00 ENGINE - Power Takeoff Drive Assembly - (72-64-00) - Introduction of PTO Drive Assembly PN 6037T72G19 and Front Frame-to-PTO Oil Tube Assembly PN

6012T90G02

Mos

Hrs

Enc

72 ENG1Eff: 18-Aug-2004


Generated: 6-Apr-2016 1:16 PM328/429








6012T90G02

Mos

Hrs

Enc

72 ENG2Eff: 18-Aug-2004


6012T90G02

Mos

Hrs

Enc

72 ENG1Eff: 21-Oct-2004


6012T90G02

Mos

Hrs

Enc

72 ENG2Eff: 21-Oct-2004


6012T90G02

Mos

Hrs

Enc

72 ENG1Eff: 02-Dec-2004


6012T90G02

Mos

Hrs

Enc

72 ENG2Eff: 02-Dec-2004


6012T90G02

Mos

Hrs

Enc

72 ENG1Eff: 06-Jul-2005


6012T90G02

Mos

Hrs

Enc

72 ENG2Eff: 06-Jul-2005


6012T90G02

Mos

Hrs

Enc

72 ENG1Eff: 31-Aug-2005


6012T90G02

Mos

Hrs

Enc

72 ENG2Eff: 31-Aug-2005


Generated: 6-Apr-2016 1:16 PM329/429








6012T90G02

Mos

Hrs

Enc

72 ENG1Eff: 15-Dec-2005


6012T90G02

Mos

Hrs

Enc

72 ENG2Eff: 15-Dec-2005


6012T90G02

Mos

Hrs

Enc

72 ENG1Eff: 31-Mar-2006


6012T90G02

Mos

Hrs

Enc

72 ENG2Eff: 31-Mar-2006


6012T90G02

Mos

Hrs

Enc

72 ENG1Eff: 07-Jun-2007


6012T90G02

Mos

Hrs

Enc

72 ENG2Eff: 07-Jun-2007

Cat. 5 - RecommendedT (A/R)72-0163 R08 ENGINE - Power Takeoff Drive Assembly - (72-64-00) - Introduction of PTO Drive Assembly PN 6037T72G19 and Front Frame-to-PTO Oil Tube Assembly PN

6012T90G02

Mos

Hrs

Enc

72 ENG1Eff: 30-Jul-2008


Cat. 5 - RecommendedT (A/R)72-0163 R08 ENGINE - Power Takeoff Drive Assembly - (72-64-00) - Introduction of PTO Drive Assembly PN 6037T72G19 and Front Frame-to-PTO Oil Tube Assembly PN

6012T90G02

Mos

Hrs

Enc

72 ENG2Eff: 30-Jul-2008



Mos

Hrs

Enc

72 ENG1Eff: 20-Jun-2004


Generated: 6-Apr-2016 1:16 PM330/429








Mos

Hrs

Enc

72 ENG2Eff: 20-Jun-2004


Mos

Hrs

Enc

72 ENG1Eff: 25-Jul-2004


Mos

Hrs

Enc

72 ENG2Eff: 25-Jul-2004

Cat. 7 - OptionalRE (-)72-0166 R00 ENGINE - High Pressure Turbine Rotor (72-46-00) - Introduction of Destructive Evaluation Method for Stage 1 High Pressure Turbine Blades

Mos

Hrs

Enc

72 ENG1Eff: 03-Nov-2004

Cat. 7 - OptionalRE (-)72-0166 R00 ENGINE - High Pressure Turbine Rotor (72-46-00) - Introduction of Destructive Evaluation Method for Stage 1 High Pressure Turbine Blades

Mos

Hrs

Enc

72 ENG2Eff: 03-Nov-2004

Cat. 7 - OptionalT (A/R)72-0166 R01 ENGINE - High Pressure Turbine Rotor (72-46-00) - Introduction of Destructive Evaluation Method for Stage 1 High Pressure Turbine Blades

Mos

Hrs

Enc

72 ENG1Eff: 26-Mar-2012

Cat. 7 - OptionalT (A/R)72-0166 R01 ENGINE - High Pressure Turbine Rotor (72-46-00) - Introduction of Destructive Evaluation Method for Stage 1 High Pressure Turbine Blades

Mos

Hrs

Enc

72 ENG2Eff: 26-Mar-2012


Mos

Hrs

Enc

72 ENG1Eff: 22-Aug-2004


Mos

Hrs

Enc

72 ENG2Eff: 22-Aug-2004

Cat. 7 - OptionalRE (-)72-0171 R00 ENGINE - Fan Stator Assembly (72-23-00) - Introduction of New No. 1 and 2 Bearing Housing Assembly PN 6047T69G04

Mos

Hrs

Enc

72 ENG1Eff: 20-Jan-2005

Cat. 7 - OptionalRE (-)72-0171 R00 ENGINE - Fan Stator Assembly (72-23-00) - Introduction of New No. 1 and 2 Bearing Housing Assembly PN 6047T69G04

Mos

Hrs

Enc

72 ENG2Eff: 20-Jan-2005


Generated: 6-Apr-2016 1:16 PM331/429







Cat. 7 - OptionalT (A/R)72-0171 R01 ENGINE - Fan Stator Assembly (72-23-00) - Introduction of New No. 1 and 2 Bearing Housing Assembly PN 6047T69G04

Mos

Hrs

Enc

72 ENG1Eff: 15-Dec-2005

Cat. 7 - OptionalT (A/R)72-0171 R01 ENGINE - Fan Stator Assembly (72-23-00) - Introduction of New No. 1 and 2 Bearing Housing Assembly PN 6047T69G04

Mos

Hrs

Enc

72 ENG2Eff: 15-Dec-2005

Cat. 7 - OptionalRE (-)72-0172 R00 ENGINE - Low Pressure Turbine Stator Assembly (72-54-00) - Introduction of Stage 3 through 6 Shroud and Seal Sectors

Mos

Hrs

Enc

72 ENG1Eff: 02-Dec-2004

Cat. 7 - OptionalRE (-)72-0172 R00 ENGINE - Low Pressure Turbine Stator Assembly (72-54-00) - Introduction of Stage 3 through 6 Shroud and Seal Sectors

Mos

Hrs

Enc

72 ENG2Eff: 02-Dec-2004


Mos

Hrs

Enc

72 ENG1Eff: 24-Oct-2004


Mos

Hrs

Enc

72 ENG2Eff: 24-Oct-2004

Cat. 5 - RecommendedRE (-)72-0175 R00 ENGINE - Compressor Rotor (72-00-00) - Removal of the Stages 10 through 14 Compressor Rotor Spool PN 6037T83P03 PN 6037T83P04 and PN 6087T02P01

Mos

Hrs

Enc

72 ENG1Eff: 30-Mar-2005

(NOTE: GE recommends that you replace and discard the stages 10 through 14 compressor rotor spool PN 6037T83P03, PN 6037T83P04, and

PN 6087T02P01 when they are removed from the engine/module)


Mos

Hrs

Enc

72 ENG2Eff: 30-Mar-2005




Mos

Hrs

Enc

72 ENG1Eff: 15-Dec-2005




Mos

Hrs

Enc

72 ENG2Eff: 15-Dec-2005




Generated: 6-Apr-2016 1:16 PM332/429







Cat. 3 - RecommendedT (A/R)72-0175 R02 ENGINE - Compressor Rotor (72-00-00) - Removal of the Stages 10 through 14 Compressor Rotor Spool PN 6037T83P03 PN 6037T83P04 and PN 6087T02P01

Mos

Hrs

Enc

72 ENG1Eff: 29-May-2012



Cat. 3 - RecommendedT (A/R)72-0175 R02 ENGINE - Compressor Rotor (72-00-00) - Removal of the Stages 10 through 14 Compressor Rotor Spool PN 6037T83P03 PN 6037T83P04 and PN 6087T02P01

Mos

Hrs

Enc

72 ENG2Eff: 29-May-2012



Cat. 4 - RecommendedRE (-)72-0176 R00 ENGINE - Combustion Chamber Frame and B-Sump (72-41-00) - Introduction of No. 5 Roller Bearings PN 5042T13P04 PN 5042T13P05 PN 5022T87P04 and PN

5022T87P05

Mos

Hrs

Enc

72 ENG1Eff: 17-Dec-2004


5022T87P05

Mos

Hrs

Enc

72 ENG2Eff: 17-Dec-2004


5022T87P05

Mos

Hrs

Enc

72 ENG1Eff: 18-Feb-2005


5022T87P05

Mos

Hrs

Enc

72 ENG2Eff: 18-Feb-2005


5022T87P05

Mos

Hrs

Enc

72 ENG1Eff: 06-Apr-2005


5022T87P05

Mos

Hrs

Enc

72 ENG2Eff: 06-Apr-2005


5022T87P05

Mos

Hrs

Enc

72 ENG1Eff: 15-Dec-2005


Generated: 6-Apr-2016 1:16 PM333/429








5022T87P05

Mos

Hrs

Enc

72 ENG2Eff: 15-Dec-2005

Cat. 4 - RecommendedT (A/R)72-0176 R04 ENGINE - Combustion Chamber Frame and B-Sump (72-41-00) - Introduction of No. 5 Roller Bearings PN 5042T13P04 PN 5042T13P05 PN 5022T87P04 and PN

5022T87P05

Mos

Hrs

Enc

72 ENG1Eff: 10-Jul-2006


Cat. 4 - RecommendedT (A/R)72-0176 R04 ENGINE - Combustion Chamber Frame and B-Sump (72-41-00) - Introduction of No. 5 Roller Bearings PN 5042T13P04 PN 5042T13P05 PN 5022T87P04 and PN

5022T87P05

Mos

Hrs

Enc

72 ENG2Eff: 10-Jul-2006


Cat. 8 - InformationalT (A/R)72-0177 R00 ENGINE - General - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2 Turbofan Engines

Mos

Hrs

Enc

72 ENG1Eff: 30-Jan-2005

Cat. 8 - InformationalT (A/R)72-0177 R00 ENGINE - General - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2 Turbofan Engines

Mos

Hrs

Enc

72 ENG2Eff: 30-Jan-2005

Cat. 5 - RecommendedRE (-)72-0179 R00 ENGINE - Compressor Stator (72-32-00) - Introduction of a New Redesigned IGV Inner Support Shroud PN 5026T65G06

Mos

Hrs

Enc

72 ENG1Eff: 06-Apr-2005

(NOTE: For CF34-3B engines: Category 3GE recommends that the IGV inner support shroud P/N 5026T65G05 be replaced with the redesigned

IGV inner support shroud P/N 5026T65G06 at next engine shop visit.For CF34-1A and CF34-3A engines: Category 5GE recommends that the

IGV inner support shroud P/N 5026T65G05 be replaced with the redesigned IGV inner support shroud P/N 5026T65G06 when the part is

removed from the engine.)


Mos

Hrs

Enc

72 ENG2Eff: 06-Apr-2005






Mos

Hrs

Enc

72 ENG1Eff: 24-May-2005






Generated: 6-Apr-2016 1:16 PM334/429








Mos

Hrs

Enc

72 ENG2Eff: 24-May-2005






Mos

Hrs

Enc

72 ENG1Eff: 15-Dec-2005






Mos

Hrs

Enc

72 ENG2Eff: 15-Dec-2005






Mos

Hrs

Enc

72 ENG1Eff: 08-Aug-2006






Mos

Hrs

Enc

72 ENG2Eff: 08-Aug-2006






Mos

Hrs

Enc

72 ENG1Eff: 07-Sep-2007






Mos

Hrs

Enc

72 ENG2Eff: 07-Sep-2007






Generated: 6-Apr-2016 1:16 PM335/429








Mos

Hrs

Enc

72 ENG1Eff: 01-Jul-2008






Mos

Hrs

Enc

72 ENG2Eff: 01-Jul-2008





Cat. 3 - RecommendedRE (-)72-0179 R06 ENGINE - Compressor Stator (72-32-00) - Introduction of a New Redesigned IGV Inner Support Shroud P/N 5026T65G06

Mos

Hrs

Enc

72 ENG1Eff: 20-Sep-2010





Cat. 3 - RecommendedRE (-)72-0179 R06 ENGINE - Compressor Stator (72-32-00) - Introduction of a New Redesigned IGV Inner Support Shroud P/N 5026T65G06

Mos

Hrs

Enc

72 ENG2Eff: 20-Sep-2010





Cat. 3 - RecommendedT (A/R)72-0179 R07 ENGINE - Compressor Stator (72-32-00) - Introduction of a New Redesigned IGV Inner Support Shroud P/N 5026T65G06

Mos

Hrs

Enc

72 ENG1Eff: 04-Apr-2011





Cat. 3 - RecommendedT (A/R)72-0179 R07 ENGINE - Compressor Stator (72-32-00) - Introduction of a New Redesigned IGV Inner Support Shroud P/N 5026T65G06

Mos

Hrs

Enc

72 ENG2Eff: 04-Apr-2011





Cat. 7 - OptionalRE (-)72-0181 R04 ENGINE - High Pressure Turbine Stator (72-45-00) - Introduction of N2 Alloy Stage 1 HP Turbine Shrouds Shroud Hangers Segment Seals

Mos

Hrs

Enc

72 ENG1Eff: 20-Aug-2008


Mos

Hrs

Enc

72 ENG2Eff: 20-Aug-2008


Generated: 6-Apr-2016 1:16 PM336/429








Mos

Hrs

Enc

72 ENG1Eff: 24-Jun-2014


Mos

Hrs

Enc

72 ENG2Eff: 24-Jun-2014

Cat. 6 - RecommendedRE (-)72-0182 R00 ENGINE - Combustion Liner Assembly (72-41-00) - Combustion Liner Field Modification and Repair Configuration

Mos

Hrs

Enc

72 ENG1Eff: 09-Feb-2006


Mos

Hrs

Enc

72 ENG2Eff: 09-Feb-2006


Mos

Hrs

Enc

72 ENG1Eff: 30-Mar-2006


Mos

Hrs

Enc

72 ENG2Eff: 30-Mar-2006


Mos

Hrs

Enc

72 ENG1Eff: 18-May-2006


Mos

Hrs

Enc

72 ENG2Eff: 18-May-2006

Cat. 6 - RecommendedT (A/R)72-0182 R03 ENGINE - Combustion Liner Assembly (72-41-00) - Combustion Liner Field Modification and Repair Configuration

Mos

Hrs

Enc

72 ENG1Eff: 22-Jun-2006

Cat. 6 - RecommendedT (A/R)72-0182 R03 ENGINE - Combustion Liner Assembly (72-41-00) - Combustion Liner Field Modification and Repair Configuration

Mos

Hrs

Enc

72 ENG2Eff: 22-Jun-2006


Mos

Hrs

Enc

72 ENG1Eff: 29-May-2005


Generated: 6-Apr-2016 1:16 PM337/429








Mos

Hrs

Enc

72 ENG2Eff: 29-May-2005


Mos

Hrs

Enc

72 ENG1Eff: 15-Aug-2007


Mos

Hrs

Enc

72 ENG2Eff: 15-Aug-2007

Cat. 6 - RecommendedT (A/R)72-0185 R00 ENGINE - Combustion Chamber Frame and B-Sump Assembly (72-41-00) - Introduction of Reworked B-Sump Housing PN 4923T00G01

Mos

Hrs

Enc

72 ENG1Eff: 29-Sep-2005


Cat. 6 - RecommendedT (A/R)72-0185 R00 ENGINE - Combustion Chamber Frame and B-Sump Assembly (72-41-00) - Introduction of Reworked B-Sump Housing PN 4923T00G01

Mos

Hrs

Enc

72 ENG2Eff: 29-Sep-2005



Mos

Hrs

Enc

72 ENG1Eff: 28-Aug-2005


Mos

Hrs

Enc

72 ENG2Eff: 28-Aug-2005

Cat. 8 - InformationalRE (-)72-0189 R00 ENGINE - General - Spare Parts Release for CF34-1A/-3A/3A1/-3A2/-3B Turbofan Engines

Mos

Hrs

Enc

72 ENG1Eff: 25-Oct-2005

Cat. 8 - InformationalRE (-)72-0189 R00 ENGINE - General - Spare Parts Release for CF34-1A/-3A/3A1/-3A2/-3B Turbofan Engines

Mos

Hrs

Enc

72 ENG2Eff: 25-Oct-2005

Cat. 8 - InformationalT (A/R)72-0189 R01 ENGINE - General - Spare Parts Release for CF34-1A/-3A/3A1/-3A2/-3B Turbofan Engines

Mos

Hrs

Enc

72 ENG1Eff: 11-May-2006


Generated: 6-Apr-2016 1:16 PM338/429








Mos

Hrs

Enc

72 ENG2Eff: 11-May-2006

Cat. 5 - RecommendedRE (-)72-0190 R00 ENGINE - Accessory Gearbox Assembly (72-62-00) - Introduction of AGB Carbon Seals PNs 5018T49P05 5016T32P05 and 4138T09P03

Mos

Hrs

Enc

72 ENG1Eff: 22-Nov-2005

Cat. 5 - RecommendedRE (-)72-0190 R00 ENGINE - Accessory Gearbox Assembly (72-62-00) - Introduction of AGB Carbon Seals PNs 5018T49P05 5016T32P05 and 4138T09P03

Mos

Hrs

Enc

72 ENG2Eff: 22-Nov-2005

Cat. 5 - RecommendedRE (-)72-0190 R01 ENGINE - Accessory Gearbox Assembly (72-62-00) - Introduction of AGB Carbon Seals PNs 4138T09P02 4138T09P03 5016T32P05 5016T32P06 5018T48P04

5018T48P05 5018T49P05 and 5018T49P06

Mos

Hrs

Enc

72 ENG1Eff: 14-Jun-2007


5018T48P05 5018T49P05 and 5018T49P06

Mos

Hrs

Enc

72 ENG2Eff: 14-Jun-2007


5018T48P05 5018T49P05 and 5018T49P06

Mos

Hrs

Enc

72 ENG1Eff: 03-Jan-2008


5018T48P05 5018T49P05 and 5018T49P06

Mos

Hrs

Enc

72 ENG2Eff: 03-Jan-2008


5018T48P05 5018T49P05 and 5018T49P06

Mos

Hrs

Enc

72 ENG1Eff: 20-Aug-2008

Cat. 5 - RecommendedT (A/R)72-0190 R03 ENGINE - Accessory Gearbox Assembly (72-62-00) - Introduction of AGB Carbon Seals PNs 4138T09P02 4138T09P03 5016T32P05 5016T32P06 5018T48P04

5018T48P05 5018T49P05 and 5018T49P06

Mos

Hrs

Enc

72 ENG2Eff: 20-Aug-2008

Cat. 2 - RecommendedRE (-)72-0193 R00 ENGINE - Compressor Stator Assembly (72-32-00) - Inspection of HPC Stage 2 VG Turnbuckles

25-Jul-2008Mos

11,528.2Hrs

6,334Enc

72 ENG1Complied With

(NOTE: GE recommends that you do this Service Bulletin as soon as possible without effect on revenue service but within 2,500 cycles since

last shop visit. If over 2,500 cycles since last shop visit or within 250 cycles since issuance of this Service Bulletin for ESNs affected)


Generated: 6-Apr-2016 1:16 PM339/429







Cat. 2 - RecommendedRE (-)72-0193 R00 ENGINE - Compressor Stator Assembly (72-32-00) - Inspection of HPC Stage 2 VG Turnbuckles

25-Jul-2008Mos

11,411.2Hrs

6,293Enc

72 ENG2Eff: 18-May-2006 Not Applicable

Cat. 7 - OptionalRE (-)72-0195 R00 ENGINE - General (72-00-00) - Upgrade of CF34-1A and CF34-3A Model Engines to CF34-3A2 Model Engine

Mos

Hrs

Enc

72 ENG1Eff: 09-Jun-2006

Cat. 7 - OptionalRE (-)72-0195 R00 ENGINE - General (72-00-00) - Upgrade of CF34-1A and CF34-3A Model Engines to CF34-3A2 Model Engine

Mos

Hrs

Enc

72 ENG2Eff: 09-Jun-2006

Cat. 7 - OptionalRE (-)72-0195 R01 ENGINE - General (72-00-00) - Upgrade of CF34-1A and CF34-3A Model Engines to CF34-3A2

Mos

Hrs

Enc

72 ENG1Eff: 16-Feb-2010


Mos

Hrs

Enc

72 ENG2Eff: 16-Feb-2010


Mos

Hrs

Enc

72 ENG1Eff: 21-Apr-2010


Mos

Hrs

Enc

72 ENG2Eff: 21-Apr-2010


Mos

Hrs

Enc

72 ENG1Eff: 18-Aug-2010


Mos

Hrs

Enc

72 ENG2Eff: 18-Aug-2010


Mos

Hrs

Enc

72 ENG1Eff: 06-Apr-2011


Mos

Hrs

Enc

72 ENG2Eff: 06-Apr-2011


Generated: 6-Apr-2016 1:16 PM340/429








Mos

Hrs

Enc

72 ENG1Eff: 31-Oct-2011


Mos

Hrs

Enc

72 ENG2Eff: 31-Oct-2011


Mos

Hrs

Enc

72 ENG1Eff: 09-Feb-2012


Mos

Hrs

Enc

72 ENG2Eff: 09-Feb-2012


Mos

Hrs

Enc

72 ENG1Eff: 29-Aug-2012


Mos

Hrs

Enc

72 ENG2Eff: 29-Aug-2012


Mos

Hrs

Enc

72 ENG1Eff: 16-Jul-2013


Mos

Hrs

Enc

72 ENG2Eff: 16-Jul-2013

Category 7RE (-)72-0195 R09 ENGINE - General (72-00-00) - Upgrade of CF34-1A and CF34-3A Model Engines to CF34-3A2

Mos

Hrs

Enc

72 ENG1Eff: 10-Feb-2015

(AVG MAN HRS: 200)

Category 7RE (-)72-0195 R09 ENGINE - General (72-00-00) - Upgrade of CF34-1A and CF34-3A Model Engines to CF34-3A2

Mos

Hrs

Enc

72 ENG2Eff: 10-Feb-2015

(AVG MAN HRS: 200)


Mos

Hrs

Enc

72 ENG1Eff: 30-Apr-2006


Generated: 6-Apr-2016 1:16 PM341/429








Mos

Hrs

Enc

72 ENG2Eff: 30-Apr-2006

Cat. 5 - RecommendedRE (-)72-0197 R00 ENGINE - Accessory Drive Section (72-62-00) - Introduction of Improved Accessory Gear Box Axis K Cranking Plug PN 4189T24G01 and Retain Ring PN AS3217-127

Mos

Hrs

Enc

72 ENG1Eff: 12-Jun-2006


Mos

Hrs

Enc

72 ENG2Eff: 12-Jun-2006


Mos

Hrs

Enc

72 ENG1Eff: 12-Oct-2006


Mos

Hrs

Enc

72 ENG2Eff: 12-Oct-2006


Mos

Hrs

Enc

72 ENG1Eff: 10-Apr-2007


Mos

Hrs

Enc

72 ENG2Eff: 10-Apr-2007

Cat. 5 - RecommendedT (-)72-0197 R03 ENGINE - Accessory Drive Section (72-62-00) - Introduction of Improved Accessory Gear Box Axis K Cranking Plug PN 4189T24G01 and Retainer Ring PN AS3217-127

Mos

Hrs

Enc

72 ENG1Eff: 11-Aug-2008


Mos

Hrs

Enc

72 ENG2Eff: 11-Aug-2008

Cat. 5 - RecommendedRE (-)72-0197 R04 ENGINE - Accessory Drive Section (72-62-00) - Introduction of Improved Accessory Gear Box Axis K Cranking Plug PN 4189T24G01 and Retainer Ring PN AS3217-127

Mos

Hrs

Enc

72 ENG1Eff: 08-Jan-2015


Mos

Hrs

Enc

72 ENG2Eff: 08-Jan-2015


Generated: 6-Apr-2016 1:16 PM342/429







Cat. 5 - RecommendedRE (-)72-0197 R05 ENGINE - Accessory Drive Section (72-62-00) - Introduction of Improved Accessory Gear Box Axis K Cranking Plug PN 4189T24G01 and Retainer Ring PN AS3217-127

Mos

Hrs

Enc

72 ENG1Eff: 01-Jun-2015

Cat. 5 - RecommendedT (A/R)72-0197 R05 ENGINE - Accessory Drive Section (72-62-00) - Introduction of Improved Accessory Gear Box Axis K Cranking Plug PN 4189T24G01 and Retainer Ring PN AS3217-127

Mos

Hrs

Enc

72 ENG2Eff: 01-Jun-2015


Mos

Hrs

Enc

72 ENG1Eff: 28-May-2006


Mos

Hrs

Enc

72 ENG2Eff: 28-May-2006

Cat. 6 - RecommendedRE (-)72-0201 R00 ENGINE - (72-42-00) - Rework of the Stage 1 HPT Nozzle Support

Mos

Hrs

Enc

72 ENG1Eff: 13-Apr-2007

Cat. 6 - RecommendedRE (-)72-0201 R00 ENGINE - (72-42-00) - Rework of the Stage 1 HPT Nozzle Support

Mos

Hrs

Enc

72 ENG2Eff: 13-Apr-2007

Cat. 6 - RecommendedT (A/R)72-0201 R01 ENGINE - (72-42-00) - Rework of the Stage 1 HPT Nozzle Support

Mos

Hrs

Enc

72 ENG1Eff: 16-Nov-2007

Cat. 6 - RecommendedT (A/R)72-0201 R01 ENGINE - (72-42-00) - Rework of the Stage 1 HPT Nozzle Support

Mos

Hrs

Enc

72 ENG2Eff: 16-Nov-2007

Cat. 7 - OptionalRE (-)72-0203 R00 ENGINE - Low Pressure Turbine Stator Assembly (72-52-00) - Introduction of Stage 3 Shroud Sector PN 5099T32G02 for CF34-3A1 Engine Models

Mos

Hrs

Enc

72 ENG1Eff: 04-Oct-2006


Mos

Hrs

Enc

72 ENG2Eff: 04-Oct-2006


Mos

Hrs

Enc

72 ENG1Eff: 26-Jan-2007


Generated: 6-Apr-2016 1:16 PM343/429








Mos

Hrs

Enc

72 ENG2Eff: 26-Jan-2007


Mos

Hrs

Enc

72 ENG1Eff: 11-Apr-2007


Mos

Hrs

Enc

72 ENG2Eff: 11-Apr-2007

Cat. 7 - OptionalRE (-)72-0203 R03 ENGINE - Low Pressure Turbine Stator Assembly (72-52-00) - Introduction of Stage 3 Shroud Sector PN 5099T32G02 PN 6020T00G04 and PN 6020T00G06 for use on

CF34-1A/-3A/-3A2/-3A1 Engine Models.

