Maintenance Inspections 10.pdf · 05nr08 renewal of insurance certificate mth 12 29-sep-2019 -1 d over due 05nr09 renewal of aircraft radio licence mth 18-oct-2018 120 mth 28-sep-2018

0:0225-Sep-2019125:48AIR COND

0:2825-Sep-2019265324:25ENG 2

0:2825-Sep-2019265324:25ENG 1

0:2825-Sep-2019265324:25AIRCRAFT

Average DailyUtilization

Last ActualDate

Events/LandingsHoursTracking Rate

HB-VTBReg No:

30-Sep-2019 5:15AM

23-Jun-2017

Owner: TC AVIATION AG

Print Date:

Airworthiness:

Aircraft Serial:

Aircraft Model: CITATION M2

Unit:

525-0947

CESCOM 10 - Aircraft Status Report

(ENG) DUE 2

(ENG) DUE 1

Maintenance Inspections

City Part Serial No

Part Number C/W Time 1

C/W Time 2 + or -

Adj. TBO 1

TBO 2 TSO 2

TSO 1

Remains

RemainsDescription

Drawing # / Task #Position

Item Code

Mod Lvl

MTH 18-Oct-2018 -E1

E063-180921 REVIEW FJ44-1AP LMM REV 39

MTH 18-Oct-2018 -E2


MTH 14-Jan-2019 -E1


MTH 14-Jan-2019 -E2


MTH 01-Apr-2019 -E1


MTH 01-Apr-2019 -E2


MTH 06-Aug-2019 -E1


MTH 06-Aug-2019 -E2


MTH 23-Jun-2017 O/C055001 ACCOMPLISH CHECK HARD/OVERWEIGHT LANDINGS

MTH 23-Jun-2017 O/C055002 ACCOMPLISH CHECK OVERSPEED

MTH 23-Jun-2017 O/C

055003 ACCOMPLISH CHECK SEVERE AIR TURBULANCE OR SEVERE MANEUVERS

MTH 23-Jun-2017 O/C055004 ACCOMPLISH CHECK LIGHTING STRIKE

MTH 23-Jun-2017 O/C055005 ACCOMPLISH CHECK FOREIGN OBJECT DAMAGE

MTH 23-Jun-2017 O/C

055006 ACCOMPLISH CHECK TOWING WITH A LARGE FUEL UNBALANCE OR HIGH DRAG/SIDE LOADS DUE TO GROUND HANDLING

LDG

HRS

MTH

215

267:04

19-Jun-2019 6 31-Dec-2019 3 m 0 d

05CPCP01

LSZH

PERFORM SPEED BRAKE COVE AREA CORROSION INSPECTION IAW. CIL-99-03 (CPCP)

LDG

HRS

MTH

215

267:04

19-Jun-2019 6 31-Dec-2019 3 m 0 d

05CPCP02

LSZH

PERFORM FLAP COVE AREA CORROSION INSPECTION IAW. CIL-99-03 (CPCP)

LDG

HRS

MTH

215

267:04

19-Jun-2019 6 31-Dec-2019 3 m 0 d

05CPCP03

LSZH

PERFORM RUDDER COVE AREA CORROSION INSPECTION IAW. CIL-99-03 (CPCP)

LDG

HRS

MTH

215

267:04

19-Jun-2019 6 31-Dec-2019 3 m 0 d

05CPCP04

LSZH

PERFORM ELEVATOR COVE AREA CORROSION INSPECTION IAW. CIL-99-03 (CPCP)

LDG

HRS

MTH

251

303:19

27-Sep-2019 36 27-Sep-2022 35 m 27 d

05NR01

LSZH

PERFORM FULL AIRWORTHINESS REVIEW IAW. M.A.710/M.A.901

LDG

HRS

MTH

114

172:54

25-Oct-2018 12 25-Oct-2020 12 m 25 d05NR02 PERFORM 1ST EXTENSION OF THE ARC IAW. M.A.901

LDG

HRS

MTH

114

172:54

25-Oct-2018 24 25-Oct-2021 24 m 25 d05NR03 PERFORM 2ND EXTENSION OF THE ARC IAW. M.A.901

Page 1 of 51NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from PrintDate for calendar items.

0:0225-Sep-2019125:48AIR COND

0:2825-Sep-2019265324:25ENG 2

0:2825-Sep-2019265324:25ENG 1

0:2825-Sep-2019265324:25AIRCRAFT


Last ActualDate


HB-VTBReg No:

30-Sep-2019 5:15AM

23-Jun-2017


Print Date:

Airworthiness:

Aircraft Serial:


Unit:

525-0947


(ENG) DUE 2

(ENG) DUE 1


City Part Serial No


C/W Time 2 + or -

Adj. TBO 1

TBO 2 TSO 2

TSO 1

Remains

RemainsDescription


Item Code

Mod Lvl

LDG

HRS

MTH

215

267:04

19-Jun-2019

N/A

12 30-Jun-2020 9 m 0 d

05NR04

LSZH

PERFORM ANNUAL CHECK OF THE AVIONIC EQUIPMENT IAW. FOCA TM 02.020-10

LDG

HRS

MTH

215

267:04

19-Jun-2019

N/A

12 30-Jun-2020 9 m 0 d

05NR05

LSZH

PERFORM CHECK OF THE STATIC PRESSURE- AND BAROMETRIC ALTIMETER EQUIPMENT IAW. FOCA TM 20.020-20

LDG

HRS

MTH

215

267:04

19-Jun-2019 24 30-Jun-2021 21 m 0 d

05NR06

LSZH

PERFORM TRANSPONDER SYSTEM TEST IAW. FOCA TM 20.100-20

LDG

HRS

MTH

133

194:27

07-Dec-2018 120 31-Dec-2028 111 m 0 d

05NR07

EDDL

PERFORM WEIGHING OF THE AIRCRAFT IAW. FOCA TM 73.920-12

MTH 12 29-Sep-2019 -1 d05NR08 RENEWAL OF INSURANCE CERTIFICATE

Over Due

MTH 18-Oct-2018 12005NR09 RENEWAL OF AIRCRAFT RADIO LICENCE

MTH 28-Sep-2018 12 28-Sep-2019 -2 d

05NR11 PERFORM YEARLY CHECK OF AIRCRAFT MAINTENANCE PROGRAMME IAW. M.A.302

Over Due

HRS

MTH

0

23-Jun-2017

300

12

400

31-Dec-2019

75:35

3 m 0 d05NR14 PERFORM ENGINE NO.1 COMPRESSOR WASH

HRS

MTH

0

23-Jun-2017

300

12

400

31-Dec-2019

75:35

3 m 0 d05NR15 PERFORM ENGINE NO.2 COMPRESSOR WASH

LDG

HRS

MTH

215

267:04

19-Jun-2019 12 19-Jun-2020 8 m 19 d05NR18

LSZH

AIRCRAFT YEARLY INSPECTION IAW. FOCA TM 02.020-10

LDG

HRS

MTH

248

300:25

16-Aug-2019

300 600:25 276

5-12-01

LSZH

INSPECTION DOCUMENT 01

LDG

HRS

MTH

215

267:04

19-Jun-2019 12 30-Jun-2020 9 m 0 d5-12-02

LSZH


LDG

HRS

MTH

215

267:04

19-Jun-2019 12C-90386139

C352TS 30-Jun-2020 9 m 0 dCABIN

B262201

LSZH

FUNCTIONAL (WEIGHT) CHECK PORTABLE FIRE EXTINGUISHER : INSPECTION DOCUMENT 2

MTH 23-Jun-2017 245-12-03 INSPECTION DOCUMENT 03

MTH 23-Jun-2017 36

5-12-04 INSPECTION DOCUMENT 04 (PLEASE REFER TO INDIVIDUAL SUBTASKS FOR DUE TIMES)

MTH 01-Nov-2016 369239

40005320-2 30-Nov-2019 2 m 0 d

B323201 RESTORATION (HYDROSTATIC TEST) EMERGENCY GEAR BOTTLE : INSPECTION DOCUMENT 04

MTH 23-Jun-2017 60



0:0225-Sep-2019125:48AIR COND

0:2825-Sep-2019265324:25ENG 2

0:2825-Sep-2019265324:25ENG 1

0:2825-Sep-2019265324:25AIRCRAFT


Last ActualDate


HB-VTBReg No:

30-Sep-2019 5:15AM

23-Jun-2017


Print Date:

Airworthiness:

Aircraft Serial:


Unit:

525-0947


(ENG) DUE 2

(ENG) DUE 1


City Part Serial No


C/W Time 2 + or -

Adj. TBO 1

TBO 2 TSO 2

TSO 1

Remains

RemainsDescription


Item Code

Mod Lvl

MTH 08-Aug-2016 6074363B1

30401102-2 31-Aug-2021 23 m 0 d

B262005 RESTORATION (HYDROSTATIC TEST) ENGINE FIRE EXTINGUISHER BOTTLE : INSPECTION DOCUMENT 05

MTH 23-Jun-2017 72


MTH 23-Jun-2017 72C-90386139

C352TS 30-Jun-2023 45 m 0 dCABIN

A262201 DETAILED INSPECTION PORTABLE FIRE EXTINGUISHER : INSPECTION DOCUMENT 06

MTH 23-Jun-2017 144


MTH 01-Jan-2017 144C-90386139

C352TS 31-Jan-2029 112 m 0 dCABIN

B262203 RESTORATION (HYDROSTATIC TEST) PORTABLE FIRE EXTINGUISHER : INSPECTION DOCUMENT 07

LDG

HRS

MTH

215

267:04

19-Jun-2019

300

24

567:04

30-Jun-2021

242:39

21 m 0 d5-12-08

LSZH


LDG

HRS

MTH

215

267:04

19-Jun-2019

200

4

5-12-09

LSZH

INSPECTION DOCUMENT 09 (PLEASE REFER TO INDIVIDUAL SUBTASKS FOR DUE TIMES)

LDG

HRS

MTH

215

267:04

19-Jun-2019

200

440930268

RG-380E/44LA5

467:04

31-Oct-2019

142:39

1 m 0 d

B243603

LSZH

FUNCTIONAL CHECK BATTERY LEAD ACID BATTERY (CAPACITY CHECK): INSPECTION DOCUMENT 09

HRS

MTH

0

23-Jun-2017

1200

36

1200

30-Jun-2020

875:35

9 m 0 d5-12-10 INSPECTION DOCUMENT 10

HRS

MTH

0

23-Jun-2017

2400

72

2400

30-Jun-2023

2075:35

45 m 0 d5-12-11 INSPECTION DOCUMENT 11

LDG

HRS

MTH

215

267:04

19-Jun-2019 12 30-Jun-2020 9 m 0 d5-12-12

LSZH

INSPECTION DOCUMENT 12 (14 CFR 91.207)

LDG

HRS

MTH

215

267:04

19-Jun-2019 12252-00986

453-5060 30-Jun-2020 9 m 0 d

A256201

LSZH

DETAILED INSPECTION EMERGENCY LOCATOR TRANSMITTER ARTEX (ELT): INSPECTION DOCUMENT 12

LDG

HRS

MTH

215

267:04

19-Jun-2019 12 30-Jun-2020 9 m 0 d

B256203

LSZH

OPERATIONAL CHECK ARTEX C406-N EMERGENCY LOCATOR TRANSMITTER: INSPECTION DOCUMENT 12

LDG

HRS

MTH

215

267:04

19-Jun-2019 24

5-12-13

LSZH


LDG

HRS

MTH

215

267:04

19-Jun-2019 24 30-Jun-2021 21 m 0 dLEFT

B341101

LSZH

FUNCTIONAL CHECK PITOT-STATIC SYSTEM: INSPECTION DOCUMENT 13

MTH 18-Jun-2019 241U6100440

011-02337-01 30-Jun-2021 21 m 0 dNO. 1

B341101

LSZH

CALIBRATION TEST -- (FAR 91.411): INSPECTION DOCUMENT 13

MTH 18-Jun-2019 241U6101471

011-02337-01 30-Jun-2021 21 m 0 dNO. 2

B341101

LSZH

CALIBRATION TEST -- (FAR 91.411): INSPECTION DOCUMENT 13

LDG

HRS

MTH

215

267:04

19-Jun-2019 24 30-Jun-2021 21 m 0 dRIGHT

B341101

LSZH

FUNCTIONAL CHECK PITOT-STATIC SYSTEM: INSPECTION DOCUMENT 13


0:0225-Sep-2019125:48AIR COND

0:2825-Sep-2019265324:25ENG 2

0:2825-Sep-2019265324:25ENG 1

0:2825-Sep-2019265324:25AIRCRAFT


Last ActualDate


HB-VTBReg No:

30-Sep-2019 5:15AM

23-Jun-2017


Print Date:

Airworthiness:

Aircraft Serial:


Unit:

525-0947


(ENG) DUE 2

(ENG) DUE 1


City Part Serial No


C/W Time 2 + or -

Adj. TBO 1

TBO 2 TSO 2

TSO 1

Remains

RemainsDescription


Item Code

Mod Lvl

MTH 18-Jun-2019 243213

9200-32100-0201 30-Jun-2021 21 m 0 d

B341101

LSZH

CALIBRATION TEST ELECTRONIC STANDBY INDICATOR (4-IN-1) DISPLAY (FAR 91.411): INSPECTION DOCUMENT 13

MTH 17-Jun-2019 2420S007752

011-01997-00 30-Jun-2021 21 m 0 dLEFT

B345701

LSZH

CALIBRATION CHECK GTX 3000 MODE S TCAS II TRANSPONDER ATC SYSTEM (FAR 91.413): INSPECTION DOCUMENT 13

MTH 17-Jun-2019 2420S007734

011-01997-00 30-Jun-2021 21 m 0 dRIGHT

B345701

LSZH

CALIBRATION CHECK GTX 3000 MODE S TCAS II TRANSPONDER ATC SYSTEM (FAR 91.413): INSPECTION DOCUMENT 13

MTH 23-Jun-2017 A/R


MTH 23-Jun-2017 T/C2170

3-1527-2LEFT

A324201 SPECIAL DETAIL INSPECT WHEEL (NDI): INSPECTION DOCUMENT 14

MTH 23-Jun-2017 T/C9472

3-1418NOSE

A324201 SPECIAL DETAIL INSPECT WHEEL ASSY (NDI): INSPECTION DOCUMENT 14

MTH 23-Jun-2017 T/CT0001

3-1527-2RIGHT

A324201 SPECIAL DETAIL INSPECT WHEEL (NDI): INSPECTION DOCUMENT 14

LDG

HRS

DAYS

215

267:04

19-Jun-2019 14 30-Nov-2019 2 m 0 d

5-12-15

LSZH


ACH

LDG

HRS

MTH

65:06

51

78:18

25-Jan-2018

100

5-12-17

KICT


LDG

HRS

MTH

215

267:04

19-Jun-2019

600

24

867:04

30-Jun-2021

542:39

21 m 0 d5-12-21

LSZH


HRS

MTH

0

23-Jun-2017

7200 7200 6875:35

5-12-29 INSPECTION DOCUMENT 29

HRS

MTH

0

23-Jun-2017

7200 7200 6875:35

A530003 ZONAL INSPECTION COCKPIT AND CABIN ABOVE AND BELOW FLOORBOARD: INSPECTION DOCUMENT 29

LDG

HRS

MTH

215

267:04

19-Jun-2019

300

12

567:04

30-Jun-2020

242:39

9 m 0 d5-12-33

LSZH


LDG

HRS

MTH

215

267:04

19-Jun-2019 6 31-Dec-2019 3 m 0 d5-12-36

LSZH


ACH

MTH

0

23-Jun-2017

500 500 374:12

5-12-37 INSPECTION DOCUMENT 37

LDG

HRS

MTH

248

300:25

16-Aug-2019

300 600:25 276

5-12-MA

LSZH

INSPECTION DOCUMENT MA

LDG

MTH

0

23-Jun-2017

5000 5000 4735

5-12-MD INSPECTION DOCUMENT MD

HRS

MTH

0

23-Jun-2017

6000 6000 5675:35

5-12-MF INSPECTION DOCUMENT MF

HRS

MTH

0

23-Jun-2017

6000 6000 5675:35

5-12-MG INSPECTION DOCUMENT MG

HRS

MTH

0

23-Jun-2017

6000 6000 5675:35

5-12-MH INSPECTION DOCUMENT MH

HRS

MTH

0

23-Jun-2017

7200 7200 6875:35

5-12-MI INSPECTION DOCUMENT MI


0:0225-Sep-2019125:48AIR COND

0:2825-Sep-2019265324:25ENG 2

0:2825-Sep-2019265324:25ENG 1

0:2825-Sep-2019265324:25AIRCRAFT


Last ActualDate


HB-VTBReg No:

30-Sep-2019 5:15AM

23-Jun-2017


Print Date:

Airworthiness:

Aircraft Serial:


Unit:

525-0947


(ENG) DUE 2

(ENG) DUE 1


City Part Serial No


C/W Time 2 + or -

Adj. TBO 1

TBO 2 TSO 2

TSO 1

Remains

RemainsDescription


Item Code

Mod Lvl

HRS

MTH

0

23-Jun-2017

7200 7200 6875:35

5-12-MJ INSPECTION DOCUMENT MJ

HRS

MTH

0

23-Jun-2017

7900 7900 7575:35

5-12-MK INSPECTION DOCUMENT MK

HRS

MTH

0

23-Jun-2017

12000 12000 11675:35

5-12-MM INSPECTION DOCUMENT MM

HRS

MTH

0

23-Jun-2017

12000 12000 11675:35

5-12-MN INSPECTION DOCUMENT MN

HRS

MTH

0

23-Jun-2017

15200 15200 14875:35

5-12-MO INSPECTION DOCUMENT MO

LDG

HRS

MTH

215

267:04

19-Jun-2019

250

12

517:04

30-Jun-2020

192:39

9 m 0 d5-12-MP

LSZH

INSPECTION DOCUMENT MP

LDG

HRS

MTH

248

300:25

16-Aug-2019

300 (600:25)600:25 276E1

052001 FJ44 CHECK 1

LDG

HRS

MTH

248

300:25

16-Aug-2019

300 (600:25)600:25 276E2

052001 LSZHFJ44 CHECK 1

HRS

MTH

0

23-Jun-2017

600 (600)600 275:35E1

052002 FJ44 CHECK 2

HRS

MTH

0

23-Jun-2017

600 (600)600 275:35E2

052002 FJ44 CHECK 2

HRS

MTH

0

23-Jun-2017

600HW43765

117810

(600)600 275:35

E1

723003 CLEAN FAN ROTOR AND PHYSICALLY INSPECT FOR DEFECTS (FEEL WITH FINGERS)

HRS

MTH

0

23-Jun-2017

600HW43761

117810

(600)600 275:35

E2

723003 CLEAN FAN ROTOR AND PHYSICALLY INSPECT FOR DEFECTS (FEEL WITH FINGERS)

HRS

MTH

0

23-Jun-2017

15000 (2500)2500 2175:35E1

052003

-12500

FJ44 CHECK 3

HRS

MTH

0

23-Jun-2017

15000 (2500)2500 2175:35E2

052003

-12500

FJ44 CHECK 3

HRS

MTH

0

23-Jun-2017

5000 (5000)5000 4675:35E1

052004 FJ44 CHECK 4

HRS

MTH

0

23-Jun-2017

5000 (5000)5000 4675:35E2

052004 FJ44 CHECK 4

HRS

MTH

0

23-Jun-2017

7500 (7500)7500 7175:35E1

052005 FJ44 CHECK 5

HRS

MTH

0

23-Jun-2017

7500 (7500)7500 7175:35E2

052005 FJ44 CHECK 5

HRS

MTH

0

23-Jun-2017

10000 (10000)10000 9675:35E1

052006 FJ44 CHECK 6

HRS

MTH

0

23-Jun-2017

10000 (10000)10000 9675:35E2

052006 FJ44 CHECK 6

HRS

MTH

0

23-Jun-2017

12500 (12500)12500 12175:35E1

052007 FJ44 CHECK 7

HRS

MTH

0

23-Jun-2017

12500 (12500)12500 12175:35E2

052007 FJ44 CHECK 7

HRS

MTH

0

23-Jun-2017

15000 (15000)15000 14675:35E1

052008 FJ44 CHECK 8

HRS

MTH

0

23-Jun-2017

15000 (15000)15000 14675:35E2

052008 FJ44 CHECK 8

HRS

MTH

0

23-Jun-2017

17500 (17500)17500 17175:35E1

052009 FJ44 CHECK 9

HRS

MTH

0

23-Jun-2017

17500 (17500)17500 17175:35E2

052009 FJ44 CHECK 9

HRS

MTH

0

23-Jun-2017

20000 (20000)20000 19675:35E1

052010 FJ44 CHECK 10


0:0225-Sep-2019125:48AIR COND

0:2825-Sep-2019265324:25ENG 2

0:2825-Sep-2019265324:25ENG 1

0:2825-Sep-2019265324:25AIRCRAFT


Last ActualDate


HB-VTBReg No:

30-Sep-2019 5:15AM

23-Jun-2017


Print Date:

Airworthiness:

Aircraft Serial:


Unit:

525-0947


(ENG) DUE 2

(ENG) DUE 1


City Part Serial No


C/W Time 2 + or -

Adj. TBO 1

TBO 2 TSO 2

TSO 1

Remains

RemainsDescription


Item Code

Mod Lvl

HRS

MTH

0

23-Jun-2017

20000 (20000)20000 19675:35E2

052010 FJ44 CHECK 10

LDG

HRS

MTH

215

267:04

19-Jun-2019 24 30-Jun-2021 21 m 0 d

05NR17

LSZH

- CHECK OF MAGNETIC COMPASS SYSTEMS - PER FOCA TM 20.040-00

LDG

HRS

MTH

215

267:04

19-Jun-2019 12 30-Jun-2020 9 m 0 d

05SWEEPON01_COPLT LSZH

INSPECT COPILOT OXYGEN MASK - VISUAL AND FUNCTIONAL CONDITION CHECK - CMM 35-11-73 / PG 14001

LDG

HRS

MTH

215

267:04

19-Jun-2019 12 30-Jun-2020 9 m 0 d

05SWEEPON01_PLT LSZH

INSPECT PILOT OXYGEN MASK - VISUAL AND FUNCTIONAL CONDITION CHECK - CMM 35-11-73 / PG 14001

MTH 23-Jun-2017 60 30-Jun-2022 33 m 0 d

05SWEEPON02_COPLT

TEST COPILOT OXYGEN MASK - PERFORMANCE PARAMETERS TEST - CMM 35-11-73 / PG 14001

MTH 23-Jun-2017 60 30-Jun-2022 33 m 0 d

05SWEEPON02_PLT

TEST PILOT OXYGEN MASK - PERFORMANCE PARAMETERS TEST - CMM 35-11-73 / PG 14001

MTH 31-May-2018 60

1895-824

176276-5031-May-2023 44 m 0 d350002

LSZH

RESTORATION (HYDROSTATIC TEST) OXYGEN BOTTLE

HRS

MTH

0

23-Jun-2017

14000 14000 13675:35

551010 EXAMINE HORIZONTAL STABILIZER FRONT UPPER SPAR CAP AT SS 4.78

HRS

MTH

0

23-Jun-2017

13200 13200 12875:35

571010 EXAMINE LOWER MAIN SPAR SPLICE AT WS 93.00

HRS

MTH

0

23-Jun-2017

15600 15600 15275:35

571015 EXAMINE LOWER REAR SPAR SPLICE AT WS 93.00

HRS

MTH

0

23-Jun-2017

15000 15000 14675:35

571020 EXAMINE MAIN SPAR CARRY-THROUGH LOWER CAP (RWS 42.0 TO LWS 42.0)

HRS

MTH

0

23-Jun-2017

15000 15000 14675:35

571025 EXAMINE REAR SPAR CARRY-THROUGH LOWER CAP (RWS 42.0 TO LWS 42.0)

HRS

MTH

0

23-Jun-2017

15000 15000 14675:35

571030 EXAMINE MAIN SPAR OUTBOARD LOWER CAP (WS 120.0 TO WS 152.00)

MTH 23-Jun-2017 A/RE1

710000 WATER RINSE


710000 WATER RINSE


710015 COMPRESSOR CLEANING


710015 COMPRESSOR CLEANING

LDG

HRS

MTH

215

267:04

19-Jun-2019 A/RE1

72ENGWASH01

LSZH

WATER RINSE - REFER TO WI TASK 71-00-03-170-801 CLEAN THE POWER PLANT - WATER RINSE

LDG

HRS

MTH

215

267:04

19-Jun-2019 A/RE2

72ENGWASH02

LSZH

WATER RINSE - REFER TO WI TASK 71-00-03-170-801 CLEAN THE POWER PLANT - WATER RINSE


0:0225-Sep-2019125:48AIR COND

0:2825-Sep-2019265324:25ENG 2

0:2825-Sep-2019265324:25ENG 1

0:2825-Sep-2019265324:25AIRCRAFT


Last ActualDate


HB-VTBReg No:

30-Sep-2019 5:15AM

23-Jun-2017


Print Date:

Airworthiness:

Aircraft Serial:


Unit:

525-0947


(ENG) DUE 2

(ENG) DUE 1


City Part Serial No


C/W Time 2 + or -

Adj. TBO 1

TBO 2 TSO 2

TSO 1

Remains

RemainsDescription


Item Code

Mod Lvl

MTH 23-Jun-2017 N/AE1

731020 REPLACE FDU-TO-FLOWMETER FUEL TUBEASSEMBLY, FLOWMETER-TO-MANIFOLDFUEL TUBE ASSEMBLY, AND 69233 LOOPCLAMP BRACKET(RENTAL ENGINES ONLY)

MTH 23-Jun-2017 N/AE2

731020 REPLACE FDU-TO-FLOWMETER FUEL TUBEASSEMBLY, FLOWMETER-TO-MANIFOLDFUEL TUBE ASSEMBLY, AND 69233 LOOPCLAMP BRACKET(RENTAL ENGINES ONLY)


0:0225-Sep-2019125:48AIR COND

0:2825-Sep-2019265324:25ENG 2

0:2825-Sep-2019265324:25ENG 1

0:2825-Sep-2019265324:25AIRCRAFT


Last ActualDate


HB-VTBReg No:

30-Sep-2019 5:15AM

23-Jun-2017


Print Date:

Airworthiness:

Aircraft Serial:


Unit:

525-0947


(ENG) DUE 2

(ENG) DUE 1

Components

City Part Serial No


C/W Time 2 + or -

Adj. TBO 1

TBO 2 TSO 2

TSO 1

Remains

RemainsDescription


Item Code

Mod Lvl

MTH 23-Jun-2017 0O/C1403

10840A211003 HEAT PRESSURE EXCHANGER

MTH 23-Jun-2017 0O/C12BN48

27241287-24211004 HEAT EXCHANGER SHUTOFF VALVE

MTH 23-Jun-2017 0O/C1524

2601-23211005 EMERGENCY PRESS SHUTOFF VALVE

MTH 23-Jun-2017 0O/C2551

0113-12212001 UNDERFLOOR INLET AIR BLOWER

MTH 23-Jun-2017 0O/C4378

1173T42-3212003 TEMP PRESS COMPRESSION SWITCH

MTH 23-Jun-2017 0O/C12BN244

27221274

AFT

212011 TEMP UNDERFLOOR SENSOR

MTH 23-Jun-2017 0O/CNSN

D113204212202 OVERHEAD AIR VALVE SOLENOID

MTH 23-Jun-2017 0O/C2115

7003-200212302 BLOWER - WINDSHIELD AIR MOTOR

MTH 23-Jun-2017 0O/C5317

52811-103213003 PRESSURIZATION CONTROLLER

MTH 23-Jun-2017 0O/C5217

52812-102

LEFT

213004 KAPS II OUTFLOW VALVE

MTH 23-Jun-2017 0O/C5272

52812-102

RIGHT

213004 KAPS II OUTFLOW VALVE

MTH 23-Jun-2017 0O/C409

1134820-13

FORWARD

215001 EVAPORATOR

MTH 23-Jun-2017 0O/C509

1134820-14

AFT

215002 EVAPORATOR


1250211-7

AFT

215003 EVAPORATOR MOTOR


1250211-7

FORWARD

215003 EVAPORATOR MOTOR

MTH 23-Jun-2017 0O/C507A

1134400-31215004 AIR CONDITIONER COMPRESSOR

MTH 23-Jun-2017 0O/C5896

1134104-5215006 COMPRESSOR DRIVE MOTOR

MTH 23-Jun-2017 0O/C1648915

GBC300-82215010 FREON A/C-BAROMETRIC SWITCH

ACH

MTH

0

23-Jun-2017

0

0

500SN-UNKNOWN

PN 500 374:12

215012 COMPRESSOR DRIVE MOTOR BRUSHES


1250218

AFT

215013 EXPANSION VALVE


1250218

FORWARD

215013 EXPANSION VALVE

MTH 23-Jun-2017 0O/C8BN231

1E86-1216002 TEMPERATURE CONTROLLER

MTH 23-Jun-2017 0O/C1BP15

27221274216003 TEMP CNTL SYS SENSOR

MTH 23-Jun-2017 0O/C19Z010250

011-00877-20

AILERON

221003 SERVO

MTH 23-Jun-2017 0O/C19Z010248

011-00877-20

RUDDER

221004 SERVO

MTH 23-Jun-2017 0O/C1A1016437

011-00878-20

ELEVATOR TRIM

221005 GSA 81 SERVO

MTH 23-Jun-2017 0O/C22008172

011-01020-10221009 GMC 710 AFCS MODE CONTROLLER

MTH 23-Jun-2017 0O/C1A1016445

011-00878-20

ELEVATOR

221010 GSA 81 SERVO


0:0225-Sep-2019125:48AIR COND

0:2825-Sep-2019265324:25ENG 2

0:2825-Sep-2019265324:25ENG 1

0:2825-Sep-2019265324:25AIRCRAFT


Last ActualDate


HB-VTBReg No:

30-Sep-2019 5:15AM

23-Jun-2017


Print Date:

Airworthiness:

Aircraft Serial:


Unit:

525-0947


(ENG) DUE 2

(ENG) DUE 1

Components

City Part Serial No


C/W Time 2 + or -

Adj. TBO 1

TBO 2 TSO 2

TSO 1

Remains

RemainsDescription


Item Code

Mod Lvl

MTH 23-Jun-2017 0O/C1GK018028

011-02490-14

AILERON

221011 GSM 86 SERVO MOUNT

MTH 23-Jun-2017 0O/C1GK014772

011-02490-15

RUDDER


MTH 23-Jun-2017 0O/C1GK017881

011-02490-16

ELEVATOR


MTH 23-Jun-2017 0O/C

1GJ006030

011-02490-17

221014 GSM 86 SERVO (ELEVATOR TRIM) MOUNT

MTH 23-Jun-2017 0O/C222005531

011-02303-00231008 GDR 66 VHF DATALINK RADIO

MTH 23-Jun-2017 0O/C2550

VHF10-829

BOTTOM

232008 COMM 2 ANTENNA

MTH 23-Jun-2017 0O/C874-1009

S72-1735-26

LWR

232008 TCAS ANTENNA

MTH 23-Jun-2017 0O/C2562

VHF10-829

NO. 3

232008 VHF-COM ANTENNA

MTH 23-Jun-2017 0O/C2503

VHF10-829

TOP

232008 COMM 1 ANTENNA

MTH 23-Jun-2017 0O/C874-0999

S72-1735-26

UPPER

232008 TCAS ANTENNA

LDG

HRS

MTH

133

194:27

07-Dec-2018

0

0O/CS00009

744000-10-70

CABIN

232009

EDDL

CABIN PHONE HANDSET

MTH 23-Jun-2017 0O/C47769649

011-00987-00232010 SATELITE DATA LINK TRANSCEIVER

MTH 23-Jun-2017 0O/C2JH006154

011-01457-01

LH

232014 GSD 41 DATA CONCENTRATOR

MTH 23-Jun-2017 0O/C2JH006160

011-01457-01

RH

232014 GSD 41 DATA CONCENTRATOR

MTH 23-Jun-2017 0O/C211610

TRAB24/49003P

AFT

232023 WIFI ANTENNA

MTH 23-Jun-2017 0O/C6281610

TRAB24/49003P

FWD

232033 WIFI ANTENNA

MTH 23-Jun-2017 0O/C529847

CI428-410

NO. 1

235001 GPS/XM ANTENNA

MTH 23-Jun-2017 0O/C527941

CI428-410

NO. 2

235001 GPS/XM ANTENNA

MTH 23-Jun-2017 0O/C1HF007415

011-01793-00

LEFT

235006 GMA 36 REMOTE AUDIO PROCESSOR

MTH 23-Jun-2017 0O/C1HF007425

011-01793-00

RIGHT

235006 GMA 36 REMOTE AUDIO PROCESSOR

MTH 23-Jun-2017 0O/C5570816

102025-1235009 PA AMPLIFIER

MTH 23-Jun-2017 0O/C7573

SS50

AUX

242001 AC CONVERTER

MTH 23-Jun-2017 0O/CP7495

51525-001F

LEFT

243002 GENERATOR CONTROL UNIT

MTH 23-Jun-2017 0O/CP7701

51525-001F

RIGHT

243002 GENERATOR CONTROL UNIT

LDG

HRS

MTH

89

134:30

19-Jun-2018

0

0

0O/C40930268

RG-380E/44LA5243003

S3597-8

DNAMAIN BATTERY

LDG

HRS

MTH

215

267:04

19-Jun-2019

0

0

0O/CG03030964

7243-16T243007

LSZH

16 AHR BATTERY ASSY


0:0225-Sep-2019125:48AIR COND

0:2825-Sep-2019265324:25ENG 2

0:2825-Sep-2019265324:25ENG 1

0:2825-Sep-2019265324:25AIRCRAFT


Last ActualDate


HB-VTBReg No:

30-Sep-2019 5:15AM

23-Jun-2017


Print Date:

Airworthiness:

Aircraft Serial:


Unit:

525-0947


(ENG) DUE 2

(ENG) DUE 1

Components

City Part Serial No


C/W Time 2 + or -

Adj. TBO 1

TBO 2 TSO 2

TSO 1

Remains

RemainsDescription


Item Code

Mod Lvl

MTH 23-Jun-2017 0O/C81924

501-1712-01243012 STANDBY BATTERY

MTH 23-Jun-2017 0O/C523

6318349-26245001 PRESSURIZATION PCB ASSY

MTH 23-Jun-2017 0O/C1513

6318037-6

LEFT

245002 ASSEMBLY-FUEL CONTROL PCB

MTH 23-Jun-2017 0O/C1507

6318037-6

RIGHT

245002 ASSEMBLY-FUEL CONTROL PCB

MTH 23-Jun-2017 0O/C982

6318388-7

LEFT

245003 ASSEMBLY-IGNITOR PCB

MTH 23-Jun-2017 0O/C993

6318388-7

RIGHT

245003 ASSEMBLY-IGNITOR PCB

MTH 23-Jun-2017 0O/C611

6318390-1

LEFT

245004 ANTI ICE PCB ASSY

MTH 23-Jun-2017 0O/C618

6318390-1

RIGHT

245004 ANTI ICE PCB ASSY

MTH 23-Jun-2017 0O/C559

6318046-9245005 DIAGNOSTICS PCB ASSY

MTH 23-Jun-2017 0O/C682

6318358-20245006 ENVIRONMENTAL PCB ASSY

MTH 23-Jun-2017 0O/C1682

6318038-1

LEFT

245007 PCB-START LOGIC ASSY

MTH 23-Jun-2017 0O/C1686

6318038-1

RIGHT

245007 PCB-START LOGIC ASSY

MTH 23-Jun-2017 0O/C1637004

85-230-2245011 FUEL FLOW XMITTER PCB ASSY

MTH 23-Jun-2017 0O/C809

6318034-6245012 SPEEDBRAKE CONTROL PCB ASSY

MTH 23-Jun-2017 0O/C882

6318043-1245013 TAIL DEICE MONITOR PCB ASSY

MTH 23-Jun-2017 0O/C872

6318044-1245014 TAIL DEICE CONTROL PCB ASSY

MTH 23-Jun-2017 0O/C797

6318035-7245015 HYDRAULIC PCB ASSY

MTH 23-Jun-2017 0O/C777

6318387-11245020 FADEC INTERFACE NZ116 ASSY

MTH 23-Jun-2017 0O/C772

6318387-11245022 FADEC INTERFACE NZ117 ASSY

MTH 23-Jun-2017 0O/C822

6318398-6

NO. 1

245026 LANDING GEAR PCB

MTH 23-Jun-2017 0O/C794

6318399-11

NO. 2

245027 LANDING GEAR PCB

MTH 23-Jun-2017 0O/C1794

7018119-1

CABIN

245200 ALT MODULE ASSY

MTH 23-Jun-2017 0O/C896

6318397-21245023 LANDING GEAR MONITOR PCB ASSY

MTH 23-Jun-2017 0O/C252-00986

453-5060256001 EMERGENCY LOCATOR TRANSMITTER

MTH 23-Jun-2017 0O/C527824

110-340256004 ELT ANTENNA

MTH 60370437-035

452-0133 01-Sep-2021 23 m 1 d256005 ELT BEACON BATTERY PACK

MTH 23-Jun-2017 012017011610068

PO1074-207 19-Jan-2027 87 m 19 dCO-PILOT

256006 LIFE VEST

MTH 23-Jun-2017 012016111750065

PO1074-207 22-Nov-2026 85 m 22 dLAVATORY

256006 LIFE VEST

MTH 23-Jun-2017 012017011640039

PO1074-207 19-Jan-2027 87 m 19 dNO. 3

256006 LIFE VEST


0:0225-Sep-2019125:48AIR COND

0:2825-Sep-2019265324:25ENG 2

0:2825-Sep-2019265324:25ENG 1

0:2825-Sep-2019265324:25AIRCRAFT


Last ActualDate


HB-VTBReg No:

30-Sep-2019 5:15AM

23-Jun-2017


Print Date:

Airworthiness:

Aircraft Serial:


Unit:

525-0947


(ENG) DUE 2

(ENG) DUE 1

Components

City Part Serial No


C/W Time 2 + or -

Adj. TBO 1

TBO 2 TSO 2

TSO 1

Remains

RemainsDescription


Item Code

Mod Lvl

MTH 23-Jun-2017 012016111750072

PO1074-207 22-Nov-2026 85 m 22 dNO. 4

256006 LIFE VEST

MTH 23-Jun-2017 012017011640072

PO1074-207 19-Jan-2027 87 m 19 dNO. 5

256006 LIFE VEST

MTH 23-Jun-2017 012017011640065

PO1074-207 19-Jan-2027 87 m 19 dNO. 6

256006 LIFE VEST

MTH 23-Jun-2017 012017011640047

PO1074-207 19-Jan-2027 87 m 19 dPILOT

256006 LIFE VEST

MTH 23-Jun-2017 012017011640010

PO1074-207 19-Jan-2027 87 m 19 dSFS

256006 SIDE FACING SEAT (NO. 7) LIFE VEST

MTH 23-Jun-2017 0O/C215171

3001-212-1004/455-9

LEFT

261002 FIRE DETECT SENSOR

MTH 23-Jun-2017 0O/C215154

3001-212-1004/455-9

RIGHT

261002 FIRE DETECT SENSOR

MTH 23-Jun-2017 0O/C74363B1

30401102-2262001 ENGINE FIRE EXTINGUISHER BOTTLE

MTH 01-Aug-2016 072NSN

13083-5 31-Aug-2022 35 m 0 dNO. 1

262002 FIRE EXTINGUISHER CARTRIDGE

Manufacture Date: 01-Aug-2016

MTH 01-Aug-2016 072NSN

13083-5 31-Aug-2022 35 m 0 dNO. 2

262002 FIRE EXTINGUISHER CARTRIDGE

Manufacture Date: 01-Aug-2016

MTH 23-Jun-2017 0O/CC-90386139

C352TS

CABIN

262003 PORTABLE FIRE EXTINGUISHER

MTH 23-Jun-2017 0O/C1259C

6360115-1

LH

271001 CONTROL WHEEL ASSY

MTH 23-Jun-2017 0O/C1236C

6360115-2

RH

271001 CONTROL WHEEL ASSY

MTH 23-Jun-2017 0O/C168138A-01

201

LEFT

273001 SHAKER CONTROL


6396022-3

LEFT HAND

273006 ACTUATOR ASSEMBLY


6396022-4

RIGHT HAND



6396022-5

RUDDER



6396022-8273006 AILERON TRIM ACTUATOR

MTH 23-Jun-2017 0O/C1404

4083-1275001 SHUTOFF VALVE

MTH 23-Jun-2017 0O/C2696

1542000-9

LEFT

275002 FLAP HYD ACTUATOR

MTH 23-Jun-2017 0O/C2702

1542000-9

RIGHT

275002 FLAP HYD ACTUATOR

LDG

HRS

MTH

105

157:06

07-Sep-2018

0

0

0O/C27889533

6325100-82

RIGHT

275004 ICTFLAP ASSEMBLY

MTH 23-Jun-2017 0O/C2685A

1542100-5

LEFT

276001 SPEEDBRAKE ACTUATOR

MTH 23-Jun-2017 0O/C2689A

1542100-5

RIGHT

276001 SPEEDBRAKE ACTUATOR

MTH 23-Jun-2017 0O/C6397

35C10D

LEFT

281001 FUEL SURGE VALVE

MTH 23-Jun-2017 0O/C6455

35C10D

RIGHT

281001 FUEL SURGE VALVE

MTH 23-Jun-2017 0O/C11BN64

1C7-13

LEFT

282001 ELECTRIC FUEL PUMP


0:0225-Sep-2019125:48AIR COND

0:2825-Sep-2019265324:25ENG 2

0:2825-Sep-2019265324:25ENG 1

0:2825-Sep-2019265324:25AIRCRAFT


Last ActualDate


HB-VTBReg No:

30-Sep-2019 5:15AM

23-Jun-2017


Print Date:

Airworthiness:

Aircraft Serial:


Unit:

525-0947


(ENG) DUE 2

(ENG) DUE 1

Components

City Part Serial No


C/W Time 2 + or -

Adj. TBO 1

TBO 2 TSO 2

TSO 1

Remains

RemainsDescription


Item Code

Mod Lvl

MTH 23-Jun-2017 0O/C11BN67

1C7-13

RIGHT

282001 ELECTRIC FUEL PUMP

MTH 23-Jun-2017 0O/CB4691

RG45880

LEFT

282002 FUEL TRANSFER PUMP

MTH 23-Jun-2017 0O/CB4645

RG45880

RIGHT

282002 FUEL TRANSFER PUMP

MTH 23-Jun-2017 0O/CAA602341

AV24B1507

LEFT

282004 FUEL MOTOR ACTUATED VALVE

MTH 23-Jun-2017 0O/CAA602338

AV24B1507

RIGHT

282004 FUEL MOTOR ACTUATED VALVE

MTH 23-Jun-2017 0O/CC4191

RG45310

LEFT

282005 FUEL TRANSFER EJECTOR

MTH 23-Jun-2017 0O/CC3918

RG45310

RIGHT

282005 FUEL TRANSFER EJECTOR

MTH 23-Jun-2017 0O/C16-1115718

ZSV57282006 TRANSFER VALVE

MTH 23-Jun-2017 0O/CMN41038

10307T01Y00

LH

284001 NO.5 TRANSMITTER FUEL PROBE

MTH 23-Jun-2017 0O/CMN41037

10307T01Y00

RH



16080936

10310B01Y02

284003 FUEL QUANTITY SIGNAL CONDITIONER

MTH 23-Jun-2017 0O/CMN36905

10305T01Y00

LH


MTH 23-Jun-2017 0O/CMN40230

10305T01Y00

RH


MTH 23-Jun-2017 0O/CMN39806

10306T01Y00

LH


MTH 23-Jun-2017 0O/CMN40437

10306T01Y00

RH


MTH 23-Jun-2017 0O/CMN40820

10304T01Y00

LH


MTH 23-Jun-2017 0O/CMN40824

10304T01Y00

RH


MTH 23-Jun-2017 0O/CMN41285

10303T01Y00

LH


MTH 23-Jun-2017 0O/CMN41282

10303T01Y00

RH



L16H-14

LEFT

284008 FUEL LOW LEVEL SWITCH


GIF5400-40

RIGHT

284008 FUEL LOW LEVEL SWITCH

MTH 23-Jun-2017 0O/CMN41012

10309T03Y00

LH


MTH 23-Jun-2017 0O/CMN41018

10309T03Y00

RH



CV02-193291003 HYDRAULIC CHECK VALVE

LDG

HRS

MTH

29

45:48

05-Oct-2017

0

0O/C1729010

9912373-6291007 KAUSPRESSURE SWITCH

MTH 23-Jun-2017 0O/C0633B

4120-046000

LEFT

291009 ENGINE DRIVEN HYDRAULIC PUMP

LDG

HRS

MTH

105

157:06

07-Sep-2018

0

0

0O/C0140B

4120-046000

RIGHT

291009

KICT

ENGINE DRIVEN HYDRAULIC PUMP


0:0225-Sep-2019125:48AIR COND

0:2825-Sep-2019265324:25ENG 2

0:2825-Sep-2019265324:25ENG 1

0:2825-Sep-2019265324:25AIRCRAFT


Last ActualDate


HB-VTBReg No:

30-Sep-2019 5:15AM

23-Jun-2017


Print Date:

Airworthiness:

Aircraft Serial:


Unit:

525-0947


(ENG) DUE 2

(ENG) DUE 1

Components

City Part Serial No


C/W Time 2 + or -

Adj. TBO 1

TBO 2 TSO 2

TSO 1

Remains

RemainsDescription


Item Code

Mod Lvl

MTH 23-Jun-2017 0O/C1682A

2576-2291009A HYDRAULIC RELIEF VALVE

MTH 23-Jun-2017 0O/CAA595339

AV24B1388-2

LEFT

291010 HYDRAULIC SHUTOFF VALVE ASSY

MTH 23-Jun-2017 0O/CAA589477

AV24B1388-2

RIGHT

291010 HYDRAULIC SHUTOFF VALVE ASSY

LDG

HRS

MTH

105

157:06

07-Sep-2018

105

157:06

15O/C2140A

9912194-5

LEFT

291011

KICT

FLOW SWITCH/CHECK HYD VALVE

LDG

HRS

MTH

105

157:06

07-Sep-2018

105

157:06

15O/C2281A

9912194-5

RIGHT

291011

KICT

FLOW SWITCH/CHECK HYD VALVE


1352

4082-6

291012 SPEED BRAKE DUMP VALVE SOLENOID

MTH 23-Jun-2017 0O/C1801

4134-4291013 LOADING VALVE SOLENOID

MTH 23-Jun-2017 0O/C1369

4051-4291014 LANDING GEAR VALVE SOLENOID

MTH 23-Jun-2017 0O/C2774

9505-1

LEFT

291016 SPEED BRAKE PORTION VALVE

MTH 23-Jun-2017 0O/C2775

9505-1

RIGHT

291016 SPEED BRAKE PORTION VALVE

MTH 23-Jun-2017 0O/C1406

2577-1291017 SPEED BRAKE PORTION VALVE

MTH 23-Jun-2017 0O/C1412

9503-2291018 PNUEMATIC DUMP VALVE

MTH 23-Jun-2017 0O/C1444

4052-3291020 SPEEDBRAKE VALVE SOLENOID

MTH 23-Jun-2017 0O/C1445

4052-4291021 FLAP VALVE SOLENOID

MTH 23-Jun-2017 0O/C2620

2602-36301001 SHUTOFF ISOLATION VALVE

MTH 23-Jun-2017 0O/C11149A

1106P55-1

LEFT

301002 PNUEMATIC DEICE SWITCH

MTH 23-Jun-2017 0O/C11144A

1106P55-1

RIGHT

301002 PNUEMATIC DEICE SWITCH


3452

5285-00-3LEFT

301003 BLEED AIR PRESSURE REGULATOR SHUTOFF VALVE


3450

5285-00-3RIGHT

301003 BLEED AIR PRESSURE REGULATOR SHUTOFF VALVE

MTH 23-Jun-2017 0O/C5218

1173T42-4

LEFT

301004 TEMPERATURE DEICE SWITCH

MTH 23-Jun-2017 0O/C5220

1173T42-4

RIGHT

301004 TEMPERATURE DEICE SWITCH

MTH 23-Jun-2017 0O/CNDQ0300

29S4D5244-11

LEFT

301010 HORIZONTAL STABILIZER BOOT

MTH 23-Jun-2017 0O/CNDR2270

29S4D5244-12

RIGHT

301010 HORIZONTAL STABILIZER BOOT


1BP1

1H127-4LEFT

301012

9912402-9

WING SHUTOFF PRESSURE REGULATING VALVE


1BP2

1H127-4RIGHT

301012

9912402-9

WING SHUTOFF PRESSURE REGULATING VALVE


0:0225-Sep-2019125:48AIR COND

0:2825-Sep-2019265324:25ENG 2

0:2825-Sep-2019265324:25ENG 1

0:2825-Sep-2019265324:25AIRCRAFT


Last ActualDate


HB-VTBReg No:

30-Sep-2019 5:15AM

23-Jun-2017


Print Date:

Airworthiness:

Aircraft Serial:


Unit:

525-0947


(ENG) DUE 2

(ENG) DUE 1

Components

City Part Serial No


C/W Time 2 + or -

Adj. TBO 1

TBO 2 TSO 2

TSO 1

Remains

RemainsDescription


Item Code

Mod Lvl

MTH 23-Jun-2017 0O/CAS07162746

PH502

LEFT

303002 HEATED PITOT TUBE

MTH 23-Jun-2017 0O/CAS01167476

PH502

RIGHT

303002 HEATED PITOT TUBE

MTH 23-Jun-2017 0O/C4917

1169-1

LH

304001 B/A TEMP MONITOR-

MTH 23-Jun-2017 0O/C2489

10653A304002 HEAT EXCHANGER

MTH 23-Jun-2017 0O/C1BP6

1H127-4304003 WINDSHIELD S/O VALVE

MTH 23-Jun-2017 0O/C13714

76250-6

LEFT

304004 PITOT STATIC CURRENT SENSOR

MTH 23-Jun-2017 0O/C13707

76250-6

RIGHT

304004 PITOT STATIC CURRENT SENSOR

MTH 23-Jun-2017 0O/C11385

76552-1

LEFT

304005 SENSOR

MTH 23-Jun-2017 0O/C11330

76552-1

RIGHT

304005 SENSOR

MTH 23-Jun-2017 0O/C8BN48

1E58-1304006 TEMP BLEED AIR CONTROLLER

MTH 23-Jun-2017 0O/C12BN50P

27241287304007 TEMP CONTROL BLEED AIR VALVE

MTH 23-Jun-2017 0O/CN162532

3D2353-06

LEFT

304009 SOLENOID DEICE VALVE

MTH 23-Jun-2017 0O/CN162533

3D2353-06

RIGHT

304009 SOLENOID DEICE VALVE


6508092-4304010 ALCOHOL PUMP ASSEMBLY

MTH 23-Jun-2017 0O/C5997

1403-25

LEFT

304012 WINDSHIELD BLEED AIR VALVE

MTH 23-Jun-2017 0O/C5998

1403-25

RIGHT

304012 WINDSHIELD BLEED AIR VALVE

MTH 23-Jun-2017 0O/C5409AB

1115P25304013 PRESSURE WINDSHIELD SWITCH


1BP12

27221274AFT

304014 TEMPERATURE EVAPORATOR SENSOR


C664503-0104313001 FLIGHT HOUR METER


1567

6918236-20

313003 ARES II 24-CH FLIGHT DATA RECORDER

LDG

MTH

0

23-Jun-2017

0

0

2250026187623

6342000-43 22500 22235NOSE LANDINGGEAR

321001 STRUT AND ATTACHING HARDWARE ASSEMBLY

LDG

MTH

0

23-Jun-2017

0

0

931026273022A

6341007-15

9310 9045LEFT MAINLANDING GEAR

321003 TRUNNION ASSEMBLY

LDG

MTH

0

23-Jun-2017

0

0

931026243725A

6341007-16

9310 9045RIGHT MAINLANDING GEAR

321004 TRUNNION ASSEMBLY

LDG

MTH

0

23-Jun-2017

0

0

2110026405966

6341002-27

21100 20835LEFT

321005 TRAILING LINK AND AXLE ASSEMBLY

LDG

MTH

0

23-Jun-2017

0

0

2110026405939

6341002-28

21100 20835RIGHT

321006 TRAILING LINK AND AXLE ASSEMBLY

MTH 23-Jun-2017 0O/C26196468A

6343001-10321007 SHIMMY DAMPER ASSEMBLY

LDG

MTH

0

23-Jun-2017

0

0

2110026306218

6341130-12

21100 20835LEFT

321008 OLEO ASSEMBLY


0:0225-Sep-2019125:48AIR COND

0:2825-Sep-2019265324:25ENG 2

0:2825-Sep-2019265324:25ENG 1

0:2825-Sep-2019265324:25AIRCRAFT


Last ActualDate


HB-VTBReg No:

30-Sep-2019 5:15AM

23-Jun-2017


Print Date:

Airworthiness:

Aircraft Serial:


Unit:

525-0947


(ENG) DUE 2

(ENG) DUE 1

Components

City Part Serial No


C/W Time 2 + or -

Adj. TBO 1

TBO 2 TSO 2

TSO 1

Remains

RemainsDescription


Item Code

Mod Lvl

LDG

MTH

0

23-Jun-2017

0

0

2110026267162

6341130-12

21100 20835RIGHT

321008 OLEO ASSEMBLY

LDG

MTH

0

23-Jun-2017

0

0

1250026097455

6342000-39

12500 12235

321009 FORK AND PISTON ASSEMBLY

LDG

MTH

0

23-Jun-2017

0

0

75001924

1541900-7

7500 7235NOSE LANDINGGEAR

323000

9912370-5

ACTUATOR ASSEMBLY

LDG

MTH

0

23-Jun-2017

0

0

89521758

1541800-13

8952 8687LEFT MAINLANDING GEAR

323001

9912397-8

ACTUATOR ASSEMBLY

LDG

MTH

0

23-Jun-2017

0

0

89521765

1541800-13

8952 8687RIGHT MAINLANDING GEAR

323002

9912397-8

ACTUATOR ASSEMBLY

MTH 23-Jun-2017 0O/C1924

6327504-7323003 NG UPLOCK ACTUATOR

MTH 23-Jun-2017 0O/C4056

6327504-6

LEFT

323005 MLG UPLOCK ACTUATOR

MTH 23-Jun-2017 0O/C4053

6327504-6

RIGHT

323005 MLG UPLOCK ACTUATOR

MTH 23-Jun-2017 0O/C5115A

95784323006 HYD SHUTTLE VALVE

MTH 23-Jun-2017 0O/C2170

3-1527-2

LEFT

324001

9912398-7

MAIN LANDING GEAR WHEEL

MTH 23-Jun-2017 0O/CT0001

3-1527-2

RIGHT

324001

9912398-7

MAIN LANDING GEAR WHEEL

MTH 23-Jun-2017 0O/C9472

3-1418

NOSE

324002 LANDING GEAR WHEEL ASSY

LDG

HRS

MTH

248

300:25

16-Aug-2019

0

0O/C90832339

277K08-1

LEFT

324005 LSZHMLG TIRE

LDG

HRS

MTH

215

267:04

19-Jun-2019

0

0

0O/C90822299

277K08-1

RIGHT

324005 LSZHMLG TIRE

MTH 23-Jun-2017 0O/C6019S00339

030-611-0

NOSE

324007 LANDING GEAR TIRE

MTH 23-Jun-2017 0O/C2412

2-1559-3

LEFT MAINLANDING GEAR

324016 BRAKE ASSY

MTH 23-Jun-2017 0O/C2385

2-1559-3

RIGHT MAINLANDING GEAR

324016 BRAKE ASSY

MTH 23-Jun-2017 0O/C10733

40-955

LEFT

324102 ANTISKID TRANSDUCER ASSEMBLY

MTH 23-Jun-2017 0O/C10732

40-955

RIGHT

324102 ANTISKID TRANSDUCER ASSEMBLY

MTH 23-Jun-2017 0O/C1682

42-707-1324103 BRAKE CONTROL BOX

MTH 23-Jun-2017 0O/C5135

MP50B1324106 HYDRAULIC PUMP MOTOR

MTH 23-Jun-2017 0O/CV594

878208-05324110 EMERGENCY BRAKE VALVE ASSY


65-430087

LEFT

324111 MLG UP & LOCK SWITCH


65-430087

RIGHT

324111 MLG UP & LOCK SWITCH


65-430087324111 NLG UP & LOCK SWITCH


0:0225-Sep-2019125:48AIR COND

0:2825-Sep-2019265324:25ENG 2

0:2825-Sep-2019265324:25ENG 1

0:2825-Sep-2019265324:25AIRCRAFT


Last ActualDate


HB-VTBReg No:

30-Sep-2019 5:15AM

23-Jun-2017


Print Date:

Airworthiness:

Aircraft Serial:


Unit:

525-0947


(ENG) DUE 2

(ENG) DUE 1

Components

City Part Serial No


C/W Time 2 + or -

Adj. TBO 1

TBO 2 TSO 2

TSO 1

Remains

RemainsDescription


Item Code

Mod Lvl

MTH 23-Jun-2017 0O/C1092

38-747502324112 PRESSURE ANTISKID SWITCH


6342000-42325001 NOSE LANDING GEAR ASSEMBLY


1EN118-6

LEFT

326001 M/G DOWN&LOCK SWITCH


1EN118-6

RIGHT

326001 M/G DOWN&LOCK SWITCH


1EN118-6326002 N/G DOWN&LOCK SWITCH

MTH 01-Nov-2016 02889239

40005320-2 30-Nov-2040 254 m 0 d326006

9912368-2

EMERGENCY GEAR BOTTLE

Manufacture Date: 01-Nov-2016

MTH 23-Jun-2017 0O/C176

273-1

CENTER

330001 PANEL LIGHTS DIMMER

MTH 23-Jun-2017 0O/C500006079

CLC500-01331003 INDIRECT LIGHTING CONTROL BOX

MTH 23-Jun-2017 0O/C221003961

CLE221-02

L4

332009 21" LIGHT ASSY

MTH 23-Jun-2017 0O/C221003881

CLE221-02

R4


MTH 23-Jun-2017 0O/C236027488

CLE236-02

L1


MTH 23-Jun-2017 0O/C236028692

CLE236-02

L2


MTH 23-Jun-2017 0O/C236028681

CLE236-02

L3


MTH 23-Jun-2017 0O/C236028727

CLE236-02

R1


MTH 23-Jun-2017 0O/C236028721

CLE236-02

R2


MTH 23-Jun-2017 0O/C236028728

CLE236-02

R3


MTH 23-Jun-2017 0O/C720

84003-3334001 GROUND RECOGNITION LIGHT

MTH 23-Jun-2017 0O/C06010A

01-0770966-00334007 TAIL LIGHT ASSEMBLY

MTH 23-Jun-2017 0O/C162

87-03916-001

LEFT

334008 PTA WINGTIP LIGHT

MTH 23-Jun-2017 0O/C152

87-03917-001

RIGHT

334008 PTA WINGTIP LIGHT

MTH 23-Jun-2017 0O/C115008887

OWL100-03

LH

334009 OVER WING LIGHT

MTH 23-Jun-2017 0O/C115008959

OWL100-03

RH

334009 OVER WING LIGHT

MTH 23-Jun-2017 0O/C206001471

LDL100-02

LEFT

334010 LED LANDING LIGHT

MTH 23-Jun-2017 0O/C206001476

LDL100-02

RIGHT

334010 LED LANDING LIGHT

LDG

HRS

MTH

105

157:06

09-Sep-2018 O/C172570-01

C12406-5341001 ICTAOA COMPUTER

LDG

HRS

MTH

133

194:27

07-Dec-2018

0

0O/C169362-08

C12463-3341002 EDDLAOA INDEXER


0:0225-Sep-2019125:48AIR COND

0:2825-Sep-2019265324:25ENG 2

0:2825-Sep-2019265324:25ENG 1

0:2825-Sep-2019265324:25AIRCRAFT


Last ActualDate


HB-VTBReg No:

30-Sep-2019 5:15AM

23-Jun-2017


Print Date:

Airworthiness:

Aircraft Serial:


Unit:

525-0947


(ENG) DUE 2

(ENG) DUE 1

Components

City Part Serial No


C/W Time 2 + or -

Adj. TBO 1

TBO 2 TSO 2

TSO 1

Remains

RemainsDescription


Item Code

Mod Lvl

LDG

HRS

MTH

133

194:27

07-Dec-2018 O/C1006

C12417-2341009 EDDLAOA SENSOR

MTH 23-Jun-2017 0O/C543-84728

S67-2002

AFT

341010 RADIO ALTIMETER ANTENNA

MTH 23-Jun-2017 0O/C543-84714

S67-2002

FORWARD

341010 RADIO ALTIMETER ANTENNA

LDG

HRS

MTH

133

194:27

07-Dec-2018

0

0O/C586

C12421-1341033

EDDL

AOA INDEXER CONTROLLER

MTH 23-Jun-2017 0O/C42034897

011-00868-10

LEFT

342015 AHRS COMPUTER

MTH 23-Jun-2017 0O/C42034929

011-00868-10

RIGHT

342015 AHRS COMPUTER

MTH 23-Jun-2017 0O/C558

9118009-4342056 MULTI-FUNCTION MODULE

LDG

HRS

MTH

133

194:27

07-Dec-2018

0

0O/C2HU005773

011-02268-01342059

EDDL

GSR 56 IRIDIUM TRANSCEIVER

MTH 23-Jun-2017 0O/C1MB506604

011-01924-10LEFT

342061 GTC 570 PORTRAIT-ORIENTED TOUCHSCREEN CONTROLLER

MTH 23-Jun-2017 0O/C1MB5066606

011-01924-10RIGHT

342061 GTC 570 PORTRAIT-ORIENTED TOUCHSCREEN CONTROLLER

LDG

HRS

MTH

40

61:06

01-Nov-2017

40

61:06

5O/C1Z1006144

011-00831-05

LEFT

342062

KIWA

GEA 71 ENGINE & AIRFRAME IO UNIT

LDG

HRS

MTH

40

61:06

01-Nov-2017

40

61:06

5O/C1Z1006140

011-00831-05

RIGHT

342062

KIWA

GEA 71 ENGINE & AIRFRAME IO UNIT

MTH 23-Jun-2017 0O/C2DC003166

011-01105-40LEFT

342077 GIA 63W INTEGRATED AVIONICS, NAV, COM, GPS/WAAS, FD UNIT

MTH 23-Jun-2017 0O/C2DC003165

011-01105-40RIGHT

342077 GIA 63W INTEGRATED AVIONICS, NAV, COM, GPS/WAAS, FD UNIT

MTH 23-Jun-2017 0O/C1DP007348

011-01768-00342079 GWX 70 WEATHER RADAR


3213

9200-32100-0201

342082 ELECTRONIC STANDBY INDICATOR (4-IN-1) DISPLAY


1F1005655

011-01910-00CENTER

342084 GDU 1400W (MFD) MULTIFUNCTION FLIGHT DISPLAY


1F1005671

011-01910-00COPILOT

342084 GDU 1400W (PFD) PRIMARY FLIGHT DISPLAY


1F1005651

011-01910-00PILOT

342084 GDU 1400W (PFD) PRIMARY FLIGHT DISPLAY


1U6100440

011-02337-01NO. 1

342085 NO. 1 GDC 7400 RVSM AIR DATA COMPUTER


0:0225-Sep-2019125:48AIR COND

0:2825-Sep-2019265324:25ENG 2

0:2825-Sep-2019265324:25ENG 1

0:2825-Sep-2019265324:25AIRCRAFT


Last ActualDate


HB-VTBReg No:

30-Sep-2019 5:15AM

23-Jun-2017


Print Date:

Airworthiness:

Aircraft Serial:


Unit:

525-0947


(ENG) DUE 2

(ENG) DUE 1

Components

City Part Serial No


C/W Time 2 + or -

Adj. TBO 1

TBO 2 TSO 2

TSO 1

Remains

RemainsDescription


Item Code

Mod Lvl


1U6101471

011-02337-01NO. 2

342085 NO. 2 GDC 7400 RVSM AIR DATA COMPUTER

MTH 23-Jun-2017 0O/C1698

117-00254-01342090 GWX70 ANTENNA

MTH 23-Jun-2017 0O/C1CM019362

011-00870-10

LEFT

342800 GMU 44 MAGNETOMETER

MTH 23-Jun-2017 0O/C1CM019380

011-00870-10

RIGHT

342800 GMU 44 MAGNETOMETER

MTH 23-Jun-2017 0O/C5053

DMB20-20343010 MARKER BEACON COUPLER

MTH 23-Jun-2017 0O/C8303

DGSC20-02344001 ANTENNA GLIDESLOPE COUPLER

MTH 23-Jun-2017 0O/C4TTPH

822-0615-206344024 RADIO ALTIMETER INDICATOR

LDG

HRS

MTH

133

194:27

07-Dec-2018 O/C1EJ006356

011-01746-00

344401

EDDL

GDL 59 FLIGHT PARAMETER RECORDER AND WI-FI DATALINK UNIT

MTH 23-Jun-2017 0O/C8454

L10-611-14

LOWER AFT

345001 DME #2 ANTENNA

MTH 23-Jun-2017 0O/C8497

L10-611-14

L/H LOWER

345004 TRANSPONDER ANTENNA

MTH 23-Jun-2017 0O/C8496

L10-611-14

L/H UPPER


MTH 23-Jun-2017 0O/C8554

L10-611-14

R/H LOWER


MTH 23-Jun-2017 0O/C8451

L10-611-14

R/H UPPER


MTH 23-Jun-2017 0O/C2240

MB10-754345005 MARKER BEACON ANTENNA

MTH 23-Jun-2017 0O/C19014

RGS10-48345006 GLIDESLOPE ANTENNA

MTH 23-Jun-2017 0O/C4TY3D

822-1466-001

LEFT

345008 DME 1 RECEIVER

MTH 23-Jun-2017 0O/C180-10771

S65-247-38

LEFT

345022 NAVIGATION(VOR/LOC/GS) ANTENNA

MTH 23-Jun-2017 0O/C180-10772

S65-247-38

RIGHT

345022 NAVIGATION(VOR/LOC/GS) ANTENNA


20S007752

011-01997-00LEFT

345070 GTX 3000 MODE S TCAS II TRANSPONDER


20S007734

011-01997-00RIGHT

345070 GTX 3000 MODE S TCAS II TRANSPONDER

LDG

HRS

MTH

133

194:27

07-Dec-2018

0

0O/C82597

78-8060-6086-5346006

EDDL

STORMSCOPE PROCESSOR

LDG

HRS

MTH

133

194:27

07-Dec-2018

0

0O/CSN-UNKNOWN

78-8051-9200-8346007

EDDL

STORMSCOPE ANTENNA

MTH 23-Jun-2017 0O/C28P006797

011-02571-00346030 TCAS PROCESSOR

MTH 23-Jun-2017 0O/C1U7105159

011-01983-01

LH

346102 GCU 275 PFD CONTROLLER


0:0225-Sep-2019125:48AIR COND

0:2825-Sep-2019265324:25ENG 2

0:2825-Sep-2019265324:25ENG 1

0:2825-Sep-2019265324:25AIRCRAFT


Last ActualDate


HB-VTBReg No:

30-Sep-2019 5:15AM

23-Jun-2017


Print Date:

Airworthiness:

Aircraft Serial:


Unit:

525-0947


(ENG) DUE 2

(ENG) DUE 1

Components

City Part Serial No


C/W Time 2 + or -

Adj. TBO 1

TBO 2 TSO 2

TSO 1

Remains

RemainsDescription


Item Code

Mod Lvl

MTH 23-Jun-2017 0O/C1U7105176

011-01983-01

RH

346102 GCU 275 PFD CONTROLLER

LDG

HRS

MTH

133

194:27

07-Dec-2018

0

0O/C449-8669

S67-1575-165349000

EDDL

IRIDIUM GPS ANTENNA

LDG

HRS

MTH

171

227:30

21-Mar-2019 101801895-824

176276-50 31-May-2033 164 m 0 d350006 LSZHOXYGEN BOTTLE

Manufacture Date: 31-May-2018

MTH 01-Feb-2017 014441768

174252-96 28-Feb-2029 113 m 0 dCOPILOT

351002

9914771-1

OXYGEN MASK

MTH 01-Jan-2017 014441758

174252-96 31-Jan-2029 112 m 0 dPILOT

351002

9914771-1

OXYGEN MASK

MTH 23-Jun-2017 0O/C2817

P21007351008 OXYGEN 3 POSITION VALVE


8373-10-604

APT-389-1000-2400SG

351010 OXYGEN PRESSURE TRANSDUCER

MTH 23-Jun-2017 0O/C11BN165

27431501-10

LEFT

361001 TEMPERATURE SENSOR

MTH 23-Jun-2017 0O/C11BN169

27431501-10

RIGHT

361001 TEMPERATURE SENSOR

HRS

MTH

3500

108

S4883T1660

8161-2 3500

30-Jun-2026

3175:35

81 m 0 dLEFT

361002

9914402-4

REPLACE LEFT B/A PRECOOLER ASSEMBLY

HRS

MTH

3500

108

S4883T1677

8161-2 3500

30-Jun-2026

3175:35

81 m 0 dRIGHT

361002

9914402-4

REPLACE RIGHT B/A PRECOOLER ASSEMBLY

MTH 23-Jun-2017 0O/C12BN76

1H75-25361003

9912510-1

PNEUMATIC REGULATOR

MTH 23-Jun-2017 0O/C1939

2601-21

LEFT

361004 PNEUMATIC SHUTOFF VALVE ASSY

MTH 23-Jun-2017 0O/C1931

2601-21

RIGHT

361004 PNUEMATIC SHUTOFF VALVE ASSY

MTH 23-Jun-2017 0O/C8124

1173T181-2

LEFT

361007 OVER TEMP BLEED AIR SWITCH

MTH 23-Jun-2017 0O/C8134

1173T181-2

RIGHT

361007 OVER TEMP BLEED AIR SWITCH

MTH 23-Jun-2017 0O/C4813

5060-00-1

LEFT

361008 PRECOOLER DOOR VALVE

MTH 23-Jun-2017 0O/C4814

5060-00-1

RIGHT

361008 PRECOOLER DOOR VALVE

MTH 23-Jun-2017 0O/C4002

5253-00-1

LEFT

361009 FLOW CONTROL VALVE

MTH 23-Jun-2017 0O/C4001

5253-00-1

RIGHT

361009 FLOW CONTROL VALVE

MTH 23-Jun-2017 0O/C3853

1553-00-18

LEFT

361010 CHECK VALVE

MTH 23-Jun-2017 0O/C3856

1553-00-18

RIGHT

361010 CHECK VALVE

MTH 23-Jun-2017 0O/C12BN75

1H139-1

LEFT

361011 PRECOOLER ACTUATOR

MTH 23-Jun-2017 0O/C11BN75

1H139-2

RIGHT

361011 PRECOOLER ACTUATOR


MJV3361012 DOOR SEAL CONTROL VALVE


S15501-4522001 DOOR INFLATABLE SEAL


0:0225-Sep-2019125:48AIR COND

0:2825-Sep-2019265324:25ENG 2

0:2825-Sep-2019265324:25ENG 1

0:2825-Sep-2019265324:25AIRCRAFT


Last ActualDate


HB-VTBReg No:

30-Sep-2019 5:15AM

23-Jun-2017


Print Date:

Airworthiness:

Aircraft Serial:


Unit:

525-0947


(ENG) DUE 2

(ENG) DUE 1

Components

City Part Serial No


C/W Time 2 + or -

Adj. TBO 1

TBO 2 TSO 2

TSO 1

Remains

RemainsDescription


Item Code

Mod Lvl

MTH 23-Jun-2017 0O/C5944

P18M30522004 PRESSURE SWITCH

LDG

MTH

0

23-Jun-2017

0

0

2250060424-9

5513056-7

22500 22235LEFT

531000 TRUNNION SUPPORT FITTING

LDG

MTH

0

23-Jun-2017

0

0

22500J55356-9

5513056-8

22500 22235RIGHT

531000 TRUNNION SUPPORT FITTING

LDG

MTH

0

23-Jun-2017

0

0

2250026167445U

6511105-1

22500 22235

531001 ACTUATOR SUPPORT FITTING


6313101-47531201 RADOME ASSEMBLY

MTH 23-Jun-2017 0O/CINYN4

93200-15

LEFT

561001 WINDSHIELD ASSY, (LH)

MTH 23-Jun-2017 0O/C1313

93200-16

RIGHT

561001 WINDSHIELD ASSY, (LH)

MTH 23-Jun-2017 0O/CINV67

6311123-11-1

L1

561002 CABIN DOOR WINDOW

MTH 23-Jun-2017 0O/CINXT5

6311123-11-1

L2

561002 CABIN WINDOW

MTH 23-Jun-2017 0O/CIN6D8-01

6311123-11-1

L3

561002 CABIN WINDOW

MTH 23-Jun-2017 0O/CINV66

6311123-11-1

R1

561002 CABIN WINDOW

MTH 23-Jun-2017 0O/CINXS9

6311123-11-1

R2

561002 CABIN WINDOW


6311123-11-1

R3

561002 CABIN WINDOW


6311123-11-1

R4

561002 CABIN WINDOW

MTH 23-Jun-2017 0O/CIMQM5

6311263-1

PILOT

561003 SIDE WINDOW

MTH 23-Jun-2017 0O/CIMSP0-01

6311263-2

COPILOT

561004 SIDE WINDOW

LDG

MTH

0

23-Jun-2017

0

0

2110026204698C

6322070-21

21100 20835LEFT AFT

571000 TRUNNION ATTACH FITTING

LDG

MTH

0

23-Jun-2017

0

0

2110026204697C

6322070-20

21100 20835RIGHT AFT


LDG

MTH

0

23-Jun-2017

0

0

2110026102897M

6322060-19

21100 20835LEFT FORWARD


LDG

MTH

0

23-Jun-2017

0

0

2110026076665K

6322060-20

21100 20835RIGHT FORWARD


LDG

MTH

0

23-Jun-2017

0

0

2110026102906C

6322080-25

21100 20835LEFT

571002 SIDE BRACE FITTING

LDG

MTH

0

23-Jun-2017

0

0

2110026307369A

6322080-24

21100 20835RIGHT

571002 SIDE BRACE FITTING

HRS

MTH

0

23-Jun-2017

0

0

5000LK3876

LM601SA4

5000 4675:35LEFT ENGINE AFT

712001 ISOLATOR MOUNT

HRS

MTH

0

23-Jun-2017

0

0

50005595

LM601SA5

5000 4675:35LEFT ENGINEFORWARDBOTTOM


HRS

MTH

0

23-Jun-2017

0

0

50005588

LM601SA5

5000 4675:35LEFT ENGINEFORWARD TOP


HRS

MTH

0

23-Jun-2017

0

0

5000LK3864

LM601SA4

5000 4675:35RIGHT ENGINEAFT



0:0225-Sep-2019125:48AIR COND

0:2825-Sep-2019265324:25ENG 2

0:2825-Sep-2019265324:25ENG 1

0:2825-Sep-2019265324:25AIRCRAFT


Last ActualDate


HB-VTBReg No:

30-Sep-2019 5:15AM

23-Jun-2017


Print Date:

Airworthiness:

Aircraft Serial:


Unit:

525-0947


(ENG) DUE 2

(ENG) DUE 1

Components

City Part Serial No


C/W Time 2 + or -

Adj. TBO 1

TBO 2 TSO 2

TSO 1

Remains

RemainsDescription


Item Code

Mod Lvl

HRS

MTH

0

23-Jun-2017

0

0

50005602

LM601SA5

5000 4675:35RIGHT ENGINEFORWARDBOTTOM


HRS

MTH

0

23-Jun-2017

0

0

50005601

LM601SA5

5000 4675:35RIGHT ENGINEFORWARD TOP


MTH 23-Jun-2017 0O/C7749

1173T0759

LH

716000 TEMPERATURE SWITCH

MTH 23-Jun-2017 0O/C7659

1173T0759

RH

716000 TEMPERATURE SWITCH

E/C290299

72100-201

NO. 1

71EN1 ENGINE

E/C290300

72100-201

NO. 2

71EN2 ENGINE

MTH 23-Jun-2017 0O/CAU22669

122141

E1

720007 1ST LP TURBINE NOZZLE

MTH 23-Jun-2017 0O/CAU22664

122141

E2

720007 1ST LP TURBINE NOZZLE

MTH 23-Jun-2017 0O/CABK893

123069

E1

720060 ACCESSORY DRIVE SHAFT

MTH 23-Jun-2017 0O/CABK917

123069

E2

720060 ACCESSORY DRIVE SHAFT

LDG

MTH

0

23-Jun-2017

0

0

10000HW43765

117810

(10000)10000 9735E1

723001 FAN ROTOR

LDG

MTH

0

23-Jun-2017

0

0

10000HW43761

117810

(10000)10000 9735E2

723001 FAN ROTOR

LDG

MTH

0

23-Jun-2017

0

0

8000HW44232

122723

(8000)8000 7735E1

723010 HP COMPRESSOR ROTOR

LDG

MTH

0

23-Jun-2017

0

0

8000HW44236

122723

(8000)8000 7735E2

723010 HP COMPRESSOR ROTOR

LDG

MTH

0

23-Jun-2017

0

0

10000HW44861

66032

(10000)10000 9735E1

723015 IP COMPRESSOR ROTOR

LDG

MTH

0

23-Jun-2017

0

0

10000HW44863

66032

(10000)10000 9735E2

723015 IP COMPRESSOR ROTOR

MTH 23-Jun-2017 0O/CAU22336

114614

E1

723022 DIFFUSER CASE ASSEMBLY

MTH 23-Jun-2017 0O/CAU22335

114614

E2

723022 DIFFUSER CASE ASSEMBLY

MTH 23-Jun-2017 0O/CRX16RT3268

118924

E1

723061 HIGH PRESSURE SHAFT

MTH 23-Jun-2017 0O/CRX16RT3261

118924

E2

723061 HIGH PRESSURE SHAFT

MTH 23-Jun-2017 0O/CRX16NG0744

121728

E1

723092 COMPLETE LP SHAFT ASSEMBLY

MTH 23-Jun-2017 0O/CRX16NG0769

121728

E2

723092 COMPLETE LP SHAFT ASSEMBLY

MTH 23-Jun-2017 0O/CAU22454

69885

E1

723149 HP COMPRESSOR COVER ASSY

MTH 23-Jun-2017 0O/CAU22453

69885

E2

723149 HP COMPRESSOR COVER ASSY

MTH 23-Jun-2017 0O/CHW43729

111386

E1

724035 HP TURBINE ROTOR ASSEMBLY

MTH 23-Jun-2017 0O/CHW43207

111386

E2

724035 HP TURBINE ROTOR ASSEMBLY

MTH 23-Jun-2017 0O/CAU201165

115471

E1

724045 SEAL AND FUEL SLINGER ASSEMBLY

MTH 23-Jun-2017 0O/CAU201167

115471

E2

724045 SEAL AND FUEL SLINGER ASSEMBLY


0:0225-Sep-2019125:48AIR COND

0:2825-Sep-2019265324:25ENG 2

0:2825-Sep-2019265324:25ENG 1

0:2825-Sep-2019265324:25AIRCRAFT


Last ActualDate


HB-VTBReg No:

30-Sep-2019 5:15AM

23-Jun-2017


Print Date:

Airworthiness:

Aircraft Serial:


Unit:

525-0947


(ENG) DUE 2

(ENG) DUE 1

Components

City Part Serial No


C/W Time 2 + or -

Adj. TBO 1

TBO 2 TSO 2

TSO 1

Remains

RemainsDescription


Item Code

Mod Lvl

LDG

MTH

0

23-Jun-2017

0

0

8000HW43729

73853

(8000)8000 7735E1

725010 HP TURBINE DISK

LDG

MTH

0

23-Jun-2017

0

0

8000HW42307

73853

(8000)8000 7735E2

725010 HP TURBINE DISK

LDG

MTH

0

23-Jun-2017

0

0

10000HW43343

72704

(10000)10000 9735E1

725020

411

1ST LP TURBINE DISK

LDG

MTH

0

23-Jun-2017

0

0

10000HW43778

72704

(10000)10000 9735E2

725020

411

1ST LP TURBINE DISK

LDG

MTH

0

23-Jun-2017

0

0

10000HW43821

66993

(10000)10000 9735E1

725030 2ND LP TURBINE DISK

LDG

MTH

0

23-Jun-2017

0

0

10000HW43825

66993

(10000)10000 9735E2

725030 2ND LP TURBINE DISK


MX21593

120746E1

726011 ACCESSORY DRIVE GEARBOX ASSEMBLY


MX21587

120746E2

726011 ACCESSORY DRIVE GEARBOX ASSEMBLY

MTH 23-Jun-2017 0O/C11184

1103P0448

LEFT ENGINE

730001 FUEL PRESSURE SWITCH

MTH 23-Jun-2017 0O/C11232

1103P0448

RIGHT ENGINE

730001 FUEL PRESSURE SWITCH

MTH 23-Jun-2017 0O/CGE-6074

57847

NO. 1

732301 ELECTRIC IND-FUEL FILTER

MTH 23-Jun-2017 0O/CGE-6090

57847

NO. 2

732301 ELECTRIC IND-FUEL FILTER

MTH 23-Jun-2017 0O/CCL16AW2975

122108

LEFT ENGINE

732500 FADEC

LDG

HRS

MTH

248

300:25

16-Aug-2019 O/CCL12AW1986

122108

RIGHT ENGINE

732500 LSZHFADEC

MTH 23-Jun-2017 0O/CAAT3371

1573-4

LEFT ENGINE

733001 FUEL FLOW TRANSMITTER

MTH 23-Jun-2017 0O/CAAT3369

1573-4

RIGHT ENGINE

733001 FUEL FLOW TRANSMITTER

MTH 23-Jun-2017 0O/CBCC-00003380

50817

E1

730002

115

FUEL NOZZLE ASSEMBLY

MTH 23-Jun-2017 0O/CBCC-00004057

50817

E2

730002

115

FUEL NOZZLE ASSEMBLY

MTH 23-Jun-2017 0O/CAU22607

121784

E1

731040 FUEL MANIFOLD ASSEMBLY

MTH 23-Jun-2017 0O/CAU22608

121784

E2

731040 FUEL MANIFOLD ASSEMBLY

MTH 23-Jun-2017 0O/CGE-6074

57847

E1

732301 ELEC FUEL FILTER INDICATOR

MTH 23-Jun-2017 0O/CGE-6090

57847

E2

732301 ELEC FUEL FILTER INDICATOR

HRS

MTH

0

23-Jun-2017

0

0

8000CL6ATW1183

119148

(8000)8000 7675:35E1

732401 FUEL DELIVERY UNIT

HRS

MTH

0

23-Jun-2017

0

0

8000CL6ATW1166

119148

(8000)8000 7675:35E2

732401 FUEL DELIVERY UNIT

MTH 23-Jun-2017 0O/CCK-1601236

68145

E1 INBOARD

741010 IGNITION EXCITER

MTH 23-Jun-2017 0O/CCK-1601237

68145

E2 INBOARD


MTH 23-Jun-2017 0O/CCK-1601248

68145

E1 OUTBOARD



0:0225-Sep-2019125:48AIR COND

0:2825-Sep-2019265324:25ENG 2

0:2825-Sep-2019265324:25ENG 1

0:2825-Sep-2019265324:25AIRCRAFT


Last ActualDate


HB-VTBReg No:

30-Sep-2019 5:15AM

23-Jun-2017


Print Date:

Airworthiness:

Aircraft Serial:


Unit:

525-0947


(ENG) DUE 2

(ENG) DUE 1

Components

City Part Serial No


C/W Time 2 + or -

Adj. TBO 1

TBO 2 TSO 2

TSO 1

Remains

RemainsDescription


Item Code

Mod Lvl

MTH 23-Jun-2017 0O/CCK-1601249

68145

E2 OUTBOARD


MTH 23-Jun-2017 0O/CCK-1600842

68032

E1 INBOARD

742201 IGNITOR

MTH 23-Jun-2017 0O/CCK-1600821

68032

E1 OUTBOARD

742201 IGNITOR

MTH 23-Jun-2017 0O/CCK-1600803

68032

E2 INBOARD

742201 IGNITOR

MTH 23-Jun-2017 0O/CCK-1600763

68032

E2 OUTBOARD

742201 IGNITOR

MTH 23-Jun-2017 0O/CMD-0189411

57355

E1

771005 N1 DUAL MAGNETIC SPEED SENSOR

MTH 23-Jun-2017 0O/CMD-0189415

57355

E2


MTH 23-Jun-2017 0O/CAXT0201938

114944

E1

771005A TT2 SENSOR

MTH 23-Jun-2017 0O/CAXT0201886

114944

E2

771005A TT2 SENSOR

MTH 23-Jun-2017 0O/CMD-0188295

54831

E1


MTH 23-Jun-2017 0O/CMD-0189352

54831

E2


MTH 23-Jun-2017 0O/CEMX003622

75378

E1

772002 ITT HARNESS

MTH 23-Jun-2017 0O/CEMX003623

75378

E2

772002 ITT HARNESS

MTH 23-Jun-2017 0O/C199302

MS28034-3

LEFT ENGINE

793002 OIL TEMPERATURE TRANSMITTER

MTH 23-Jun-2017 0O/C199212

MS28034-3

RIGHT ENGINE

793002 OIL TEMPERATURE TRANSMITTER

MTH 23-Jun-2017 0O/C4137

S1103P89-3

LEFT ENGINE

793006 OIL PRESSURE SWITCH

MTH 23-Jun-2017 0O/C4043

S1103P89-3

RIGHT ENGINE

793006 OIL PRESSURE SWITCH

MTH 23-Jun-2017 0O/C08-07-8404

S2800-1128

LEFT

793008 OIL TRANSDUCER

MTH 23-Jun-2017 0O/C8404-8-749

S2800-1128

RIGHT

793008 OIL TRANSDUCER

MTH 23-Jun-2017 0O/CPP2220

121535

E1

792201 LUBE OIL COOLER

MTH 23-Jun-2017 0O/CPP2219

121535

E2

792201 LUBE OIL COOLER

HRS

MTH

0

23-Jun-2017

0

0

5000MX20238

125142

(5000)5000 4675:35E1

792401 LUBE AND SCAVENGE PUMP

HRS

MTH

0

23-Jun-2017

0

0

5000MX20114

125142

(5000)5000 4675:35E2

792401 LUBE AND SCAVENGE PUMP

HRS

MTH

0

23-Jun-2017

0

0

1000628

MG94D-4

1000 675:35LEFT ENGINE

801101 STARTER/GENERATOR

HRS

MTH

0

23-Jun-2017

0

0

1000555

MG94D-4

1000 675:35RIGHT ENGINE

801101 STARTER/GENERATOR


0:0225-Sep-2019125:48AIR COND

0:2825-Sep-2019265324:25ENG 2

0:2825-Sep-2019265324:25ENG 1

0:2825-Sep-2019265324:25AIRCRAFT


Last ActualDate


HB-VTBReg No:

30-Sep-2019 5:15AM

23-Jun-2017


Print Date:

Airworthiness:

Aircraft Serial:


Unit:

525-0947


(ENG) DUE 2

(ENG) DUE 1

Service Bulletins

City Part Serial No


C/W Time 2 + or -

Adj. TBO 1

TBO 2 TSO 2

TSO 1

Remains

RemainsDescription


Item Code

Mod Lvl

MTH -INFORMATIONAL

SL CIL-03-01 CERTIFICATION REQUIREMENTS - SUPPLEMENTAL TYPE CERTIFICATE (STC)

MOC :

MTH -RECOMMENDED Complete

SL CIL-99-03 R01 MISCELLANEOUS - CORROSION PREVENTION AND CONTROL PROGRAM (CPCP)

COMPLIED WITH - TASKS 05CPC01 THRU 05CPCP04 FULFILLS THIS CIL / DE.MG.0011 / CDE / 11-OCT-2018MOC :

MTH -INFORMATIONAL

SL 525-02-01 MISCELLANEOUS - YEAR 2000 READINESS DISCLOSURE

MOC :

MTH -INFORMATIONAL

SL 525-02-02 MISCELLANEOUS - CESSNA CD-ROM TECHNICAL LIBRARY

MOC :

MTH -INFORMATIONAL

SL 525-03-02 CERTIFICATION REQUIREMENTS - AIRPLANE FLIGHT MANUAL REPLACEMENT

MOC :

MTH -

SL 525-99-01 R01 CANCELLATION OF SL525-99-01, CD-ROM TECHNICAL LIBRARY

MOC :

MTH -

SL 525-99-02 R05 MISCELLANEOUS - CESCOM PRICES (THIS SL CANCELS SL525-99-02 R4 AND PREVIOUS)

MOC :

MTH -INFORMATIONAL

SL CIL-99-04 MISCELLANEOUS - INCREMENTAL LIBRARY UPDATES FOR CESVIEW

MOC :

MTH -INFORMATIONAL

SL 525-03-01 R01 SUPPLEMENTAL TYPE CERTIFICATE (THIS SL IS REPLACED BY CIL-03-01)

MOC :

MTH -INFORMATIONAL

SL 525-99-04 R02 MISCELLANEOUS - TRANSMITTAL OF CESSNA'S CERTIFICATION REQUIREMENTS FOR PORTABLE ELECTRONIC DEVICE USAGE

MOC :

MTH -INFORMATIONAL

SL 525-05-01 TIME LIMITS/MAINTENANCE CHECKS - SKIN SEAM INSPECTION REQUIREMENTS

MOC :

MTH -INFORMATIONAL

SL 525-05-02 TIME LIMITS/MAINTENANCE CHECKS - CORROSIVE ENVIRONMENT INSPECTION

MOC :

MTH -INFORMATIONAL N/A

SL 525-05-06 TIME LIMITS/MAINTENANCE CHECKS - LANDING GEAR LIFE LIMIT EXEMPTION

NOT APPLICABLE - TO SERIAL NUMBER / DE.MG.0011 / CDE / 20-NOV-2018MOC :

MTH -INFORMATIONAL

SL CIL-99-01 R02 USE OF CORROSION INHIBITING COMPOUNDS

MOC :


0:0225-Sep-2019125:48AIR COND

0:2825-Sep-2019265324:25ENG 2

0:2825-Sep-2019265324:25ENG 1

0:2825-Sep-2019265324:25AIRCRAFT


Last ActualDate


HB-VTBReg No:

30-Sep-2019 5:15AM

23-Jun-2017


Print Date:

Airworthiness:

Aircraft Serial:


Unit:

525-0947


(ENG) DUE 2

(ENG) DUE 1

Service Bulletins

City Part Serial No


C/W Time 2 + or -

Adj. TBO 1

TBO 2 TSO 2

TSO 1

Remains

RemainsDescription


Item Code

Mod Lvl

MTH -RECOMMENDED

SL CIL-99-02 MISCELLANEOUS - AVOID OPERATIONS ON RUNWAYS TREATED WITH RUNWAY DE-ICE (RDI) FLUIDS. AIRCRAFT WASHING RECOMMENDED AFTEREXPOSURE TO RDI FLUIDS

- THIS SERVICE LETTER CONTAINS CESSNA RECOMMENDATIONS THAT WILL ASSIST IN PREVENTING CORROSION ONAIRPLANES FROM EXPOSURE TO RDI FLUIDS.

MOC :

MTH -INFORMATIONAL

SL 525-12-01 SERVICING - BEARING, MAIN LANDING GEAR TRUNNION PIN BEARING

MOC :

MTH -INFORMATIONAL

SL CIL-20-01 R02 STANDARD PRACTICES - CESSNA CERTIFICATION OF NONDESTRUCTIVE TESTING FACILITIES/PERSONNEL

MOC :

MTH -INFORMATIONAL

SL 525-20-01 R19 STANDARD PRACTICES - CESSNA CERTIFICATION OF NONDESTRUCTIVE TESTING FACILITIES/PERSONNEL (SUPERSEDED BY CIL-20-01 R2)

MOC :

MTH -INFORMATIONAL

SL 525-20-02 STANDARD PRACTICES - WING LEADING EDGE PAINT PROCEDURE VIDEO AND SPECIAL TOOLS

MOC :

MTH -INFORMATIONAL

SL 525-20-03 STANDARD PRACTICES - HAZARDOUS AIR POLLUTANTS

MOC :

-INFORMATIONAL

SL 525-20-06 STANDARD PRACTICES - CESSNA STANDARD PRACTICES MANUAL

MOC :

MTH -OPTIONAL

SB 525-23-08 COMMUNICATIONS - ALLIEDSIGNAL 8.33 KHZ COMMUNICATION RADIO INSTALLATION

MOC :

MTH -RECOMMENDED

N/ASB 525-23-11 COMMUNICATIONS - GARMIN RADIO MODIFICATION

NOT APPLICABLE - NOT EQUIPPED WITH GNS 420, GNC 430 OR GNC 530 / DE.MG.0011 / CDE / 11-OCT-2018MOC :

MTH -OPTIONAL

SB 525-23-13 COMMUNICATIONS - GARMIN RADIO REPLACEMENT

MOC :

MTH -INFORMATIONAL

SL 525-23-01 COMMUNICATIONS - TRANSMITTAL OF LORAL DATA SYSTEMS FIELD SERVICE BULLETIN GACVR 010, ALTERNATE SUPPLIERS FOR UNDERWATERLOCATOR BEACONS

MOC :

MTH -INFORMATIONAL

SL 525-23-02 COMMUNICATIONS - TRANSMITTAL OF LORAL DATA SYSTEMS FIELD SERVICE BULLETIN CVR163 ANDN CVR164

MOC :

-OPTIONAL

SL 525-23-11 COMMUNICATIONS - ATG 5000 SOFTWARE UPGRADE

MOC :

-OPTIONAL

SL 525-23-12 COMMUNICATIONS - ATG 5000 SOFTWARE UPDATE TO VERSION 2.8

MOC :

MTH -OPTIONAL

SB 525-24-07 R02 ELECTRICAL POWER - 44 AMP HOUR BATTERY INSTALLATION

MOC :


0:0225-Sep-2019125:48AIR COND

0:2825-Sep-2019265324:25ENG 2

0:2825-Sep-2019265324:25ENG 1

0:2825-Sep-2019265324:25AIRCRAFT


Last ActualDate


HB-VTBReg No:

30-Sep-2019 5:15AM

23-Jun-2017


Print Date:

Airworthiness:

Aircraft Serial:


Unit:

525-0947


(ENG) DUE 2

(ENG) DUE 1

Service Bulletins

City Part Serial No


C/W Time 2 + or -

Adj. TBO 1

TBO 2 TSO 2

TSO 1

Remains

RemainsDescription


Item Code

Mod Lvl

MTH -OPTIONAL

SB 525-24-19 R02 ELECTRICAL POWER - CONCORDE LEAD ACID BATTERY INSTALLATION

MOC :

MTH -OPTIONAL

SB 525-24-25 ELECTRICAL POWER - NICKEL-CADMIUM BATTERY INSTALLATION

MOC :

ACH

LDG

HRS

MTH

65:06

51

78:18

25-Jan-2018 -RECOMMENDED Complete

SB 525-24-31 R01

KICT

ELECTRICAL POWER - POWER J-BOX START RELAY MODIFICATION

COMPLIED WITH - ACCOMPLISHED SB525-24-31 R1; POWER J-BOX START RELAY MODIFICATION, DATED DECEMBER 31, 2017.MOC :

MTH -OPTIONAL

SB 525-25-22 R01 EQUIPMENT/FURNISHINGS - GLARESHIELD LEATHER STRIP INSTALLATION

MOC :

MTH -OPTIONAL

SB 525-25-23 R01 EQUIPMENT/FURNISHINGS - THREE FREQUENCY EMERGENCY LOCATOR TRANSMITTER (ELT) WITH NAVIGATION INTERFACE INSTALLATION

MOC :

MTH -OPTIONAL

SB 525-25-30 R01 EXTENDED RECLINE RIGHT FORWARD DIVIDER INSTALLATION

MOC :

MTH 60RECOMMENDED 23-Jun-2022 32 m 23 d

SAIB CE-19-12 ACR ELECTRONICS, INC. EMERGENCY LOCATOR TRANSMITTERS (ELT) G406-4, C406-1, C406-1HM, C406-2, C406-2HM, C406-N AND C406-NHM -EQUIPMENT/FURNISHINGS: EMERGENCY LOCATOR BEACON, G-SWITCH - REPLACE G-SWITCH

MOC :

-OPTIONAL

SL 525-25-07 EQUIPMENT/FURNISHINGS - TOILET DRIP TRAY INSTALLATION

MOC :

MTH -OPTIONAL

SL 525-25-08 EQUIPMENT/FURNISHINGS - MODIFICATION OF THE PASSENGER SEATS

MOC :