Mos

Hrs

Enc

72 ENG1Eff: 20-May-2009

Also ConsiderDUE:1. T A/R | 2. RE -ENGINE - Low Pressure Turbine Stator Assembly (72-52-00) - I...72-0241 R01ENG172

Cat. 7 - OptionalRE (-)72-0203 R03 ENGINE - Low Pressure Turbine Stator Assembly (72-52-00) - Introduction of Stage 3 Shroud Sector PN 5099T32G02 PN 6020T00G04 and PN 6020T00G06 for use on

CF34-1A/-3A/-3A2/-3A1 Engine Models.

Mos

Hrs

Enc

72 ENG2Eff: 20-May-2009

Also ConsiderDUE:1. T A/R | 2. RE -ENGINE - Low Pressure Turbine Stator Assembly (72-52-00) - I...72-0241 R01ENG272

Cat. 7 - OptionalRE (-)72-0204 R00 ENGINE - Turbine Transition Assembly (72-51-00) - Rework of HPT Stator Components for Borescope Capability

Mos

Hrs

Enc

72 ENG1Eff: 05-Jan-2007

Cat. 7 - OptionalRE (-)72-0204 R00 ENGINE - Turbine Transition Assembly (72-51-00) - Rework of HPT Stator Components for Borescope Capability

Mos

Hrs

Enc

72 ENG2Eff: 05-Jan-2007

Cat. 7 - OptionalT (A/R)72-0204 R01 ENGINE - Turbine Transition Assembly (72-51-00) - Rework of HPT Stator Components for Borescope Capability

Mos

Hrs

Enc

72 ENG1Eff: 02-Aug-2007

Cat. 7 - OptionalT (A/R)72-0204 R01 ENGINE - Turbine Transition Assembly (72-51-00) - Rework of HPT Stator Components for Borescope Capability

Mos

Hrs

Enc

72 ENG2Eff: 02-Aug-2007


Mos

Hrs

Enc

72 ENG1Eff: 27-Aug-2006


Generated: 6-Apr-2016 1:16 PM344/429








Mos

Hrs

Enc

72 ENG2Eff: 27-Aug-2006


Mos

Hrs

Enc

72 ENG1Eff: 15-Oct-2008


Mos

Hrs

Enc

72 ENG2Eff: 15-Oct-2008


Mos

Hrs

Enc

72 ENG1Eff: 08-Feb-2013


Mos

Hrs

Enc

72 ENG2Eff: 08-Feb-2013

Cat. 7 - OptionalRE (-)72-0206 R00 ENGINE - High Pressure Turbine Stator Assembly (72-45-00) - Introduction of Alternate Blind Rivets to Replace Aft Flange Gang Channels

Mos

Hrs

Enc

72 ENG1Eff: 21-Nov-2006

Cat. 7 - OptionalRE (-)72-0206 R00 ENGINE - High Pressure Turbine Stator Assembly (72-45-00) - Introduction of Alternate Blind Rivets to Replace Aft Flange Gang Channels

Mos

Hrs

Enc

72 ENG2Eff: 21-Nov-2006

Cat. 7 - OptionalT (A/R)72-0206 R01 ENGINE - High Pressure Turbine Stator Assembly (72-45-00) - Introduction of Alternate Blind Rivets to Replace Aft Flange Gang Channels

Mos

Hrs

Enc

72 ENG1Eff: 02-Jun-2009

Cat. 7 - OptionalT (A/R)72-0206 R01 ENGINE - High Pressure Turbine Stator Assembly (72-45-00) - Introduction of Alternate Blind Rivets to Replace Aft Flange Gang Channels

Mos

Hrs

Enc

72 ENG2Eff: 02-Jun-2009


Mos

Hrs

Enc

72 ENG1Eff: 26-Nov-2006


Mos

Hrs

Enc

72 ENG2Eff: 26-Nov-2006


Generated: 6-Apr-2016 1:16 PM345/429







Cat. 3 - Recommended ≈21-Apr-2047T72-0209 R00 ENGINE - Fan Rotor (72-21-00) - Introduction of a Redesigned Fan Blade Retaining Pin

Mos

Hrs

11,231 Enc18,00018,000Enc

72 ENG1

(NOTE: GE recommends if the engine is over 18,000 cycles to replace with the new fan blade retaining pins at the next shop visit.)

Cat. 3 - Recommended ≈02-Jun-2047T72-0209 R00 ENGINE - Fan Rotor (72-21-00) - Introduction of a Redesigned Fan Blade Retaining Pin

Mos

Hrs

11,272 Enc18,00018,000Enc

72 ENG2

(NOTE: GE recommends if the engine is over 18,000 cycles to replace with the new fan blade retaining pins at the next shop visit.)


Mos

Hrs

Enc

72 ENG1Eff: 15-Feb-2007


Mos

Hrs

Enc

72 ENG2Eff: 15-Feb-2007

Cat. 7 - OptionalT (A/R)72-0214 R00 ENGINE - Fan Rotor Assembly and Components (72-21-00) - Introduction of Spiral Painting to the Forward Outer Spinner

Mos

Hrs

Enc

72 ENG1Eff: 05-May-2008

Cat. 7 - OptionalT (A/R)72-0214 R00 ENGINE - Fan Rotor Assembly and Components (72-21-00) - Introduction of Spiral Painting to the Forward Outer Spinner

Mos

Hrs

Enc

72 ENG2Eff: 05-May-2008

Cat. 3 - RecommendedRE (-)72-0215 R00 ENGINE - Fan Rotor Assembly (72-21-00) - ECI Inspection of Fan Blade Pin Hole

Mos

Hrs

Enc

72 ENG1Eff: 14-Jun-2007

(NOTE: Inspection recommended anytime fan blades are in for shop visit, provided blades have been in service 3,000 cycles or more since

prior shop visit inspection.)


Mos

Hrs

Enc

72 ENG2Eff: 14-Jun-2007




25-Jul-2008Mos

11,411.2Hrs

6,293Enc

72 ENG2BY PART S/N INSTALLEDEff: 07-Aug-2007 Not

Applicable




Mos

Hrs

Enc

72 ENG1Eff: 07-Aug-2007




Generated: 6-Apr-2016 1:16 PM346/429







Cat. 3 - RecommendedT (-)72-0215 R02 ENGINE - Fan Rotor Assembly (72-21-00) - ECI Inspection of Fan Blade Pin Hole

Mos

Hrs

Enc

72 ENG1Eff: 01-Jun-2011



Cat. 3 - RecommendedT (-)72-0215 R02 ENGINE - Fan Rotor Assembly (72-21-00) - ECI Inspection of Fan Blade Pin Hole

Mos

Hrs

Enc

72 ENG2Eff: 01-Jun-2011



Category 3T (A/R)72-0215 R03 ENGINE - Fan Rotor Assembly (72-21-00) - ECI Inspection of Fan Blade Pin Hole

Mos

Hrs

Enc

72 ENG1Eff: 14-Apr-2015

(AVG MAN HRS: 7) (NOTE: The fan blades P/N 6018T30P14 with serial numbers (S/N) thatstart with "MAE" are affected by this Service Bulletin)


Category 3T (A/R)72-0215 R03 ENGINE - Fan Rotor Assembly (72-21-00) - ECI Inspection of Fan Blade Pin Hole

Mos

Hrs

Enc

72 ENG2Eff: 14-Apr-2015

(AVG MAN HRS: 7) (NOTE: The fan blades P/N 6018T30P14 with serial numbers (S/N) thatstart with "MAE" are affected by this Service Bulletin)



Mos

Hrs

Enc

72 ENG1Eff: 27-May-2007


Mos

Hrs

Enc

72 ENG2Eff: 27-May-2007

Cat. 5 - RecommendedRE (-)72-0217 R00 ENGINE - (72-42-00) - Rework of the Air Balance Piston Stationary Seal

Mos

Hrs

Enc

72 ENG1Eff: 27-Jul-2007

Also ConsiderDUE:1. T A/R | 2. RE -ENGINE - (72-42-00) - Rework of the Stage 1 HPT Nozzle Suppo...72-0201 R01ENG172

Cat. 5 - RecommendedT (A/R)72-0217 R00 ENGINE - (72-42-00) - Rework of the Air Balance Piston Stationary Seal

Mos

Hrs

Enc

72 ENG2Eff: 27-Jul-2007

Also ConsiderDUE:1. T A/R | 2. RE -ENGINE - (72-42-00) - Rework of the Stage 1 HPT Nozzle Suppo...72-0201 R01ENG272


Mos

Hrs

Enc

72 ENG1Eff: 23-Sep-2007


Generated: 6-Apr-2016 1:16 PM347/429








Mos

Hrs

Enc

72 ENG2Eff: 23-Sep-2007

Cat. 8 - InformationalT (A/R)72-0219 R00 ENGINE - General (72-00-00) - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Engines

Mos

Hrs

Enc

72 ENG1Eff: 28-Oct-2007


Mos

Hrs

Enc

72 ENG2Eff: 28-Oct-2007

Cat. 7 - OptionalRE (-)72-0221 R00 ENGINE - Fan Rotor Assembly (72-21-00) - Introduction of Fan Blade P/N 6018T30P15

Mos

Hrs

Enc

72 ENG1Eff: 07-Jan-2008


Mos

Hrs

Enc

72 ENG2Eff: 07-Jan-2008


Mos

Hrs

Enc

72 ENG1Eff: 30-Jan-2009

Cat. 7 - OptionalT (A/R)72-0221 R01 ENGINE - Fan Rotor Assembly (72-21-00) - Introduction of Fan Blade P/N 6018T30P15

Mos

Hrs

Enc

72 ENG2Eff: 30-Jan-2009

Cat. 7 - OptionalRE (-)72-0222 R00 ENGINE - General - Introduction of a New Hydraulic Drain Line

Mos

Hrs

Enc

72 ENG1Eff: 09-Jan-2008


Mos

Hrs

Enc

72 ENG2Eff: 09-Jan-2008


Mos

Hrs

Enc

72 ENG1Eff: 12-Jul-2011


Mos

Hrs

Enc

72 ENG2Eff: 12-Jul-2011


Generated: 6-Apr-2016 1:16 PM348/429








Mos

Hrs

Enc

72 ENG1Eff: 11-May-2013


Mos

Hrs

Enc

72 ENG2Eff: 11-May-2013


Mos

Hrs

Enc

72 ENG1Eff: 23-Dec-2007


Mos

Hrs

Enc

72 ENG2Eff: 23-Dec-2007

Cat. 8 - InformationalT (A/R)72-0224 R00 ENGINE - General (72-00-00) - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2 Engines

Mos

Hrs

Enc

72 ENG1Eff: 08-Feb-2008

Cat. 8 - InformationalT (A/R)72-0224 R00 ENGINE - General (72-00-00) - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2 Engines

Mos

Hrs

Enc

72 ENG2Eff: 08-Feb-2008

Cat. 3 - RecommendedT (A/R)72-0225 R00 ENGINE - Compressor Rotor Assembly (72-33-00) - Reblade of Engines Shipped with Non-Standard Stage 9 Compressor Blade Count

Mos

Hrs

Enc

72 ENG1Eff: 11-Feb-2008

(NOTE: THIS SERVICE BULLETIN IS FOR LIMITED DISTRIBUTION)

Cat. 3 - RecommendedT (A/R)72-0225 R00 ENGINE - Compressor Rotor Assembly (72-33-00) - Reblade of Engines Shipped with Non-Standard Stage 9 Compressor Blade Count

Mos

Hrs

Enc

72 ENG2Eff: 11-Feb-2008



Mos

Hrs

Enc

72 ENG1Eff: 10-Mar-2008


Mos

Hrs

Enc

72 ENG2Eff: 10-Mar-2008

Cat. 8 - InformationalT (A/R)72-0227 R00 ENGINE - General (72-00-00) - Spare Parts Release for CF34-1A/-3A/-3A2 Engines

Mos

Hrs

Enc

72 ENG1Eff: 11-Mar-2008


Generated: 6-Apr-2016 1:16 PM349/429








Mos

Hrs

Enc

72 ENG2Eff: 11-Mar-2008


Mos

Hrs

Enc

72 ENG1Eff: 28-Mar-2008


Mos

Hrs

Enc

72 ENG2Eff: 28-Mar-2008

Cat. 2 - RecommendedRE (-)72-0229 R00 ENGINE - Fan Rotor (72-21-00) - Field Management Program of Fan Blades P/N 6018T30P14 Made From VSMPO Mill Source Material

25-Jul-2008Mos

11,528.2Hrs

6,334Enc

72 ENG1BY PART S/N INSTALLEDEff: 10-Apr-2008 Not

Applicable

(NOTE: If the CSN on the part reaches 1,200 CSN prior to completing the ECI per this Service Bulletin, it is recommended that a visual

inspection of the fan containment case abradable rub strip be completed at repeat intervals as described in CF34-BJ S/B 72-0231 until the ECI

or fan blade replacement can be complied with. It does not apply to field modified fan blades P/N 4923T56G08, even if the serial number is

listed in paragraph 4., APPENDIX A and paragraph 5., APPENDIX B. Refer to CF34-BJ S/B 72-0230 for these blades.)


Mos

Hrs

Enc

72 ENG2Eff: 10-Apr-2008





Cat. 2 - Recommended ≈16-Aug-2016RE72-0229 R01 ENGINE - Fan Rotor (72-21-00) - Field Management Program of Fan Blades P/N 6018T30P14 Made From VSMPO Mill Source Material

20-May-2009Mos

11,437.8Hrs

186 Enc6,9146006,314Enc

72 ENG2BY PART NUMBER INSTALLEDEff: 10-Apr-2008 Not

Applicable






Mos

Hrs

Enc

72 ENG1Eff: 30-Jul-2008

Cat. 2 - RecommendedRE (-)72-0230 R00 ENGINE - Fan Rotor (72-21-00) - Field Management Program of Fan Blades P/N 4923T56G08 Made From VSMPO Mill Source Material

20-May-2009Mos

11,437.8Hrs

6,314Enc

72 ENG2BY PART NUMBER INSTALLEDEff: 10-Apr-2008 Not

Applicable

Cat. 2 - RecommendedRE (-)72-0230 R00 ENGINE - Fan Rotor (72-21-00) - Field Management Program of Fan Blades P/N 4923T56G08 Made From VSMPO Mill Source Material

25-Jul-2008Mos

11,528.2Hrs

6,334Enc

72 ENG1BY PART S/N INSTALLEDEff: 10-Apr-2008 Not

Applicable


Generated: 6-Apr-2016 1:16 PM350/429







Cat. 2 - Recommended ≈31-Mar-2018T72-0230 R01 ENGINE - Fan Rotor (72-21-00) - Field Management Program of Fan Blades P/N 4923T56G08 Made From VSMPO Mill Source Material

Mos

Hrs

770 Enc≈7,5391,200Enc

72 ENG1Eff: 30-Jul-2008

(NOTE: GE recommends that you do this Service Bulletin without effect on revenue service as close as possible, but prior to 1,200 additional

flight cycles from when the pinhole bushing was installed.)


Cat. 2 - Recommended ≈31-Mar-2018T72-0230 R01 ENGINE - Fan Rotor (72-21-00) - Field Management Program of Fan Blades P/N 4923T56G08 Made From VSMPO Mill Source Material

Mos

Hrs

770 Enc≈7,4981,200Enc

72 ENG2Eff: 30-Jul-2008

(NOTE: GE recommends that you do this Service Bulletin without effect on revenue service as close as possible, but prior to 1,200 additional

flight cycles from when the pinhole bushing was installed.)


Cat. 2 - RecommendedRE (-)72-0231 R00 ENGINE - Fan Stator (72-23-00) - Visual Inspection of Fan Case Abradable Rub Strip for Fan Blade Tip Contact

Mos

Hrs

Enc

72 ENG1Eff: 31-Jul-2008


Mos

Hrs

Enc

72 ENG2Eff: 31-Jul-2008


Mos

Hrs

Enc

72 ENG1Eff: 01-Oct-2008


Mos

Hrs

Enc

72 ENG2Eff: 01-Oct-2008


20-May-2009Mos

11,437.8Hrs

6,314Enc

72 ENG2Eff: 26-Nov-2008 Not Applicable



25-Jul-2008Mos

11,528.2Hrs

6,334Enc

72 ENG1BY PART S/N INSTALLEDEff: 26-Nov-2008 Not

Applicable


Cat. 8 - InformationalT (A/R)72-0232 R00 ENGINE - General (72-00-00) - Spare Parts Release for CF34-1A/-3A Engines

Mos

Hrs

Enc

72 ENG1Eff: 19-Aug-2008


Generated: 6-Apr-2016 1:16 PM351/429







Cat. 8 - InformationalT (A/R)72-0232 R00 ENGINE - General (72-00-00) - Spare Parts Release for CF34-1A/-3A Engines

Mos

Hrs

Enc

72 ENG2Eff: 19-Aug-2008

Cat. 8 - InformationalRE (-)72-0236 R00 ENGINE - General (72-00-00) - Spare Parts Release for CF34-BJ Engines

Mos

Hrs

Enc

72 ENG1Eff: 03-Oct-2008

Cat. 8 - InformationalRE (-)72-0236 R00 ENGINE - General (72-00-00) - Spare Parts Release for CF34-BJ Engines

Mos

Hrs

Enc

72 ENG2Eff: 03-Oct-2008


Mos

Hrs

Enc

72 ENG1Eff: 16-Oct-2008


Mos

Hrs

Enc

72 ENG2Eff: 16-Oct-2008

Cat. 8 - InformationalT (A/R)72-0237 R00 ENGINE - General (72-00-00) - Spare Parts Release for CF34-1A/-3A/-3A2/-3B Engines

Mos

Hrs

Enc

72 ENG1Eff: 14-Oct-2008

Cat. 8 - InformationalT (A/R)72-0237 R00 ENGINE - General (72-00-00) - Spare Parts Release for CF34-1A/-3A/-3A2/-3B Engines

Mos

Hrs

Enc

72 ENG2Eff: 14-Oct-2008

Cat. 2 - RecommendedRE (-)72-0238 R00 ENGINE - Compressor Rotor Assembly (72-33-00) - Stages 3 through 8 Compressor Rotor Spool - Field Management Plan Due to Quality Issue

Mos

Hrs

Enc

72 ENG1Eff: 16-Jan-2009

Cat. 2 - RecommendedRE (-)72-0238 R00 ENGINE - Compressor Rotor Assembly (72-33-00) - Stages 3 through 8 Compressor Rotor Spool - Field Management Plan Due to Quality Issue

Mos

Hrs

Enc

72 ENG2Eff: 16-Jan-2009

Cat. 7 - OptionalT (A/R)72-0240 R00 ENGINE - Combustion Liner Assembly (72-42-00) - Introduction of Combustor Inner Liner

Mos

Hrs

Enc

72 ENG1Eff: 08-Jun-2009

Cat. 7 - OptionalT (A/R)72-0240 R00 ENGINE - Combustion Liner Assembly (72-42-00) - Introduction of Combustor Inner Liner

Mos

Hrs

Enc

72 ENG2Eff: 08-Jun-2009


Generated: 6-Apr-2016 1:16 PM352/429







Cat. 7 - OptionalRE (-)72-0241 R00 ENGINE - Low Pressure Turbine Stator Assembly (72-52-00) - Introduction of Shroud Sector Part Numbers for Stage 4 and Stage 5

Mos

Hrs

Enc

72 ENG1Eff: 20-May-2009

Cat. 7 - OptionalRE (-)72-0241 R00 ENGINE - Low Pressure Turbine Stator Assembly (72-52-00) - Introduction of Shroud Sector Part Numbers for Stage 4 and Stage 5

Mos

Hrs

Enc

72 ENG2Eff: 20-May-2009

Cat. 7 - OptionalT (A/R)72-0241 R01 ENGINE - Low Pressure Turbine Stator Assembly (72-52-00) - Introduction of Shroud Sector Part Numbers for Stage 4 and Stage 5

Mos

Hrs

Enc

72 ENG1Eff: 15-Jan-2013

Cat. 7 - OptionalT (A/R)72-0241 R01 ENGINE - Low Pressure Turbine Stator Assembly (72-52-00) - Introduction of Shroud Sector Part Numbers for Stage 4 and Stage 5

Mos

Hrs

Enc

72 ENG2Eff: 15-Jan-2013


Mos

Hrs

Enc

72 ENG1Eff: 03-Mar-2009


Mos

Hrs

Enc

72 ENG2Eff: 03-Mar-2009


Mos

Hrs

Enc

72 ENG1Eff: 17-Jun-2009


Mos

Hrs

Enc

72 ENG2Eff: 17-Jun-2009


Mos

Hrs

Enc

72 ENG1Eff: 24-Aug-2009


Mos

Hrs

Enc

72 ENG2Eff: 24-Aug-2009

Cat. 7 - OptionalRE (-)72-0247 R00 ENGINE - Compressor Stator - Introduction of New VG Spindle Nut P/N 4037T84P04

Mos

Hrs

Enc

72 ENG1Eff: 24-Mar-2010


Generated: 6-Apr-2016 1:16 PM353/429








Mos

Hrs

Enc

72 ENG2Eff: 24-Mar-2010


Mos

Hrs

Enc

72 ENG1Eff: 20-Jul-2010


Mos

Hrs

Enc

72 ENG2Eff: 20-Jul-2010

Cat. 8 - InformationalT (A/R)72-0249 R00 ENGINE - General (72-00-00) - Spare Parts Release for CF34-BJ Engines

Mos

Hrs

Enc

72 ENG1Eff: 10-Aug-2010

Cat. 8 - InformationalT (A/R)72-0249 R00 ENGINE - General (72-00-00) - Spare Parts Release for CF34-BJ Engines

Mos

Hrs

Enc

72 ENG2Eff: 10-Aug-2010

Cat. 2 - RecommendedRE (-)72-0250 R00 ENGINE - Fan Rotor (72-21-00) - Replacement of Fan Blades P/N 6018T30P14 or P/N 4923T56G08 Made from ALLVAC Mill Source Material

Mos

Hrs

Enc

72 ENG1Eff: 30-Aug-2010


Mos

Hrs

Enc

72 ENG2Eff: 30-Aug-2010


03-Dec-2015Mos

12,115.2Hrs

6,751Enc



03-Dec-2015Mos

11,998.2Hrs

6,710Enc


Cat. 7 - OptionalRE (-)72-0251 R00 ENGINE - Compressor Rotor (72-33-00) - Inspection for Part Number Remarking and Introduction of Stage 1 Compressor Rotor Blisk P/N 5087T84P02

Mos

Hrs

Enc

72 ENG1Eff: 24-Jan-2011


Mos

Hrs

Enc

72 ENG2Eff: 24-Jan-2011


Generated: 6-Apr-2016 1:16 PM354/429








Mos

Hrs

Enc

72 ENG1Eff: 23-Feb-2011


Mos

Hrs

Enc

72 ENG2Eff: 23-Feb-2011


Mos

Hrs

Enc

72 ENG1Eff: 14-Apr-2011


Mos

Hrs

Enc

72 ENG2Eff: 14-Apr-2011

Cat. 6 - RecommendedRE (-)72-0252 R00 ENGINE - Combustion Chamber Frame and B-Sump (72-41-00) - Introduction of Improved No. 5 Roller Bearing P/N 5042T13P06

Mos

Hrs

Enc

72 ENG1Eff: 31-Mar-2011

Cat. 6 - RecommendedRE (-)72-0252 R00 ENGINE - Combustion Chamber Frame and B-Sump (72-41-00) - Introduction of Improved No. 5 Roller Bearing P/N 5042T13P06

Mos

Hrs

Enc

72 ENG2Eff: 31-Mar-2011

Cat. 8 - InformationalT (A/R)72-0253 R00 ENGINE - General (72-00-00) - Spare Parts Release for CF34-BJ Turbofan Engines

Mos

Hrs

Enc

72 ENG1Eff: 04-May-2011


Mos

Hrs

Enc

72 ENG2Eff: 04-May-2011

Cat. 9 - InformationalT (A/R)72-0254 R00 ENGINE - General (72-00-00) - CF34-BJ Engine Serialization - Manufacturing Sequence

Mos

Hrs

Enc

72 ENG1Eff: 09-Sep-2011

Cat. 9 - InformationalT (A/R)72-0254 R00 ENGINE - General (72-00-00) - CF34-BJ Engine Serialization - Manufacturing Sequence

Mos

Hrs

Enc

72 ENG2Eff: 09-Sep-2011

Cat. 3 - RecommendedRE (-)72-0256 R00 ENGINE - Stages IGV Through 13 Compressor Stator (72-32-00) - Introduction of Redesigned Pinned IGV Inner Support Shroud IGV Outer Bushing IGV Bushing and

IGV Upper and Lower Shroud Ring Segments

Mos

Hrs

Enc

72 ENG1Eff: 13-Apr-2012


Generated: 6-Apr-2016 1:16 PM355/429









Mos

Hrs

Enc

72 ENG2Eff: 13-Apr-2012



Mos

Hrs

Enc

72 ENG1Eff: 05-Nov-2013



Mos

Hrs

Enc

72 ENG2Eff: 05-Nov-2013

Cat. 5 - RecommendedT (A/R)72-0258 R00 ENGINE - Fan Stator (72-23-00) - Introduction of New Shim P/N 2448M31P01

Mos

Hrs

Enc

72 ENG1Eff: 30-Jul-2012

Cat. 5 - RecommendedT (A/R)72-0258 R00 ENGINE - Fan Stator (72-23-00) - Introduction of New Shim P/N 2448M31P01

Mos

Hrs

Enc

72 ENG2Eff: 30-Jul-2012


Mos

Hrs

Enc

72 ENG1Eff: 17-May-2013


Mos

Hrs

Enc

72 ENG2Eff: 17-May-2013

Cat. 7 - OptionalRE (-)72-0260 R00 ENGINE - Accessory Gearbox Assembly (72-62-00) - Introduction of Alternate Accessory Gearbox Assembly Hardware

Mos

Hrs

Enc

72 ENG1Eff: 16-Jan-2013


Mos

Hrs

Enc

72 ENG2Eff: 16-Jan-2013


Mos

Hrs

Enc

72 ENG1Eff: 19-Apr-2013


Generated: 6-Apr-2016 1:16 PM356/429








Mos

Hrs

Enc

72 ENG2Eff: 19-Apr-2013


Mos

Hrs

Enc

72 ENG1Eff: 19-Aug-2013


Mos

Hrs

Enc

72 ENG2Eff: 19-Aug-2013


Mos

Hrs

Enc

72 ENG1Eff: 04-Oct-2013


Mos

Hrs

Enc

72 ENG2Eff: 04-Oct-2013

Category 7T (A/R)72-0263 R00 ENGINE - General (72-00-00) - Change of CF34-3A and CF34-3A2 Engines from a Scheduled Interval Maintenance Plan to a Combined Scheduled Interval and Task

Oriented Maintenance Plan

Mos

Hrs

Enc

72 ENG1Eff: 08-Apr-2013



Mos

Hrs

Enc

72 ENG2Eff: 08-Apr-2013

Category 7RE (-)72-0263 R01 ENGINE - General (72-00-00) - Change of CF34-3A and CF34-3A2 Engines from a Scheduled Interval Maintenance Plan to a Combined Scheduled Interval and Task


Mos

Hrs

Enc

72 ENG1Eff: 25-Nov-2014

(AVG MAN HRS: 1)

Category 7RE (-)72-0263 R01 ENGINE - General (72-00-00) - Change of CF34-3A and CF34-3A2 Engines from a Scheduled Interval Maintenance Plan to a Combined Scheduled Interval and Task


Mos

Hrs

Enc

72 ENG2Eff: 25-Nov-2014

(AVG MAN HRS: 1)


Generated: 6-Apr-2016 1:16 PM357/429









Mos

Hrs

Enc

72 ENG1Eff: 27-Jan-2015

(AVG MAN HRS: 60)


Also ConsiderDUE:1. RE -ENGINE - Rework of the Forward Fan Shaft72-0016 R02ENG172

Also ConsiderDUE:1. RE -ENGINE - Power Takeoff (PTO) Drive Assembly: Replacement of ...72-0021 R02ENG172

Also ConsiderDUE:1. RE -FUEL SYSTEM - Accessory Drive Gearbox (AGB) - Replacement of...72-0057 R03ENG172



Mos

Hrs

Enc

72 ENG2Eff: 27-Jan-2015

(AVG MAN HRS: 60)


Also ConsiderDUE:1. RE -ENGINE - Rework of the Forward Fan Shaft72-0016 R02ENG272

Also ConsiderDUE:1. RE -ENGINE - Power Takeoff (PTO) Drive Assembly: Replacement of ...72-0021 R02ENG272

Also ConsiderDUE:1. RE -FUEL SYSTEM - Accessory Drive Gearbox (AGB) - Replacement of...72-0057 R03ENG272

Cat. 9 - InformationalT (A/R)72-0265 R00 ENGINE - Fan Stator (72-23-00) - Patent Plates Deleted from CF34-BJ (SEI-581) IPC

Mos

Hrs

Enc

72 ENG1Eff: 19-Apr-2013

Cat. 9 - InformationalT (A/R)72-0265 R00 ENGINE - Fan Stator (72-23-00) - Patent Plates Deleted from CF34-BJ (SEI-581) IPC

Mos

Hrs

Enc

72 ENG2Eff: 19-Apr-2013

Cat. 9 - InformationalT (A/R)72-0266 R00 ENGINE - High Pressure Turbine Rotor (72-46-00) - Part Usage Clarification

Mos

Hrs

Enc

72 ENG1Eff: 04-Oct-2013

Cat. 9 - InformationalT (A/R)72-0266 R00 ENGINE - High Pressure Turbine Rotor (72-46-00) - Part Usage Clarification

Mos

Hrs

Enc

72 ENG2Eff: 04-Oct-2013

Cat. 2 - RecommendedRE (-)72-0270 R00 ENGINE - Fan Stator Assembly (72-00-23) - Forward Mount Rib Inspection

Mos

Hrs

Enc

72 ENG1Eff: 20-Aug-2013

(NOTE: This Service Bulletin is applicable to all CF34-BJ engines that have been removed from wing at least one time.)


Mos

Hrs

Enc

72 ENG2Eff: 20-Aug-2013



Mos

Hrs

Enc

72 ENG1Eff: 05-Nov-2013



Generated: 6-Apr-2016 1:16 PM358/429








Mos

Hrs

Enc

72 ENG2Eff: 05-Nov-2013


Cat. 2 - RecommendedT (-)72-0270 R02 ENGINE - Fan Stator Assembly (72-00-23) - Forward Mount Rib Inspection

Mos

Hrs

Enc

72 ENG1Eff: 15-Apr-2014



Mos

Hrs

Enc

72 ENG2Eff: 15-Apr-2014



Mos

Hrs

Enc

72 ENG1Eff: 09-Jan-2015


Mos

Hrs

Enc

72 ENG2Eff: 09-Jan-2015

Cat. 2 - RecommendedT (A/R)72-0270 R04 ENGINE - Fan Stator Assembly (72-00-23) - Forward Mount Rib Inspection

Mos

Hrs

Enc

72 ENG1Eff: 29-May-2015

Cat. 2 - RecommendedT (A/R)72-0270 R04 ENGINE - Fan Stator Assembly (72-00-23) - Forward Mount Rib Inspection

Mos

Hrs

Enc

72 ENG2Eff: 29-May-2015

Category 8T (A/R)72-0272 R00 ENGINE - General (72-00-00) - Spare Parts Release for CF34-BJ Engines

Mos

Hrs

Enc

72 ENG1Eff: 20-Mar-2015

Category 8T (A/R)72-0272 R00 ENGINE - General (72-00-00) - Spare Parts Release for CF34-BJ Engines

Mos

Hrs

Enc

72 ENG2Eff: 20-Mar-2015

Cat. 3 - RecommendedRE (-)72-0276 R00 ENGINE - Exhaust Components (72-54-00) - Release of New Improved Scavenge Adapter and Scavenge Connector to the CF34-BJ Engine Models

Mos

Hrs

Enc

72 ENG1Eff: 13-Mar-2014

Cat. 3 - RecommendedRE (-)72-0276 R00 ENGINE - Exhaust Components (72-54-00) - Release of New Improved Scavenge Adapter and Scavenge Connector to the CF34-BJ Engine Models

Mos

Hrs

Enc

72 ENG2Eff: 13-Mar-2014


Generated: 6-Apr-2016 1:16 PM359/429







Cat. 7 - OptionalRE (-)72-0277 R00 ENGINE - Fan Rotor Assembly (72-21-00) - Introduction of New Self-Wrenching Bolt P/N 4020T53P04

Mos

Hrs

Enc

72 ENG1Eff: 02-Apr-2014

Cat. 7 - OptionalRE (-)72-0277 R00 ENGINE - Fan Rotor Assembly (72-21-00) - Introduction of New Self-Wrenching Bolt P/N 4020T53P04

Mos

Hrs

Enc

72 ENG2Eff: 02-Apr-2014


Mos

Hrs

Enc

72 ENG1Eff: 16-May-2014


Mos

Hrs

Enc

72 ENG2Eff: 16-May-2014

Cat. 6 - RecommendedRE (-)72-0281 R00 ENGINE - Combustion Section (72-43-00) - Introduction of New Support Bracket P/N 2583M77G01 For White W3 Cable Assembly

Mos

Hrs

Enc

72 ENG1Eff: 03-Oct-2014

(AVG MAN HRS: 2)

Cat. 6 - RecommendedRE (-)72-0281 R00 ENGINE - Combustion Section (72-43-00) - Introduction of New Support Bracket P/N 2583M77G01 For White W3 Cable Assembly

Mos

Hrs

Enc

72 ENG2Eff: 03-Oct-2014

(AVG MAN HRS: 2)

Cat. 8 - InformationalRE (-)72-0284 R00 ENGINE - General (72-00-00) - Spare Parts Release for CF34-BJ Turbofan Engines

Mos

Hrs

Enc

72 ENG1Eff: 03-Oct-2014

Cat. 8 - InformationalRE (-)72-0284 R00 ENGINE - General (72-00-00) - Spare Parts Release for CF34-BJ Turbofan Engines

Mos

Hrs

Enc

72 ENG2Eff: 03-Oct-2014

Cat. 7 - OptionalRE (-)72-0287 R00 ENGINE - Accessory Gearbox Assembly (72-62-00) - CF34 Accessory Gearbox (AGB) Interchangeability Modifications

Mos

Hrs

Enc

72 ENG1Eff: 23-Oct-2014

(AVG MAN HRS: 6)

Cat. 7 - OptionalRE (-)72-0287 R00 ENGINE - Accessory Gearbox Assembly (72-62-00) - CF34 Accessory Gearbox (AGB) Interchangeability Modifications

Mos

Hrs

Enc

72 ENG2Eff: 23-Oct-2014

(AVG MAN HRS: 6)

Category 3T (A/R)72-0294 R00 Engine - Compressor Stator Assembly (72-00-32) - Inspection of VG System to Check For Looseness

Mos

Hrs

Enc

72 ENG1Eff: 12-Aug-2015

(AVG MAN HRS: 8)


Generated: 6-Apr-2016 1:16 PM360/429







Category 3T (A/R)72-0294 R00 Engine - Compressor Stator Assembly (72-00-32) - Inspection of VG System to Check For Looseness

Mos

Hrs

Enc

72 ENG2Eff: 12-Aug-2015

(AVG MAN HRS: 8)

Category 4T (A/R)72-0296 R00 Engine - Turbine Transition Assembly - Replacement of Silver Plated Nuts with Dry-Film Coated Nuts on Thermocouple Probes and PT5 Probe

Mos

Hrs

Enc

72 ENG1Eff: 11-Mar-2016

(AVG MAN HRS: 4) (NOTE: The plain nut P/N MS9357-10, washer tab lock (washer) P/N3056T13P01, and self-locking nut P/N R1181P004

(used with nowasher) are affected by this Service Bulletin)

Category 4T (A/R)72-0296 R00 Engine - Turbine Transition Assembly - Replacement of Silver Plated Nuts with Dry-Film Coated Nuts on Thermocouple Probes and PT5 Probe

Mos

Hrs

Enc

72 ENG2Eff: 11-Mar-2016

(AVG MAN HRS: 4) (NOTE: The plain nut P/N MS9357-10, washer tab lock (washer) P/N3056T13P01, and self-locking nut P/N R1181P004

(used with nowasher) are affected by this Service Bulletin)

Cat. 9 - InformationalRE (-)72-A0088 R00 ENGINE - Fan Rotor Assembly (72-21-00) - Fan Disk Field Management Plan

Mos

Hrs

Enc

72 ENG1Eff: 21-Sep-2000


Mos

Hrs

Enc

72 ENG2Eff: 21-Sep-2000


Mos

Hrs

Enc

72 ENG1Eff: 30-Oct-2000


Mos

Hrs

Enc

72 ENG2Eff: 30-Oct-2000


Mos

Hrs

Enc

72 ENG1Eff: 15-Jun-2001


Mos

Hrs

Enc

72 ENG2Eff: 15-Jun-2001

Cat. 1 - RecommendedRE (-)72-A0088 R03 ENGINE - Fan Rotor Assembly (72-21-00) - Fan Disk Field Management Plan

13-May-2005Mos

Hrs

Enc

72 ENG1NEW PART INSTALLEDEff: 13-May-2005 Not

Applicable

(NOTE: Information only. GE recommends you no longer do this Alert Service Bulletin. This Alert Service Bulletin is superseded by CF34-BJ S/B

72-A0212.)


Generated: 6-Apr-2016 1:16 PM361/429







Cat. 1 - RecommendedRE (-)72-A0088 R03 ENGINE - Fan Rotor Assembly (72-21-00) - Fan Disk Field Management Plan

13-May-2005Mos

Hrs

Enc

72 ENG2Eff: 13-May-2005 Complied With


72-A0212.)

Cat. 9 - InformationalT (A/R)72-A0088 R04 ENGINE - Fan Rotor Assembly (72-21-00) - Fan Disk Field Management Plan

Mos

Hrs

Enc

72 ENG1Eff: 13-Mar-2007


72-A0212.)

Cat. 9 - InformationalT (A/R)72-A0088 R04 ENGINE - Fan Rotor Assembly (72-21-00) - Fan Disk Field Management Plan

Mos

Hrs

Enc

72 ENG2Eff: 13-Mar-2007


72-A0212.)

Cat. 2 - RecommendedRE (-)72-A0097 R00 ENGINE - High Pressure Turbine Stator (72-45-00) - One-Time Inspection of HPT Borescope Plugs

Mos

Hrs

Enc

72 ENG1Eff: 16-Jul-2001

Cat. 2 - RecommendedRE (-)72-A0097 R00 ENGINE - High Pressure Turbine Stator (72-45-00) - One-Time Inspection of HPT Borescope Plugs

Mos

Hrs

Enc

72 ENG2Eff: 16-Jul-2001

Cat. 1 - RecommendedRE (-)72-A0140 R00 ENGINE - Compressor Rotor (72-33-00) - Compressor Rotor Spool Stages 3 thru 8 Field Management Plan

Mos

Hrs

Enc

72 ENG1Eff: 13-Apr-2004

(NOTE: GE recommends that you do this Service Bulletin on the affected compressor rotor spool stages 3 thru 8, PN 6078T56P03 and PN

6078T56P04, with greater than 6,000 accumulated cycles as follows (Refer to Maintenance Manual SEI-580, Chapter 5-11-02 or SEI-780,

Chapter 5-11-02 as applicable): (a) If the applicable Engine Manual Chapter 5 life limit for the affected compressor rotor spool stages 3 thru

8, is less than 22,000 part operating cycles-since-new (CSN), do at piece part exposure for compressor rotor spool stages 3 thru 8 with greater

than 6,000 accumulated cycles, or at the Chapter 5 life limit, whichever is lower. (b) If the applicable Engine Manual Chapter 5 life limit for the

affected compressor rotor spool stages 3 thru 8, is greater than 22,000 part operating cycles since new, do at piece part exposure for

compressor rotor spool stages 3 thru 8 with greater than 6,000 accumulated cycles, but prior to accumulating 22,000 part operating cycles

since new.)


Mos

Hrs

Enc

72 ENG2Eff: 13-Apr-2004

(NOTE: GE recommends that you do this Service Bulletin on the affected compressor rotor spool stages 3 thru 8, PN 6078T56P03 and PN

6078T56P04, with greater than 6,000 accumulated cycles as follows (Refer to Maintenance Manual SEI-580, Chapter 5-11-02 or SEI-780,

Chapter 5-11-02 as applicable): (a) If the applicable Engine Manual Chapter 5 life limit for the affected compressor rotor spool stages 3 thru

8, is less than 22,000 part operating cycles-since-new (CSN), do at piece part exposure for compressor rotor spool stages 3 thru 8 with greater

than 6,000 accumulated cycles, or at the Chapter 5 life limit, whichever is lower. (b) If the applicable Engine Manual Chapter 5 life limit for the

affected compressor rotor spool stages 3 thru 8, is greater than 22,000 part operating cycles since new, do at piece part exposure for

compressor rotor spool stages 3 thru 8 with greater than 6,000 accumulated cycles, but prior to accumulating 22,000 part operating cycles

since new.)


13-May-2005Mos

Hrs

Enc

72 ENG1BY PART S/N INSTALLEDEff: 15-Jun-2004 Not

Applicable


Generated: 6-Apr-2016 1:16 PM362/429








15-Jun-2004Mos

Hrs

Enc

72 ENG2Eff: 15-Jun-2004 Not Applicable

Cat. 3 - RecommendedRE (-)72-A0148 R00 ENGINE - Low Pressure Turbine (LPT) Rotor (72-53-00) - Replacement or Inspection of Stages 5 and 6 LPT Rotor Disks and Inspection of Stages 3 and 4 LPT Disk Arms

for Arc Out

Mos

Hrs

Enc

72 ENG1Eff: 02-Sep-2004

(NOTE: GE recommends that you do this Alert Service Bulletin at the next piece part exposure of affected stage 5 and/or stage 6 LPT disks.

NOTE: Alert Service Bulletin CF34-BJ 72-A0152 requires removal of LPT modules or engines which contain stage 5 and/or stage 6 disk list in

Appendix (Table 1 or Table 2) within specific intervals, based on accumulated cycles on the affected stage 5 and stage 6 LPT disk, for

replacement or performance of the inspections in this Alert Service Bulletin CF34-BJ 72-A0148. Refer to Alert Service Bulletin CF34-BJ 72-

A0152, Removal Plan to Inspect or replace LPT disks for arc-out indications. Inspection Limitations: A. Prior to January 1, 2010, affected

stage 5 and stage 6 LPT disks listed in (Table 1) may be inspected in accordance with this Alert Service Bulletin CF34-BJ 72-A0148 provided the

disk(s) are reinstalled in the engine or LPT module they were removed from. B. January 1, 2010 and later, stage 5 and stage 6 LPT disks listed

in (Table 1) may be re-inspected in accordance with this Alert Service Bulletin CF34-BJ 72-A0148 provided the stage 5 and stage 6 was initially

inspected prior to January 1, 2010 and the disk(s) are reinstalled in the engine or LPT module they were removed from. C. Disks not inspected

prior to January 1, 2010 in accordance with this Alert Service Bulletin CF34-BJ 72-A0148 must be replaced with disks not listed in Appendix

(Table 1 or Table 2) of this Alert Service Bulletin. Replace disks listed in Appendix (Table 2). Do not inspect or return to service. Refer to CF34-

BJ 72-0098. Use of replacement engines or LPT modules: Replacement engine or LPT module is defines as an engine or LPT module not

installed on an operational aircraft on August 31, 2004. The replacement engine or LPT module will contain a stage 5 and stage 6 LPT disks

not listed in Appendix (Table 1 or Table 2) of this Alert Service Bulletin CF34-BJ 72-A0148. OR A. Prior to January 1, 2010, replacement

engines or LPT modules shall contain stage 5 or stage 6 LPT disks listed in Appendix (Table 1) and visually inspected in accordance with this

Alert Service Bulletin CF34-BJ 72-A0148. B. January 1, 2010 and later, the replacement engine or module contains a stage 5 and or stage 6

LPT disk listed in Appendix (Table 1) and initially inspected prior to June 1, 2005 and are in compliance with the interval inspection requirement

in Alert Service Bulletin CF34-BJ 72-A0152. C. Replacement engine or LPT modules containing a stage 5 or stage 6 disk listed in Appendix

(Table 1) and not inspected prior to June 1, 2005, the suspect disk must be replaced with a disk not listed in the Appendix (Table 1 or Table 2)

of this Alert Service Bulletin. D. Replace disk listed in Appendix (Table 2). Do not inspect or return to service. Refer to CF34-BJ S/B 72-0098.)


for Arc Out

Mos

Hrs

Enc

72 ENG2Eff: 02-Sep-2004






















Generated: 6-Apr-2016 1:16 PM363/429








for Arc Out

Mos

Hrs

Enc

72 ENG1Eff: 10-Mar-2005






















for Arc Out

Mos

Hrs

Enc

72 ENG2Eff: 10-Mar-2005






















Generated: 6-Apr-2016 1:16 PM364/429








for Arc Out

Mos

Hrs

Enc

72 ENG1Eff: 24-May-2005






















for Arc Out

Mos

Hrs

Enc

72 ENG2Eff: 24-May-2005






















Generated: 6-Apr-2016 1:16 PM365/429








for Arc Out

06-May-2009Mos

11,438.9Hrs

6,316Enc

72 ENG2Eff: 05-Aug-2009 Complied With






















for Arc Out

01-Apr-2009Mos

11,555.9Hrs

6,357Enc























Generated: 6-Apr-2016 1:16 PM366/429







Cat. 1 - RecommendedRE (-)72-A0152 R00 ENGINE - Low Pressure Turbine Rotor (72-53-00) - Removal Plan to Replace or Inspect LPT Disks for Arc-out Indications

Mos

Hrs

Enc

72 ENG1Eff: 10-Mar-2005

(NOTE: It is recommended that all CF34-1A, -3A, -3A1, -3A2 and CF34-3B engines or LPT modules, that have the affected stage 5 or stage 6

LPT disks installed, be removed within the following intervals, for replacement or performance of the LPT disk inspections in CF34-BJ Alert

Service Bulletin 72-A0148:(a) LPT stage 5 and 6 disks with greater than or equal to 14,750 cycles since new (CSN) on the effective date of this

Alert Service Bulletin and which have not been fluorescent penetrant inspected (FPI) at a prior piece part exposure, prior to accumulating an

additional 250 cycles in service (CIS) since the effective date of this Alert Service Bulletin.(b) LPT stage 5 and 6 disks with greater than or equal

to 14,750 CSN on the effective date of this Alert Service Bulletin and which have been fluorescent penetrant inspected (FPI) at a prior piece part

exposure, prior to accumulating an additional 500 CIS since the effective date of this Alert Service Bulletin.(c) LPT stage 5 and 6 disks with

greater than or equal to 14,500 CSN and less than 14,750 CSN, on the effective date of this Alert Service Bulletin, at piece part exposure, but

prior to accumulating an additional 500 CIS since the effective date of this Alert Service Bulletin.(d) LPT stage 5 and 6 disks with greater than or

equal to 14,250 CSN and less than 14,500 CSN, on the effective date of this Alert Service Bulletin, at piece part exposure, but prior to

accumulating an additional 750 CIS since the effective date of this Alert Service Bulletin.(e) LPT stage 5 and 6 disks with greater than or equal

to 13,000 CSN and less than 14,250 CSN, on the effective date of this Alert Service Bulletin, at piece part exposure, but prior to accumulating

an additional 1,000 CIS since the effective date of this Alert Service Bulletin.(f) LPT stage 5 and 6 disks with greater than or equal to 2,500 CSN

and less than 13,000 CSN on the effective date of this Alert Service Bulletin, at piece part exposure, but prior to accumulating an additional

4,000 CIS since the effective date of this Alert Service Bulletin, or 14,000 CSN, whichever comes first.g) LPT stage 5 and 6 disks with fewer than

2,500 CSN on the effective date of this Alert Service Bulletin, at piece part exposure, but no later than 6,500 CSN.(2) Replace all affected disk on

or before January 1, 2013, not to exceed published life cycles of the disks. (3) Re-inspection of all affected LPT disks. Remove affected engines

or LPT modules and reinspect all affected disk every 3,100 disk cycles since last inspection, not to exceed 3,100 disk cycles since last inspection

as defined in Alert Service Bulletin CF34-BJ S/B 72-A0148, until the affected disks are replaced with disks not listed in the Appendix (Table 1 or

Table 2) not to exceed the published life limits of the LPT disks, refer to the current revision of SEI-580 or SEI-780, Chapter 05 which ever is

applicable.)


Mos

Hrs

Enc

72 ENG2Eff: 10-Mar-2005

(NOTE: It is recommended that all CF34-1A, -3A, -3A1, -3A2 and CF34-3B engines or LPT modules, that have the affected stage 5 or stage 6

LPT disks installed, be removed within the following intervals, for replacement or performance of the LPT disk inspections in CF34-BJ Alert

Service Bulletin 72-A0148:(a) LPT stage 5 and 6 disks with greater than or equal to 14,750 cycles since new (CSN) on the effective date of this

Alert Service Bulletin and which have not been fluorescent penetrant inspected (FPI) at a prior piece part exposure, prior to accumulating an

additional 250 cycles in service (CIS) since the effective date of this Alert Service Bulletin.(b) LPT stage 5 and 6 disks with greater than or equal

to 14,750 CSN on the effective date of this Alert Service Bulletin and which have been fluorescent penetrant inspected (FPI) at a prior piece part

exposure, prior to accumulating an additional 500 CIS since the effective date of this Alert Service Bulletin.(c) LPT stage 5 and 6 disks with

greater than or equal to 14,500 CSN and less than 14,750 CSN, on the effective date of this Alert Service Bulletin, at piece part exposure, but

prior to accumulating an additional 500 CIS since the effective date of this Alert Service Bulletin.(d) LPT stage 5 and 6 disks with greater than or

equal to 14,250 CSN and less than 14,500 CSN, on the effective date of this Alert Service Bulletin, at piece part exposure, but prior to

accumulating an additional 750 CIS since the effective date of this Alert Service Bulletin.(e) LPT stage 5 and 6 disks with greater than or equal

to 13,000 CSN and less than 14,250 CSN, on the effective date of this Alert Service Bulletin, at piece part exposure, but prior to accumulating

an additional 1,000 CIS since the effective date of this Alert Service Bulletin.(f) LPT stage 5 and 6 disks with greater than or equal to 2,500 CSN

and less than 13,000 CSN on the effective date of this Alert Service Bulletin, at piece part exposure, but prior to accumulating an additional

4,000 CIS since the effective date of this Alert Service Bulletin, or 14,000 CSN, whichever comes first.g) LPT stage 5 and 6 disks with fewer than

2,500 CSN on the effective date of this Alert Service Bulletin, at piece part exposure, but no later than 6,500 CSN.(2) Replace all affected disk on

or before January 1, 2013, not to exceed published life cycles of the disks. (3) Re-inspection of all affected LPT disks. Remove affected engines

or LPT modules and reinspect all affected disk every 3,100 disk cycles since last inspection, not to exceed 3,100 disk cycles since last inspection

as defined in Alert Service Bulletin CF34-BJ S/B 72-A0148, until the affected disks are replaced with disks not listed in the Appendix (Table 1 or

Table 2) not to exceed the published life limits of the LPT disks, refer to the current revision of SEI-580 or SEI-780, Chapter 05 which ever is

applicable.)