MTH -RECOMMENDED N/A

SL 525-25-09 EQUIPMENT/FURNISHINGS - INSPECTION OF THE MILLENNIUM CREW SEAT ASSEMBLIES FOR INCORRECTLY INSTALLED SEAT PAN TILT MECHANISMSNAP RINGS (MILLENNIUM SERVICE BULLETIN SB2049-25-20-02)

NOT APPLICABLE - By Effectivity: CH.MG.7033 - A.GrefMOC :

MTH -OPTIONAL

SB 525-27-16 R02 FLIGHT CONTROLS - STEEP APPROACH CERTIFICATION - SPEED BRAKE SWITCH ADJUSTMENT

MOC :

MTH -MANDATORY

N/ASB CAS1480ISSUE A

TAMARACK ATLAS ENHANCEMENTS IMPLEMENTATION

NOT APPLICABLE - NOT EQUIPPED WITH TAMARACK ATLAS WINGLETS / DE.MG.0011 / CDE / 12-JUL-2019MOC :

MTH -MANDATORY

N/ASL 525-27-06 R01 FLIGHT CONTROLS - ELEVATOR HARDWARE INSPECTION

NOT APPLICABLE - TO S/N / DE.MG.0011 / CDE / 14-JUN-2019MOC :

MTH -INFORMATIONAL

SL CIL-30-01 R01 ICE AND RAIN PROTECTION - APPROVED DEICING PROGRAM UPDATES

MOC :


0:0225-Sep-2019125:48AIR COND

0:2825-Sep-2019265324:25ENG 2

0:2825-Sep-2019265324:25ENG 1

0:2825-Sep-2019265324:25AIRCRAFT


Last ActualDate


HB-VTBReg No:

30-Sep-2019 5:15AM

23-Jun-2017


Print Date:

Airworthiness:

Aircraft Serial:


Unit:

525-0947


(ENG) DUE 2

(ENG) DUE 1

Service Bulletins

City Part Serial No


C/W Time 2 + or -

Adj. TBO 1

TBO 2 TSO 2

TSO 1

Remains

RemainsDescription


Item Code

Mod Lvl

MTH -MANDATORY N/A

SL 525-30-05 R02 ICE AND RAIN PROTECTION - WINDSHIELD TEMPERATURE SENSOR INSPECTION


-INFORMATIONAL

SL CIL-31-01 INDICATING/RECORDING SYSTEMS - CVR, FDR, AND CVDR 90-DAY BATTERY UNDERWATER LOCATOR BEACON (ULB) INSTALLATION

MOC :

MTH -INFORMATIONAL

SL CIL-32-01 LANDING GEAR - IMPROVED NOSE WHEEL GREASE SEAL

MOC :

MTH -INFORMATIONAL

SL CIL-32-04 WIRELESS TIRE PRESSURE MONITORING SYSTEM INSTALLATION

MOC :

MTH -INFORMATIONAL

SL 525-32-03 LANDING GEAR - TRANSMITTAL OF BF GOODRICH SERVICE BULLETIN 2-1559-32-1 LANDING GEAR-MAIN BRAKE ASSEMBLY-CRACKED STATOR DISKS

MOC :

MTH -INFORMATIONAL

SL 525-32-04 LANDING GEAR - TRANSMITTAL OF BFGOODRICH SERVICE LETTER SL1636 REVISION 1, NOSE WHEEL IMPROVED GREASE SEAL

MOC :

MTH -INFORMATIONAL

SL 525-32-05 LANDING GEAR - INFORMATION REGARDING TIRE MANUFACTURERS

MOC :

MTH -INFORMATIONAL

SL 525-32-07 LANDING GEAR - GEAR UNLOCK IN-FLIGHT SYSTEM CHECK

MOC :

MTH -INFORMATIONAL

SL 525-32-16 LANDING GEAR - TRANSMITTAL OF BF GOODRICH SERVICE LETTER SL1878, EFFECT OF DISINFECTANT ON WHEEL AND BRAKE ASSEMBLIES

MOC :

MTH -OPTIONAL

SL 525-32-17 R01 LANDING GEAR - NOSE LANDING GEAR ICE PROTECTION BOOT INSTALLATION

MOC :

MTH -INFORMATIONAL

SL 525-32-18 LANDING GEAR - MAIN LANDING GEAR SIMULATOR TEST BOX

MOC :

MTH -OPTIONAL

N/ASB 525-33-10 LIGHTS - WING TIP LED LIGHT MODIFICATION

NOT APPLICABLE - N/A TO S/N / DE.MG.0011 / CDE / 02-APR-2019MOC :

MTH -INFORMATIONAL

SL CIL-33-01 LIGHTS - TRANSMITTAL OF RADIANT POWER CORP. SB-RPC-001, PROCEDURE TO REPLACE OBSOLETE CONNECTOR ASSEMBLY FOR CBS28EMERGENCY BATTERY

MOC :

MTH -RECOMMENDED

N/ASB 525-34-30 R01 NAVIGATION - ART 2000-6 RADAR MODIFICATION

NOT APPLICABLE - NOT EQUIPPED WITH ART 2000-6 RADAR / DE.MG.0011 / CDE / 11-OCT-2018MOC :

MTH -OPTIONAL

SB 525-34-40 R02 NAVIGATION - REDUCED VERTICAL SEPARATION MINIMUM (RVSM) OPERATION MODIFICATION

MOC :


0:0225-Sep-2019125:48AIR COND

0:2825-Sep-2019265324:25ENG 2

0:2825-Sep-2019265324:25ENG 1

0:2825-Sep-2019265324:25AIRCRAFT


Last ActualDate


HB-VTBReg No:

30-Sep-2019 5:15AM

23-Jun-2017


Print Date:

Airworthiness:

Aircraft Serial:


Unit:

525-0947


(ENG) DUE 2

(ENG) DUE 1

Service Bulletins

City Part Serial No


C/W Time 2 + or -

Adj. TBO 1

TBO 2 TSO 2

TSO 1

Remains

RemainsDescription


Item Code

Mod Lvl

MTH -OPTIONAL

SB 525-34-60 NAVIGATION - GARMIN GNS-530A RADIOS/FMS AND GTX-330D TRANSPONDER INSTALLATION

MOC :

MTH -OPTIONAL

SB 525-34-63 NAVIGATION - MST-67A DIVERSITY TRANSPONDER INSTALLATION

MOC :

MTH -OPTIONAL

SB 525-34-74 NAVIGATION - DIVERSITY ANTENNA INSTALLATION FOR ENHANCED SURVEILLANCE TRANSPONDERS

MOC :

LDG

HRS

MTH

133

194:27

07-Dec-2018 -OPTIONAL

CompleteSB 525-34-91

EDDL

NAVIGATION - STORMSCOPE SYSTEM INSTALLATION

COMPLIED WITH - WX1000E STORMSCOPE (OPTIONAL EQUIPMENT #629S) STORMSCOPE (OPTIONAL EQUIPMENT #629S)INSTALLED IAW SB525-34-91 NAVIGATION - STORMSCOPE SYSTEM INSTALLATION. ALL WORK PERFORMED IAW SB525-34-91INSTRUCTIONS REV. DECEMBER 18, 2015. STORMSCOPE PROCESSOR PN: 78-8060-6086-5 SN: 82597 STATUS: NEW

MOC :

MTH -OPTIONAL

SB 525-34-92 NAVIGATION - GARMIN G3000 SURFACEWATCH INSTALLATION

MOC :

MTH -CANCELLED

SL CIL-34-05 R01 TRANSMITTAL OF GARMIN SERVICE ALERT 1478, LP AND LPV APPROACHES

MOC :

MTH -INFORMATIONAL

SL CIL-34-07 NAVIGATION - TRANSMITTAL OF GARMIN SERVICE ADVISORY 1604 WORLDWIDE NAVIGATION DATABASE

MOC :

MTH -INFORMATIONAL

SL 525-34-07 NAVIGATION - B-RNAV OPERATION NAVIGATION SYSTEM APPROVAL

MOC :

LDG

HRS

MTH

106

157:42

13-Sep-2018 -MANDATORY N/A

SL 525-34-08

ICT

NAVIGATION - TRANSMITTAL OF BFGOODRICH ALERT SERVICE BULLETIN 78A

NOT APPLICABLE - SL525-34-08; TRANSMITTAL OF BF GOODRICH ASB 78A; DOES NOT APPLY DUE TO EQUIPMENT NOTINSTALLED.

MOC :

LDG

HRS

MTH

106

157:42


SL 525-34-09

ICT

NAVIGATION - TRANSMITTAL OF BF GOODRICH ALERT SERVICE BULLETIN #79

NOT APPLICABLE - SL525-34-09; TRANSMITTAL OF BF GOODRICH ASB 79; DOES NOT APPLY DUE TO EQUIPMENT NOTINSTALLED.

MOC :

MTH -INFORMATIONAL

SL 525-34-11 NAVIGATION - TRANSMITTAL OF HONEYWELL SERVICE BULLETIN KT 70-5 FOR KT 70 MODE S TRANSPONDER

MOC :

MTH -INFORMATIONAL

SL 525-34-17 NAVIGATION - TRANSMITTAL OF ROCKWELL COLLINS OPERATORS BULLETIN OPSB 0034-03, FLIGHT DIRECTOR ANOMALLY: FAILURE TO PROVIDEPROPER GUIDANCE

MOC :


0:0225-Sep-2019125:48AIR COND

0:2825-Sep-2019265324:25ENG 2

0:2825-Sep-2019265324:25ENG 1

0:2825-Sep-2019265324:25AIRCRAFT


Last ActualDate


HB-VTBReg No:

30-Sep-2019 5:15AM

23-Jun-2017


Print Date:

Airworthiness:

Aircraft Serial:


Unit:

525-0947


(ENG) DUE 2

(ENG) DUE 1

Service Bulletins

City Part Serial No


C/W Time 2 + or -

Adj. TBO 1

TBO 2 TSO 2

TSO 1

Remains

RemainsDescription


Item Code

Mod Lvl

MTH -INFORMATIONAL

SL 525-34-21 NAVIGATION - TRANSMITTAL OF GARMIN SERVICE ALERT, DIRECT-TO-WAYPOINT SELECTION SERVICE ALERT: 050721-00

MOC :

MTH -INFORMATIONAL

SL 525-34-25 NAVIGATION - TRANSMITTAL OF L-3 COMMUNICATIONS AVIONICS SYSTEMS¿ SERVICE LETTER SL-230 (REV. A)

MOC :

MTH -INFORMATIONAL

SL 525-34-28 TRANSMITTAL OF GARMIN SERVICE ADVISORY NO. 1433 POTENTIAL GWX 70 POWER AMPLIFIER FAILURE IN GROUND MAP MODE

MOC :

MTH -INFORMATIONAL

SL 525-34-29 NAVIGATION - TRANSMITTAL OF GARMIN SERVICE ADVISORY NO. 1529, PROCEDURE LEGS IN TERMINAL PROCEDURES

MOC :

MTH -INFORMATIONAL

SL 525-34-30 NAVIGATION - TRANSMITTAL OF GARMIN SERVICE ADVISORY NO. 1514, POTENTIAL ERRONEOUS LATERAL GUIDANCE

MOC :

MTH -INFORMATIONAL

SL 525-34-33 NAVIGATION - TRANSMITTAL OF GARMIN SERVICE ADVISORY NO 1612 2015 IGRF (INTERNATIONAL GEOMAGNETIC REFERENCE FIELD) MAGNETICFIELD MODEL

MOC :

-INFORMATIONAL

SL 525-34-34 NAVIGATION - TRANSMITTAL OF GARMIN SERVICE ADVISORY 1802 INCORRECT DIRECT-TO NAVIGATION FOLLOWING INTERCEPT (INTRCPT) LEG ANDSERVICE ADVISORY 1822 DME/DME NAVIGATION

MOC :

LDG

HRS

MTH

106

157:42


SLA 525-34-04

ICT

NAVIGATION - KLN89B,KLN90B AND KLN900 GPS INSTRUMENT LANDING SYSTEM APPOROACH RESTRICTIONS

NOT APPLICABLE - SLA525-34-04; KLN89B, KLN90B & KLN900 GPS INSTRUMENT LANDING SYSTEM APPOROACHRESTRICTIONS. DOES NOT APPLY DUE TO EQUIPMENT NOT INSTALLED.

MOC :

LDG

HRS

DAYS

106

157:42


SL CIL-35-05

ICT

OXYGEN - TRANSMITTAL OF ZODIAC AEROSPACE SB MCF-SBU-35-001

NOT APPLICABLE - SL CIL-35-05; TRANSMITTAL OF ZODIAC AEROSPACE SB MCF-SBU-35-001; DOES NOT APPLY DUE TO PARTNUMBER INSTALLED.

MOC :

MTH -INFORMATIONAL

SL 525-35-01 OXYGEN - TRANSMITTAL OF SCOTT/EROS SERVICE INFORMATION LETTER NUMBER 15

MOC :

LDG

HRS

MTH

251

303:19

18-Sep-2019 -INFORMATIONAL Complete

COM MC 525-002 PURGE MOISTURE FROM SERVICE AIR PRIOR TO CLOSING DOOR

COMPLIED WITH - INFORMATIONAL ONLY: CH.MG.7033 - A.GREFMOC :

MTH -OPTIONAL

SB 525-53-07 R02 FUSELAGE - AFT BAGGAGE SECTION SKI OPTION INSTALLATION

MOC :


0:0225-Sep-2019125:48AIR COND

0:2825-Sep-2019265324:25ENG 2

0:2825-Sep-2019265324:25ENG 1

0:2825-Sep-2019265324:25AIRCRAFT


Last ActualDate


HB-VTBReg No:

30-Sep-2019 5:15AM

23-Jun-2017


Print Date:

Airworthiness:

Aircraft Serial:


Unit:

525-0947


(ENG) DUE 2

(ENG) DUE 1

Service Bulletins

City Part Serial No


C/W Time 2 + or -

Adj. TBO 1

TBO 2 TSO 2

TSO 1

Remains

RemainsDescription


Item Code

Mod Lvl

MTH -INFORMATIONAL

SL 525-53-01 FUSELAGE - LIGHTNING DIVERTER STRIP INSTALLATION/REPAIR PROCEDURE CHANGE (RADOME)

MOC :

MTH -MANDATORY N/A

SL 525-53-09 R01 FUSELAGE - NOSE WHEEL WELL RIVET INSPECTION/INSTALLATION


DAYS

MTH -MANDATORY N/A

SL 525-53-10 R01 FUSELAGE - WIRE BUNDLE ANCHOR INSPECTION ON FORWARD FAIRING


DAYS

MTH -MANDATORY N/A

SL 525-55-03 R01 STABILIZERS - HORIZONTAL STABILIZER FASTENER INSPECTION


MTH -OPTIONAL

N/AVSB SBATLAS-57-05

TACS CENTERING STRIP MODIFICATION

NOT APPLICABLE - NOT EQUIPPED WITH TAMARACK ATLAS WINGLETS / DE.MG.0011 / CDE / 06-MAY-2019MOC :

MTH -INFORMATIONAL

SL 525-71-02 POWER PLANTS - TRANSMITTAL OF AEROQUIP AEROSPACE SERVICE BULLETIN ASB125 HOW TO REPAIR SILICONE COVERED HOSE ABRASIONSUSING AE272 FLEXWRAP FIRESLEEVE

MOC :

MTH -INFORMATIONAL

SL 525-71-04 POWER PLANT - ENGINE - DESALINIZATION RINSE - REMOVE BLEED CAP REQUIREMENT

MOC :

MTH -MANDATORY N/A

SL 525-71-07 R01 POWER PLANT - OIL PRESSURE TRANSMITTER TUBE ASSEMBLY INSPECTION/REPLACEMENT


LDG

HRS

MTH

144

208:40

16-Jan-2019 -CANCELLED CompleteE1

SL WI-71-1064-CN CANCELED - POWER PLANT - WATER RINSE PROCEDURE - REVISION TO MAINTENANCE MANUAL

COMPLIED WITH - INFORMATIONAL ONLY: SL CANCELLED / DE.MG.0011 / CDE / 16-JAN-2019MOC :

LDG

HRS

MTH

144

208:40

16-Jan-2019 -CANCELLED CompleteE2

SL WI-71-1064-CN CANCELED - POWER PLANT - WATER RINSE PROCEDURE - REVISION TO MAINTENANCE MANUAL

COMPLIED WITH - INFORMATIONAL ONLY: SL CANCELLED / DE.MG.0011 / CDE / 16-JAN-2019MOC :

- CompleteE1

SL WI-71-1064 POWER PLANT - WATER RINSE PROCEDURE - REVISION TO MAINTENANCE MANUAL

COMPLIED WITH - INFORMATIONAL ONLY: REVISION TO MAINTENANCE MANUAL / DE.MG.0011 / CDE / 10-OCT-2018MOC :

- CompleteE2

SL WI-71-1064 POWER PLANT - WATER RINSE PROCEDURE - REVISION TO MAINTENANCE MANUAL

COMPLIED WITH - INFORMATIONAL ONLY: REVISION TO MAINTENANCE MANUAL / DE.MG.0011 / CDE / 10-OCT-2018MOC :

MTH -INFORMATIONAL

SL 525-72-04 ENGINE - TRANSMITTAL OF WILLIAMS/ROLLS SERVICE BULLETIN FJ44-72-27 GEARBOX ASSEMBLY - INSPECTION OF BREATHER PORT MAGNETICCARBON SEAL AND REWORK OF BREATHER TUBE

MOC :


0:0225-Sep-2019125:48AIR COND

0:2825-Sep-2019265324:25ENG 2

0:2825-Sep-2019265324:25ENG 1

0:2825-Sep-2019265324:25AIRCRAFT


Last ActualDate


HB-VTBReg No:

30-Sep-2019 5:15AM

23-Jun-2017


Print Date:

Airworthiness:

Aircraft Serial:


Unit:

525-0947


(ENG) DUE 2

(ENG) DUE 1

Service Bulletins

City Part Serial No


C/W Time 2 + or -

Adj. TBO 1

TBO 2 TSO 2

TSO 1

Remains

RemainsDescription


Item Code

Mod Lvl

LDG

HRS

MTH

106

157:42


SL 525-72-06

ICT

ENGINE - TRANSMITTAL OF WILLIAMS ROLLS SERVICE LETTER SL44-72-72 GEARBOX CARBON SEALS-MAINTENANCE REQUIREMENTS

NOT APPLICABLE - SL525-70-06; TRANSMITTAL OF WILLIAMS SL44-72-72 GEARBOX CARBON SEALS. DOES NOT APPLY DUE TOENGINE SERIAL NUMBER.

MOC :

LDG

HRS

MTH

106

157:42


SL 525-72-08

ICT

ENGINE - TRANSMITTAL OF WILLIAMS ROLLS SERVICE BULLETIN FJ44-72-050, ENGINE-DIFFUSER HOLLOW BOLT FUEL DRAIN INSTALL

NOT APPLICABLE - SL525-72-08; TRANSMITTAL OF WILLIAMS SB FJ44-72-050 ENGINE DIFFUSER HOLLOW BOLT FUEL DRAININSTALL. DOES NOT APPLY DUE TO ENGINE SERIAL NUMBER.

MOC :

LDG

HRS

MTH

106

157:42


SL 525-72-09

ICT

ENGINE - TRANSMITTAL OF WILLIAMS ROLLS SERVICE BULLETIN FJ44-72-052, ENGINE-IP COMPRESSOR ROTOR-REPLACE

NOT APPLICABLE - SL525-72-09; TRANSMITTAL OF WILLIAMS SB FJ44-72-052 ENGINE IP COMPRESSOR ROTORREPLACEMENT. DOES NOT APPLY DUE TO ENGINE SERIAL NUMBER.

MOC :

-INFORMATIONAL

E1

SB FJ44-05-002R02

UNSERVICEABLE PARTS - NOTIFICATION

MOC :

-INFORMATIONAL

E2

SB FJ44-05-002R02


MOC :

LDG

HRS

MTH

168

225:06

13-Mar-2019 -INFORMATIONAL

Complete

E1

SB FJ44-05-002R03


COMPLIED WITH - INFORMATIONAL ONLY: THIS SERVICE BULLETIN IS INFORMATIONAL ONLY AND NO MAINTENANCE ACTIONIS REQUIRED / DE.MG.0011 / CDE / 13-MAR-2019

MOC :

LDG

HRS

MTH

168

225:06

13-Mar-2019 -INFORMATIONAL

Complete

E2

SB FJ44-05-002R03


COMPLIED WITH - INFORMATIONAL ONLY: THIS SERVICE BULLETIN IS INFORMATIONAL ONLY AND NO MAINTENANCE ACTIONIS REQUIRED / DE.MG.0011 / CDE / 13-MAR-2019

MOC :

MTH -MANDATORY N/AE1

SB FJ44-72-129R01

INNER GUIDED ROLLER BEARING (NO. 3 BEARING) - REPLACE

NOT APPLICABLE - TO SERIAL NUMBER / DE.MG.0011 / CDE / 23-JAN-2019MOC :


SB FJ44-72-129R01

INNER GUIDED ROLLER BEARING (NO. 3 BEARING) - REPLACE


MTH -RECOMMENDED

N/A

E1

SB FJ44-72-130R02

HP COMPRESSOR ROTOR - INSPECTION

NOT APPLICABLE - TO SERIAL NUMBER / DE.MG.0011 / CDE / 11-OCT-2018MOC :

MTH -RECOMMENDED

N/A

E2

SB FJ44-72-130R02

HP COMPRESSOR ROTOR - INSPECTION



0:0225-Sep-2019125:48AIR COND

0:2825-Sep-2019265324:25ENG 2

0:2825-Sep-2019265324:25ENG 1

0:2825-Sep-2019265324:25AIRCRAFT


Last ActualDate


HB-VTBReg No:

30-Sep-2019 5:15AM

23-Jun-2017


Print Date:

Airworthiness:

Aircraft Serial:


Unit:

525-0947


(ENG) DUE 2

(ENG) DUE 1

Service Bulletins

City Part Serial No


C/W Time 2 + or -

Adj. TBO 1

TBO 2 TSO 2

TSO 1

Remains

RemainsDescription


Item Code

Mod Lvl


E1

SB FJ44-72-131R02

1ST LP TURBINE NOZZLE - REPLACE



E2

SB FJ44-72-131R02

1ST LP TURBINE NOZZLE - REPLACE


MTH -RECOMMENDED

N/A

E1

SB FJ44-72-150R02

LP REAR BEARING SEAL RETAINER - REPLACE

NOT APPLICABLE - TO PART NUMBER / DE.MG.0011 / CDE / 30-OCT-2018MOC :

MTH -RECOMMENDED

N/A

E2

SB FJ44-72-150R02


NOT APPLICABLE - TO PART NUMBER / DE.MG.0011 / CDE / 30-OCT-2018MOC :

MTH -RECOMMENDED

N/A

E1

SB FJ44-72-150R03


NOT APPLICABLE - TO ENGINE S/N / DE.MG.0011 / CDE / 04-JUL-2019MOC :

MTH -RECOMMENDED

N/A

E2

SB FJ44-72-150R03


NOT APPLICABLE - TO ENGINE S/N / DE.MG.0011 / CDE / 04-JUL-2019MOC :

MTH -OPTIONAL

SB 525-73-03 ENGINE FUEL AND CONTROL - FUEL CONTROL UNIT (FCU) FIELD REPLACEMENT

- OPTIONAL - THIS SERVICE DOCUMENT PROVIDES PARTS AND INSTRUCTIONS TO REPLACE A REDUCER IN THE FUELPRESSURE SWITCH TUBE ASSEMBLY / DE.MG.0011 / CDE / 04-JUL-2019

MOC :

MTH -INFORMATIONAL

SL 525-73-02 ENGINE FUEL AND CONTROL - TRANSMIT WILLIAMS/ROLLS SERVICE BULLETIN FJ44-73-7, FCU-TO-CONTROLVALVE FUEL TUBE ASSEMBLY AND LOOPCLAMP - REPLACE

MOC :

MTH -INFORMATIONAL

SL 525-73-03 R01 ENGINE FUEL AND CONTROL - TRANSMITTAL OF WILLIAMS SERVICE BULLETIN FJ44-73-10, FUEL PUMP FILTER REPLACEMENT

MOC :


SB FJ44-73-044R07

ENGINE FUEL AND CONTROL - FUEL DELIVERY UNIT - REPLACE



SB FJ44-73-044R07

ENGINE FUEL AND CONTROL - FUEL DELIVERY UNIT - REPLACE


-MANDATORY N/AE1

SB WI-73-1002 R02 ENGINE FUEL AND CONTROL - FUEL TUBE ASSEMBLIES - REPLACE (CANCELLED)

NOT APPLICABLE - CANCELLED / DE.MG.0011 / CDE / 11-OCT-2018MOC :

-MANDATORY N/AE2

SB WI-73-1002 R02 ENGINE FUEL AND CONTROL - FUEL TUBE ASSEMBLIES - REPLACE (CANCELLED)

NOT APPLICABLE - CANCELLED / DE.MG.0011 / CDE / 11-OCT-2018MOC :

-MANDATORY N/AE1

SB WI-73-1002 ENGINE FUEL AND CONTROL - FUEL TUBE ASSEMBLIES - REPLACE (SUPERSEDED BY WISB-73-1002 R01)

NOT APPLICABLE - SUPERSEDED / DE.MG.0011 / CDE / 11-OCT-2018MOC :

-MANDATORY N/AE2

SB WI-73-1002 ENGINE FUEL AND CONTROL - FUEL TUBE ASSEMBLIES - REPLACE (SUPERSEDED BY WISB-73-1002 R01)



0:0225-Sep-2019125:48AIR COND

0:2825-Sep-2019265324:25ENG 2

0:2825-Sep-2019265324:25ENG 1

0:2825-Sep-2019265324:25AIRCRAFT


Last ActualDate


HB-VTBReg No:

30-Sep-2019 5:15AM

23-Jun-2017


Print Date:

Airworthiness:

Aircraft Serial:


Unit:

525-0947


(ENG) DUE 2

(ENG) DUE 1

Service Bulletins

City Part Serial No


C/W Time 2 + or -

Adj. TBO 1

TBO 2 TSO 2

TSO 1

Remains

RemainsDescription


Item Code

Mod Lvl

MTH -CANCELLED N/AE1

SB WI-73-1007 R01-CN

CANCELLED - ENGINE FUEL AND CONTROL - ENGINE MAINTENANCE TERMINAL (EMT) SOFTWARE UPGRADE TO CP356.10.02

NOT APPLICABLE - CANCELLED / DE.MG.0011 / CDE / 18-JUL-2019MOC :

MTH -CANCELLED N/AE2

SB WI-73-1007 R01-CN

CANCELLED - ENGINE FUEL AND CONTROL - ENGINE MAINTENANCE TERMINAL (EMT) SOFTWARE UPGRADE TO CP356.10.02

NOT APPLICABLE - CANCELLED / DE.MG.0011 / CDE / 18-JUL-2019MOC :

LDG

HRS

MTH

178

232:46

01-Apr-2019 - CompleteE1

SB WI-73-1007 R01 ENGINE FUEL AND CONTROL - ENGINE MAINTENANCE TERMINAL (EMT) SOFTWARE UPGRADE TO CP356.10.02 (CANCELLED)

COMPLIED WITH - INFORMATIONAL ONLY: DE.MG.0011 / CDE / 01-APR-2019MOC :

LDG

HRS

MTH

178

232:46

01-Apr-2019 - CompleteE2

SB WI-73-1007 R01 ENGINE FUEL AND CONTROL - ENGINE MAINTENANCE TERMINAL (EMT) SOFTWARE UPGRADE TO CP356.10.02 (CANCELLED)

COMPLIED WITH - INFORMATIONAL ONLY: DE.MG.0011 / CDE / 01-APR-2019MOC :

MTH -RECOMMENDED N/AE1

SB WI-73-1008 R01 ENGINE FUEL AND CONTROL - OIL COOLER TO FDU FUEL TUBE - REPLACE





MTH

DUE

DUERECOMMENDED N/AE1


NOT APPLICABLE - SUPERSEDED / DE.MG.0011 / CDE / 29-JAN-2019MOC :

MTH

DUE




MTH

DUE



NOT APPLICABLE - SUPERSEDED / DE.MG.0011 / CDE / 25-FEB-2019MOC :

MTH

DUE



NOT APPLICABLE - SUPERSEDED / DE.MG.0011 / CDE / 25-FEB-2019MOC :

HRS

MTH

DUE

DUE

DUERECOMMENDED

(400)400 75:35

E1


MOC :

HRS

MTH

DUE

DUE

DUERECOMMENDED

(400)400 75:35

E2


MOC :

-RECOMMENDED N/AE1

SB WI-73-1008 ENGINE FUEL AND CONTROL - OIL COOLER TO FDU FUEL TUBE - REPLACE



0:0225-Sep-2019125:48AIR COND

0:2825-Sep-2019265324:25ENG 2

0:2825-Sep-2019265324:25ENG 1

0:2825-Sep-2019265324:25AIRCRAFT


Last ActualDate


HB-VTBReg No:

30-Sep-2019 5:15AM

23-Jun-2017


Print Date:

Airworthiness:

Aircraft Serial:


Unit:

525-0947


(ENG) DUE 2

(ENG) DUE 1

Service Bulletins

City Part Serial No


C/W Time 2 + or -

Adj. TBO 1

TBO 2 TSO 2

TSO 1

Remains

RemainsDescription


Item Code

Mod Lvl

-RECOMMENDED N/AE2

SB WI-73-1008 ENGINE FUEL AND CONTROL - OIL COOLER TO FDU FUEL TUBE - REPLACE



SB WI-73-1009 R01 ENGINE FUEL AND CONTROL - FUEL TUBE ASSEMBLIES - REPLACE





HRS

MTH

DUE

DUE

DUERECOMMENDED

(5000)5000 4675:35

E1


MOC :

HRS

MTH

DUE

DUE

DUERECOMMENDED

(5000)5000 4675:35

E2


MOC :

MTH -E1


- CH.MG.7033 - A.GrefMOC :

MTH -E2



HRS

MTH

CSI

2500

CSIRECOMMENDED

(2500)2500 2175:35

E1



HRS

MTH

CSI

2500

CSIRECOMMENDED

(2500)2500 2175:35

E2



-RECOMMENDED N/AE1

SB WI-73-1009 ENGINE FUEL AND CONTROL - FUEL TUBE ASSEMBLIES - REPLACE


-RECOMMENDED N/AE2

SB WI-73-1009 ENGINE FUEL AND CONTROL - FUEL TUBE ASSEMBLIES - REPLACE


MTH - N/AE1

SB WI-73-1016 ENGINE FUEL AND CONTROL - FADEC - UPDATE AIRCRAFT SERIAL NUMBER


MTH - N/AE2

SB WI-73-1016 ENGINE FUEL AND CONTROL - FADEC - UPDATE AIRCRAFT SERIAL NUMBER



0:0225-Sep-2019125:48AIR COND

0:2825-Sep-2019265324:25ENG 2

0:2825-Sep-2019265324:25ENG 1

0:2825-Sep-2019265324:25AIRCRAFT


Last ActualDate


HB-VTBReg No:

30-Sep-2019 5:15AM

23-Jun-2017


Print Date:

Airworthiness:

Aircraft Serial:


Unit:

525-0947


(ENG) DUE 2

(ENG) DUE 1

Service Bulletins

City Part Serial No


C/W Time 2 + or -

Adj. TBO 1

TBO 2 TSO 2

TSO 1

Remains

RemainsDescription


Item Code

Mod Lvl

LDG

HRS

MTH

168

225:06

18-Mar-2019 - CompleteE1

SL WI-73-1016 ENGINE FUEL AND CONTROL - REVISION TO ILLUSTRATED PARTS CATALOG

COMPLIED WITH - INFORMATIONAL ONLY: THIS SERVICE DOCUMENT IS WRITTEN AS AUTHORIZATION TO INSTALL P/N 221653ENGINE CONTROL UNIT (ECU) ON ALL FJ44-1AP P/N 72100-201 ENGINES, AS REQUIRED / DE.MG.0011 / CDE / 18-MAR-2019

MOC :

LDG

HRS

MTH

168

225:06

18-Mar-2019 - CompleteE2

SL WI-73-1016 ENGINE FUEL AND CONTROL - REVISION TO ILLUSTRATED PARTS CATALOG

COMPLIED WITH - INFORMATIONAL ONLY: THIS SERVICE DOCUMENT IS WRITTEN AS AUTHORIZATION TO INSTALL P/N 221653ENGINE CONTROL UNIT (ECU) ON ALL FJ44-1AP P/N 72100-201 ENGINES, AS REQUIRED / DE.MG.0011 / CDE / 18-MAR-2019

MOC :

LDG

HRS

MTH

248

300:25

16-Aug-2019 -MANDATORY CompleteE1

SB WI-74-1000

LSZH

IGNITION - IGNITER LEAD INSPECTION AND CLAMPING ARRANGEMENT

COMPLIED WITH - PERFORMEDMOC :

LDG

HRS

MTH

248

300:25

16-Aug-2019 -MANDATORY CompleteE2

SB WI-74-1000

LSZH

IGNITION - IGNITER LEAD INSPECTION AND CLAMPING ARRANGEMENT

COMPLIED WITH - PERFORMEDMOC :

HRS

MTH

DUE

DUE

DUERECOMMENDED (5000)5000 4675:35E1

SB WI-75-1001 R01 AIR - I.P. BLEED VALVE LEVER PIN - REPLACE

MOC :

HRS

MTH

DUE

DUE

DUERECOMMENDED (5000)5000 4675:35E2

SB WI-75-1001 R01 AIR - I.P. BLEED VALVE LEVER PIN - REPLACE

MOC :

MTH

DUE

DUERECOMMENDED

N/AE1

SB WI-75-1001 AIR - I.P. BLEED VALVE LEVER PIN - REPLACE


MTH

DUE

DUERECOMMENDED

N/AE2

SB WI-75-1001 AIR - I.P. BLEED VALVE LEVER PIN - REPLACE


MTH -OPTIONAL

SB 525-76-10 ENGINE CONTROLS - UPDATED FJ44-1AP FULL AUTHORITY ENGINE CONTROL (FADEC) FIELD REPLACEMENT

- TO INSTALL NEW 9912680-5 FADECS IF NEEDED. THE LEFT AND RIGHT 9912680-4 FADEC MUST BE REPLACED AT THESAME TIME WITH 9912680-5 FADECS / DE.MG.0011 / CDE / 04-JUL-2019

MOC :

LDG

HRS

MTH

251

303:19

09-Sep-2019 -INFORMATIONAL CompleteCOM MC M2-001 FADEC PART NUMBER CHANGE


LDG

HRS

MTH

248

300:25

04-Sep-2019 - CompleteCOM MC M2-002 ATA 76 – FADEC PART NUMBER CHANGE



SB FJ44-77-011R18

ENGINE INDICATING - FADEC ENGINE HARNESS ASSEMBLY - INSPECTION

NOT APPLICABLE - TO PART NUMBER / DE.MG.0011 / CDE / 15-NOV-2018MOC :


0:0225-Sep-2019125:48AIR COND

0:2825-Sep-2019265324:25ENG 2

0:2825-Sep-2019265324:25ENG 1

0:2825-Sep-2019265324:25AIRCRAFT


Last ActualDate


HB-VTBReg No:

30-Sep-2019 5:15AM

23-Jun-2017


Print Date:

Airworthiness:

Aircraft Serial:


Unit:

525-0947


(ENG) DUE 2

(ENG) DUE 1

Service Bulletins

City Part Serial No


C/W Time 2 + or -

Adj. TBO 1

TBO 2 TSO 2

TSO 1

Remains

RemainsDescription


Item Code

Mod Lvl


SB FJ44-77-011R18

ENGINE INDICATING - FADEC ENGINE HARNESS ASSEMBLY - INSPECTION

NOT APPLICABLE - TO PART NUMBER / DE.MG.0011 / CDE / 15-NOV-2018MOC :


SB FJ44-77-013R09

ENGINE INDICATING - FADEC ENGINE HARNESS ASSEMBLY - REWORK



SB FJ44-77-013R09

ENGINE INDICATING - FADEC ENGINE HARNESS ASSEMBLY - REWORK


-RECOMMENDED N/AE1

SB FJ44-79-013R02

OIL - OIL FILLER CAP ASSEMBLY - REPLACE (SUPERSEDED BY FJ44-79-013 R03)


-RECOMMENDED N/AE2

SB FJ44-79-013R02

OIL - OIL FILLER CAP ASSEMBLY - REPLACE (SUPERSEDED BY FJ44-79-013 R03)


MTH -RECOMMENDED

N/A

E1

SB FJ44-79-013R05

OIL - OIL FILLER CAP ASSEMBLY - REPLACE


MTH -RECOMMENDED

N/A

E2

SB FJ44-79-013R05

OIL - OIL FILLER CAP ASSEMBLY - REPLACE


MTH -RECOMMENDED

N/A

E1

SB FJ44-79-016R04

OIL - RELIEF VALVE ASSEMBLY - REPLACE


MTH -RECOMMENDED

N/A

E2

SB FJ44-79-016R04

OIL - RELIEF VALVE ASSEMBLY - REPLACE


LDG

HRS

MTH

248

300:25

01-Sep-2019 -CANCELLED Complete

SL CIL-99-01 R03 MISCELLANEOUS - USE OF CORROSION INHIBITING COMPOUNDS


LDG

HRS

MTH

248

300:25

01-Sep-2019 -CANCELLED

Complete

SL CIL-99-02 R01 MISCELLANEOUS - AVOID OPERATIONS ON RUNWAYS TREATED WITH RUNWAY DE-ICE (RDI) FLUIDS. AIRCRAFT WASHING RECOMMENDED AFTEREXPOSURE TO RDI FLUIDS


LDG

HRS

MTH

248

300:25


SL CIL-99-03 R02 MISCELLANEOUS - CORROSION PREVENTION AND CONTROL PROGRAM (CPCP)



0:0225-Sep-2019125:48AIR COND

0:2825-Sep-2019265324:25ENG 2

0:2825-Sep-2019265324:25ENG 1

0:2825-Sep-2019265324:25AIRCRAFT


Last ActualDate


HB-VTBReg No:

30-Sep-2019 5:15AM

23-Jun-2017


Print Date:

Airworthiness:

Aircraft Serial:


Unit:

525-0947


(ENG) DUE 2

(ENG) DUE 1

Service Bulletins

City Part Serial No


C/W Time 2 + or -

Adj. TBO 1

TBO 2 TSO 2

TSO 1

Remains

RemainsDescription


Item Code

Mod Lvl

LDG

HRS

MTH

248

300:25


SL CIL-99-04 R01 MISCELLANEOUS - INCREMENTAL LIBRARY UPDATES FOR CESVIEW


LDG

HRS

MTH

147

210:28

23-Jan-2019 - CompleteCOM MC 525-001 525 MODEL SERIES COMMUNIQUE ANNOUNCEMENT

COMPLIED WITH - INFORMATIONAL ONLY: DE.MG.0011 / CDE / 23-JAN-2019MOC :


0:0225-Sep-2019125:48AIR COND

0:2825-Sep-2019265324:25ENG 2

0:2825-Sep-2019265324:25ENG 1

0:2825-Sep-2019265324:25AIRCRAFT


Last ActualDate


HB-VTBReg No:

30-Sep-2019 5:15AM

23-Jun-2017


Print Date:

Airworthiness:

Aircraft Serial:


Unit:

525-0947


(ENG) DUE 2

(ENG) DUE 1

Airworthiness Directives

City Part Serial No


C/W Time 2 + or -

Adj. TBO 1

TBO 2 TSO 2

TSO 1

Remains

RemainsDescription


Item Code

Mod Lvl

MTH 29-Oct-2018 -MANDATORY N/A

FAA 2003-21-07 FLIGHT CONTROLS - ELECTRIC PITCH TRIM FAILURE CAUSING RUN AWAY PITCH TRIM CONDITION, LARGE PITCH MISTRIM AND EXCESSIVE CONTROLFORCES (SUPERSEDED BY FAA AD 2004-14-20)

NOT APPLICABLE - AIRCRAFT CERTIFICATION DATE IS 23-JUN-2017 / DE.MG.0011 / CDE / 29-OCT-2018MOC :

DAYS 29-Oct-2018 -MANDATORY N/AFAA 2006-16-18R01 PARA (F)

INSTALL PLACARD


DAYS 29-Oct-2018 -MANDATORY

N/AFAA 2006-16-18R01 PARA (G)

REVISE AIRPLANE FLIGHT MANUAL (AFM)


DAYS 29-Oct-2018 -MANDATORY N/AFAA 2006-16-18R01 PARA (H)

UPDATE SOFTWARE



FAA 2006-16-18R01

APPLIANCE AD - INSTALL UPGRADED SOFTWARE IN THE TAWS/RMI


DAYS 29-Oct-2018 -MANDATORY

N/AFAA 2013-08-05PARA (G)

INSPECTION A\C COMPRESSOR HOUR METER



FAA 2013-08-05PARA (H)

REPLACE THE AIR CONDITIONING COMPRESSOR MOTOR BRUSHES WITH NEW BRUSHES


MTH 29-Oct-2018 -MANDATORY

N/AFAA 2013-08-05PARA (I)

DEACTIVATION OF THE AIR CONDITIONING


DAYS 29-Oct-2018 -MANDATORY N/A

FAA 2013-08-05PARA (J)

RETURN OF REPLACED PARTS AND REPORTING REQUIREMENT



FAA 2013-08-05 AIR CONDITIONING - REPLACEMENT OF THE BRUSHES ON CERTAIN P/N A/C COMPRESSOR MOTORS OR DEACTIVATION OF THE A/C SYSTEM



EASA 2005-0021 APPLIANCE AD - HONEYWELL RCZ-83() AND RCZ-85() COMMUNICATION UNITS (SUPERSEDED BY EASA AD 2007-0156)



EASA 2007-0156PARA (1.A)

AMEND THE APPLICABLE AIRPLANE FLIGHT MANUAL, NORMAL PROCEDURES SECTION "AFTER COMPLETION OF ANY 4096 ATC CODE CHANGE (ALSOREFERRED TO AS MODE A CODE), CHECK THE STATUS OF THE TRANSPONDER. IF THE TRANSPONDER INDICATES THAT IT IS IN STANDBY MODE, RE-SELECT THE DESIRED MODE (I.E. THE TRANSPONDER SHOULD BE IN THE ACTIVE MODE)." FOR AEROPLANES EQUIPPED WITH HONEYWELL RCZ-833J, RCZ-833K, RCZ-851J, RCZ-851K OR RCZ-854J COMMUNICATION UNITS, P/N'S AS LISTED IN PART (1)



N/AEASA 2007-0156PARA (1.B)

MODIFY THE AFFECTED COMMUNICATIONS UNITS



N/A

EASA 2007-0156PARA (1.C)

REPLACE THE XS-852E/F MODE S TRANSPONDER OF THE COM UNIT WITH A NEW OR MODIFIED XS-852E/F MODE S TRANSPONDER THAT HAS MOD VINSTALLED



0:0225-Sep-2019125:48AIR COND

0:2825-Sep-2019265324:25ENG 2

0:2825-Sep-2019265324:25ENG 1

0:2825-Sep-2019265324:25AIRCRAFT


Last ActualDate


HB-VTBReg No:

30-Sep-2019 5:15AM

23-Jun-2017


Print Date:

Airworthiness:

Aircraft Serial:


Unit:

525-0947


(ENG) DUE 2

(ENG) DUE 1


City Part Serial No


C/W Time 2 + or -

Adj. TBO 1

TBO 2 TSO 2

TSO 1

Remains

RemainsDescription


Item Code

Mod Lvl


EASA 2007-0156PARA (2)

AMEND THE APPLICABLE AIRPLANE FLIGHT MANUAL, NORMAL PROCEDURES SECTION, TO INCLUDE THE FOLLOWING STATEMENT "AFTERCOMPLETION OF ANY 4096 ATC CODE CHANGE (ALSO REFERRED TO AS MODE A CODE), CHECK THE STATUS OF THE TRANSPONDER. IF THETRANSPONDER INDICATES THAT IT IS IN STANDBY MODE, RE-SELECT THE DESIRED MODE (I.E. THE TRANSPONDER SHOULD BE IN THE ACTIVEMODE)"



EASA 2007-0156PARA (3.A)

REPLACE THE MODIFICATION PLATE OF THE TRANSPONDER WITH A NEW PLATE AND TEST THE TRANSPONDER



EASA 2007-0156PARA (3.B)

INSTALL MOD Y INTO THE APPLICABLE MODE S TRANSPONDER



N/A

EASA 2007-0156PARA (4)

AFTER ACCOMPLISHING THE REPLACEMENTS OR MODIFICATIONS REQUIRED BY PARAGRAPH (1)(B) AND/OR (2)(B) AND (3) OF THIS DIRECTIVE, ASAPPLICABLE, THE AFM AMENDMENT REQUIRED BY PARAGRAPH (1)(A) AND/OR (2)(A) OF THIS DIRECTIVE MAY BE REMOVED FROM THE AFM



EASA 2007-0156 APPLIANCE AD - COMMUNICATION - COMM UNITS & TRANSPONDERS - MODIFICATION / REPLACEMENT



EASA 2006-0274 APPLIANCE AD - ELECTRICAL POWER - SWITCHED - INSPECTION/REPLACEMENT (SUPERSEDED BY EASA AD 2006-0375)


MTH 29-Oct-2018 -AIRWORTHINESSDIRECTIVE

N/A

EASA 2006-0375 APPLIANCE AD - ELECTRICAL POWER – SWITCHES – INSPECTION/REPLACEMENT - CARLING TECHNOLOGIES, INC.