25-Jan-2013Mos

Hrs

6,521Enc

72 ENG1Eff: 24-May-2005

(NOTE: 9621)


25-Jan-2013Mos

Hrs

6,480Enc

72 ENG2Eff: 24-May-2005


Generated: 6-Apr-2016 1:16 PM367/429







Cat. 1 - Recommended ≈12-Jan-2024RE72-A0152 R02 ENGINE - Low Pressure Turbine Rotor (72-53-00) - Removal Plan to Replace or Inspect LPT Disks for Arc-out Indications

25-Jan-2013Mos

11,802.2Hrs

2,852 Enc9,6213,1006,521Enc


Cat. 1 - Recommended ≈12-Jan-2024RE72-A0152 R02 ENGINE - Low Pressure Turbine Rotor (72-53-00) - Removal Plan to Replace or Inspect LPT Disks for Arc-out Indications

25-Jan-2013Mos

11,685.2Hrs

2,852 Enc9,5803,1006,480Enc


Cat. 2 - RecommendedRE (-)72-A0200 R00 ENGINE - Low Pressure Turbine (72-53-00) - Inspection of LPT Modules

Mos

Hrs

Enc

72 ENG1Eff: 29-Jun-2006

(NOTE: This Alert Service Bulletin is applicable to CF34-3B turbofan engines that do not have new/reworked stage 3 shroud sector P/N

5099T32G02 featuring an improved integral heat shield as well as CF34-3A1 engines that are converted to CF34-3B1)


Mos

Hrs

Enc

72 ENG2Eff: 29-Jun-2006




Mos

Hrs

Enc

72 ENG1Eff: 04-Oct-2006




Mos

Hrs

Enc

72 ENG2Eff: 04-Oct-2006



Cat. 2 - Recommended ≈10-Oct-2036RE (-)72-A0200 R02 ENGINE - Low Pressure Turbine (72-53-00) - Inspection of LPT Modules

Mos

9,919.4 Hrs[22,056.8]Hrs

Enc

72 ENG1Eff: 21-Feb-2007




Mos

9,919.4 Hrs[21,939.8]Hrs

Enc

72 ENG2Eff: 21-Feb-2007




Mos

Hrs

Enc

72 ENG1Eff: 21-May-2010




Generated: 6-Apr-2016 1:16 PM368/429








Mos

Hrs

Enc

72 ENG2Eff: 21-May-2010




Mos

9,919.4 Hrs[22,056.8]Hrs

Enc

72 ENG1Eff: 21-Jul-2010


Mos

9,919.4 Hrs[21,939.8]Hrs

Enc

72 ENG2Eff: 21-Jul-2010

Cat. 1 - RecommendedRE (-)72-A0212 R00 ENGINE - Fan Rotor Assembly (72-21-00) - Shop Level Inspection for Fan Disk Arc-Out Indications

Mos

Hrs

Enc

72 ENG1Eff: 07-Mar-2007


Mos

Hrs

Enc

72 ENG2Eff: 07-Mar-2007


Mos

Hrs

Enc

72 ENG1Eff: 16-Mar-2007


Mos

Hrs

Enc

72 ENG2Eff: 16-Mar-2007


Mos

Hrs

Enc

72 ENG1Eff: 22-Mar-2007


Mos

Hrs

Enc

72 ENG2Eff: 22-Mar-2007


Mos

Hrs

Enc

72 ENG1Eff: 27-Jun-2007


Mos

Hrs

Enc

72 ENG2Eff: 27-Jun-2007


Generated: 6-Apr-2016 1:16 PM369/429








22-Mar-2012Mos

11,674.8Hrs

6,447Enc

72 ENG1BY PART S/N INSTALLEDEff: 27-Oct-2008 Not

Applicable

Also ConsiderDUE:1. T A/R | 2. RE -ENGINE - Fan Rotor Assembly (72-21-00) - Fan Disk Field Mana...72-A0088 R04ENG172

Nextdue Share EarliestDUE:1. RE -ENGINE - Fan Rotor Assembly (72-21-00) - Shop Level Inspecti...72-A0212 R04 (Tier 1)ENG172




19-Mar-2012Mos

11,557.8Hrs

6,406Enc

72 ENG2Eff: 27-Oct-2008 Complied With

Also ConsiderDUE:1. T A/R | 2. RE -ENGINE - Fan Rotor Assembly (72-21-00) - Fan Disk Field Mana...72-A0088 R04ENG272




Cat. 1 - RecommendedRE (-)72-A0212 R04 (Tier 1) ENGINE - Fan Rotor Assembly (72-21-00) - Shop Level Inspection for Fan Disk Arc-Out Indications

Mos

Hrs

Enc

72 ENG1Eff: 27-Oct-2008


Mos

Hrs

Enc

72 ENG2Eff: 27-Oct-2008


Mos

Hrs

Enc

72 ENG1Eff: 27-Oct-2008


Mos

Hrs

Enc

72 ENG2Eff: 27-Oct-2008


Mos

Hrs

Enc

72 ENG1Eff: 27-Oct-2008


Mos

Hrs

Enc

72 ENG2Eff: 27-Oct-2008


Generated: 6-Apr-2016 1:16 PM370/429








Mos

Hrs

Enc

72 ENG1Eff: 29-May-2015

(AVG MAN HRS: 12)





Mos

Hrs

Enc

72 ENG2Eff: 29-May-2015

(AVG MAN HRS: 12)





Mos

Hrs

Enc

72 ENG1Eff: 29-May-2015

(AVG MAN HRS: 12)


Mos

Hrs

Enc

72 ENG2Eff: 29-May-2015

(AVG MAN HRS: 12)


Mos

Hrs

Enc

72 ENG1Eff: 29-May-2015

(AVG MAN HRS: 12)


Mos

Hrs

Enc

72 ENG2Eff: 29-May-2015

(AVG MAN HRS: 12)


Mos

Hrs

Enc

72 ENG1Eff: 29-May-2015

(AVG MAN HRS: 12)


Mos

Hrs

Enc

72 ENG2Eff: 29-May-2015

(AVG MAN HRS: 12)

Cat. 3 - RecommendedRE (-)72-A0234 R00 ENGINE - Fan Rotor Assembly (72-21-00) - Shop Level Eddy Current and Redundant Tactile Enhanced Visual Inspection for Fan Disk Arc-Out Indications

Mos

Hrs

Enc

72 ENG1Eff: 27-Oct-2008


Generated: 6-Apr-2016 1:16 PM371/429







Cat. 3 - RecommendedRE (-)72-A0234 R00 ENGINE - Fan Rotor Assembly (72-21-00) - Shop Level Eddy Current and Redundant Tactile Enhanced Visual Inspection for Fan Disk Arc-Out Indications

Mos

Hrs

Enc

72 ENG2Eff: 27-Oct-2008

Cat. 2 - RecommendedRE (-)72-A0235 R00 ENGINE - Fan Rotor Assembly (72-21-00) - On Wing Repetitive Eddy Current Inspection for Fan Disk Arc-Out Indications

Mos

Hrs

Enc

72 ENG1Eff: 27-Oct-2008


Mos

Hrs

Enc

72 ENG2Eff: 27-Oct-2008


Mos

Hrs

Enc

72 ENG1Eff: 01-Jun-2015

(AVG MAN HRS: 2)


Mos

Hrs

Enc

72 ENG2Eff: 01-Jun-2015

(AVG MAN HRS: 2)

EMM - Life Limit ≈22-Feb-2021RE72-EMM-001 No.5 Bearing Carbon Seal Preformed Packing - Replace

05-Jun-2009Mos

2,417.4 Hrs14,554.83,00011,554.8Hrs

6,355Enc

72 ENG1


EMM - Life Limit ≈24-Nov-2019RE72-EMM-001 No.5 Bearing Carbon Seal Preformed Packing - Replace

28-Jul-2005Mos

1,818.6 Hrs13,8393,00010,839Hrs

5,949Enc

72 ENG2


EMM - Life Limit ≈22-Feb-2021RE72-EMM-002 High Pressure Turbine Stage 2 Nozzle Retaining Ring Sector - Replace

05-Jun-2009Mos

2,417.4 Hrs14,554.83,00011,554.8Hrs

6,355Enc

72 ENG1


EMM - Life Limit ≈24-Nov-2019RE72-EMM-002 High Pressure Turbine Stage 2 Nozzle Retaining Ring Sector - Replace

28-Jul-2005Mos

1,818.6 Hrs13,8393,00010,839Hrs

5,949Enc

72 ENG2


MandatoryRE (-)88-06-07 Fuel Controls

23-Mar-1988Mos

Hrs

Enc

72 ENG1PER SB 73-05 & SB 73-06Eff: 23-Mar-1988 Not

Applicable

MandatoryRE (-)88-06-07 Fuel Controls

23-Mar-1988Mos

Hrs

Enc

72 ENG2PER SB 73-05 & SB 73-06Eff: 23-Mar-1988 Not

Applicable


Generated: 6-Apr-2016 1:16 PM372/429








11-Jul-2008Mos

11,411.2Hrs

6,293Enc


Applicable


11-Mar-1997Mos

Hrs

Enc

72 ENG1NEW FAN INSTALLEDEff: 27-May-1997 Not

Applicable

MandatoryRE (-)97-06-15 HPC Stage 1 rotor disk

11-Jul-2008Mos

11,411.2Hrs

6,293Enc

72 ENG2Not Applicable

(NOTE: Engines with high pressure compressor (HPC) stage 1 rotor disks, part number 6040T79G01, installed)

MandatoryRE (-)97-06-15 HPC Stage 1 rotor disk

14-Mar-1997Mos

Hrs

Enc

72 ENG1NEW PART INSTALLEDNot Applicable

(NOTE: Engines with high pressure compressor (HPC) stage 1 rotor disks, part number 6040T79G01, installed)

MandatoryRE (-)99-22-10 High Pressure Compressor (HPC) Spool and Disk

27-Dec-1999Mos

Hrs

Enc

72 ENG1NEW PART INSTALLEDEff: 27-Dec-1999 Not

Applicable

MandatoryRE (-)99-22-10 High Pressure Compressor (HPC) Spool and Disk

27-Dec-1999Mos

Hrs

Enc

72 ENG2Eff: 27-Dec-1999 Complied With

▼ 73 - ENGINE - FUEL AND CONTROL

RE (O/C)Compressor Inlet Temperature Sensor

27-Jun-2005Mos

10,839Hrs10,839

5,949Enc5,949


WYG30324

RE (O/C)Compressor Inlet Temperature Sensor

31-May-2005Mos

10,956Hrs10,956

5,990Enc5,990


WYG30240

RE (O/C)Fuel Distributor

20-Sep-1983Mos

0Hrs

0Enc


RE (O/C)Fuel Distributor

20-Sep-1983Mos

0Hrs

0Enc


RE (O/C)Fuel Flow Indicator

20-Sep-1983Mos

0Hrs

0Ldg



Generated: 6-Apr-2016 1:16 PM373/429







RE (O/C)Fuel Flowmeter

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Fuel Flowmeter

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Fuel Heater

27-Jun-2005Mos

10,839Hrs10,839

5,949Enc5,949


JAD05017

RE (O/C)Fuel Heater

31-May-2005Mos

10,956Hrs10,956

5,990Enc5,990


JD05009

RE (O/C)Fuel Pressure Warning Low Switch

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Fuel Pressure Warning Low Switch

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Fuel Pump

27-Jun-2005Mos

10,839Hrs

Enc

73 ENG26052T06P05CDWE0453

RE (O/C)Fuel Pump

31-May-2005Mos

10,956Hrs

Enc

73 ENG16052T06P05CDWE0452

RE (O/C)Fuel Temp Indicator

12-Jan-2002Mos

7,973.5Hrs

3,823Ldg

73 A/F600-50919-1182050019M

RE (O/C)Main Fuel Control (MFC)

27-Jun-2005Mos

10,839Hrs

5,949Enc

73 ENG26047T74P13WYG33540

RE (O/C)Main Fuel Control (MFC)

31-May-2005Mos

10,956Hrs8,961

5,990Enc5,136


WYG33573


Generated: 6-Apr-2016 1:16 PM374/429







RE (O/C)Temperature Bulb

20-Sep-1983Mos

0Hrs

0Ldg



20-Sep-1983Mos

0Hrs

0Ldg



20-Sep-1983Mos

0Hrs

0Ldg



20-Sep-1983Mos

0Hrs

0Ldg


RecommendedRE (-)601-0216 Modification - Press Fuel Line and N2 Filter Harness - Compatibility with CECO Fuel Pump

Mos

Hrs

Ldg

73 A/F

RecommendedRE (-)601-0216 Rev 1 Modification - Press Fuel Line and N2 Filter Harness - Compatibility with CECO Fuel Pump

01-Oct-1991Mos

Hrs

Ldg


RecommendedRE (-)601-0593 Special Check/Modification – Fuel System – Russian and Ukrainian Fuel Requirement

1.1 Years[19-May-2017]19-May-2009Mos

Hrs

Ldg

73 A/FEff: 19-May-2009

RecommendedT (A/R)601-1029 Modification - Engine Fuel Supply - Right Fuel Heater Exhaust Duct

Mos

Hrs

Ldg

73 A/FEff: 07-Sep-1984

RecommendedRE (-)601-1039 Special Check/Modification - Motive Flow Line - Fouling on Variable Guide Vane Bellcrank Clevis

16-Jul-1986Mos

952Hrs

403Ldg

73 A/FComplied With

RecommendedRE (-)601-1039 Rev 1 Special Check/Modification - Motive Flow Line - Fouling on Variable Guide Vane Bellcrank Clevis

Mos

Hrs

Ldg

73 A/F

RecommendedT (A/R)601-1039 Rev 2 Special Check/Modification - Motive Flow Line - Fouling on Variable Guide Vane Bellcrank Clevis

Mos

Hrs

Ldg

73 A/FEff: 18-Sep-1987


Generated: 6-Apr-2016 1:16 PM375/429







RecommendedRE (-)601-1043 Modification - Fuel Low Pressure Warning System - Switch Replacement and/or Clamping

02-May-1988Mos

1,995Hrs

756Ldg


RE (-)72-0255 R00 ENGINE - Fan Stator (72-23-00) - Engine Mount Quality Issue

Mos

Hrs

Enc

73 ENG1Eff: 02-Feb-2012

RE (-)72-0255 R00 ENGINE - Fan Stator (72-23-00) - Engine Mount Quality Issue

Mos

Hrs

Enc

73 ENG2Eff: 02-Feb-2012

T (A/R)72-0255 R01 ENGINE - Fan Stator (72-23-00) - Engine Mount Quality Issue

Mos

Hrs

Enc

73 ENG1Eff: 02-Feb-2012


T (A/R)72-0255 R01 ENGINE - Fan Stator (72-23-00) - Engine Mount Quality Issue

Mos

Hrs

Enc

73 ENG2Eff: 02-Feb-2012


RecommendedRE (-)73-0001 R00 FUEL SYSTEM - Replacement of Flex-Metal Hose Assemblies

Mos

Hrs

Enc

73 ENG1

RecommendedRE (-)73-0001 R00 FUEL SYSTEM - Replacement of Flex-Metal Hose Assemblies

Mos

Hrs

Enc

73 ENG2

RecommendedRE (-)73-0003 R00 FUEL SYSTEM - Servicing/Inspection (73-00-00) - Use of Fuel System Anti-icing Additive and Inspection of Fuel Heater

Mos

Hrs

Enc

73 ENG1Eff: 05-Apr-1985


Mos

Hrs

Enc

73 ENG2Eff: 05-Apr-1985


Mos

Hrs

Enc

73 ENG1Eff: 17-Jul-1985


Mos

Hrs

Enc

73 ENG2Eff: 17-Jul-1985


Generated: 6-Apr-2016 1:16 PM376/429








Mos

Hrs

Enc

73 ENG1Eff: 15-Nov-1985


Mos

Hrs

Enc

73 ENG2Eff: 15-Nov-1985


Mos

Hrs

Enc

73 ENG1Eff: 12-Dec-1985


Mos

Hrs

Enc

73 ENG2Eff: 12-Dec-1985

RecommendedT (A/R)73-0003 R04 FUEL SYSTEM - Servicing/Inspection (73-00-00) - Use of Fuel System Anti-icing Additive and Inspection of Fuel Heater

Mos

Hrs

Enc

73 ENG1Eff: 26-Nov-2008

RecommendedT (A/R)73-0003 R04 FUEL SYSTEM - Servicing/Inspection (73-00-00) - Use of Fuel System Anti-icing Additive and Inspection of Fuel Heater

Mos

Hrs

Enc

73 ENG2Eff: 26-Nov-2008

RecommendedT (A/R)73-0007 R00 FUEL SYSTEM - Fuel Distributor Assembly: Removal and Replacement

Mos

Hrs

Enc

73 ENG1Eff: 02-Jan-1990

RecommendedT (A/R)73-0007 R00 FUEL SYSTEM - Fuel Distributor Assembly: Removal and Replacement

Mos

Hrs

Enc

73 ENG2Eff: 02-Jan-1990

RecommendedRE (-)73-0008 R01 FUEL SYSTEM - Fuel Injector Coupling Nuts: Inspection and Retorque

Mos

Hrs

Enc

73 ENG1Eff: 14-Jan-1991

Also ConsiderDUE:1. T 100 Hrs | 2. RE -FUEL SYSTEM - Replacement of Loose Fuel Injectors73-0013 R00ENG173

RecommendedRE (-)73-0008 R01 FUEL SYSTEM - Fuel Injector Coupling Nuts: Inspection and Retorque

Mos

Hrs

Enc

73 ENG2Eff: 14-Jan-1991

Also ConsiderDUE:1. T 100 Hrs | 2. RE -FUEL SYSTEM - Replacement of Loose Fuel Injectors73-0013 R00ENG273


Generated: 6-Apr-2016 1:16 PM377/429







RecommendedRE (-)73-0009 R00 FUEL SYSTEM - Removal of Nylon Indicator Plug PN JAD 52-01315-1 From Main Fuel Filter Assembly

Mos

Hrs

Enc

73 ENG1Eff: 02-May-1991

(NOTE: All CF34-1A and CF34-3A engines, below serial number 350436 which have indicator plug PN JAD 52-01315-1 installed in main fuel

filter assembly GE PN 5050T60P01 (vendor PN 74D10-6).)

RecommendedRE (-)73-0009 R00 FUEL SYSTEM - Removal of Nylon Indicator Plug PN JAD 52-01315-1 From Main Fuel Filter Assembly

Mos

Hrs

Enc

73 ENG2Eff: 02-May-1991

(NOTE: All CF34-1A and CF34-3A engines, below serial number 350436 which have indicator plug PN JAD 52-01315-1 installed in main fuel

filter assembly GE PN 5050T60P01 (vendor PN 74D10-6).)

RecommendedRE (-)73-0010 R01 FUEL SYSTEM - Improved Main Drive Shaft and Face Seal Ring on CECO Fuel Pumps

Mos

Hrs

Enc

73 ENG1Eff: 21-Apr-1993


RecommendedRE (-)73-0010 R01 FUEL SYSTEM - Improved Main Drive Shaft and Face Seal Ring on CECO Fuel Pumps

Mos

Hrs

Enc

73 ENG2Eff: 21-Apr-1993


RecommendedRE (-)73-0011 R01 FUEL SYSTEM - Main Fuel Control - Improved Main Fuel Control PN 6047T74P09

Mos

Hrs

Enc

73 ENG1Eff: 26-Mar-1992

RecommendedRE (-)73-0011 R01 FUEL SYSTEM - Main Fuel Control - Improved Main Fuel Control PN 6047T74P09

Mos

Hrs

Enc

73 ENG2Eff: 26-Mar-1992

RecommendedRE (-)73-0012 R00 FUEL SYSTEM - Main Fuel Control - Improved Main Fuel Control PN 6047T74P01, P02, P03, and P07

Mos

Hrs

Enc

73 ENG1Eff: 01-May-1991

Also ConsiderDUE: 06-May-2014, 14,674.8 Hrs1. RE -ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Rework of...73-A0033 R07ENG173

RecommendedRE (-)73-0012 R00 FUEL SYSTEM - Main Fuel Control - Improved Main Fuel Control PN 6047T74P01, P02, P03, and P07

Mos

Hrs

Enc

73 ENG2Eff: 01-May-1991

Also ConsiderDUE:1. RE -ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Rework of...73-A0033 R07ENG273

RecommendedRE (-)73-0013 R00 FUEL SYSTEM - Replacement of Loose Fuel Injectors

Mos

Hrs

Enc

73 ENG1Eff: 12-Jun-1991


Generated: 6-Apr-2016 1:16 PM378/429







RecommendedRE (-)73-0013 R00 FUEL SYSTEM - Replacement of Loose Fuel Injectors

Mos

Hrs

Enc

73 ENG2Eff: 12-Jun-1991

RecommendedRE (-)73-0014 R02 FUEL SYSTEM - Main Fuel Control PN 6047T74P09 - Rework of CDP Sensor Body Assembly

Mos

Hrs

Enc

73 ENG1Eff: 14-Mar-1994

RecommendedRE (-)73-0014 R02 FUEL SYSTEM - Main Fuel Control PN 6047T74P09 - Rework of CDP Sensor Body Assembly

Mos

Hrs

Enc

73 ENG2Eff: 14-Mar-1994

RecommendedRE (-)73-0015 R01 FUEL SYSTEM - Replacement of the Main Fuel Control To Prevent Flameout Re-occurrence

Mos

Hrs

Enc

73 ENG1Eff: 14-Mar-1994

Also ConsiderDUE:1. RE -FUEL SYSTEM - T2 Sensor Tube and Hose Assembly and Fuel Mani...73-0016 R00ENG173

RecommendedRE (-)73-0015 R01 FUEL SYSTEM - Replacement of the Main Fuel Control To Prevent Flameout Re-occurrence

Mos

Hrs

Enc

73 ENG2Eff: 14-Mar-1994

Also ConsiderDUE:1. RE -FUEL SYSTEM - T2 Sensor Tube and Hose Assembly and Fuel Mani...73-0016 R00ENG273

RecommendedRE (-)73-0016 R00 FUEL SYSTEM - T2 Sensor Tube and Hose Assembly and Fuel Manifolds Fuel Leak Inspection

Mos

Hrs

Enc

73 ENG1Eff: 22-Mar-1994

RecommendedRE (-)73-0016 R00 FUEL SYSTEM - T2 Sensor Tube and Hose Assembly and Fuel Manifolds Fuel Leak Inspection

Mos

Hrs

Enc

73 ENG2Eff: 22-Mar-1994

RecommendedRE (-)73-0017 R00 FUEL SYSTEM - Correction of the Nameplate on Main Fuel Controls

Mos

Hrs

Enc

73 ENG1Eff: 22-Mar-1994

Also ConsiderDUE:1. RE -FUEL SYSTEM - Replacement of the Main Fuel Control To Preven...73-0015 R01ENG173

RecommendedRE (-)73-0017 R00 FUEL SYSTEM - Correction of the Nameplate on Main Fuel Controls

Mos

Hrs

Enc

73 ENG2Eff: 22-Mar-1994

Also ConsiderDUE:1. RE -FUEL SYSTEM - Replacement of the Main Fuel Control To Preven...73-0015 R01ENG273

RecommendedRE (-)73-0019 R00 FUEL SYSTEM - Inspection for Fuel Leaks

Mos

Hrs

Enc

73 ENG1Eff: 29-Sep-1994


Generated: 6-Apr-2016 1:16 PM379/429







RecommendedRE (-)73-0019 R00 FUEL SYSTEM - Inspection for Fuel Leaks

Mos

Hrs

Enc

73 ENG2Eff: 29-Sep-1994

RecommendedRE (-)73-0020 R01 FUEL SYSTEM - Deletion of the Thermal Valve Assembly

Mos

Hrs

Enc

73 ENG1Eff: 27-May-1998

RecommendedRE (-)73-0020 R01 FUEL SYSTEM - Deletion of the Thermal Valve Assembly

Mos

Hrs

Enc

73 ENG2Eff: 27-May-1998

RecommendedRE (-)73-0021 R00 FUEL SYSTEM - Inspection and Retorque of Coupling Clamp PN 4024T95P01 and PN 4024T95P03

Mos

Hrs

Enc

73 ENG1Eff: 02-Jun-1995

RecommendedRE (-)73-0021 R00 FUEL SYSTEM - Inspection and Retorque of Coupling Clamp PN 4024T95P01 and PN 4024T95P03

Mos

Hrs

Enc

73 ENG2Eff: 02-Jun-1995

RecommendedRE (-)73-0023 R00 FUEL AND OIL SYSTEM - Inspection/Replacement of Specific Fuel and Lube Hoses and Hose/Tubes Manufactured Between January 1995 and May 1995

Mos

Hrs

Enc

73 ENG1Eff: 26-Nov-1996

RecommendedRE (-)73-0023 R00 FUEL AND OIL SYSTEM - Inspection/Replacement of Specific Fuel and Lube Hoses and Hose/Tubes Manufactured Between January 1995 and May 1995

Mos

Hrs

Enc

73 ENG2Eff: 26-Nov-1996

RecommendedRE (-)73-0026 R01 FUEL SYSTEM - Introduction of Main Fuel Control PNs 6078T55P08/P09/ P10 With Improved VG Cable Bracket

Mos

Hrs

Enc

73 ENG1Eff: 23-Oct-1997

Also ConsiderDUE:1. RE -ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Introduct...73-0044 R03ENG173


RecommendedRE (-)73-0026 R01 FUEL SYSTEM - Introduction of Main Fuel Control PNs 6078T55P08/P09/ P10 With Improved VG Cable Bracket

Mos

Hrs

Enc

73 ENG2Eff: 23-Oct-1997



RecommendedRE (-)73-0027 R00 FUEL SYSTEM - Replacement of Fuel Filter Assembly (PN 5071T70P01)

Mos

Hrs

Enc

73 ENG1Eff: 10-Oct-1995


Generated: 6-Apr-2016 1:16 PM380/429







RecommendedRE (-)73-0027 R00 FUEL SYSTEM - Replacement of Fuel Filter Assembly (PN 5071T70P01)

Mos

Hrs

Enc

73 ENG2Eff: 10-Oct-1995

RecommendedRE (-)73-0028 R01 FUEL SYSTEM - Replacement of Fuel Filter Housing

Mos

Hrs

Enc

73 ENG1Eff: 04-Dec-1995

(NOTE: Engines that are in compliance with GE Field Engineering Instruction (FEI) CF34-65, as recorded in the Engine Service Record Book are

considered in compliance with this Service Bulletin and no further action is required.