FAA 2001-02-13 ELECTRICAL POWER - REPLACE CERTAIN DIRECT CURRENT (DC) POWER BATTERY SWITCHES


MTH 29-Oct-2018 A/RMANDATORY N/A

FAA 2007-23-16 INCORPORATE ELECTRICAL POWER RELAY CIRCUIT PROTECTION KIT PART NUMBER SB525B-24-02



FAA 2011-21-51 REPLACE THE LITHIUM-ION MAIN AIRCRAFT BATTERY, CESSNA P/N 9914788-1



EASA 2013-0020R04 PARA (1)

INSPECT THE MARKINGS OF SAFETY BELTS AND/OR TORSO RESTRAINT SYSTEMS, TO DETERMINE IF THEY HAVE BEEN MAINTAINED OR REPAIREDBY ORGANISATIONS OTHER THAN THE DESIGN APPROVAL HOLDER



EASA 2013-0020R04 PARA (2)

VERIFY IF THE ORGANISATION IS LISTED AMONG THE AUTHORIZED MAINTENANCE OR REPAIR ORGANISATION REFERENCE DOCUMENTS QUOTED INTHE REF. PUBLICATIONS SECTION OF THIS AD



EASA 2013-0020R04 PARA (3)

REMOVE AND REPLACE BELTS NOT MEETING THE CERTIFICATION REQUIREMENTS OR MAKE RELEVANT SEAT INOPERATIVE



0:0225-Sep-2019125:48AIR COND

0:2825-Sep-2019265324:25ENG 2

0:2825-Sep-2019265324:25ENG 1

0:2825-Sep-2019265324:25AIRCRAFT


Last ActualDate


HB-VTBReg No:

30-Sep-2019 5:15AM

23-Jun-2017


Print Date:

Airworthiness:

Aircraft Serial:


Unit:

525-0947


(ENG) DUE 2

(ENG) DUE 1


City Part Serial No


C/W Time 2 + or -

Adj. TBO 1

TBO 2 TSO 2

TSO 1

Remains

RemainsDescription


Item Code

Mod Lvl


EASA 2013-0020R04 PARA (4)

AFTER 14 FEBRUARY 2013 [THE EFFECTIVE DATE OF THE ORIGINAL ISSUE OF THIS AD], DO NOT INSTALL SAFETY BELTS OR TORSO RESTRAINTSYSTEMS ON ANY AIRCRAFT, UNLESS INSPECTED AND CORRECTED IN COMPLIANCE WITH THE REQUIREMENTS OF THIS AD



EASA 2013-0020R04

APPLIANCE AD - EQUIPMENT & FURNISHINGS - SAFETY BELTS / TORSO RESTRAINT SYSTEMS - INSPECTION / REPLACEMENT



EASA 2016-0167R01 (CORR)

APPLIANCE AD - EQUIPMENT / FURNISHINGS - REAR CABIN ATTENDANT SEAT - INSPECTION / REPAIR

NOT APPLICABLE - NOT EQUIPPED WITH ZODIAC SEATS FRANCE CAS 536-SERIES ATTENDANT SEATS / DE.MG.0011 / CDE / 12-OCT-2018

MOC :

MTH 9MANDATORY N/A

EASA 2017-0192PARA (1)

MODIFY AND RE-IDENTIFY EACH AFFECTED PASSENGER SEAT

NOT APPLICABLE - NOT EQUIPPED WITH RECARO AIRCRAFT SEATING GMBH & CO. KG MODEL 3510A AND 3510D SEATS /DE.MG.0011 / CDE / 12-OCT-2018

MOC :

MTH -MANDATORY

N/A

EASA 2017-0192PARA (2)

DO NOT INSTALL (SEE NOTE 2 OF THIS AD) AN AFFECTED PASSENGER SEAT ON ANY AEROPLANE, AS REQUIRED BY PARAGRAPH (2.1) OR (2.2) OFTHIS AD, AS APPLICABLE


MOC :

MTH -MANDATORY N/A

EASA 2017-0192 APPLIANCE AD - EQUIPMENT AND FURNISHING - PASSENGER SEATS - MODIFICATION


MOC :

DAYS

MTH

30

MANDATORY N/A

EASA 2017-0225PARA (1)

INSTALL A PLACARD AS SPECIFIED IN TABLE 1 OF THIS AD IN FULL VIEW OF THE PILOT(S), AMEND THE APPLICABLE AFM, INFORM ALL FLIGHT CREWSAND, THEREAFTER, OPERATE THE AIRCRAFT ACCORDINGLY

NOT APPLICABLE - NOT EQUIPPED WITH SCHROTH SAFETY PRODUCTS SEAT RESTRAINT SYSTEMS PART NUMBER (P/N) 4-01-( ), P/N 4-02-( ), P/N 4-03-( ), P/N 4-04-( ), P/N 1-09-043201BCR, P/N 1-09-483D01 AND P/N 510100-01 REVA / DE.MG.0011 / CDE / 12-OCT-2018

MOC :

MTH -MANDATORY N/A

EASA 2017-0225PARA (3)

DO NOT INSTALL AN AFFECTED PART ON ANY AIRCRAFT THAT, ACCORDING TO THE APPLICABLE AFM, IS CERTIFICATED IN THE AEROBATICCATEGORY, AS REQUIRED BY PARAGRAPH (3.1) OR (3.2) OF THIS AD, AS APPLICABLE


MOC :

MTH -MANDATORY N/A

EASA 2017-0225 APPLIANCE AD - EQUIPMENT / FURNISHINGS - SEAT RESTRAINT SYSTEMS - AFM AMENDMENT / MODIFICATION


MOC :

MTH 6MANDATORY N/A

EASA 2018-0195 EQUIPMENT / FURNISHINGS - RESTRAINT SYSTEMS ROTARY BUCKLE SUB ASSEMBLY - REMOVAL FROM SERVICE

NOT APPLICABLE - NOT EQUIPPED WITH ANJOU AERONAUTIQUE MODEL 358 TORSO RESTRAINT SYSTEMS PART NUMBER(P/N) 358XX XXX-XX-XXX / DE.MG.0011 / CDE / 12-OCT-2018

MOC :

MTH -MANDATORY N/A

EASA 2018-0223 EQUIPMENT / FURNISHING - SEAT ENERGY ABSORBER ASSEMBLY - MODIFICATION

NOT APPLICABLE - NOT EQUIPPED WITH B/E AEROSPACE FISCHER GmbH COMMON SEATS 170/260 H160 / DE.MG.0011 / CDE /18-OCT-2018

MOC :


0:0225-Sep-2019125:48AIR COND

0:2825-Sep-2019265324:25ENG 2

0:2825-Sep-2019265324:25ENG 1

0:2825-Sep-2019265324:25AIRCRAFT


Last ActualDate


HB-VTBReg No:

30-Sep-2019 5:15AM

23-Jun-2017


Print Date:

Airworthiness:

Aircraft Serial:


Unit:

525-0947


(ENG) DUE 2

(ENG) DUE 1


City Part Serial No


C/W Time 2 + or -

Adj. TBO 1

TBO 2 TSO 2

TSO 1

Remains

RemainsDescription


Item Code

Mod Lvl

MTH -MANDATORY N/A

EASA 2018-0262PARA (1)

MODIFY AND RE-IDENTIFY EACH PRE-MOD SEAT (FOR GROUP 1 AEROPLANES) (RESTATEMENT OF EASA AD 2016-0256 (1))

NOT APPLICABLE - NOT EQUIPPED WITH IPECO HOLDING LTD, PREVIOUSLY IPECO EUROPE LTD TYPE 3A063 PILOT AND CO-PILOT SEATS / DE.MG.0011 / CDE / 07-DEC-2018

MOC :

MTH -MANDATORY N/A

EASA 2018-0262PARA (2)

DO NOT INSTALL A PRE-MOD SEAT ON ANY AEROPLANE (RESTATEMENT OF EASA AD 2016-0256 PARA (2))


MOC :

MTH -MANDATORY N/A

EASA 2018-0262PARA (3)

INSPECT ANY AFFECTED SPRING OF EACH SEAT; REPLACE BOTH SPRINGS (IF, DURING ANY INSPECTION ANY DAMAGE OR INCORRECTINSTALLATION OF AN EFFECTED SPING IS FOUND)


MOC :

DAYS

MTH -MANDATORY

N/A

EASA 2018-0262PARA (5)

IT IS ALLOWED TO DEFER ACCOMPLISHMENT OF CORRECTIVE ACTIONS REQUIRED BT PARA (4) OF THIS AD FOR THAT SEAT, PROVIDED A COPY OFTHE ATR OEB IS INCLUDED IN THE APPLICABLE AFM, PILOTS ARE INFORMED, AND THE AEROPLANE IS OPERATED IAW THE INSTRUCTIONS OF THATOEB (IF, DURING ANY INSPECTION AS REQ BY PARA (3) OF THIS AD, ANY DAMAGE OR INCORRECT INSTALLATION OF ONLY ONE AFFECTED SPRING ISFOUND ON THE PILOT OR CO-PILOT SEAT) (FOR ATR AEROPLANES)


MOC :

MTH - N/A

EASA 2018-0262PARA (8)

IT IS ALLOWED TO INSTALL AN AFFECTED SPRING ON A SEAT INSTALLED ON AN AEROPLANE PROVIDED THAT, AFTER INSTALLATION, THAT SPRINGPASSES AN INSPECTION (NO DEFECT FOUND)


MOC :

DAYS

MTH -MANDATORY N/AEASA 2018-0262PARA (9) & (10)

REPORTING


MOC :

MTH -MANDATORY N/A

EASA 2018-0262 APPLIANCE AD - EQUIPMENT / FURNISHINGS - PILOT AND CO-PILOTS SEATS - MODIFICATION / INSPECTION


MOC :

MTH -MANDATORY N/A

EASA 2018-0264R01

EQUIPMENT / FURNISHINGS - LIFE VEST POUCH - INSPECTION

NOT APPLICABLE - NOT EQUIPPED WITH CENTAURUS ECONOMY CLASS 13E, 13H AND 13K PASSENGER SEATS / DE.MG.0011 /CDE / 08-APR-2019

MOC :

MTH -MANDATORY N/A

EASA 2018-0264 APPLIANCE AD - EQUIPMENT / FURNISHINGS - LIFE VEST POUCH - INSPECTION

NOT APPLICABLE - NOT EQUIPPED WITH AVIOINTERIORS S.P.A. CENTAURUS PASSENGER SEATS / DE.MG.0011 / CDE / 10-DEC-2018

MOC :

MTH -MANDATORY N/A

EASA 2019-0010PARA (1)

REMOVE EACH AFFECTED PART FROM SERVICE AND REPLACE IT WITH A SERVICEABLE PART

NOT APPLICABLE - NOT EQUIPPED WITH ZODIAC AEROSAFETY SYSTEMS, PREVIOUSLY AERAZUR LIFE JACKETS, HAVING APART NUMBER (P/N) 210225-2, AND INFANT/SMALL CHILD LIFE JACKETS, HAVING P/N 216200-0 OR P/N 216203-0 / DE.MG.0011 /CDE / 28-JAN-2019

MOC :


0:0225-Sep-2019125:48AIR COND

0:2825-Sep-2019265324:25ENG 2

0:2825-Sep-2019265324:25ENG 1

0:2825-Sep-2019265324:25AIRCRAFT


Last ActualDate


HB-VTBReg No:

30-Sep-2019 5:15AM

23-Jun-2017


Print Date:

Airworthiness:

Aircraft Serial:


Unit:

525-0947


(ENG) DUE 2

(ENG) DUE 1


City Part Serial No


C/W Time 2 + or -

Adj. TBO 1

TBO 2 TSO 2

TSO 1

Remains

RemainsDescription


Item Code

Mod Lvl

MTH -MANDATORY

N/AEASA 2019-0010PARA (2)

DO NOT INSTALL AN AFFECTED PART ON ANY AIRCRAFT


MOC :

MTH -MANDATORY N/A

EASA 2019-0010PARA (3)

DO NOT RELEASE TO SERVICE ANY AFFECTED PART, UNLESS IT HAS BEEN REPAIRED AND RE-IDENTIFIED


MOC :

MTH -MANDATORY N/A

EASA 2019-0010 EQUIPMENT/FURNINSHING - LIFE JACKET - REMOVAL/REPAIR


MOC :

MTH -MANDATORY N/A

EASA 2019-0235PARA (1) THRU (4)

CONCURRENTLY ACCOMPLISH PARAS (1.1) AND (1.2) OF THIS AD AND ACCOMPLISH APPLICABLE CORRECTIVE ACTION(S) (IF, DISCREPANCIES AREDETECTED, AS IDENTIFIED IN THE SIL); OPERATORS MAY CONTINUE TO USE ELTS WITH THE ORIGINAL G-SWITCHES BY REDUCING THE INTERVAL OFTHE G-SWITCH TESTING, AS REQUIRED BY PARA (1.1)


MTH -MANDATORY N/A

EASA 2019-0235PARA (5)

REMOVE THE AFFECTED PART FROM SERVICE IAW THE INSTRUCTIONS OF SECTION 7 OF THE SB FOR THE PURPOSE OF IN-SHOP MODIFICATION


MTH -MANDATORY N/A

EASA 2019-0235PARA (6)

IN-SHOP CORRECTION OF AN AFFECTED PART OR MODIFICATION INTO A SERVICEABLE PART IAW THE INSTRUCTIONS OF THE SB CONSTITUTESTERMINATING ACTION FOR THE REPETITIVE INSPECTIONS AND TESTING AS REQUIRED BY THIS AD FOR THAT PART


MTH -MANDATORY N/A

EASA 2019-0235PARA (9)

DO NOT INSTALL ON ANY AIRCRAFT AN AFFECTED PART THAT HAS ACCUMULATED 10 YEAR TIS OR MORE


MTH -MANDATORY

EASA 2019-0235 APPLIANCE AD - EQUIPMENT / FURNISHINGS - EMERGENCY LOCATOR TRANSMITTER - INSPECTION / MODIFICATION / REPLACEMENT

Scheduled for next MX in Nov-2019 / CH.MG.7033 - A.GrefMOC :

MTH -MANDATORY N/A

FAA 1974-08-09R03

LAVATORY PAPER OR LINEN WASTE RECEPTACLE FIRE PREVENTION

NOT APPLICABLE - NOT VALID IN EUROPE / DE.MG.0011 / CDE / 29-OCT-2018MOC :


FAA 1994-19-06 APPLIANCE AD - SWEEP-ON MODEL 2000 CREW OXYGEN MASKS


MTH 29-Oct-2018 A/RMANDATORY N/AFAA 1998-25-10R01

APPLIANCE AD - AIRCRAFT BELTS INC


MTH 29-Oct-2018 A/RMANDATORY N/AFAA 1998-25-10 APPLIANCE AD - AIRCRAFT BELTS INC



0:0225-Sep-2019125:48AIR COND

0:2825-Sep-2019265324:25ENG 2

0:2825-Sep-2019265324:25ENG 1

0:2825-Sep-2019265324:25AIRCRAFT


Last ActualDate


HB-VTBReg No:

30-Sep-2019 5:15AM

23-Jun-2017


Print Date:

Airworthiness:

Aircraft Serial:


Unit:

525-0947


(ENG) DUE 2

(ENG) DUE 1


City Part Serial No


C/W Time 2 + or -

Adj. TBO 1

TBO 2 TSO 2

TSO 1

Remains

RemainsDescription


Item Code

Mod Lvl

LDG

HRS

MTH

106

157:42

13-Sep-2018 - N/A

FAA 2017-16-01PARA (G)

ICT

PERFORM GENERAL VISUAL INSPECTIONS OF THE ELT FOR DISCREPANCIES; CHECKS , TESTS AND VERIFICATIONS AS APPLICABLE, TO ENSURETHE ELT IS FUNCTIONING, AND ALL APPLICABLE CORRECTIVE ACTIONS

NOT APPLICABLE - AD2017-16-01 PARA (G); AMERI-KING CORPORATION MODEL AK-450 & AK-451 SERIES ELT INSPECTION,CHECKS & VERIFICATION. DOES NOT APPLY DUE TO EQUIPMENT NOT INSTALLED.

MOC :

MTH 13-Sep-2018 -MANDATORY N/A

FAA 2017-16-01PARA (J) ICT

OPTIONAL TERMINATING ACTION: REPLACE ELT WITH A SERVICEABLE FAA-APPROVED ELT

NOT APPLICABLE - AD2017-16-01 PARA (G); AMERI-KING CORPORATION MODEL AK-450 & AK-451 SERIES ELT INSPECTION,CHECKS & VERIFICATION. DOES NOT APPLY DUE TO EQUIPMENT NOT INSTALLED.

MOC :

LDG

HRS

MTH

106

157:42


FAA 2017-16-01

ICT

APPLIANCE AD - EQUIPMENT / FURNISHINGS - AMERI-KING CORPORATION MODEL AK-450() AND AK-451() SERIES EMERGENCY LOCATORTRANSMITTERS - REPETATIVE INSPECTIONS, CHECKS, TESTS AND VERIFICATIONS

NOT APPLICABLE - AD2017-16-01; AMERI-KING CORPORATION MODEL AK-450 & AK-451 SERIES ELT INSPECTION, CHECKS &VERIFICATION. DOES NOT APPLY DUE TO EQUIPMENT NOT INSTALLED.

MOC :

MTH -MANDATORY N/A

FAA 2018-19-15 APPLIANCE AD - EQUIPMENT / FURNISHINGS - SAFETY BELT ATTACHMENT BOLTS - INSPECTION / TORQUE VERIFICATION / MODIFICATION

NOT APPLICABLE - NOT EQUIPPED WITH GEVEN S.P.A. (GEVEN) TYPE D1-02 AND D1-03 SEAT ASSEMBLIES / DE.MG.0011 / CDE/ 12-JUL-2018

MOC :

MTH -MANDATORY N/A

FAA 2018-23-01PARA (G)

INSPECT THE SEAT PAN STRUCTURE IN BOTH DEPLOYED AND STOWED POSITIONS (IF CRACKS ARE FOUND, REPLACE WITH REINFORCED SEAT PANP/N F0511530 AND REMARK THE SEAT) (IF NO CRACKS ARE FOUND, REMARK THE SEAT AND REINSPECT OR REPLACE THE SEAT PAN WITHREINFORCED SEAT PAN P/N F0511530)

NOT APPLICABLE - NOT EQUIPPED WITH ZODIAC SEATS FRANCE CABIN ATTENDANT SEATS, 536 SERIES / DE.MG.0011 / CDE /28-NOV-2018

MOC :

MTH -MANDATORY N/A

FAA 2018-23-01PARA (H)

INSTALLATION OF A REINFORCED SEAT PAN, P/N F0511530, USING PARAGRAPH 2.B., ACCOMPLISHMENT INSTRUCTIONS, OF ZODIAC SEATS FRANCESB NO. 536-25-003, REV. 3, DATED JUNE 2, 2017, IS TERMINATING ACTION TO THIS AD


MOC :

MTH -MANDATORY N/A

FAA 2018-23-01 APPLIANCE AD - EQUIPMENT / FURNISHINGS - CABIN ATTENDANT SEAT - INSPECTION AND REPLACEMENT


MOC :

MTH -MANDATORY N/A

FAA 2018-23-12PARA (G)

ACCOMPLISH AN INSPECTION TO DETERMINE IF ANY PLUG HAS PART NUMBER (P/N) B13984-3, STAMPLED WITH LOT PA-21 OR PA-22

NOT APPLICABLE - NOT EQUIPPED WITH ZODIAC AERO EVACUATION SYSTEMS (ALSO KNOWN AS AIR CRUISERS COMPANY)FUSIBLE PLUGS INSTALLED ON EMERGENCY EVACUATION EQUIPMENT / DE.MG.0011 / CDE / 28-NOV-2018

MOC :

MTH -MANDATORY N/A

FAA 2018-23-12PARA (H)

REPLACE FUSIBLE PLUG WITH A SERVICEABLE FUSIBLE PLUG P/N B13984-3 THAT IS NOT STAMPED WITH LOT PA-21 OR PA-22


MOC :

MTH -MANDATORY N/A

FAA 2018-23-12PARA (I)

NO PERSON SHAL INSTALL ON ANY AIRPLANE ANY FUSIBLE PLUG HAVING P/N B13984-3, STAMPLED WITH LOT PA-21 OR PA-22


MOC :


0:0225-Sep-2019125:48AIR COND

0:2825-Sep-2019265324:25ENG 2

0:2825-Sep-2019265324:25ENG 1

0:2825-Sep-2019265324:25AIRCRAFT


Last ActualDate


HB-VTBReg No:

30-Sep-2019 5:15AM

23-Jun-2017


Print Date:

Airworthiness:

Aircraft Serial:


Unit:

525-0947


(ENG) DUE 2

(ENG) DUE 1


City Part Serial No


C/W Time 2 + or -

Adj. TBO 1

TBO 2 TSO 2

TSO 1

Remains

RemainsDescription


Item Code

Mod Lvl

MTH -MANDATORY N/A

FAA 2018-23-12 APPLIANCE AD - EQUIPMENT / FURNISHINGS - INSPECTION AND REPLACEMENT OF ZODIAC AERO (ALSO KNOWN AS AIR CRUISERS COMPANY)EVACUATION SYSTEMS FUSIBLE PLUGS


MOC :

MTH -MANDATORY N/A

FAA 2019-07-03PARA (G)

REMOVE THE SEAT FROM THE AIRCRAFT AND PERFORM A DETAILED VISUAL INSPECTION; IF CORROSION OR OTHER DAMAGE IS FOUND, BEFORENEXT FLIGHT OR BEFORE (RE)INSTALLATION OF THE SEAT ON AN AIRCRAFT, AS APPLICABLE, REPAIR THE SEAT

NOT APPLICABLE - NOT EQUIPPED WITH ZODIAC SEATS FRANCE, 536-SERIES CABIN ATTENDANT SEATS, PART NUMBER (P/N)53600 / DE.MG.0011 / CDE / 08-APR-2019

MOC :

MTH -MANDATORY

N/A

FAA 2019-07-03PARA (H)

DO NOT INSTALL ON ANY AIRCRAFT AN AFFECTED ZODIAC SEATS FRANCE 536-SERIES CABIN ATTENDANT SEAT THAT HAS ACCUMULATED MORETHAN 14 MONTHS SINCE FIRST INSTALLATION ON ANY AIRCRAFT, UNLESS IT HAS PASSED AN INSPECTION IAW THE ACCOMPLISHMENTINSTRUCTIONS, PARAGRAPH 2.B., OF ZODIAC SEATS FRANCE SB NO. 536-25-002, REVISION 3, DATED NOVEMBER 2, 2016


MOC :

MTH -MANDATORY N/A

FAA 2019-07-03PARA (I)

MODIFICATION AND RE-IDENTIFICATION (P/N CHANGE) OF A SEAT IN ACCORDANCE WITH THE ACCOMPLISHMENT INSTRUCTIONS, PARAGRAPH 2.A.,OF ZODIAC SEATS FRANCE SB NO. 536-25-004, REV. 0, DATED OCTOBER 19, 2017, CONSTITUTES A TERMINATING ACTION FOR THE REPETITIVEINSPECTIONS


MOC :

MTH -MANDATORY N/A

FAA 2019-07-03 APPLIANCE AD - EQUIPMENT / FURNISHINGS - REAR CABIN ATTENDANT SEAT - INSPECTION / REPAIR


MOC :

MTH -MANDATORY N/A

FAA 2019-08-01PARA (G)

MODIFY THE AFFECTED PASSENGER SEAT AND RE-IDENTIFY EACH MODIFIED PASSENGER SEAT

NOT APPLICABLE - NOT EQUIPPED WITH RECARO AIRCRAFT SEATING GMBH & CO. KG (RECARO) MODEL 3510A AND 3510DPASSENGER SEATS / DE.MG.0011 / CDE / 07-MAY-2019

MOC :

MTH -MANDATORY N/A

FAA 2019-08-01PARA (H)

AFTER THE EFFECTIVE DATE OF THIS AD, DO NOT INSTALL AN AFFECTED RECARO MODEL PASSENGER SEAT ON ANY AIRCRAFT, UNLESS THE SEATHAS BEEN MODIFIED AND RE-IDENTIFIED IN ACCORDANCE WITH PARAGRAPH (G)(2), (3), OR (4) OF THIS AD


MOC :

MTH -MANDATORY N/A

FAA 2019-08-01 APPLIANCE AD - EQUIPEMENT AND FURNISHINGS - MODIFICATION AND RE-IDENTIFICATION OF ALL AFFECTED RECARO AIRCRAFT SEATING GMBH &CO. KG MODEL PASSENGER SEATS


MOC :

MTH -MANDATORY N/A

FAA 2019-14-05PARA (G)

REVIEW EACH AFFECTED B/E AEROSPACE FISCHER COMMON SEAT TO DETERMINE IF REWORK HAS ALREADY BEEN PERFORMED. IF THE REWORKHAS NOT BEEN PERFORMED REWORK THE AFFECTED SEATS AND MARK THE SEAT BY INSTALLING A PLACARD


MTH -MANDATORY N/A

FAA 2019-14-05PARA (H)

DO NOT INSTALL ANY SEAT AFFECTED BY THIS AD ONTO ANY AIRCRAFT UNLESS THE SEAT IS MARKED WITH A PLACARD STATING COMPLETION OFB/E AEROSPACE FISCHER ASB NO. SB0718-004, ISSUE A, DATED JUNE 26, 2018



0:0225-Sep-2019125:48AIR COND

0:2825-Sep-2019265324:25ENG 2

0:2825-Sep-2019265324:25ENG 1

0:2825-Sep-2019265324:25AIRCRAFT


Last ActualDate


HB-VTBReg No:

30-Sep-2019 5:15AM

23-Jun-2017


Print Date:

Airworthiness:

Aircraft Serial:


Unit:

525-0947


(ENG) DUE 2

(ENG) DUE 1


City Part Serial No


C/W Time 2 + or -

Adj. TBO 1

TBO 2 TSO 2

TSO 1

Remains

RemainsDescription


Item Code

Mod Lvl

MTH -MANDATORY N/A

FAA 2019-14-05 EQUIPMENT / FURNISHING - SEAT ENERGY ABSORBER ASSEMBLY - REPLACEMENT


MTH 6MANDATORY 19-Mar-2020 5 m 19 d

FAA 2019-15-10PARA (G)

REMOVE EACH AFFECTED LIFE JACKET FROM THE AIRPLANE AND REPLACE THE LIFE JACKET WITH A LIFE JACKET ELIGIBLE FOR INSTALLATION


MTH -MANDATORY 19-Mar-2020 5 m 19 d

FAA 2019-15-10PARA (H)

DO NOT INSTALL ON ANY AIRPLANE AN AFFECTED LIFE JACKET UNLESS IT HAS BEEN REPAIRED AND MARKED TO INDICATE COMPLIANCE WITHSUCH REPAIR IN ACCORDANCE WITH ZODIAC AEROSPACE SERVICES SB 25-65-34, REVISION 01, DATED MARCH 15, 2019, OR ORIGINAL ISSUE, DATEDJANUARY 8, 2019; OR A METHOD APPROVED BY THE FAA


MTH -MANDATORY 19-Mar-2020 5 m 19 d

FAA 2019-15-10 APPLIANCE AD - EQUIPMENT / FURNISHING - LIFE JACKET - REMOVAL / REPAIR


DAYS 29-Oct-2018 - N/A

EASA 2009-0278 APPLIANCE AD - FIRE PROTECTION - PORTABLE HALON 1211 FIRE EXTINGUISHERS - IDENTIFICATION / REPLACEMENT - SICLI



FAA 2005-17-11 FIRE PROTECTION - INSTALL IDENTIFICATION SLEEVES ON THE WIRING FOR BOTH ENGINE FIRE EXTINGUISHER BOTTLES


MTH -MANDATORY N/A

EASA 2019-0086R01 PARA (1)

DEACTIVATE THE ATLAS AND MODIFY THE TACS TO RESTRICT THEIR MOVEMENT, AMEND THE APPLICABLE AFMS, AMEND ITEM 27-60-01 “ATLASINOPERATIVE” OF THE MMEL SUPPLEMENT TO REMOVE THE 10 FLIGHT HOURS (FH) TIME LIMIT,INFORM ALL FLIGHT CREWS AND, THEREAFTER,OPERATE THE AEROPLANE ACCORDINGLY


MTH -MANDATORY N/A

EASA 2019-0086R01 PARA (4)

MODIFY THE AEROPLANE IN ACCORDANCE WITH THE INSTRUCTIONS OF SECTION 7 OF THE MODIFICATION SB.