If an engine has a filter assembly marked with a "R" (for reworked) immediately after the serial number, the filter assembly has been retrofitted

with the correct packings and does not require replacement For all

affected engines with over 3000 hours: Replace filter assembly at next 300 hour inspection, or no later than next scheduled filter replacement.If

filter assembly replacement is not possible or desirable at this time, inspect for fuel leakage, and continue to inspect at each subsequent 300

hour inspection until replacement is accomplished. Suspect leak area is shown in figure 1. The leak check of suspect area should be conducted

within 15 minutes of engine shutdown.For affected engines with less than 3000 hours: Replace the filter assembly at first 3000 hour inspection

interval.)

RecommendedRE (-)73-0028 R01 FUEL SYSTEM - Replacement of Fuel Filter Housing

Mos

Hrs

Enc

73 ENG2Eff: 04-Dec-1995

(NOTE: Engines that are in compliance with GE Field Engineering Instruction (FEI) CF34-65, as recorded in the Engine Service Record Book are

considered in compliance with this Service Bulletin and no further action is required.

If an engine has a filter assembly marked with a "R" (for reworked) immediately after the serial number, the filter assembly has been retrofitted

with the correct packings and does not require replacement For all

affected engines with over 3000 hours: Replace filter assembly at next 300 hour inspection, or no later than next scheduled filter replacement.If

filter assembly replacement is not possible or desirable at this time, inspect for fuel leakage, and continue to inspect at each subsequent 300

hour inspection until replacement is accomplished. Suspect leak area is shown in figure 1. The leak check of suspect area should be conducted

within 15 minutes of engine shutdown.For affected engines with less than 3000 hours: Replace the filter assembly at first 3000 hour inspection

interval.)

Category 9RE (-)73-0029 R00 FUEL SYSTEM Main Fuel Pump PN 6052T06P03/P05, Pulsation Elimination (Cancelled)

Mos

Hrs

Enc

73 ENG1


Mos

Hrs

Enc

73 ENG2


Mos

Hrs

Enc

73 ENG1


Mos

Hrs

Enc

73 ENG2

Cat. 9 - InformationalT (A/R)73-0029 R02 FUEL SYSTEM - Main Fuel Pump PN 6052T06P03/P05 Pulsation Elimination (Cancelled)

Mos

Hrs

Enc

73 ENG1Eff: 21-Mar-2005

(NOTE: Revision 2 is issued to advise overhaul and maintenance facilities and aircraft owners that CF34-BJ S/B 73-0029 is no longer valid. GE is

requesting that operators not comply with this Service Bulletin.)


Generated: 6-Apr-2016 1:16 PM381/429







Cat. 9 - InformationalT (A/R)73-0029 R02 FUEL SYSTEM - Main Fuel Pump PN 6052T06P03/P05 Pulsation Elimination (Cancelled)

Mos

Hrs

Enc

73 ENG2Eff: 21-Mar-2005

(NOTE: Revision 2 is issued to advise overhaul and maintenance facilities and aircraft owners that CF34-BJ S/B 73-0029 is no longer valid. GE is

requesting that operators not comply with this Service Bulletin.)

RecommendedRE (-)73-0030 R00 FUEL SYSTEM - Removal and Cleaning of the Main Fuel Control To Improve Cold Soak Throttle Response

Mos

Hrs

Enc

73 ENG1Eff: 11-Jul-1996

RecommendedRE (-)73-0030 R00 FUEL SYSTEM - Removal and Cleaning of the Main Fuel Control To Improve Cold Soak Throttle Response

Mos

Hrs

Enc

73 ENG2Eff: 11-Jul-1996

T (A/R)73-0031 R01 FUEL SYSTEM - Service Introduction Program for Operation of General Electric CF34 Engines Using CIS Fuels and Additives

Mos

Hrs

Enc

73 ENG1Eff: 24-Jan-2002

(NOTE: This Service Bulletin is revised to notify users that this Service Bulletin has been superseded by CF34-BJ 73-0047.)

T (A/R)73-0031 R01 FUEL SYSTEM - Service Introduction Program for Operation of General Electric CF34 Engines Using CIS Fuels and Additives

Mos

Hrs

Enc

73 ENG2Eff: 24-Jan-2002

(NOTE: This Service Bulletin is revised to notify users that this Service Bulletin has been superseded by CF34-BJ 73-0047.)

T (A/R)73-0032 R03 ENGINE FUEL AND CONTROL - Rework of Main Fuel Control to Add Forward Flange Vent Groove

Mos

Hrs

Enc

73 ENG1Eff: 30-Aug-1999

T (A/R)73-0032 R03 ENGINE FUEL AND CONTROL - Rework of Main Fuel Control to Add Forward Flange Vent Groove

Mos

Hrs

Enc

73 ENG2Eff: 30-Aug-1999

RecommendedT (A/R)73-0034 R00 FUEL SYSTEM - Improved Preformed Packings on the Main Fuel Control-to-Fuel Pump Interface

Mos

Hrs

Enc

73 ENG1Eff: 12-Jan-1998

Also ConsiderDUE:1. T - | 2. RE -ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Inspectio...73-A0050 R08ENG173

RecommendedT (A/R)73-0034 R00 FUEL SYSTEM - Improved Preformed Packings on the Main Fuel Control-to-Fuel Pump Interface

Mos

Hrs

Enc

73 ENG2Eff: 12-Jan-1998

Also ConsiderDUE:1. T - | 2. RE -ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Inspectio...73-A0050 R08ENG273

RecommendedRE (-)73-0036 R00 FUEL SYSTEM - Inspection of Main Fuel Filter for Non-Torqued Filter Bowl

Mos

Hrs

Enc

73 ENG1Eff: 03-Dec-1998


Generated: 6-Apr-2016 1:16 PM382/429







RecommendedRE (-)73-0036 R00 FUEL SYSTEM - Inspection of Main Fuel Filter for Non-Torqued Filter Bowl

Mos

Hrs

Enc

73 ENG2Eff: 03-Dec-1998

RecommendedT (A/R)73-0038 R00 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Introduction of Improved AGB-to-Fuel Pump Clamp Coupling

Mos

Hrs

Enc

73 ENG1Eff: 20-Aug-1999

RecommendedT (A/R)73-0038 R00 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Introduction of Improved AGB-to-Fuel Pump Clamp Coupling

Mos

Hrs

Enc

73 ENG2Eff: 20-Aug-1999

Category 5RE (-)73-0041 R00 ENGINE FUEL AND CONTROL Fuel System (73-00-00) - Introduction of CF34 Main Fuel Controls with Relocated PressureRelief Groove

Mos

Hrs

Enc

73 ENG1Eff: 12-Aug-1999

Category 5RE (-)73-0041 R00 ENGINE FUEL AND CONTROL Fuel System (73-00-00) - Introduction of CF34 Main Fuel Controls with Relocated PressureRelief Groove

Mos

Hrs

Enc

73 ENG2Eff: 12-Aug-1999

Cat. 5 - RecommendedRE (-)73-0041 R01 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Introduction of CF34 Main Fuel Controls with Relocated Pressure-Relief Groove

Mos

Hrs

Enc

73 ENG1Eff: 01-Nov-1999

Cat. 5 - RecommendedRE (-)73-0041 R01 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Introduction of CF34 Main Fuel Controls with Relocated Pressure-Relief Groove

Mos

Hrs

Enc

73 ENG2Eff: 01-Nov-1999

Cat. 5 - RecommendedT (A/R)73-0041 R02 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Introduction of CF34 Main Fuel Controls with Relocated Pressure-Relief Groove

Mos

Hrs

Enc

73 ENG1Eff: 06-Dec-2013



Cat. 5 - RecommendedT (A/R)73-0041 R02 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Introduction of CF34 Main Fuel Controls with Relocated Pressure-Relief Groove

Mos

Hrs

Enc

73 ENG2Eff: 06-Dec-2013



Cat. 6 - RecommendedRE (-)73-0043 R00 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Rework of Variable Geometry Actuator PN 5050T37G01

Mos

Hrs

Enc

73 ENG1Eff: 31-Oct-2002


Generated: 6-Apr-2016 1:16 PM383/429








Mos

Hrs

Enc

73 ENG2Eff: 31-Oct-2002


Mos

Hrs

Enc

73 ENG1Eff: 11-Mar-2003


Mos

Hrs

Enc

73 ENG2Eff: 11-Mar-2003


Mos

Hrs

Enc

73 ENG1Eff: 17-Apr-2003


Mos

Hrs

Enc

73 ENG2Eff: 17-Apr-2003

Cat. 6 - RecommendedT (A/R)73-0043 R03 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Rework of Variable Geometry Actuator PN 5050T37G01

Mos

Hrs

Enc

73 ENG1Eff: 07-Apr-2010

Cat. 6 - RecommendedT (A/R)73-0043 R03 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Rework of Variable Geometry Actuator PN 5050T37G01

Mos

Hrs

Enc

73 ENG2Eff: 07-Apr-2010

Cat. 6 - RecommendedRE (-)73-0044 R00 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Introduction of CF34 Main Fuel Controls with Product Improvement Package

Mos

Hrs

Enc

73 ENG1Eff: 09-Mar-2001


Mos

Hrs

Enc

73 ENG2Eff: 09-Mar-2001


Mos

Hrs

Enc

73 ENG1Eff: 21-Feb-2002


Mos

Hrs

Enc

73 ENG2Eff: 21-Feb-2002


Generated: 6-Apr-2016 1:16 PM384/429








Mos

Hrs

Enc

73 ENG1Eff: 13-Dec-2012


Mos

Hrs

Enc

73 ENG2Eff: 13-Dec-2012


Mos

Hrs

Enc

73 ENG1Eff: 08-Nov-2013


Mos

Hrs

Enc

73 ENG2Eff: 08-Nov-2013

Cat. 6 - RecommendedRE (-)73-0045 R00 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Introduction of Modified Fuel Valve Bushing into MFC

Mos

Hrs

Enc

73 ENG1Eff: 31-Jan-2001


Mos

Hrs

Enc

73 ENG2Eff: 31-Jan-2001


Mos

Hrs

Enc

73 ENG1Eff: 05-Jul-2001


Mos

Hrs

Enc

73 ENG2Eff: 05-Jul-2001


Mos

Hrs

Enc

73 ENG1Eff: 06-Dec-2013


Mos

Hrs

Enc

73 ENG2Eff: 06-Dec-2013

Cat. 2 - RecommendedRE (-)73-0046 R00 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Inspection of Main Fuel Controls for Throttle Body Leakage

Mos

Hrs

Enc

73 ENG1Eff: 13-Jun-2001

(NOTE: This Service Bulletin is applicable to these CF34 turbofan engines that have the following serial numbers and that have main fuel

controls (MFC) that have not previously complied with CF34-BJ Service Bulletins 73-0042 and 73-0044, or 73-0045)


Generated: 6-Apr-2016 1:16 PM385/429







Cat. 2 - RecommendedRE (-)73-0046 R00 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Inspection of Main Fuel Controls for Throttle Body Leakage

Mos

Hrs

Enc

73 ENG2Eff: 13-Jun-2001

(NOTE: This Service Bulletin is applicable to these CF34 turbofan engines that have the following serial numbers and that have main fuel

controls (MFC) that have not previously complied with CF34-BJ Service Bulletins 73-0042 and 73-0044, or 73-0045)

Category 9RE (-)73-0047 R00 ENGINE FUEL AND CONTROL Fuel System (730000) CF341A/3A/3A1/3A2/3B TS1 Fuels Fleet Leader Sampling Program (Cancelled)

Mos

Hrs

Enc

73 ENG1Eff: 24-Jan-2002

Category 9RE (-)73-0047 R00 ENGINE FUEL AND CONTROL Fuel System (730000) CF341A/3A/3A1/3A2/3B TS1 Fuels Fleet Leader Sampling Program (Cancelled)

Mos

Hrs

Enc

73 ENG2Eff: 24-Jan-2002

Cat. 7 - OptionalRE (-)73-0047 R01 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - CF34-1A/-3A/-3A1/-3A2/-3B TS-1 Fuels Fleet Leader Sampling Program (Cancelled)

Mos

Hrs

Enc

73 ENG1Eff: 30-Mar-2006

(NOTE: This Service Bulletin is superseded by CF34-BJ S/B 73-0060.)

Cat. 7 - OptionalRE (-)73-0047 R01 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - CF34-1A/-3A/-3A1/-3A2/-3B TS-1 Fuels Fleet Leader Sampling Program (Cancelled)

Mos

Hrs

Enc

73 ENG2Eff: 30-Mar-2006


Cat. 9 - InformationalT (A/R)73-0047 R02 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - CF34-1A/-3A/-3A1/-3A2/-3B TS-1 Fuels Fleet Leader Sampling Program (Cancelled)

Mos

Hrs

Enc

73 ENG1Eff: 30-Aug-2007


Cat. 9 - InformationalT (A/R)73-0047 R02 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - CF34-1A/-3A/-3A1/-3A2/-3B TS-1 Fuels Fleet Leader Sampling Program (Cancelled)

Mos

Hrs

Enc

73 ENG2Eff: 30-Aug-2007


Cat. 8 - InformationalT (A/R)73-0048 R00 ENGINE FUEL AND CONTROL - Variable Geometry Actuation System (73-00-00) - Spare Parts Release for Variable Geometry Actuator Repair Kit

Mos

Hrs

Enc

73 ENG1Eff: 31-Jul-2002

Cat. 8 - InformationalT (A/R)73-0048 R00 ENGINE FUEL AND CONTROL - Variable Geometry Actuation System (73-00-00) - Spare Parts Release for Variable Geometry Actuator Repair Kit

Mos

Hrs

Enc

73 ENG2Eff: 31-Jul-2002

Cat. 2 - RecommendedRE (-)73-0049 R00 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Replacement of Selected CF34 Main Fuel Controls

Mos

Hrs

Enc

73 ENG1Eff: 21-Feb-2003


Mos

Hrs

Enc

73 ENG2Eff: 21-Feb-2003


Generated: 6-Apr-2016 1:16 PM386/429







Cat. 8 - InformationalRE (-)73-0049 R01 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Replacement of Selected CF34 Main Fuel Controls

Mos

Hrs

Enc

73 ENG1Eff: 29-May-2003

Cat. 8 - InformationalRE (-)73-0049 R01 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Replacement of Selected CF34 Main Fuel Controls

Mos

Hrs

Enc

73 ENG2Eff: 29-May-2003


Mos

Hrs

Enc

73 ENG1Eff: 02-Apr-2004


Mos

Hrs

Enc

73 ENG2Eff: 02-Apr-2004


Mos

Hrs

Enc

73 ENG1Eff: 06-Dec-2013


Mos

Hrs

Enc

73 ENG2Eff: 06-Dec-2013

Cat. 7 - OptionalRE (-)73-0051 R00 FUEL SYSTEM - Fuel Manifold (73-00-00) - Introduction of Fuel Injectors PN 6078T63P07 and PN 6078T64P07

Mos

Hrs

Enc

73 ENG1Eff: 15-Jun-2004

(NOTE: GE recommends you do this Service Bulletin at next shop visit field or overhaul, beyond 10,000 hours, of the engine.)


Mos

Hrs

Enc

73 ENG2Eff: 15-Jun-2004



Mos

Hrs

Enc

73 ENG1Eff: 15-Dec-2005



Mos

Hrs

Enc

73 ENG2Eff: 15-Dec-2005


Cat. 7 - OptionalRE (-)73-0051 R02 FUEL SYSTEM - Fuel Manifold (73-00-00) - Introduction of Fuel Injectors PN 5083T10P03 PN 5083T11P03 PN 5083T12P03 PN 6078T63P07 and PN 6078T64P07

Mos

Hrs

Enc

73 ENG1Eff: 02-Nov-2006



Generated: 6-Apr-2016 1:16 PM387/429







Cat. 7 - OptionalRE (-)73-0051 R02 FUEL SYSTEM - Fuel Manifold (73-00-00) - Introduction of Fuel Injectors PN 5083T10P03 PN 5083T11P03 PN 5083T12P03 PN 6078T63P07 and PN 6078T64P07

Mos

Hrs

Enc

73 ENG2Eff: 02-Nov-2006


Cat. 5 - RecommendedRE (-)73-0051 R03 FUEL SYSTEM - Fuel Manifold (73-00-00) - Introduction of Fuel Injectors PN 5083T10P03 PN 5083T11P03 PN 5083T12P03 PN 6078T63P07 and PN 6078T64P07

Mos

Hrs

Enc

73 ENG1Eff: 23-May-2008


Cat. 5 - RecommendedRE (-)73-0051 R03 FUEL SYSTEM - Fuel Manifold (73-00-00) - Introduction of Fuel Injectors PN 5083T10P03 PN 5083T11P03 PN 5083T12P03 PN 6078T63P07 and PN 6078T64P07

Mos

Hrs

Enc

73 ENG2Eff: 23-May-2008


Cat. 3 - RecommendedT (ESV)73-0051 R04 FUEL SYSTEM - Fuel Manifold (73-00-00) - Introduction of Fuel Injectors PN 5083T10P03 PN 5083T11P03 PN 5083T12P03 PN 6078T63P07 and PN 6078T64P07

Mos

Hrs

Enc

73 ENG1Eff: 22-Jun-2009


Cat. 3 - RecommendedT (ESV)73-0051 R04 FUEL SYSTEM - Fuel Manifold (73-00-00) - Introduction of Fuel Injectors PN 5083T10P03 PN 5083T11P03 PN 5083T12P03 PN 6078T63P07 and PN 6078T64P07

Mos

Hrs

Enc

73 ENG2Eff: 22-Jun-2009


Cat. 5 - RecommendedRE (-)73-0055 R00 FUEL SYSTEM - (73-00-00) - Actuator Hose Fire Sleeve Improvement

Mos

Hrs

Enc

73 ENG1Eff: 25-Oct-2006

(NOTE: Revision 01 is to inform aircraft owners that Service Bulletin CF34-BJ S/B 73-0055 has been superseded by CF34-BJ S/B 73-0056)


Mos

Hrs

Enc

73 ENG2Eff: 25-Oct-2006



Mos

Hrs

Enc

73 ENG1Eff: 06-Feb-2007


Cat. 5 - RecommendedT (A/R)73-0055 R01 FUEL SYSTEM - (73-00-00) - Actuator Hose Fire Sleeve Improvement

Mos

Hrs

Enc

73 ENG2Eff: 06-Feb-2007


Cat. 3 - RecommendedRE (-)73-0056 R00 FUEL SYSTEM - (73-00-00) - Introduction of Improved VG Actuator Hose (Final Fix)

Mos

Hrs

Enc

73 ENG1Eff: 06-Feb-2007


Mos

Hrs

Enc

73 ENG2Eff: 06-Feb-2007


Generated: 6-Apr-2016 1:16 PM388/429








Mos

Hrs

Enc

73 ENG1Eff: 02-Aug-2007

Cat. 3 - RecommendedT (A/R)73-0056 R01 FUEL SYSTEM - (73-00-00) - Introduction of Improved VG Actuator Hose (Final Fix)

Mos

Hrs

Enc

73 ENG2Eff: 02-Aug-2007

Cat. 9 - InformationalRE (-)73-0060 R00 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Fuel and Additives - Requirements for and Approval of

Mos

Hrs

Enc

73 ENG1Eff: 30-Aug-2007


Mos

Hrs

Enc

73 ENG2Eff: 30-Aug-2007


Mos

Hrs

Enc

73 ENG1Eff: 14-Jul-2011


Mos

Hrs

Enc

73 ENG2Eff: 14-Jul-2011

Cat. 9 - InformationalT (-)73-0060 R02 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Fuel and Additives - Requirements for and Approval of

Mos

Hrs

Enc

73 ENG1Eff: 22-Jun-2012

Cat. 9 - InformationalT (-)73-0060 R02 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Fuel and Additives - Requirements for and Approval of

Mos

Hrs

Enc

73 ENG2Eff: 22-Jun-2012

Category 9T (A/R)73-0060 R03 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Fuel and Additives - Requirements for and Approval of

Mos

Hrs

Enc

73 ENG1Eff: 20-Nov-2015

Category 9T (A/R)73-0060 R03 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Fuel and Additives - Requirements for and Approval of

Mos

Hrs

Enc

73 ENG2Eff: 20-Nov-2015

Cat. 2 - RecommendedRE (-)73-0062 R00 ENGINE - Fuel System (73-00-00) - Inspection of Connection Orientation Between the Aft Actuator Head Hose Assembly and the Main Fuel Control

Mos

Hrs

Enc

73 ENG1Eff: 01-Apr-2008


Generated: 6-Apr-2016 1:16 PM389/429








Mos

Hrs

Enc

73 ENG2Eff: 01-Apr-2008


Mos

Hrs

Enc

73 ENG1Eff: 01-Jul-2008


Mos

Hrs

Enc

73 ENG2Eff: 01-Jul-2008


Mos

Hrs

Enc

73 ENG1Eff: 27-Aug-2008


Mos

Hrs

Enc

73 ENG2Eff: 27-Aug-2008

Cat. 2 - RecommendedRE (-)73-0063 R00 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Replacement of High Time Fuel Valve Thrust Bushing and Clip

Mos

Hrs

Enc

73 ENG1Eff: 09-Feb-2012

(NOTE: Based on field event history, it is recommended that this Service Bulletin be accomplished before the MFC thrust bushing and clip have

accumulated more than 10,000 hours of field service. If utilization history (hours) of the bushing and clip are unknown, it is recommended that

this Service Bulletin be incorporated at the next MFC shop visit.Design improvements introduced per CF34-BJ S/B 73-0044 are available for

some models and would eliminate the need for this Service Bulletin. If CF34-BJ S/B 73-0044 is not accomplished or is not applicable, this

Service Bulletin should continue to be repeated per the described compliance recommendation.)


Mos

Hrs

Enc

73 ENG2Eff: 09-Feb-2012

(NOTE: Based on field event history, it is recommended that this Service Bulletin be accomplished before the MFC thrust bushing and clip have

accumulated more than 10,000 hours of field service. If utilization history (hours) of the bushing and clip are unknown, it is recommended that

this Service Bulletin be incorporated at the next MFC shop visit.Design improvements introduced per CF34-BJ S/B 73-0044 are available for

some models and would eliminate the need for this Service Bulletin. If CF34-BJ S/B 73-0044 is not accomplished or is not applicable, this

Service Bulletin should continue to be repeated per the described compliance recommendation.)


Mos

Hrs

Enc

73 ENG1Eff: 31-May-2013


Mos

Hrs

Enc

73 ENG2Eff: 31-May-2013


Generated: 6-Apr-2016 1:16 PM390/429







Category 6RE (-)73-0064 R01 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Replacement of Min Speed Adjustment Lever

Mos

Hrs

Enc

73 ENG1Eff: 04-Aug-2015

(AVG MAN HRS: 2)

Category 6RE (-)73-0064 R01 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Replacement of Min Speed Adjustment Lever

Mos

Hrs

Enc

73 ENG2Eff: 04-Aug-2015

(AVG MAN HRS: 2)

MRB ≈24-Nov-2019RE73-10-11-204 Fuel Pump Assembly - General Visual Inspection of the engine fuel pump assembly

27-Jun-2005Mos

1,818.6 Hrs (+40)(13,839)-/+403,00010,839Hrs

Enc

(PKG 3000 Eng Hour)

73 ENG2


MRB ≈24-Nov-2019RE73-10-11-204 Fuel Pump Assembly - General Visual Inspection of the engine fuel pump assembly

31-May-2005Mos

1,818.6 Hrs (+40)13,956-/+403,00010,956Hrs

Enc

(PKG 3000 Eng Hour)

73 ENG1


MRB ≈25-Sep-2016RE73-10-16-208 Fuel Heater Assembly - Check for evidence of leakage from fuel heater

10-Feb-2016Mos

300 Hrs (+40)(12,437.4)-/+4030012,137.4Hrs

6,769Enc

(PKG 300 Eng Hour)

73 ENG1


MRB ≈25-Sep-2016RE73-10-16-208 Fuel Heater Assembly - Check for evidence of leakage from fuel heater

10-Feb-2016Mos

300 Hrs (+40)(12,320.4)-/+4030012,020.4Hrs

6,728Enc

(PKG 300 Eng Hour)

73 ENG2


MRB ≈25-Sep-2016RE73-10-21-202 Fuel Filter Assembly - Check bypass indicator and carry out a visual check of mounting bracket

10-Feb-2016Mos

300 Hrs (+40)(12,320.4)-/+4030012,020.4Hrs

6,728Enc

(PKG 300 Eng Hour)

73 ENG2

Ref.:G.E. MM SEI-580 Section 5-21-00 (SOURCE: TLMC 05-20-15) (NOTE: If bypass indicator is protruding check fuel filter element.)

MRB ≈25-Sep-2016RE73-10-21-202 Fuel Filter Assembly - Check bypass indicator and carry out a visual check of mounting bracket

10-Feb-2016Mos

300 Hrs (+40)(12,437.4)-/+4030012,137.4Hrs

6,769Enc

(PKG 300 Eng Hour)

73 ENG1

Ref.:G.E. MM SEI-580 Section 5-21-00 (SOURCE: TLMC 05-20-15) (NOTE: If bypass indicator is protruding check fuel filter element.)

MRB ≈10-May-2017RE73-10-21-203 Fuel Filter Assembly - Check Fuel filter element

10-Feb-2016Mos

600 Hrs (+40)(12,737.4)-/+4060012,137.4Hrs

6,769Enc

(PKG 600 Eng Hour)

73 ENG1

(SOURCE: TLMC 05-20-15) (NOTE: Install new fuel filter element.)

MRB ≈03-May-2017RE73-10-21-203 Fuel Filter Assembly - Check Fuel filter element

10-Feb-2016Mos

590.8 Hrs (+40)(12,611.2)-/+4060012,020.4Hrs

6,728Enc

(PKG 600 Eng Hour)

73 ENG2

(Tol. Adjustment: -9.2 Hrs) (SOURCE: TLMC 05-20-15) (NOTE: Install new fuel filter element.)

MRB ≈22-Feb-2021RE73-20-11-206 Fuel Control Unit - General Visual Inspection of main fuel control assembly

05-Jun-2009Mos

2,417.4 Hrs (+40)(14,554.8)-/+403,00011,554.8Hrs

Enc

(PKG 3000 Eng Hour)

73 ENG1



Generated: 6-Apr-2016 1:16 PM391/429







MRB ≈24-Nov-2019RE73-20-11-206 Fuel Control Unit - General Visual Inspection of main fuel control assembly

28-Jul-2005Mos

1,818.6 Hrs (+40)(13,839)-/+403,00010,839Hrs

Enc

(PKG 3000 Eng Hour)

73 ENG2


MRB ≈25-Sep-2016RE73-20-16-210 N1 Speed Control Amplifier - Visual Check of control amplifier isolators

10-Feb-2016Mos

300 Hrs (+40)(12,437.4)-/+4030012,137.4Hrs

6,769Enc

(PKG 300 Eng Hour)

73 ENG1


MRB ≈25-Sep-2016RE73-20-16-210 N1 Speed Control Amplifier - Visual Check of control amplifier isolators

10-Feb-2016Mos

300 Hrs (+40)(12,320.4)-/+4030012,020.4Hrs

6,728Enc

(PKG 300 Eng Hour)

73 ENG2


Recommended - AlertRE (-)73-A0032 REV 2 ENGINE FUEL AND CONTROL - Rework of Main Fuel Control to Add Forward Flange Vent Groove

Mos

Hrs

Enc

73 ENG1

Recommended - AlertRE (-)73-A0032 REV 2 ENGINE FUEL AND CONTROL - Rework of Main Fuel Control to Add Forward Flange Vent Groove

Mos

Hrs

Enc

73 ENG2

AlertRE (-)73-A0033 R00 ENGINE FUEL AND CONTROL Fuel System (730000) Rework of Main Fuel Control for Overspeed Protection

Mos

Hrs

Enc

73 ENG1Eff: 21-Nov-1997


Mos

Hrs

Enc

73 ENG2Eff: 21-Nov-1997


Mos

Hrs

Enc

73 ENG1Eff: 29-May-1998


Mos

Hrs

Enc

73 ENG2Eff: 29-May-1998


Mos

Hrs

Enc

73 ENG1Eff: 09-Mar-1999


Mos

Hrs

Enc

73 ENG2Eff: 09-Mar-1999


Generated: 6-Apr-2016 1:16 PM392/429








Mos

Hrs

Enc

73 ENG1Eff: 09-Sep-1999


Mos

Hrs

Enc

73 ENG2Eff: 09-Sep-1999

Cat. 1 - RecommendedRE (-)73-A0033 R04 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Rework of Main Fuel Control for Overspeed Protection

Mos

Hrs

Enc

73 ENG1Eff: 01-Nov-1999


Mos

Hrs

Enc

73 ENG2Eff: 01-Nov-1999


Mos

Hrs

Enc

73 ENG1Eff: 13-Sep-2004


Mos

Hrs

Enc

73 ENG2Eff: 13-Sep-2004


Mos

Hrs

Enc

73 ENG1Eff: 02-Dec-2004


Mos

Hrs

Enc

73 ENG2Eff: 02-Dec-2004


OVD[06-May-2014]Mos

2,537.4 Hrs[14,674.8]Hrs

Enc

73 ENG1Eff: 06-May-2009

Also ConsiderDUE:1. T A/R | 2. RE -ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Introduct...73-0041 R02ENG173




Generated: 6-Apr-2016 1:16 PM393/429








Mos

Hrs

Enc

73 ENG2Eff: 06-May-2009

Also ConsiderDUE:1. T A/R | 2. RE -ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Introduct...73-0041 R02ENG273



RecommendedRE (-)73-A0035 R01 FUEL SYSTEM - Inspection for Possible Missing Fuel Filter Plug

Mos

Hrs

Enc

73 ENG1Eff: 02-Dec-1998

(NOTE: Main fuel filters PN 5050T60P01 are of two different configurations. One configuration has two filter housing ports that are plugged

and safety-wired and the other configuration does not have ports that require plugs and safety wire. This Service Bulletin applies to these CF34

turbofan engines that have a main fuel filter PN 5050T60P01 that is equipped with filter housing ports and plugs)

RecommendedRE (-)73-A0035 R01 FUEL SYSTEM - Inspection for Possible Missing Fuel Filter Plug

Mos

Hrs

Enc

73 ENG2Eff: 02-Dec-1998

(NOTE: Main fuel filters PN 5050T60P01 are of two different configurations. One configuration has two filter housing ports that are plugged

and safety-wired and the other configuration does not have ports that require plugs and safety wire. This Service Bulletin applies to these CF34

turbofan engines that have a main fuel filter PN 5050T60P01 that is equipped with filter housing ports and plugs)

RecommendedRE (-)73-A0037 R00 FUEL SYSTEM - Replacement of Selected CF34 Main Fuel Controls

Mos

Hrs

Enc

73 ENG1Eff: 22-Jan-1999

RecommendedRE (-)73-A0037 R00 FUEL SYSTEM - Replacement of Selected CF34 Main Fuel Controls

Mos

Hrs

Enc

73 ENG2Eff: 22-Jan-1999

RecommendedRE (-)73-A0039 R00 FUEL SYSTEM - Inspection and Replacement of Main Fuel Filter PN 4106T62P01

Mos

Hrs

Enc

73 ENG1Eff: 26-Mar-1999

RecommendedRE (-)73-A0039 R00 FUEL SYSTEM - Inspection and Replacement of Main Fuel Filter PN 4106T62P01

Mos

Hrs

Enc

73 ENG2Eff: 26-Mar-1999

Cat. 2 - RecommendedRE (-)73-A0040 R00 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Replacement of Buna-N Material Preformed Packing

Mos

Hrs

Enc

73 ENG1Eff: 07-Jul-1999

(NOTE: The improvement described in this Service Bulletin has been introduced on these CF34 turbofan production engines. However, if the

main fuel control was replaced in the field using Buna-N material preformed packings, the packings must be replaced. CF34-3A1 engines,

serial numbers 807515 and up CF34-3B engines, serial numbers 872272 and up.)

Cat. 2 - RecommendedRE (-)73-A0040 R00 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Replacement of Buna-N Material Preformed Packing

Mos

Hrs

Enc

73 ENG2Eff: 07-Jul-1999

(NOTE: The improvement described in this Service Bulletin has been introduced on these CF34 turbofan production engines. However, if the

main fuel control was replaced in the field using Buna-N material preformed packings, the packings must be replaced. CF34-3A1 engines,

serial numbers 807515 and up CF34-3B engines, serial numbers 872272 and up.)


Generated: 6-Apr-2016 1:16 PM394/429







Cat. 2 - RecommendedRE (-)73-A0050 R00 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Inspection of Main Fuel Control Input Drive Shaft Spline Main Fuel Pump Control Drive Shaft Spline and Main

Fuel Pump Secondary Drive Shaft Spline

Mos

Hrs

Enc

73 ENG1Eff: 26-Jul-2004



Mos

Hrs

Enc

73 ENG2Eff: 26-Jul-2004



Mos

Hrs

Enc

73 ENG1Eff: 02-Dec-2004



Mos

Hrs

Enc

73 ENG2Eff: 02-Dec-2004



Mos

Hrs

Enc

73 ENG1Eff: 20-Jan-2006



Mos

Hrs

Enc

73 ENG2Eff: 20-Jan-2006



Mos

Hrs

Enc

73 ENG1Eff: 10-Oct-2007



Mos

Hrs

Enc

73 ENG2Eff: 10-Oct-2007



Mos

Hrs

Enc

73 ENG1Eff: 25-Apr-2008


Generated: 6-Apr-2016 1:16 PM395/429









Mos

Hrs

Enc

73 ENG2Eff: 25-Apr-2008



Mos

Hrs

Enc

73 ENG1Eff: 05-Jan-2011

(NOTE: This Alert Service Bulletin is applicable to all CF34-1A, -3A, -3A1, -3A2, -3B, turbofan engine main fuel controls (MFCs) and main fuel

pumps (MFPs).

These regions apply to operators re-fueling in that region more than 50 percent of the time. For MFCs that have already accumulated the

operating hours bellow, do within 500 operating hours from the issue date of this Alert Service Bulletin. (b) Repeat this Service Bulletin

inspection procedure at intervals shown bellow. Region/Country Inspection Interval of MFC Asia (1) 4,000 operating hours- China (2, 3, 4)

Shop visit or 20,000 operating hours- India (2, 3, 4) Shop visit or 20,000 operating hours- Japan 1,500 operating hours Middle East (2) 10,000

operating hours Commonwealth of Independent States (CIS) (2) 10,000 operating hours Africa (2) 10,000 operating hours North America (2, 3,

4) Shop visit or 20,000 operating hours Central America and the Caribbean (1) 10,000 operating hours- US Virgin Islands 4,000 operating

hours South America (2) 10,000 operating hours Europe (2) 10,000 operating hours Australia (2) 10,000 operating hours Unknown 1,500

operating hours 1 Exceptions to the Asian, Central American and the Caribbean regions are provided below. 2 If the aircraft is re-fueled in

the Asian region more than 50 percent of the time since the initial Service Bulletin inspection, re-inspect per the Asian region inspection

intervals. 3 If the aircraft is re-fueled outside this region since the initial Service Bulletin inspection, and has not been operated in the Asian

region, re-inspect every 10,000 operating hours. 4 Inspect at every shop visit or 20,000 operating hours, whichever occurs later.)



Mos

Hrs

Enc

73 ENG2Eff: 05-Jan-2011


pumps (MFPs).














Mos

Hrs

Enc

73 ENG1Eff: 28-Sep-2011



Mos

Hrs

Enc

73 ENG2Eff: 28-Sep-2011


Generated: 6-Apr-2016 1:16 PM396/429









Mos

Hrs

Enc

73 ENG1Eff: 05-Dec-2011



Mos

Hrs

Enc

73 ENG2Eff: 05-Dec-2011

Cat. 2 - RecommendedT (-)73-A0050 R08 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Inspection of Main Fuel Control Input Drive Shaft Spline Main Fuel Pump Control Drive Shaft Spline and Main


Mos

Hrs

Enc

73 ENG1Eff: 26-Jul-2004


pumps (MFPs).












Cat. 2 - RecommendedT (-)73-A0050 R08 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Inspection of Main Fuel Control Input Drive Shaft Spline Main Fuel Pump Control Drive Shaft Spline and Main


Mos

Hrs

Enc

73 ENG2Eff: 26-Jul-2004


pumps (MFPs).












Alert, Cat. 2 - Recommended ≈21-Jun-2016T73-A0050 R09 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Inspection of Main Fuel Control Input Drive Shaft Spline Main Fuel Pump Control Drive Shaft Spline and Main


Mos

174.27 Hrs≈12,311.67500Hrs

Enc

73 ENG1Eff: 29-Mar-2015

Also ConsiderDUE:1. T A/R | 2. RE -FUEL SYSTEM - Improved Preformed Packings on the Main Fuel C...73-0034 R00ENG173


Generated: 6-Apr-2016 1:16 PM397/429







Alert, Cat. 2 - Recommended ≈21-Jun-2016T73-A0050 R09 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Inspection of Main Fuel Control Input Drive Shaft Spline Main Fuel Pump Control Drive Shaft Spline and Main


Mos

174.27 Hrs≈12,194.67500Hrs

Enc

73 ENG2Eff: 29-Mar-2015

Also ConsiderDUE:1. T A/R | 2. RE -FUEL SYSTEM - Improved Preformed Packings on the Main Fuel C...73-0034 R00ENG273

MandatoryRE (-)99-23-26 Main Fuel Control (MFC)

Mos

Hrs

Enc

73 ENG1Eff: 05-Nov-1999

MandatoryRE (-)99-23-26 Main Fuel Control (MFC)

Mos

Hrs

Enc

73 ENG2Eff: 05-Nov-1999

MandatoryRE (-)99-23-26 R1 Main Fuel Control (MFC)

27-Dec-1999Mos

Hrs

Enc

73 ENG1FOUND P/C/WEff: 17-Feb-2000 Complied

With

MandatoryRE (-)99-23-26 R1 Main Fuel Control (MFC)

27-Dec-1999Mos

Hrs

Enc

73 ENG2FOUND P/C/WEff: 17-Feb-2000 Complied

With

AlertRE (-)A601-0144 Modification - Fuel Temperature Indicator - Decal Addition

18-Sep-1984Mos

Hrs

Ldg


AlertRE (-)A601-1049 Modification - Fuel Temperature Bulb - Seal Replacement

Mos

Hrs

Ldg

73 A/F

AlertT (A/R)A601-1049 Rev 1 Modification - Fuel Temperature Bulb - Seal Replacement

Mos

Hrs

Ldg

73 A/FEff: 15-Sep-1985

▼ 74 - IGNITION

RE (O/C)Fan Inlet Temperature Sensor

27-Jun-2005Mos

10,839Hrs10,839

5,949Enc5,949


UNKNOWN

RE (O/C)Fan Inlet Temperature Sensor

31-May-2005Mos

10,956Hrs

5,990Enc

74 ENG14033T65P03EGN10383


Generated: 6-Apr-2016 1:16 PM398/429







RE (O/C)Igniter Plug

15-Sep-2007Mos

11,280.5Hrs

Enc

No.174 ENG14048T30P06CSP52897


15-Sep-2007Mos

11,163.5Hrs

Enc

No.174 ENG24048T30P06CSP56214


15-Sep-2007Mos

11,280.5Hrs

Enc

No.274 ENG14048T30P06TDG00869


15-Sep-2007Mos

11,163.5Hrs

Enc

No.274 ENG24048T30P06TDG00868

RE (O/C)Ignition Exciter

27-Jun-2005Mos

10,839Hrs

5,949Enc

No.174 ENG25027T49P02SNT4234R


31-May-2005Mos

10,956Hrs10,956

5,990Enc5,999

No.174 ENG1Overhauled5027T49P02

4600


20-Sep-1983Mos

0Hrs

0Enc



20-Sep-1983Mos

0Hrs

0Enc


RE (O/C)Static Ignition Inverter

20-Sep-1983Mos

0Hrs0

0Ldg0

74 A/FNewASH671-2

UNKNOWN

MRB ≈03-May-2017RE74-00-00-204 (Left) Ignition System Operational Test - Ignition System

10-Feb-2016Mos

590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs

6,326Ldg

(PKG 600 Hour)

74 A/F


MRB ≈03-May-2017RE74-00-00-204 (Right) Ignition System Operational Test - Ignition System

10-Feb-2016Mos

590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs

6,326Ldg

(PKG 600 Hour)

74 A/F



Generated: 6-Apr-2016 1:16 PM399/429







RecommendedRE (-)74-0002 R02 ELECTRICAL SYSTEM - Installation of N2 Electrical Filter

Mos

Hrs

Enc

74 ENG1Eff: 12-Sep-1989

RecommendedRE (-)74-0002 R02 ELECTRICAL SYSTEM - Installation of N2 Electrical Filter

Mos

Hrs

Enc

74 ENG2Eff: 12-Sep-1989

RecommendedRE (-)74-0004 R01 ELECTRICAL SYSTEM - N1 Control Amplifier Adjustment

Mos

Hrs

Enc

74 ENG1Eff: 10-Mar-1989

RecommendedRE (-)74-0004 R01 ELECTRICAL SYSTEM - N1 Control Amplifier Adjustment

Mos

Hrs

Enc

74 ENG2Eff: 10-Mar-1989

RecommendedT (A/R)74-0006 R00 ELECTRICAL SYSTEM - Verification of Ignition Leads for Correct Installation

Mos

Hrs

Enc

74 ENG1Eff: 26-Feb-1993

RecommendedT (A/R)74-0006 R00 ELECTRICAL SYSTEM - Verification of Ignition Leads for Correct Installation

Mos

Hrs

Enc

74 ENG2Eff: 26-Feb-1993

RecommendedRE (-)74-0007 R00 ELECTRICAL SYSTEM - Upgrade of the Engine Ignition Leads

Mos

Hrs

Enc

74 ENG1Eff: 15-Dec-1993

RecommendedRE (-)74-0007 R00 ELECTRICAL SYSTEM - Upgrade of the Engine Ignition Leads

Mos

Hrs

Enc

74 ENG2Eff: 15-Dec-1993

RecommendedRE (-)74-0008 R00 ELECTRICAL SYSTEM - Replacement of the Green Jumper Cable on CF34-3A2 Engines

Mos

Hrs

Enc

74 ENG1Eff: 27-Jul-1994

(NOTE: All CF34-3A2 engines with green jumper cable PN 5085T35P01)

RecommendedRE (-)74-0008 R00 ELECTRICAL SYSTEM - Replacement of the Green Jumper Cable on CF34-3A2 Engines

Mos

Hrs

Enc

74 ENG2Eff: 27-Jul-1994

(NOTE: All CF34-3A2 engines with green jumper cable PN 5085T35P01)

RecommendedRE (-)74-0009 R00 ELECTRICAL SYSTEM - Ignition Exciter Replacement

Mos

Hrs

Enc

74 ENG1Eff: 21-Oct-1994


Generated: 6-Apr-2016 1:16 PM400/429







RecommendedRE (-)74-0009 R00 ELECTRICAL SYSTEM - Ignition Exciter Replacement

Mos

Hrs

Enc

74 ENG2Eff: 21-Oct-1994

OptionalRE (-)74-0010 R00 ELECTRICAL INFORMATION - Upgrade Program for Control Amplifier PN 5071T98P01

Mos

Hrs

Enc

74 ENG1Eff: 29-Apr-1997

OptionalRE (-)74-0010 R00 ELECTRICAL INFORMATION - Upgrade Program for Control Amplifier PN 5071T98P01

Mos

Hrs

Enc

74 ENG2Eff: 29-Apr-1997

Cat. 6 - RecommendedRE (-)74-0015 R00 IGNITION - Electrical System (74-00-00) - Ignition Exciter P/N 9238M66P08 Inspection

Mos

Hrs

Enc

74 ENG1Eff: 21-Apr-2010

Cat. 6 - RecommendedRE (-)74-0015 R00 IGNITION - Electrical System (74-00-00) - Ignition Exciter P/N 9238M66P08 Inspection

Mos

Hrs

Enc

74 ENG2Eff: 21-Apr-2010

Cat. 7 - OptionalRE (-)74-0016 R00 IGNITION - Electrical System (74-00-00) - Introduction of New Ignition Exciter VIN 10-631045-3 (P/N 9238M66P11)

Mos

Hrs

Enc

74 ENG1Eff: 07-Oct-2010


Mos

Hrs

Enc

74 ENG2Eff: 07-Oct-2010


Mos

Hrs

Enc

74 ENG1Eff: 26-Jul-2011


Mos

Hrs

Enc

74 ENG2Eff: 26-Jul-2011

MRB ≈25-Sep-2016RE74-10-11-203 Ignition Exciter - Visual Check

10-Feb-2016Mos

300 Hrs (+40)(12,320.4)-/+4030012,020.4Hrs

6,728Enc

(PKG 300 Eng Hour)

74 ENG2


MRB ≈25-Sep-2016RE74-10-11-203 Ignition Exciter - Visual Check

10-Feb-2016Mos

300 Hrs (+40)(12,437.4)-/+4030012,137.4Hrs

6,769Enc

(PKG 300 Eng Hour)

74 ENG1



Generated: 6-Apr-2016 1:16 PM401/429







MRB ≈25-Sep-2016RE74-10-16-202 Igniter Plug - Inspect Igniter plugs

10-Feb-2016Mos

300 Hrs (+40)(12,437.4)-/+4030012,137.4Hrs

6,769Enc

(PKG 300 Eng Hour)

74 ENG1


MRB ≈25-Sep-2016RE74-10-16-202 Igniter Plug - Inspect Igniter plugs

10-Feb-2016Mos

300 Hrs (+40)(12,320.4)-/+4030012,020.4Hrs

6,728Enc

(PKG 300 Eng Hour)

74 ENG2


AlertRE (-)A601-0131 Modification - Start Relays - Additional Diodes

18-Sep-1985Mos

Hrs

Ldg


▼ 75 - BLEED AIR

RE (O/C)B-Sump Regulator Valve

20-Sep-1983Mos

0Hrs0

0Enc0


UNKNOWN

RE (O/C)B-Sump Vent Regulator Valve

20-Sep-1983Mos

0Hrs

0Enc


RE (O/C)B-Sump Vent Regulator Valve

20-Sep-1983Mos

0Hrs

0Enc



29-Jan-2005Mos

10,580.3Hrs

5,376Enc

75 ENG1601-97097-71767


20-Sep-1983Mos

0Hrs0

0Enc0


UNKNOWN

RE (O/C)Vaiable Geometry Actuator

20-Sep-1983Mos

0Hrs

0Enc


RE (O/C)Vaiable Geometry Actuator

20-Sep-1983Mos

0Hrs

0Enc


RE (O/C)Variable Geometry Actuator

20-Sep-1983Mos

0Hrs

0Enc



Generated: 6-Apr-2016 1:16 PM402/429








20-Sep-1983Mos

0Hrs

0Enc



20-Sep-1983Mos

0Hrs

0Enc



20-Sep-1983Mos

0Hrs

0Enc



20-Sep-1983Mos

0Hrs

0Enc



20-Sep-1983Mos

0Hrs

0Enc


RecommendedRE (-)601-1007 Modification - Cooling - Inlet Guide Vane (IGV) Control

Mos

Hrs

Ldg

75 A/F

RecommendedT (A/R)601-1007 Rev 1 Modification - Cooling - Inlet Guide Vane (IGV) Control

Mos

Hrs

Ldg

75 A/FEff: 18-Dec-1984

RecommendedT (A/R)601-1034 Modification - Engine Bleed Air Duct - Hardware

Mos

Hrs

Ldg

75 A/FEff: 22-Oct-1984

Cat. 6 - RecommendedRE (-)74-0011 R00 IGNITION - Electrical System (74-00-00) - Introduction of Improved W2 Blue Cable Assembly

Mos

Hrs

Enc

75 ENG1Eff: 06-Jun-2001

Cat. 6 - RecommendedRE (-)74-0011 R00 IGNITION - Electrical System (74-00-00) - Introduction of Improved W2 Blue Cable Assembly

Mos

Hrs

Enc

75 ENG2Eff: 06-Jun-2001

RecommendedRE (-)75-0001 R01 AIR SYSTEM - Rework B-Sump Regulator Valve

Mos

Hrs

Enc

75 ENG1Eff: 11-Aug-1995


Generated: 6-Apr-2016 1:16 PM403/429







RecommendedRE (-)75-0001 R01 AIR SYSTEM - Rework B-Sump Regulator Valve

Mos

Hrs

Enc

75 ENG2Eff: 11-Aug-1995

RecommendedRE (-)75-0002 R04 AIR - Introduction of New and Reworked B-Sump Vent Regulator Valves

Mos

Hrs

Enc

75 ENG1Eff: 28-Jun-2000


RecommendedRE (-)75-0002 R04 AIR - Introduction of New and Reworked B-Sump Vent Regulator Valves

Mos

Hrs

Enc

75 ENG2Eff: 28-Jun-2000


RecommendedRE (-)75-0003 R00 ENGINE - Air System - Introduction of Air Tube Spacer PN 3049T28P01

Mos

Hrs

Enc

75 ENG1Eff: 03-Dec-1998

RecommendedRE (-)75-0003 R00 ENGINE - Air System - Introduction of Air Tube Spacer PN 3049T28P01

Mos

Hrs

Enc

75 ENG2Eff: 03-Dec-1998

MRB ≈25-Sep-2016RE75-30-00-201 Variable Geometry Control - Visual Check of VG system, paying particular attention to rod end bushings, actuator shaft bearings, lever arms, feedback cable, actuator

attachment points, turnbuckles, actuator ring and torque shaft forward bearing for migration / Lubricate VG rod end bearings (24 locations)

10-Feb-2016Mos

300 Hrs (+40)(12,320.4)-/+4030012,020.4Hrs

6,728Enc

(PKG 300 Eng Hour)

75 ENG2


MRB ≈25-Sep-2016RE75-30-00-201 Variable Geometry Control - Visual Check of VG system, paying particular attention to rod end bushings, actuator shaft bearings, lever arms, feedback cable, actuator

attachment points, turnbuckles, actuator ring and torque shaft forward bearing for migration / Lubricate VG rod end bearings (24 locations)

10-Feb-2016Mos

300 Hrs (+40)(12,437.4)-/+4030012,137.4Hrs

6,769Enc

(PKG 300 Eng Hour)

75 ENG1


▼ 76 - ENGINE CONTROLS

AWL - Life LimitRE (O/C)Auto-Throttle Retard System Clevis Pin

27-Jan-1987Mos

1,267Hrs

470Ldg

Left76 A/FNOT APPLICABLE

AWL - Life LimitRE (O/C)Auto-Throttle Retard System Clevis Pin

27-Jan-1987Mos

1,267Hrs

470Ldg

Right76 A/FNOT APPLICABLE

RE (O/C)Clevis Assy, Auto-Throttle

20-Sep-1983Mos

0Hrs

0Ldg



Generated: 6-Apr-2016 1:16 PM404/429







RE (O/C)Clevis Assy, Auto-Throttle

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Engine Throttle Quadrant

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Throttle Control Gearbox Assembly

20-Sep-1983Mos

0Hrs

0Ldg


Component Inspection SimpleDUE: 12,035.4 Hrs1. T 1600 Hrs | 2. RA 1600 Hrs | 3. RA 1600 Hrs | 4. RE

1000 HrsThrottle Control Gearbox - Functional Test of the Throttle C...76-10-00-101 *A/F76

RE (O/C)Throttle Control Gearbox Assembly

20-Sep-1983Mos

0Hrs

0Ldg


Component Inspection SimpleDUE: 12,035.4 Hrs1. T 1600 Hrs | 2. RA 1600 Hrs | 3. RA 1600 Hrs | 4. RE

1000 HrsThrottle Control Gearbox - Functional Test of the Throttle C...76-10-00-101 *A/F76

MandatoryRE (-)2009-24-18 Engine controls.

26-Jan-2011Mos

11,460.7Hrs

5,905Ldg

76 A/FFOUND P/C/WEff: 08-Jan-2010 Complied

With

RecommendedRE (-)601-0086 Special Check/Modification - Throttle Quadrant - Anti-Torque Shaft Retention

Mos

Hrs

Ldg

76 A/F

RecommendedRE (-)601-0086 Rev 1 Special Check/Modification - Throttle Quadrant - Anti-Torque Shaft Retention

21-Nov-1984Mos

Hrs

Ldg


RecommendedRE (-)601-0106 Special Check/Replacement - Controlex Cable - Seal Nut

06-Sep-1985Mos

607Hrs

261Ldg


OptionalT (A/R)601-0317 Modification - Controlex Throttle Control Cables - Routing

Mos

Hrs

Ldg

76 A/FEff: 31-Oct-1990

RecommendedRE (-)601-0410 Special Check/Modification - Throttle Quadrant - Inadvertent Shut-off

05-Apr-1994Mos

Hrs

Ldg



Generated: 6-Apr-2016 1:16 PM405/429







RecommendedRE (-)601-0538 Special Check/Modification - Engine Controls - Possible Failure of Engine Throttle Push/Pull Control-Assembly

05-Aug-2003Mos

9,585.6Hrs

4,797Ldg


RecommendedT (A/R)601-0583 Special Check/Modification - Throttle Controls - Inspection/Replacement of the Throttle Gear Box Part No. 2100140-003, 2100140-005 and 2100140-007

Mos

Hrs

Ldg

76 A/FEff: 31-May-2006

RecommendedRE (-)601-1018 Modification - Throttle Controls - Auto-Throttle Retarder System

02-Nov-1992Mos

1,267Hrs

480Ldg

76 A/FComplied With

RecommendedT (A/R)601-1018 Rev 1 Modification - Throttle Controls - Auto-Throttle Retarder System

Mos

Hrs

Ldg

76 A/FEff: 24-Aug-1984

RecommendedRE (-)601-1020 Modification - Throttle Controls - Replacement of Throttle Rod End Assemblies

Mos

Hrs

Ldg

76 A/F

RecommendedT (A/R)601-1020 Rev 1 Modification - Throttle Controls - Replacement of Throttle Rod End Assemblies

Mos

Hrs

Ldg

76 A/FEff: 09-Apr-1984

RecommendedRE (-)601-1044 Modification - ATR Control - Clevis Assembly

16-Jul-1986Mos

952Hrs

403Ldg


RecommendedRE (-)601-1054 Special Check/Modification - Throttle Controls - Auto Throttle Retarder Cable Assembly

02-May-1988Mos

1,995Hrs

756Ldg


RecommendedRE (-)601-1074 Special Check/Modification - Controlex Cable - Tang Wear and Spiral Wrap Addition

20-Nov-2000Mos

Hrs

Ldg


OptionalT (A/R)601-1076 Throttle Control Rod Assembly - Adjustment Facility

Mos

Hrs

Ldg

76 A/FEff: 18-Mar-1991

AWL ≈06-Feb-2016RE76-10-00-101 * Throttle Control Gearbox - Functional Test of the Throttle Control Gearbox Assembly Part Numbers 2100140-003/-005/-007

22-Mar-2007Mos

OVD12,035.41,00011,035.4Hrs

Ldg




Generated: 6-Apr-2016 1:16 PM406/429







AWL ≈06-Feb-2016RE76-10-00-101 * Throttle Control Gearbox - Functional Test of the Throttle Control Gearbox Assembly Part Numbers 2100140-003/-005/-007

22-Mar-2007Mos

OVD12,035.41,00011,035.4Hrs

Ldg



MandatoryRE (-)95-03-06 Engine Throttle Quadrant

28-Apr-1995Mos

4,555Hrs

1,824Ldg

76 A/FSI 601-0410Eff: 31-Mar-1995 Complied

With

Compliance Share DoubleDUE:1. T A/R | 2. RE -Special Check/Modification - Throttle Quadrant - Inadvertent...601-0410A/F76

Compliance Share DoubleDUE:1. T A/R | 2. RE -Special Check/Modification - Throttle Quadrant - Idle Stop P...A601-0374 Rev 1A/F76

RecommendedRE (-)A601-0374 Special Check/Modification - Throttle Quadrant - Idle Stop Pawl

Mos

Hrs

Ldg

76 A/F

RecommendedRE (-)A601-0374 Rev 1 Special Check/Modification - Throttle Quadrant - Idle Stop Pawl

31-Oct-1993Mos

Hrs

Ldg


▼ 77 - ENGINE INDICATING

RE (O/C)Engine Apr Control Amplifier

31-May-2005Mos

10,956Hrs

5,990Enc

77 ENG14074T27G01UNKNOWN

RE (O/C)Engine Apr Control Amplifier

20-Sep-1983Mos

0Hrs

0Enc


RE (O/C)Engine Instrument Control Panel

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Engine Vibration Accelerometer

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Engine Vibration Accelerometer

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Engine Vibration Indicator

20-Sep-1983Mos

0Hrs0

0Ldg0

77 A/FNew124-497-1

UNKNOWN


Generated: 6-Apr-2016 1:16 PM407/429







RE (O/C)Engine Vibration Monitor

18-Oct-2003Mos

9,808.2Hrs

4,927Ldg

77 A/F6632M1438718

RE (O/C)Inlet Turbine Temperature Indicator

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)N1 Fan Rpm Indicator

21-Aug-2004Mos

10,458.3Hrs

5,306Ldg

77 A/F418-098-119776

RE (O/C)N2 Speed Sensor

20-Sep-1983Mos

0Hrs

0Enc


RE (O/C)N2 Speed Sensor(Right)

24-Feb-2003Mos

9,253.9Hrs9,253.9

4,606Enc4,606

77 ENG2418-098-12829

RE (O/C)N2 Turbine Rpm Indicator

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Signal Data Converter

20-Sep-1983Mos

0Hrs

0Ldg


RecommendedRE (-)601-0057 Modification - Engine Vibration Monitoring System - Shield Ground

26-Jan-1987Mos

1,267Hrs

470Ldg


OptionalRE (-)601-0238 Modification – Inter Turbine Temperature Indicating – Use of CF34-3A Engines at -3A Power Settings on CL-601 Aircraft

26-Aug-2002Mos

8,743.6Hrs

4,289Ldg


▼ 78 - EXHAUST

AWL - Life Limit ≈04-Aug-2016RE10 O'Clock Actuator Rod End

20-Sep-1983Mos

0Hrs0

174 Ldg6,5006,5000Ldg0


UNKNOWN

(NOTE: Note: For P/N 3236757-1 applicable only if ever operated with PDI P/N 126758-3 or lower dash number)


Generated: 6-Apr-2016 1:16 PM408/429








20-Sep-1983Mos

0Hrs0

174 Ldg6,5006,5000Ldg0


UNKNOWN


AWL - Life Limit ≈04-Aug-2016RE10 O'Clock Anti-Rotation Tang

20-Sep-1983Mos

0Hrs0

174 Ldg6,5006,5000Ldg0


UNKNOWN

(NOTE: Note: Applicable only if ever operated with PDI P/N 126758-3 or lower dash number)


20-Sep-1983Mos

0Hrs0

174 Ldg6,5006,5000Ldg0


UNKNOWN



20-Sep-1983Mos

0Hrs0

174 Ldg6,5006,5000Ldg0


UNKNOWN



20-Sep-1983Mos

0Hrs0

174 Ldg6,5006,5000Ldg0


UNKNOWN



20-Sep-1983Mos

0Hrs0

174 Ldg6,5006,5000Ldg0


UNKNOWN



20-Sep-1983Mos

0Hrs0

174 Ldg6,5006,5000Ldg0


UNKNOWN



20-Sep-1983Mos

0Hrs0

174 Ldg6,5006,5000Ldg0


UNKNOWN



20-Sep-1983Mos

0Hrs0

174 Ldg6,5006,5000Ldg0


UNKNOWN



Generated: 6-Apr-2016 1:16 PM409/429







AWL - Life Limit ≈02-Jul-2021RE4 O'Clock Anti-Rotation Tang

30-Sep-2004Mos

4,399Hrs0

1,942 Ldg8,2686,5001,768Ldg0


UNKNOWN



20-Sep-1983Mos

0Hrs0

174 Ldg6,5006,5000Ldg0


UNKNOWN



20-Sep-1983Mos

0Hrs0

174 Ldg6,5006,5000Ldg0


UNKNOWN



20-Sep-1983Mos

0Hrs0

174 Ldg6,5006,5000Ldg0


UNKNOWN



17-May-2013Mos

11,788.8Hrs0

6,317 Ldg12,6436,5006,143Ldg0


UNKNOWN



20-Sep-1983Mos

0Hrs0

174 Ldg6,5006,5000Ldg0


UNKNOWN


AWL - Life Limit ≈24-Dec-2042REBallscrew Actuator

20-Sep-1983Mos

0Hrs0

9,674 Ldg16,00016,0000Ldg0

Left No.178 A/FNew3272570-2

UNKNOWN

(NOTE: Note: With Gimbal (P/N 3235452) and Housing (P/N 3233436) only)


20-Sep-1983Mos

0Hrs0

9,674 Ldg16,00016,0000Ldg0


UNKNOWN



20-Sep-1983Mos

0Hrs0

9,674 Ldg16,00016,0000Ldg0


UNKNOWN



Generated: 6-Apr-2016 1:16 PM410/429








20-Sep-1983Mos

0Hrs0

9,674 Ldg16,00016,0000Ldg0


UNKNOWN



20-Sep-1983Mos

0Hrs0

9,674 Ldg16,00016,0000Ldg0

Right No.178 A/FNew3272570-2

UNKNOWN



20-Sep-1983Mos

0Hrs0

9,674 Ldg16,00016,0000Ldg0


UNKNOWN


AWL - Life Limit ≈27-Feb-2050REBallscrew Actuator

27-Feb-1999Mos

5,912Hrs0

12,258 Ldg18,58416,0002,584Ldg0


UNKNOWN


AWL - Life Limit ≈01-May-2054REBallscrew Actuator

11-May-2002Mos

8,425.9Hrs0

13,761 Ldg20,08716,0004,087Ldg0


UNKNOWN


RE (O/C)Stow Thrust Reverser Switch

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Stow Thrust Reverser Switch

20-Sep-1983Mos

0Hrs

0Ldg


AWL - Life LimitRE (O/C)T/R Latch Interlock Fittings

20-Sep-1983Mos

0Hrs0

0Ldg0

Left78 A/FNew228-50790-113

NOT APPLICABLE

(NOTE: N/A per report furnished)

AWL - Life LimitRE (O/C)T/R Latch Interlock Fittings

20-Sep-1983Mos

0Hrs0

0Ldg0

Right78 A/FNew228-50790-113

NOT APPLICABLE

RE (O/C)Thrust Reverser (PDU)

20-Sep-1983Mos

0Hrs

0Ldg



Generated: 6-Apr-2016 1:16 PM411/429







RE (O/C)Thrust Reverser (PDU)

12-Sep-2008Mos

11,455.7Hrs

5,898Ldg

No.278 A/F126758-6-2P-188C

RE (O/C)Thrust Reverser Interlock Fittings

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Thrust Reverser Interlock Fittings

20-Sep-1983Mos

0Hrs

0Ldg


RecommendedRE (-)601-0045 Modification - Thrust Reverser - Anti-Ice/Wheel Spin-up

Mos

Hrs

Ldg

78 A/F

RecommendedRE (-)601-0045 Rev 1 Modification - Thrust Reverser - Anti-Ice/Wheel Spin-up

Mos

Hrs

Ldg

78 A/FEff: 23-Apr-1984

RecommendedRE (-)601-0046 Modification - Thrust Reverser - Activation

Mos

Hrs

Ldg

78 A/F

RecommendedT (A/R)601-0046 Rev 1 Modification - Thrust Reverser - Activation

Mos

Hrs

Ldg

78 A/FEff: 10-Jul-1984

RecommendedRE (-)601-0047 Modification - 14th Stage Bleed Air - Control System

Mos

Hrs

Ldg

78 A/F

RecommendedRE (-)601-0047 Rev 1 Modification - 14th Stage Bleed Air - Control System

Mos

Hrs

Ldg

78 A/FEff: 05-Jun-1984

RecommendedRE (-)601-0050 Modification - Thrust Reverser - EMI Suppression

Mos

Hrs

Ldg

78 A/F

RecommendedRE (-)601-0050 Rev 1 Modification - Thrust Reverser - EMI Suppression

Mos

Hrs

Ldg

78 A/FEff: 09-Apr-1984


Generated: 6-Apr-2016 1:16 PM412/429







OptionalRE (-)601-0400 Modification - Thrust Reverser - Prevent Power Interruption and Relocate Stow and Throttle Lockout Microswitches

Mos

Hrs

Ldg

78 A/F

OptionalT (A/R)601-0400 Rev 1 Modification - Thrust Reverser - Prevent Power Interruption and Relocate Stow and Throttle Lockout Microswitches

Mos

Hrs

Ldg

78 A/FEff: 29-Feb-2000

OptionalRE (-)601-0409 Modification - Thrust Reverser Unlocked Annunciation Wiring Change

Mos

Hrs

Ldg

78 A/FEff: 15-May-1995

OptionalT (A/R)601-0578 Modification - Thrust Reverser - Replacement of PDU Engine Nose Cowl Internal Pockets

Mos

Hrs

Ldg

78 A/FEff: 30-Jan-2007

Recommended ≈05-Jan-2022T (A/R)601-0582 Modification - Exhaust Nozzle Assembly - Replacement of the Exhaust Nozzle and Tail Pipe Attachment Bolts

Mos

2,833.8 Hrs[14,875]Hrs

Ldg

78 A/FEff: 28-Aug-2006

RecommendedRE (-)601-1013 Modification - Thrust Reverser - Stowed and Throttle Lockout Microswitches

Mos

Hrs

Ldg

78 A/F

RecommendedRE (-)601-1013 Rev 1 Modification - Thrust Reverser - Stowed and Throttle Lockout Microswitches

07-Aug-1985Mos

Hrs

Ldg


RecommendedRE (-)601-1015 Modification - Thrust Reverser - Blocker Door Numbers 8 and 9

Mos

Hrs

Ldg

78 A/F

RecommendedRE (-)601-1015 Rev 1 Modification - Thrust Reverser - Blocker Door Numbers 8 and 9

26-Jan-1987Mos

1,267Hrs

480Ldg


RecommendedRE (-)601-1017 Modification - Thrust Reverser - Upper Pylon Cascade and Upper Center Cascade

Mos

Hrs

Ldg

78 A/F

RecommendedT (A/R)601-1017 Rev 1 Modification - Thrust Reverser - Upper Pylon Cascade and Upper Center Cascade

Mos

Hrs

Ldg

78 A/FEff: 09-Apr-1984


Generated: 6-Apr-2016 1:16 PM413/429







RecommendedRE (-)601-1019 Modification - Thrust Reverser - Power Drive Unit Actuator

Mos

Hrs

Ldg

78 A/F

RecommendedT (A/R)601-1019 Rev 1 Modification - Thrust Reverser - Power Drive Unit Actuator

Mos

Hrs

Ldg

78 A/FEff: 07-Jun-1984

RecommendedRE (-)601-1021 Modification - Thrust Reverser - Systems

Mos

Hrs

Ldg

78 A/F

RecommendedT (A/R)601-1021 Rev 1 Modification - Thrust Reverser - Systems

Mos

Hrs

Ldg

78 A/FEff: 02-Apr-1984

RecommendedRE (-)601-1023 Modification - Thrust Reverser - Air Tube Installation

Mos

Hrs

Ldg

78 A/F

RecommendedT (A/R)601-1023 Rev 1 Modification - Thrust Reverser - Air Tube Installation

Mos

Hrs

Ldg

78 A/FEff: 18-May-1984

RecommendedRE (-)601-1024 Modification - Thrust Reverser - Replacement of Interlock Latch Fittings

Mos

Hrs

Ldg

78 A/F

RecommendedRE (-)601-1024 Rev 1 Modification - Thrust Reverser - Replacement of Interlock Latch Fittings

18-Sep-1985Mos

607Hrs

261Ldg


RecommendedRE (-)601-1026 Modification - Thrust Reverser - Replacement of Blocker Door Stops and Bumpers

21-Mar-1991Mos

3,182Hrs

1,266Ldg

78 A/FComplied With

RecommendedRE (-)601-1026 Rev 1 Modification - Thrust Reverser - Replacement of Blocker Door Stops and Bumpers

Mos

Hrs

Ldg

78 A/F

RecommendedRE (-)601-1026 Rev 2 Modification - Thrust Reverser - Replacement of Blocker Door Stops and Bumpers

Mos

Hrs

Ldg

78 A/F


Generated: 6-Apr-2016 1:16 PM414/429







RecommendedT (A/R)601-1026 Rev 3 Modification - Thrust Reverser - Replacement of Blocker Door Stops and Bumpers

Mos

Hrs

Ldg

78 A/FEff: 04-Feb-1986

RecommendedRE (-)601-1038 Modification - Thrust Reverser Diverter Fairing - Addition of Drain Hole

02-May-1988Mos

1,995Hrs

756Ldg


RecommendedRE (-)601-1042 Special Check/Replacement - Thrust Reverser - Blocker Doors

Mos

Hrs

Ldg

78 A/F

RecommendedRE (-)601-1042 Rev 1 Special Check/Replacement - Thrust Reverser - Blocker Doors

02-May-1988Mos

1,995Hrs

756Ldg


RecommendedRE (-)601-1056 Modification - Exhaust Nozzle Fairing - Installation of New Bolts and Bushings

13-Oct-1992Mos

3,754Hrs

1,519Ldg


RecommendedRE (-)601-1057 Modification - Thrust Reverser Main Tracks - Slider Block Assemblies

Mos

Hrs

Ldg

78 A/F

RecommendedRE (-)601-1057 Rev 1 Modification - Thrust Reverser Main Tracks - Slider Block Assemblies

Mos

Hrs

Ldg

78 A/F

RecommendedRE (-)601-1057 Rev 2 Modification - Thrust Reverser Main Tracks - Slider Block Assemblies

23-Mar-1992Mos

3,584Hrs

1,446Ldg


RecommendedRE (-)601-1058 Modification - Thrust Reverser - Deploy Microswitch Target

Mos

Hrs

Ldg

78 A/F

RecommendedRE (-)601-1058 Rev 1 Modification - Thrust Reverser - Deploy Microswitch Target

Mos

Hrs

Ldg

78 A/F

RecommendedRE (-)601-1058 Rev 2 Modification - Thrust Reverser - Deploy Microswitch Target

23-Mar-1992Mos

3,584Hrs

1,446Ldg



Generated: 6-Apr-2016 1:16 PM415/429







RecommendedRE (-)601-1061 Modification - Thrust Reverser Blocker Doors - Improved Retention

Mos

Hrs

Ldg

78 A/F

RecommendedRE (-)601-1061 Rev 1 Modification - Thrust Reverser Blocker Doors - Improved Retention

25-Mar-1991Mos

3,182Hrs

1,266Ldg


RecommendedRE (-)601-1065 Modification - Auto-Throttle Retarder Control - Cable Protection

23-Feb-1990Mos

2,687Hrs

1,034Ldg


RecommendedRE (-)601-1066 Modification - Thrust Reverser Torque Box - DrainageThrust Reverser Torque Box - Drainage

Mos

Hrs

Ldg

78 A/F

RecommendedRE (-)601-1066 Rev 1 Modification - Thrust Reverser Torque Box - DrainageThrust Reverser Torque Box - Drainage

21-Feb-1991Mos

3,142Hrs

1,250Ldg


RecommendedRE (-)601-1069 Modification - Thrust Reverser - Introduction of -6 PDU

Mos

Hrs

Ldg

78 A/F

RecommendedT (A/R)601-1069 Rev 1 Modification - Thrust Reverser - Introduction of -6 PDU

Mos

Hrs

Ldg

78 A/FEff: 10-Jan-1990

RecommendedRE (-)601-1070 Special Check/Modification/Rework - Thrust Reverser - Upper Pylon Cascades

25-Mar-1991Mos

3,182Hrs

1,266Ldg

78 A/F2BEff: 31-Aug-1990 Complied

With

RecommendedRE (-)601-1071 Rework -Thrust Reverser - Interlocking Latch Fitting Attach Rivets

Mos

Hrs

Ldg

78 A/F

RecommendedRE (-)601-1071 Rev 1 Rework -Thrust Reverser - Interlocking Latch Fitting Attach Rivets

Mos

Hrs

Ldg

78 A/FEff: 15-Apr-1993

OptionalT (A/R)601-1073 Modification - Thrust Reverser - No. 7 Blocker Door Link Housing Replacement

Mos

Hrs

Ldg

78 A/FEff: 06-Mar-1991


Generated: 6-Apr-2016 1:16 PM416/429







OptionalT (A/R)601-1075 Modification - Thrust Reverser - Blocker Door Link Housing Covers

Mos

Hrs

Ldg

78 A/FEff: 30-Apr-1990

RecommendedRE (-)601-1079 Special Check/Modification - Thrust Reverser - Pneumatic Drive Unit Flexshaft Bolts

21-Feb-1991Mos

3,142Hrs

1,250Ldg


RecommendedRE (-)601-1084 Special Check/Modification - Thrust Reverser - Blocker Doors and Sound Attenuating Material (SAM) Panels

Mos

Hrs

Ldg

78 A/F

RecommendedRE (-)601-1084 Rev 1 Special Check/Modification - Thrust Reverser - Blocker Doors and Sound Attenuating Material (SAM) Panels

26-Jan-1996Mos

4,785Hrs

1,932Ldg


OptionalRE (-)601-1089 Modification - Translating Cowl Doors Support Struts - Addition of Dampening Pad and Retention Bracket

Mos

Hrs

Ldg

78 A/F

OptionalT (A/R)601-1089 Rev 1 Modification - Translating Cowl Doors Support Struts - Addition of Dampening Pad and Retention Bracket

Mos

Hrs

Ldg

78 A/FEff: 15-Apr-1997

OptionalT (A/R)601-1094 Modification - Thrust Reverser Main Track - Repl Eccentric Bushings With Concentric

Mos

Hrs

Ldg

78 A/FEff: 28-Nov-1997

RecommendedRE (-)601-1100 Special Check/Rework - Thrust Reverser - Examine Condition of Actuator Attachment Fittings

Mos

Hrs

Ldg

78 A/F

RecommendedT (A/R)601-1100 Rev 1 Special Check/Rework - Thrust Reverser - Examine Condition of Actuator Attachment Fittings

Mos

Hrs

Ldg

78 A/FEff: 19-Oct-2001

MRB ≈20-Oct-2017RE78-10-00-211 (Left) Exhaust Nozzle Assembly Remove exhaust nozzle fairing and carry out a visual check off airing, nozzle, stiffeners, attachment links and brackets. Reinstall fairing

29-Oct-2012Mos

812.3 Hrs (+40)(12,853.5)-/+401,20011,653.5Hrs

Ldg

(PKG 1200 Hour)

78 A/F


MRB ≈20-Oct-2017RE78-10-00-211 (Right) Exhaust Nozzle Assembly Remove exhaust nozzle fairing and carry out a visual check off airing, nozzle, stiffeners, attachment links and brackets. Reinstall fairing

29-Oct-2012Mos

812.3 Hrs (+40)(12,853.5)-/+401,20011,653.5Hrs

Ldg

(PKG 1200 Hour)

78 A/F



Generated: 6-Apr-2016 1:16 PM417/429







AWL ≈23-May-2017RE78-30-00-101 * (Left) Thrust Reverser - Main Track - Aft Lugs - NDT Check

20-May-2009Mos

617.4 Hrs12,658.61,20011,458.6Hrs

Ldg

78 A/F

Ref.:PSP 612 Part 6 ET-78-30-01 (SOURCE: TLMC 05-10-30) (NOTE: With PDU Part Number 126758-3 Installed)

AWL ≈23-May-2017RE78-30-00-101 * (Right) Thrust Reverser - Main Track - Aft Lugs - NDT Check

20-May-2009Mos

617.4 Hrs12,658.61,20011,458.6Hrs

Ldg

78 A/F


AWL ≈24-Aug-2023RE78-30-00-102 * (Left) Thrust Reverser - Main Upper and Lower Pylon Tracks - NDT Check

08-Aug-2005Mos

3,618.6 Hrs15,659.84,80010,859.8Hrs

Ldg

78 A/F


AWL ≈24-Aug-2023RE78-30-00-102 * (Right) Thrust Reverser - Main Upper and Lower Pylon Tracks - NDT Check

08-Aug-2005Mos

3,618.6 Hrs15,659.84,80010,859.8Hrs

Ldg

78 A/F


AWL ≈23-Jul-2016RE78-30-00-103 * (Left) Thrust Reverser - Main Track Attachment Fittings - NDT Check

22-Jul-2004Mos

217.1 Hrs12,258.31,80010,458.3Hrs

Ldg

78 A/F


AWL ≈23-Jul-2016RE78-30-00-103 * (Right) Thrust Reverser - Main Track Attachment Fittings - NDT Check

22-Jul-2004Mos

217.1 Hrs12,258.31,80010,458.3Hrs

Ldg

78 A/F


AWL ≈06-Jul-2018RE78-30-00-104 * (Left) Thrust Reverser - Main Tracks - Lower Flange - NDT Check

21-Apr-2000Mos

1,155.2 Hrs13,196.46,6006,596.4Hrs

Ldg

78 A/F


AWL ≈06-Jul-2018RE78-30-00-104 * (Right) Thrust Reverser - Main Tracks - Lower Flange - NDT Check

21-Apr-2000Mos

1,155.2 Hrs13,196.46,6006,596.4Hrs

Ldg

78 A/F


AWL ≈17-Oct-2020RE78-30-00-105 * (Left) Thrust Reverser - Service Pylon Support Rail - NDT Check

14-Nov-2000Mos

2,248.7 Hrs14,289.97,2007,089.9Hrs

Ldg

78 A/F


AWL ≈17-Oct-2020RE78-30-00-105 * (Right) Thrust Reverser - Service Pylon Support Rail - NDT Check

14-Nov-2000Mos

2,248.7 Hrs14,289.97,2007,089.9Hrs

Ldg

78 A/F


AWL ≈09-Apr-2022T78-30-00-106 * (Left) Service Pylon - Upper and Lower Pylon Track Support Bed - Visual Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

78 A/F



Generated: 6-Apr-2016 1:16 PM418/429







AWL ≈09-Apr-2022T78-30-00-106 * (Right) Service Pylon - Upper and Lower Pylon Track Support Bed - Visual Check

Mos

2,958.8 Hrs15,00015,000Hrs

Ldg

78 A/F


MRB ≈20-Oct-2017RE78-30-00-202 (Left) Thrust Reverser Functional Test of auto stow system

29-Oct-2012Mos

812.3 Hrs (+40)(12,853.5)-/+401,20011,653.5Hrs

Ldg

(PKG 1200 Hour)

78 A/F


MRB ≈20-Oct-2017RE78-30-00-202 (Right) Thrust Reverser Functional Test of auto stow system

29-Oct-2012Mos

812.3 Hrs (+40)(12,853.5)-/+401,20011,653.5Hrs

Ldg

(PKG 1200 Hour)

78 A/F


MRB ≈18-Sep-2016RE78-30-00-208 Thrust Reverser With thrust reversers manually deployed, visual check of blockerdoors, actuators, links and hinges - With thrust reversers stowed, carry out a visual

check to ensure that blocker doors are closed and faired

10-Feb-2016Mos

290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs

6,326Ldg

(PKG 300 Hour)

78 A/F


MRB ≈08-May-2018RE78-30-00-212 Thrust Reverser General Visual Check of the torque box, torque box molded seal,fittings, inner and outer skin panels, rib assemblies, ringsegments and attaching

cascades

05-Apr-2005Mos

1,076.8 Hrs (+40)13,118-/+402,40010,718Hrs

Ldg

(PKG 2400 Hour)

78 A/F


MRB ≈13-Jul-2017RE78-30-00-215 Thrust Reverser Thrust Reverser Warning Circuit Functional Test

04-May-2004Mos

684 Hrs (+30)(12,725.2)-/+402,40010,325.2Hrs

Ldg

(PKG 2400 Hour)

78 A/F


MRB ≈20-Oct-2017RE78-30-00-216 (Left) Thrust Reverser Thrust Reverser Unlocked Light Functional Test

29-Oct-2012Mos

812.3 Hrs (+40)(12,853.5)-/+401,20011,653.5Hrs

Ldg

(PKG 1200 Hour)

78 A/F


MRB ≈20-Oct-2017RE78-30-00-216 (Right) Thrust Reverser Thrust Reverser Unlocked Light Functional Test

29-Oct-2012Mos

812.3 Hrs (+40)(12,853.5)-/+401,20011,653.5Hrs

Ldg

(PKG 1200 Hour)

78 A/F


MRB ≈03-May-2017RE78-30-00-218 Ballscrew Actuators Lubrication of Ballscrew Actuators and Mounts

10-Feb-2016Mos

590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs

6,326Ldg

(PKG 600 Hour)

78 A/F


≈09-Apr-2022RE78-30-00-403 T/R MAIN TRACK UPPER FLANGE NDT

20-Sep-1983Mos

2,958.8 Hrs15,00015,0000Hrs

Ldg

78 A/F


Generated: 6-Apr-2016 1:16 PM419/429







≈06-Jun-2016RE78-30-00-407 T/R MAIN TRACK ACT FIT ATT HOLE NDT

07-Jun-2004Mos

155 Hrs12,196.21,80010,396.2Hrs

Ldg

78 A/F

MRB ≈03-May-2017RE78-30-11-209 Cascades/Pylon Tracks Visual Check

10-Feb-2016Mos

590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs

6,326Ldg

(PKG 600 Hour)

78 A/F


MRB ≈18-Sep-2016RE78-30-16-219 Thrust Reverser (Pre SB 601-1084) Detailed Inspection of the 6 o’clock SAM Panel and Underlying Brackets

10-Feb-2016Mos

290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs

6,326Ldg

(PKG 300 Hour)

78 A/F


MRB ≈08-May-2018RE78-30-26-204 Blocker Doors Special Detailed Inspection of Blocker Door Bushings

05-Apr-2005Mos

1,076.8 Hrs (+40)13,118-/+402,40010,718Hrs

Ldg

(PKG 2400 Hour)

78 A/F


MRB ≈03-May-2017RE78-30-31-210 Main Tracks Visual Check of the main track and attachments

10-Feb-2016Mos

590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs

6,326Ldg

(PKG 600 Hour)

78 A/F


MRB ≈20-Oct-2017RE78-30-41-201 (Left) Main and Pylon Track Slider Blocks Detailed Inspection of slider block

29-Oct-2012Mos

812.3 Hrs (+40)(12,853.5)-/+401,20011,653.5Hrs

Ldg

(PKG 1200 Hour)

78 A/F


MRB ≈20-Oct-2017RE78-30-41-201 (Right) Main and Pylon Track Slider Blocks Detailed Inspection of slider block

29-Oct-2012Mos

812.3 Hrs (+40)(12,853.5)-/+401,20011,653.5Hrs

Ldg

(PKG 1200 Hour)

78 A/F


MRB ≈03-May-2017RE78-30-46-206 Pneumatic Drive/Flexshaft Lock Unit (Pre Allied Signal SB 126758-78-1487) - Remove filter from flexshaft lock, check and reinstall

10-Feb-2016Mos

590.8 Hrs (+40)12,611.2-/+4060012,020.4Hrs

6,728Enc

(PKG 600 Eng Hour)

78 ENG2

(Tol. Adjustment: -9.2 Hrs) (SOURCE: TLMC 05-20-15) (NOTE: (Pre Allied Signal SB 126758-78-1487))

MRB ≈03-May-2017RE78-30-46-206 Pneumatic Drive/Flexshaft Lock Unit (Pre Allied Signal SB 126758-78-1487) - Remove filter from flexshaft lock, check and reinstall

10-Feb-2016Mos

590.8 Hrs (+40)12,728.2-/+4060012,137.4Hrs

6,769Enc

(PKG 600 Eng Hour)

78 ENG1

(Tol. Adjustment: -9.2 Hrs) (SOURCE: TLMC 05-20-15) (NOTE: (Pre Allied Signal SB 126758-78-1487))

MRB ≈08-May-2018RE78-30-51-217 Flexshafts Special Detailed Inspection of Flexshaft

05-Apr-2005Mos

1,076.8 Hrs (+40)13,118-/+402,40010,718Hrs

Ldg

(PKG 2400 Hour)

78 A/F


MRB ≈08-May-2018RE78-30-56-214 Ballscrew Actuators Inspection Detailed Inspection of Ballscrew Actuator

05-Apr-2005Mos

1,076.8 Hrs (+40)13,118-/+402,40010,718Hrs

Ldg

(PKG 2400 Hour)

78 A/F



Generated: 6-Apr-2016 1:16 PM420/429







MRB ≈20-Oct-2017RE78-30-61-213 (Left) Auto-Throttle Retarder Control Functional Test of Auto-Throttle Retarder and Throttle Lock

29-Oct-2012Mos

812.3 Hrs (+40)(12,853.5)-/+401,20011,653.5Hrs

Ldg

(PKG 1200 Hour)

78 A/F


MRB ≈20-Oct-2017RE78-30-61-213 (Right) Auto-Throttle Retarder Control Functional Test of Auto-Throttle Retarder and Throttle Lock

29-Oct-2012Mos

812.3 Hrs (+40)(12,853.5)-/+401,20011,653.5Hrs

Ldg

(PKG 1200 Hour)

78 A/F


CPCPREC78-00-801 Thrust Reverser - CPCP Check including the following items: (1) Pylon / (2) Pylon track and support rail / (3) Main tracks with attachment fitiings

5.8 Months (+30

Days)(26-Sep-2016)-/+16026-Sep-2011Mos

Hrs

Ldg

(PKG 60 Month)

78 A/F


▼ 79 - OIL

RE (O/C)A-Sump Scavenge Pump

27-Jun-2005Mos

10,839Hrs

5,949Enc

79 ENG24018T11P02LJA39980

RE (O/C)A-Sump Scavenge Pump

20-Sep-1983Mos

0Hrs0

0Enc0


LJA11682

RE (O/C)Engine Oil Filter

04-May-2004Mos

10,325.2Hrs

5,223Enc

79 ENG24012373-81282063649

RE (O/C)Engine Oil Filter

20-Sep-1983Mos

0Hrs

0Enc


RE (O/C)Engine Oil Level Control

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Engine Oil Pressure Switch

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Engine Oil Pressure Switch

20-Sep-1983Mos

0Hrs

0Ldg



Generated: 6-Apr-2016 1:16 PM421/429







RE (O/C)Engine Oil Pressure Transducer

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Engine Oil Pressure Transducer

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Lube & Scavenge Pump

15-Sep-2007Mos

11,073.6Hrs

6,114Enc

79 ENG24022T27G22NMAA0807

RE (O/C)Lube & Scavenge Pump

31-May-2005Mos

10,956Hrs10,956

5,990Enc5,990


NMAA0611

RE (O/C)Lubricating System Pump

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Oil Cooler

27-Jun-2005Mos

10,839Hrs10,839

5,949Enc5,949


AEY02609

RE (O/C)Oil Cooler

31-May-2005Mos

10,956Hrs10,956

5,990Enc5,990


AEY02491

RE (O/C)Oil Filter Bypass Sensor

20-Sep-1983Mos

0Hrs

0Enc



20-Sep-1983Mos

0Hrs

0Enc



20-Sep-1983Mos

0Hrs0

0Ldg0

Left79 A/FNew4060T64P01

UNKNOWN


20-Sep-1983Mos

0Hrs0

0Ldg0

Right79 A/FNew4060T64P01

UNKNOWN


Generated: 6-Apr-2016 1:16 PM422/429







RE (O/C)Oil Level Probe

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Oil Level Probe

20-Sep-1983Mos

0Hrs0

0Ldg0

Right79 A/FNew20016-0000-01

UNKNOWN

RE (O/C)Oil Pressure Indicator

02-Oct-2002Mos

8,878.7Hrs

4,374Ldg

79 A/F601-50915-1663

RE (O/C)Oil Tank

20-Sep-1983Mos

0Hrs

0Enc


RE (O/C)Oil Tank

20-Sep-1983Mos

0Hrs

0Enc


RE (O/C)Oil Temperature Indicator

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Selector - Oil Repl System Valve

14-Nov-2006Mos

10,923.5Hrs

5,578Ldg

79 A/FP194-39505-1209177

OptionalT (A/R)601-0639 Modification - Indicating - Add an On/Off Power Switch for the Engine Oil Indicating Board in Junction Box JB4

Mos

Hrs

Ldg

79 A/FEff: 15-Sep-2014

RecommendedRE (-)601-1098 Modification - Oil Storage - Replacement of Oil Tank Support Beams

30-Oct-1998Mos

Hrs

Ldg

79 A/FSB 79-9Eff: 30-Oct-1998 Complied

With

Cat. 7 - OptionalRE (-)75-0004 R00 AIR - Air System (75-00-00) - Introduction of New T2 Sensor Anti-icing Air Tube

Mos

Hrs

Enc

79 ENG1Eff: 07-Mar-2000

Cat. 7 - OptionalRE (-)75-0004 R00 AIR - Air System (75-00-00) - Introduction of New T2 Sensor Anti-icing Air Tube

Mos

Hrs

Enc

79 ENG2Eff: 07-Mar-2000


Generated: 6-Apr-2016 1:16 PM423/429







RecommendedT (A/R)79-0002 R00 OIL SYSTEM - Increased Capacity C-sump Scavenge Lines

Mos

Hrs

Enc

79 ENG1Eff: 25-Apr-1991


RecommendedT (A/R)79-0002 R00 OIL SYSTEM - Increased Capacity C-sump Scavenge Lines

Mos

Hrs

Enc

79 ENG2Eff: 25-Apr-1991


RecommendedRE (-)79-0003 R01 OIL SYSTEM - A-Sump Scavenge Pump: Inspection of Drive Coupling (Muff Gear)

Mos

Hrs

Enc

79 ENG1Eff: 06-Nov-1991

RecommendedRE (-)79-0003 R01 OIL SYSTEM - A-Sump Scavenge Pump: Inspection of Drive Coupling (Muff Gear)

Mos

Hrs

Enc

79 ENG2Eff: 06-Nov-1991

RecommendedRE (-)79-0006 R03 OIL SYSTEM - Introduction and Field Installation of Improved Stainless Steel Oil Tank Support Beams

Mos

Hrs

Enc

79 ENG1Eff: 31-Mar-1999


RecommendedRE (-)79-0006 R03 OIL SYSTEM - Introduction and Field Installation of Improved Stainless Steel Oil Tank Support Beams

Mos

Hrs

Enc

79 ENG2Eff: 31-Mar-1999


RecommendedRE (-)79-0007 R01 OIL SYSTEM - Replacement of Lube and Scavenge Pump Spur Gear

Mos

Hrs

Enc

79 ENG1Eff: 16-Dec-1997

RecommendedRE (-)79-0007 R01 OIL SYSTEM - Replacement of Lube and Scavenge Pump Spur Gear

Mos

Hrs

Enc

79 ENG2Eff: 16-Dec-1997

RecommendedRE (-)79-0008 R01 OIL SYSTEM - Introduction of Improved (Non-Coated) Oil Tank on Fielded Engines and New Production Engines, and Elimination of A-sump Scavenge Pump on New

Production Engines

Mos

Hrs

Enc

79 ENG1Eff: 03-Mar-1999


Generated: 6-Apr-2016 1:16 PM424/429







RecommendedRE (-)79-0008 R01 OIL SYSTEM - Introduction of Improved (Non-Coated) Oil Tank on Fielded Engines and New Production Engines, and Elimination of A-sump Scavenge Pump on New

Production Engines

Mos

Hrs

Enc

79 ENG2Eff: 03-Mar-1999

Category 3RE (-)79-0009 R00 OIL SYSTEM Introduction and Field Installation of Improved Stainless Steel Oil Tank Support Beams

Mos

Hrs

Enc

79 ENG1Eff: 31-Jan-2011


Mos

Hrs

Enc

79 ENG2Eff: 31-Jan-2011


Mos

Hrs

Enc

79 ENG1Eff: 14-Apr-1998


Mos

Hrs

Enc

79 ENG2Eff: 14-Apr-1998

Cat. 3 - RecommendedT (A/R)79-0009 R02 OIL SYSTEM - Introduction and Field Installation of Improved Stainless Steel Oil Tank Support Beams

Mos

Hrs

Enc

79 ENG1Eff: 05-Jan-2011


Cat. 3 - RecommendedT (A/R)79-0009 R02 OIL SYSTEM - Introduction and Field Installation of Improved Stainless Steel Oil Tank Support Beams

Mos

Hrs

Enc

79 ENG2Eff: 05-Jan-2011


RecommendedT (A/R)79-0013 R00 OIL - Oil System (79-00-00) - Introduction of Flex-Metal Oil Filter Impending Bypass Hose Assemblies

Mos

Hrs

Enc

79 ENG1Eff: 03-Apr-2001


RecommendedT (A/R)79-0013 R00 OIL - Oil System (79-00-00) - Introduction of Flex-Metal Oil Filter Impending Bypass Hose Assemblies

Mos

Hrs

Enc

79 ENG2Eff: 03-Apr-2001


Cat. 7 - OptionalRE (-)79-0014 R00 OIL - Service Evaluation for Lube and Scavenge Pump Assembly

Mos

Hrs

Enc

79 ENG1Eff: 10-Apr-2001


Generated: 6-Apr-2016 1:16 PM425/429







Cat. 7 - OptionalRE (-)79-0014 R00 OIL - Service Evaluation for Lube and Scavenge Pump Assembly

Mos

Hrs

Enc

79 ENG2Eff: 10-Apr-2001

RecommendedRE (-)79-0016 R00 OIL - Lube and Scavenge Components (79-00-00) - Introduction of Improved Lube and Scavenge Pump Assembly PN 6087T04P06

Mos

Hrs

Enc

79 ENG1Eff: 18-Oct-2001

RecommendedRE (-)79-0016 R00 OIL - Lube and Scavenge Components (79-00-00) - Introduction of Improved Lube and Scavenge Pump Assembly PN 6087T04P06

Mos

Hrs

Enc

79 ENG2Eff: 18-Oct-2001

Cat. 9 - InformationalRE (-)79-0025 R00 Oil - General (79-00-00) - Approved Oils

Mos

Hrs

Enc

79 ENG1Eff: 07-Sep-2007


Mos

Hrs

Enc

79 ENG2Eff: 07-Sep-2007


Mos

Hrs

Enc

79 ENG1Eff: 09-Jul-2010


Mos

Hrs

Enc

79 ENG2Eff: 09-Jul-2010


Mos

Hrs

Enc

79 ENG1Eff: 12-Dec-2011


Mos

Hrs

Enc

79 ENG2Eff: 12-Dec-2011

Cat. 9 - InformationalT (-)79-0025 R03 Oil - General (79-00-00) - Approved Oils

Mos

Hrs

Enc

79 ENG1Eff: 08-May-2012


Mos

Hrs

Enc

79 ENG2Eff: 08-May-2012


Generated: 6-Apr-2016 1:16 PM426/429








Mos

Hrs

Enc

79 ENG1Eff: 01-Dec-2014


Mos

Hrs

Enc

79 ENG2Eff: 01-Dec-2014

Category 9T (A/R)79-0025 R05 Oil - General (79-00-00) - Approved Oils

Mos

Hrs

Enc

79 ENG1Eff: 14-Oct-2015

Category 9T (A/R)79-0025 R05 Oil - General (79-00-00) - Approved Oils

Mos

Hrs

Enc

79 ENG2Eff: 14-Oct-2015

Cat. 6 - RecommendedRE (-)79-0028 R00 OIL - Oil System (79-00-00) - Introduction of Improved Oil Filter Bypass Sensor P/N 4060T64P04

Mos

Hrs

Enc

79 ENG1Eff: 29-Jun-2010

Cat. 6 - RecommendedRE (-)79-0028 R00 OIL - Oil System (79-00-00) - Introduction of Improved Oil Filter Bypass Sensor P/N 4060T64P04

Mos

Hrs

Enc

79 ENG2Eff: 29-Jun-2010

MRB ≈10-May-2017RE79-20-21-203 Oil Filter Assembly - Inspect and install new filter element

10-Feb-2016Mos

600 Hrs (+40)(12,737.4)-/+4060012,137.4Hrs

6,769Enc

(PKG 600 Eng Hour)

79 ENG1


MRB ≈03-May-2017RE79-20-21-203 Oil Filter Assembly - Inspect and install new filter element

10-Feb-2016Mos

590.8 Hrs (+40)(12,611.2)-/+4060012,020.4Hrs

6,728Enc

(PKG 600 Eng Hour)

79 ENG2


Servicing - RecommendedRE (A/R)79-20-21-301 Oil Filter Assembly - Inspect and install new filter element on new or overhauled engine

Mos

Hrs

Enc

79 ENG1

Ref.:G.E. M.M. SEI-580 Section 5-21-00 (ZONE: 410, 420) (ACCESS: 412-AB -AT, 414-AB -AT, 422-AB -AT, 424-AB -AT) (SOURCE: MPD 3.2)

(NOTE: This is a one-time item only for new or overhauled engines. Subsequent servicing is covered by item 79-20-21-203.)

Servicing - RecommendedRE (A/R)79-20-21-301 Oil Filter Assembly - Inspect and install new filter element on new or overhauled engine

Mos

Hrs

Enc

79 ENG2

Ref.:G.E. M.M. SEI-580 Section 5-21-00 (ZONE: 410, 420) (ACCESS: 412-AB -AT, 414-AB -AT, 422-AB -AT, 424-AB -AT) (SOURCE: MPD 3.2)

(NOTE: This is a one-time item only for new or overhauled engines. Subsequent servicing is covered by item 79-20-21-203.)

MRB ≈20-Oct-2017RE79-20-26-208 Oil/Fuel Heat Exchanger Assembly - Visual Check, paying particular attention for chafing of housing from loop clamp on C-Sump aft scavenge hose

29-Oct-2012Mos

812.3 Hrs (+40)(12,949.7)-/+401,20011,749.7Hrs

Enc

(PKG 1200 Eng Hour)

79 ENG1



Generated: 6-Apr-2016 1:16 PM427/429







MRB ≈20-Oct-2017RE79-20-26-208 Oil/Fuel Heat Exchanger Assembly - Visual Check, paying particular attention for chafing of housing from loop clamp on C-Sump aft scavenge hose

29-Oct-2012Mos

812.3 Hrs (+40)(12,832.7)-/+401,20011,632.7Hrs

Enc

(PKG 1200 Eng Hour)

79 ENG2


MRB ≈03-Apr-2016RE79-20-31-201 Chip Detector - Check Chip Detector (5 per engine)

11-Nov-2015Mos

71.6 Hrs12,20910012,109Hrs

Enc

79 ENG1


MRB ≈03-Apr-2016RE79-20-31-201 Chip Detector - Check Chip Detector (5 per engine)

11-Nov-2015Mos

71.6 Hrs12,09210011,992Hrs

Enc

79 ENG2


MRB ≈22-Feb-2021RE79-21-01-202 C-Sump Scavenge Screens - Detailed Inspection

05-Jun-2009Mos

2,417.4 Hrs (+40)(14,554.8)-/+403,00011,554.8Hrs

Enc

(PKG 3000 Eng Hour)

79 ENG1


MRB ≈24-Nov-2019RE79-21-01-202 C-Sump Scavenge Screens - Detailed Inspection

28-Jul-2005Mos

1,818.6 Hrs (+40)(13,839)-/+403,00010,839Hrs

Enc

(PKG 3000 Eng Hour)

79 ENG2


MRB ≈03-May-2017RE79-30-26-204 Oil Filter Impending Bypass Sensor - Functional Test

10-Feb-2016Mos

590.8 Hrs (+40)(12,611.2)-/+4060012,020.4Hrs

6,728Enc

(PKG 600 Eng Hour)

79 ENG2


MRB ≈10-May-2017RE79-30-26-204 Oil Filter Impending Bypass Sensor - Functional Test

10-Feb-2016Mos

600 Hrs (+40)(12,737.4)-/+4060012,137.4Hrs

6,769Enc

(PKG 600 Eng Hour)

79 ENG1


RE (O/C)7930505 Pressure Switch (Oil)

Mos

Hrs

Ldg


▼ 80 - STARTING

RE (O/C)Engine Air Start Valve

20-Sep-1983Mos

0Hrs0

0Ldg0

Left80 A/FNew898930-3-1

UNKNOWN

RE (O/C)Engine Air Start Valve

20-Sep-1983Mos

0Hrs

0Ldg


RE (O/C)Engine Air Starter

20-Sep-1983Mos

0Hrs0

0Ldg0

Left80 A/FNew3505188-7-1

UNKNOWN


Generated: 6-Apr-2016 1:16 PM428/429







RE (O/C)Engine Air Starter

20-Sep-1983Mos

0Hrs

0Ldg


MRB ≈18-Sep-2016RE80-10-11-201 Air Turbine Starter/Air Turbine Starter Replenishing Visual Check - Check Oil level

10-Feb-2016Mos

290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs

6,326Ldg

(PKG 300 Hour)

80 A/F


MRB ≈10-May-2017RE80-10-11-202 (Left) Air Turbine Starter Air Turbine Starter (ATS) Oil change

10-Feb-2016Mos

600 Hrs (+40)12,641.2-/+4060012,041.2Hrs

6,326Ldg

(PKG 600 Hour)

80 A/F


MRB ≈10-May-2017RE80-10-11-202 (Right) Air Turbine Starter Air Turbine Starter (ATS) Oil change

10-Feb-2016Mos

600 Hrs (+40)12,641.2-/+4060012,041.2Hrs

6,326Ldg

(PKG 600 Hour)

80 A/F


MRB ≈03-May-2017RE80-10-11-203 Air Turbine Starter (Part No. 3505188-9 and Subs) - Detailed Inspection of the Drain-Plug Magnetic Chip-Detector

10-Feb-2016Mos

590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs

6,326Ldg

(PKG 600 Hour)

80 A/F



Generated: 6-Apr-2016 1:16 PM429/429

Documents

N213TS STATUS REPORT BOMBARDIER with relations - ASO · 4/6/2016 · Eng 2 CF34-3A 350107 10-Feb-2016 12020.4 Hrs 6728 Enc Eng 1 CF34-3A 350101 10-Feb-2016 12137.4 Hrs 6769 Enc Airframe