MTH -MANDATORY N/A

EASA 2019-0086R01 PARA (5)

MODIFICATION OF AN AEROPLANE AS REQUIRED BY PARAGRAPH (4) OF THIS AD CONSTITUTES TERMINATING ACTION FOR THE DEACTIVATION,LIMITATIONS AND REPETITIVE PRE-FLIGHT INSPECTIONS AS REQUIRED BY THIS AD FOR THAT AEROPLANE.


MTH -MANDATORY

N/A

EASA 2019-0086R01

FLIGHT CONTROLS – ACTIVE TECHNOLOGY LOAD ALLEVIATING SYSTEM – DEACTIVATION / MODIFICATION - AIRPLANE FLIGHT MANUAL SUPPLEMENT– AMENDMENT


MTH -MANDATORY N/A

EASA 2019-0086-EPARA (1)

DEACTIVATE THE ATLAS AND MODIFY THE TACS TO RESTRICT THEIR MOVEMENT


MTH -MANDATORY

N/A

EASA 2019-0086-EPARA (4)

CONTACT CRANFIELD AEROSPACE SOLUTIONS FOR APPROVED ATLAS MODIFICATION INSTRUCTIONS AND ACCOMPLISH THOSE INSTRUCTIONSACCORDINGLY


MTH -MANDATORY N/A

EASA 2019-0086-EPARA (5)

MODIFICATION OF AN AEROPLANE AS REQUIRED BY PARAGRAPH (4) OF THIS AD CONSTITUTES TERMINATING ACTION FOR THE DEACTIVATION,LIMITATIONS AND REPETITIVE PRE-FLIGHT INSPECTIONS AS REQUIRED BY THIS AD FOR THAT AEROPLANE



0:0225-Sep-2019125:48AIR COND

0:2825-Sep-2019265324:25ENG 2

0:2825-Sep-2019265324:25ENG 1

0:2825-Sep-2019265324:25AIRCRAFT


Last ActualDate


HB-VTBReg No:

30-Sep-2019 5:15AM

23-Jun-2017


Print Date:

Airworthiness:

Aircraft Serial:


Unit:

525-0947


(ENG) DUE 2

(ENG) DUE 1


City Part Serial No


C/W Time 2 + or -

Adj. TBO 1

TBO 2 TSO 2

TSO 1

Remains

RemainsDescription


Item Code

Mod Lvl

MTH -MANDATORY N/A

EASA 2019-0086-E APPLIANCE/EMERGENCY AD - FLIGHT CONTROLS - ACTIVE TECHNOLOGY LOAD ALLEVIATING SYSTEM - DEACTIVATION / MODIFICATION - AIRPLANEFLIGHT MANUAL SUPPLEMENT - AMENDMENT



N/A

FAA 2004-14-20 FLIGHT CONTROLS - REMOVE AND REPLACE AN OLD TRIM PCB ASSEMBLY WITH A NEW DESIGN ASSEMBLY OR MODIFY AN OLD TRIM PCB ASSEMBLYTO THE NEW DESIGN


MTH -MANDATORY N/A

FAA 2019-08-13 FLIGHT CONTROLS - MODELS 525, 525A, AND 525B AIRPLANES WITH TAMARACK ACTIVE LOAD ALLEVIATION SYSTEM (ATLAS) WINGLETS INSTALLEDIN ACCORDANCE WITH SUPPLEMENTAL TYPE CERTIFICATE (STC) SA03842NY - REVISE THE OPERATING LIMITATIONS SECTION OF THE AIRPLANEFLIGHT MANUAL (AFM) TO PROHIBIT FURTHER FLIGHT



N/A

FAA 1997-01-02 LANDING GEAR - REPETITIVELY INSPECTING THE MLG TRUNNION PINS FOR PROPER INSTALLATION, AND EITHER IMMEDIATELY OR EVENTUALLYREPLACING THE EXISTING DRY-FILM LUBRICATED MLG TRUNNION SLOT BEARINGS WITH SEALED AND SELF-LUBRICATING BEARINGS



EASA 2010-0003R02 PARA (1)

VERIFY AIRCRAFT TYPE MODE STRAPPING CODE S SET TO ‘0’ (ZERO) OR ‘1’, AS DEFINED IN ROCKWELL-COLLINS SERVICE LETTER TDR-94( ) SIL 07-2.



N/AEASA 2010-0003R02 PARA (2)

EXEMPTIONS: DASSAULT AEROPLANES



N/AEASA 2010-0003R02 PARA (3)

EXEMPTIONS: ATR 42 AND ATR 72 AEROPLANES



N/AEASA 2010-0003R02 PARA (4)

EXEMPTIONS: SAAB 2000 AEROPLANES



EASA 2010-0003R02 PARA (5)

EXEMPTIONS: BOMBARDIER AEROSPACE (CANADAIR) AEROPLANES: CL-600-2B16 (604 VARIANT) AND CL-600-2B19 (RJ100 AND RJ200)



EASA 2010-0003R02 PARA (6)

EXEMPTIONS: CESSNA AIRCRAFT COMPANY AEROPLANES: CESSNA MODEL 525, 525A, 525B; AND CESSNA MODEL 525, 525A, 525B, 560; 560XL



EASA 2010-0003R02 PARA (7)

EXEMPTIONS: PIAGGIO AERO INDUSTRIES AEROPLANES: P.180 (AVANTI) AND P.180 (AVANTI II)



EASA 2010-0003R02

APPLIANCE AD - NAVIGATION - MODE S TRANSPONDER AIRCRAFT TYPE MODE STRAPPING - CHECK / MODIFICATION


MTH -MANDATORY N/A

EASA 2018-0247PARA (1)

INSPECT THE INSTALLATION OF THE AFFECTED PART ON THE AIRCRAFT

NOT APPLICABLE - NOT EQUIPPED WITH TRIG AVIONICS TT31, AVIDYNE AXP340 AND BENDIXKING / HONEYWELL KT74 MODES TRANSPONDERS / DE.MG.0011 / CDE / 14-NOV-2018

MOC :


0:0225-Sep-2019125:48AIR COND

0:2825-Sep-2019265324:25ENG 2

0:2825-Sep-2019265324:25ENG 1

0:2825-Sep-2019265324:25AIRCRAFT


Last ActualDate


HB-VTBReg No:

30-Sep-2019 5:15AM

23-Jun-2017


Print Date:

Airworthiness:

Aircraft Serial:


Unit:

525-0947


(ENG) DUE 2

(ENG) DUE 1


City Part Serial No


C/W Time 2 + or -

Adj. TBO 1

TBO 2 TSO 2

TSO 1

Remains

RemainsDescription


Item Code

Mod Lvl

MTH -MANDATORY

N/A

EASA 2018-0247PARA (2)

IF, DURING THE INSPECTION AS REQUIRED BY PARAGRAPH (1) OF THIS AD, IT IS DETERMINED THAT THE INSTALLATION IS NOT A CONVENTIONALINSTALLATION, AS DEFINED IN THIS AD, BEFORE NEXT FLIGHT, REMOVE THE TRANSPONDER FROM SERVICE FOR IN-SHOP MODIFICATION.


MOC :

MTH -MANDATORY N/A

EASA 2018-0247PARA (3)

RETURNING AN AFFECTED PART, REMOVED FROM AN AIRCRAFT AS REQUIRED BY PARAGRAPH (2) OF THIS AD, TO TRIG AVIONICS FORMODIFICATION, AND RE-INSTALLATION OF THAT MODIFIED TRANSPONDER ON THAT AIRCRAFT IS AN ACCEPTABLE METHOD TO COMPLY WITH THEREQUIREMENTS OF THIS AD FOR THAT AIRCRAFT


MOC :

MTH -MANDATORY

N/A

EASA 2018-0247PARA (4)

FROM THE EFFECTIVE DATE OF THIS AD, DO NOT INSTALL AN AFFECTED PART ON ANY AIRCRAFT, UNLESS THE INSTALLATION IS CONVENTIONAL, ASDEFINED IN THIS AD


MOC :

MTH -MANDATORY N/A

EASA 2018-0247 NAVIGATION - TRANSPONDERS - INSPECTION / MODIFICATION


MOC :

DAYS

MTH -MANDATORY N/A

EASA 2019-0004 NAVIGATION - GLOBAL NAVIGATION SATELLITE SYSTEM - OPERATIONAL LIMITATIONS

NOT APPLICABLE - NOT EQUIPPED WITH THALES GLOBAL POSITIONING SYSTEM/SATELLITE BASED AUGMENTATION SYSTEM(GPS/SBAS) RECEIVERS, TOPSTAR 200 LPV, IDENTIFIED BY PART NUMBER (P/N) C17149HA01 AND P/N C17149JA02 /DE.MG.0011 / CDE / 15-JAN-2019

MOC :

DAYS

MTH -MANDATORY N/A

EASA 2019-0179PARA (1)

AMEND THE APPLICABLE AFM(S) IN ACCORNDANCE WITH THE OPSB AND INSTALL THE APPROPRIATE PLACARD; VERIFY THAT A PRESSURE ALTITUDEREPORTING TRANSPONDER IS INSTALLED AND INTRODUCE PRE-FLIGHT CHECKS


MTH -MANDATORY N/A

EASA 2019-0179PARA (2)

MODIFY THE AEROPLANE BY INSTALLING A SOFTWARE UPDATE THAT RECTIFIES THE UNSAFE CONDITION ADDRESSED BY THIS AD; BEFORE NEXTFLIGHT AFTER MODIFICATION REMOVE THE AFM CHANGES AND PLACARD AND CONCURRENT WITH REMOVAL OF THE AFM(S) CHANGE ANDPLACARD INSERT THE APPLICABLE POST-SB MTB 34-02 AFM TC


MTH -MANDATORY N/A

EASA 2019-0179 APPLIANCE AD - NAVIGATION – AIRBORNE COLLISION AVOIDANCE SYSTEM DISPLAY SOFTWARE – UPDATE



N/AFAA 1997-05-03 APPLIANCE AD - ALLIEDSIGNAL GNS-XLS & GNS-XL



FAA 2001-23-17 APPLIANCE AD - NAVIGATION - MODIFY THE UNIT TO INCORPORATE CIRCUITRY CHANGES TO THE GNS 430 UNIT'S DEVIATION AND FLAG OUTPUTS



FAA 2003-13-08 APPLIANCE AD - NAVIGATION - INSPECT THE TAWS INSTALLATION AND REMOVE ANY TAWS WHERE BOTH THE TAWS AND ANY OTHER DEVICE ARECONNECTED TO THE SAME BARO SET POTENTIOMETER (SUPERSEDED BY FAA AD 2004-08-15)



0:0225-Sep-2019125:48AIR COND

0:2825-Sep-2019265324:25ENG 2

0:2825-Sep-2019265324:25ENG 1

0:2825-Sep-2019265324:25AIRCRAFT


Last ActualDate


HB-VTBReg No:

30-Sep-2019 5:15AM

23-Jun-2017


Print Date:

Airworthiness:

Aircraft Serial:


Unit:

525-0947


(ENG) DUE 2

(ENG) DUE 1


City Part Serial No


C/W Time 2 + or -

Adj. TBO 1

TBO 2 TSO 2

TSO 1

Remains

RemainsDescription


Item Code

Mod Lvl


FAA 2004-08-15 APPLIANCE AD - NAVIGATION - INSPECT THE TAWS INSTALLATION AND REMOVE ANY TAWS WHERE BOTH THE TAWS AND ANY OTHER DEVICE ARECONNECTED TO THE SAME BARO SET POTENTIOMETER



FAA 2014-18-01 APPLIANCE AD - NAVIGATION - ROCKWELL COLLINS, INC. MODE S TRANSPONDERS - INSPECTION / MODIFICATION



N/A

FAA 2015-10-51 APPLIANCE AD - AVIDYNE INTEGRATED FLIGHT DISPLAY (IFD)- INCORPORATE OPERATIONAL LIMITATIONS INTO LIMITATIONS SECTION OF THE AFMOR AFMS


-MANDATORY

N/A

FAA 2017-22-14 NAVIGATION - INSTALLATION OF THE TSSA-4100 FLS UPGRADES ON THE ROCKWELL COLLINS, INC. TSS-4100 TRAFFIC SURVEILANCE SYSTEMPROCESSING UNITS

NOT APPLICABLE - NOT EQUIPPED WITH TSS-4100 TRAFFIC SURVEILLANCE SYSTEM PROCESSING UNITS, (RCPN) 822-2132-001 / DE.MG.0011 / CDE / 25-OCT-2018

MOC :

MTH -MANDATORY N/A

FAA 2019-01-02PARA (G)(1)

DISABLE THE AUTOMATIC DEPENDENT SURVEILLANCE-BROADCAST (ADS-B) IN FUNCTION IN EACH UNIT

NOT APPLICABLE - NOT EQUIPPED WITH ASPEN AVIONICS, INC., EVOLUTION FLIGHT DISPLAY (EFD) EFD1000 PRIMARYFLIGHT DISPLAY, EFD1000 MULTI-FUNCTION DISPLAY (MFD), EFD1000 EMERGENCY BACKUP DISPLAY, OR EFD500 MFD UNITS/ DE.MG.0011 / CDE / 28-JAN-2019

MOC :

MTH -MANDATORY N/A

FAA 2019-01-02PARA (G)(2)

REVISE THE AIRPLANE FLIGHT MANUAL SUPPLEMENT IN ACCORDANCE WITH PARAGRAPH 5.2.C OF SB2018-01


MOC :

MTH -MANDATORY

N/A

FAA 2019-01-02 APPLIANCE AD - NAVIGATION - AUTOMATIC DEPENDENT SURVEILLANCE-BROADCASET (ADS-B) IN - AIRPLANE FLIGHT MANUAL SUPPLEMENT (AFMS)- DISABLE / REVISE


MOC :

MTH -MANDATORY

N/AFAA 2019-07-10PARA (F)(1)

REMOVE THE AHRS UNIT FROM SERVICE

NOT APPLICABLE - NOT EQUIPPED WITH NORTHROP GRUMMAN LITEF GMBH LCR-100 ATTITUDE AND HEADING REFERENCESYSTEM / DE.MG.0011 / CDE / 02-MAY-2019

MOC :

MTH -MANDATORY N/A

FAA 2019-07-10PARA (F)(2)

REMOVAL FROM SERVICE OF P/N 145130-7100 TERMINATES THE REQUIREMENTS OF AD 2010-26-09 (75 FR 81424, DECEMBER 28, 2010)


MOC :

MTH -MANDATORY N/A

FAA 2019-07-10PARA (F)(3)

DO NOT INSTALL AN AHRS UNIT P/N 145130-2000, 145130-2001, 145130-7000, 145130-7001, OR 145130-7100 ON ANY AIRCRAFT


MOC :

MTH -MANDATORY N/A

FAA 2019-07-10 NAVIGATION - LITEF ATTITUDE HEADING AND REFERENCE SYSTEM (AHRS) - REMOVAL


MOC :

DAYS

MTH -MANDATORY N/A

FAA 2019-12-09 NAVIGATION - FDSA-6500 TCAS - AFM OR AFMS LIMITATIONS SECTION - REVISION / PLACARD INSTALLATION

NOT APPLICABLE - NOT EQUIPPED WITH ROCKWELL COLLINS FLIGHT DISPLAY SYSTEM APPLICATION FDSA-6500 PARTNUMBERS 810-XXX / DE.MG.0011 / CDE / 10-JUL-2019

MOC :


0:0225-Sep-2019125:48AIR COND

0:2825-Sep-2019265324:25ENG 2

0:2825-Sep-2019265324:25ENG 1

0:2825-Sep-2019265324:25AIRCRAFT


Last ActualDate


HB-VTBReg No:

30-Sep-2019 5:15AM

23-Jun-2017


Print Date:

Airworthiness:

Aircraft Serial:


Unit:

525-0947


(ENG) DUE 2

(ENG) DUE 1


City Part Serial No


C/W Time 2 + or -

Adj. TBO 1

TBO 2 TSO 2

TSO 1

Remains

RemainsDescription


Item Code

Mod Lvl


N/A

EASA 2011-0090R1

APPLIANCE AD - OXYGEN – OXYGEN MASK REGULATOR INFLATABLE HARNESS – IDENTIFICATION / REPLACEMENT - INTERTECHNIQUE (PART OFZODIAC AEROSPACE), EROS



N/A

EASA 2012-0254R1

APPLIANCE AD - OXYGEN - FLIGHT CREW OXYGEN MASK REGULATOR - IDENTIFICATION / OPERATIONAL PROCEDURE / REPLACEMENT -INTERTECHNIQUE (EROS)



EASA 2014-0142R01 PARA (1)

ACCOMPLISH ACCOMPLISH THE ACTIONS AS SPECIFIED IN PARAGRAPHS (1.1) AND (1.2) OF THIS AD - DETERMINE THE DATE OF MANUFACTURING /REPLACE THE HARNESS INFLATION HOSE P/N 445186 OR P/N 445952, AS APPLICABLE, WITH A SERVICEABLE PART, OR REMOVE THE INFLATABLEHARNESS FROM THE MASK REGULATOR AND REPLACE IT WITH A SERVICEABLE HARNESS



EASA 2014-0142R01 PARA (2)

ACCOMPLISH AN OXYGEN MASK REGULATOR EQUIPPED WITH A P/N MXH20-1 OR P/N MXH21-1 INFLATABLE HARNESS HAVING A DMF CODE OFNOVEMBER 2008 (0845-S OR 08/45-S) OR EARLIER, AND THOSE WITH A DMF OF JANUARY 2011 (1101-S OR 11/01-S) OR LATER, IS EXCLUDED FROMTHE INSPECTION AND REPLACEMENT REQUIREMENTS OF PARAGRAPH (1) OF THIS AD



EASA 2014-0142R01 PARA (3)

ACCOMPLISH IT IS ALLOWED TO INSTALL ON AN AEROPLANE A FLIGHT CREW OXYGEN MASK REGULATOR, HAVING A P/N AS IDENTIFIED IN SECTION1.A.(1) OF ZODIAC AEROTECHNICS SB MC10-35-274, PROVIDED IT HAS BEEN DETERMINED THAT A P/N MXH21-31 INFLATABLE HARNESS IS INSTALLED,OR THAT THE P/N MXH20-1 OR P/N MXH21-1 INFLATABLE HARNESS INSTALLED ON THAT FLIGHT CREW OXYGEN MASK REGULATOR HAS BEENCORRECTED, AS REQUIRED BY THIS AD



EASA 2014-0142R01

APPLIANCE AD - OXYGEN – OXYGEN MASK REGULATOR INFLATABLE HARNESS / INFLATION HOSE – IDENTIFICATION / REPLACEMENT


LDG

HRS

MTH

76

115:54

31-Mar-2018 -MANDATORY N/A

FAA 2017-18-12PARA (G)

INSPECTION RETAINED FROM AD 2016-11-20 FOR AIRPLANES WITH PBE, P/N 119003-11, INSTALLED

NOT APPLICABLE - FAA 2017-18-12 PARA (I) & (J) IS NOT APPLICABLE TO OUR AIRCRAFT AS WE DO NOT HAVE PBE'SONBOARD.

MOC :

LDG

HRS

MTH

76

115:54


FAA 2017-18-12PARA (H)

REPLACEMENT RETAINED FROM AD 2016-11-20 FOR AIRPLANES WITH PBE, P/N 119003-11, INSTALLED


MOC :

LDG

HRS

MTH

76

115:54


FAA 2017-18-12PARA (I) & (J)

INSPECT TO DETERMINE IF THE S/N OF THE INSTALLED PBE, P/N 119003-21, IS WITHIN THE RANGE OF 004-14768M THROUGH 004-21093M OR 004-02393M THROUGH 004-03033M AND IF FOUND WITHIN THE S/N RANGE REPLACE IT.


MOC :


0:0225-Sep-2019125:48AIR COND

0:2825-Sep-2019265324:25ENG 2

0:2825-Sep-2019265324:25ENG 1

0:2825-Sep-2019265324:25AIRCRAFT


Last ActualDate


HB-VTBReg No:

30-Sep-2019 5:15AM

23-Jun-2017


Print Date:

Airworthiness:

Aircraft Serial:


Unit:

525-0947


(ENG) DUE 2

(ENG) DUE 1


City Part Serial No


C/W Time 2 + or -

Adj. TBO 1

TBO 2 TSO 2

TSO 1

Remains

RemainsDescription


Item Code

Mod Lvl

LDG

HRS

MTH

76

115:54


FAA 2017-18-12 APPLIANCE AD - OXYGEN - INSPECTION AND REPLACEMENT OF B/E AEROSPACE PROTECTIVE BREATHING EQUIPMENT (PBE), PART NUMBER 119003-11 AND 119003-21 THAT ARE INSTALLED ON AIRPLANES


MOC :

MTH -MANDATORY N/AFAA 2018-21-14PARA (G)

REQUIRED ACTIONS

NOT APPLICABLE - EQUIPPED WITH B/E AEROSPACE PN: 174252-96/-N6 SERIES MASKS / DE.MG.0011 / CDE / 22-FEB-2019MOC :

MTH -MANDATORY N/A

FAA 2018-21-14PARA (H)

DO NOT INSTALL ON ANY AIRPLANE A FLIGHT CREW OXYGEN MASK REGULATOR WITH A P/N LISTED IN PLANNING INFORMATION, PARAGRAPH 1.A.(1),OF ZODIAC SB MC10-35-274 R02, DATED JUNE 25, 2014, UNLESS IT MEETS THE DEFINITION OF A PART ELIGIBLE FOR INSTALLATION IN PARA (I) OFTHIS AD


MTH -MANDATORY N/A

FAA 2018-21-14 OXYGEN - OXYGEN MASK REGULATOR HARNESS INFLATION HOSES - INSPECTION / REPLACEMENT


MTH -MANDATORY N/A

EASA 2018-0259PARA (1)

MODIFY EACH AFFECTED PART IN ACCORDANCE WITH THE INSTRUCTIONS OF THE APPLICABLE SB/EB

NOT APPLICABLE - NOT EQUIPPED WITH LONE STAR AVIATION, CORP. USB RECEPTACLES, HAVING PART NUMBER (P/N) LS03-05050-A / DE.MG.0011 / CDE / 03-DEC-2018

MOC :

MTH -MANDATORY N/A

EASA 2018-0259PARA (2)

AFTER MODIFICATION OF AN AEROPLANE AS REQUIRED BY PARAGRAPH (1) OF THIS AD, DO NOT INSTALL AN AFFECTED PART ON THAT AEROPLANE.


MOC :

MTH -MANDATORY N/A

EASA 2018-0259 APPLIANCE AD - INFORMATION SYSTEMS - ELECTRONIC FLIGHT BAG UNIVERSAL SERIAL BUS RECEPTACLE - MODIFICATION


MOC :


FAA 2008-03-10 FUSELAGE - INSPECT THE LOWER WING SKIN STRUCTURE, FORWARD WING SPAR, LOWER FUSELAGE SKIN, FAIRINGS, AND THE EXTERNAL FAIRINGFRAMES FOR CORROSION; REPAIR ANY DAMAGE FOUND; APPLY A CORROSION INHIBITIVE SEALANT TO THE FUSELAGE FAIRINGS BEFOREREINSTALLING; AND DISABLE THE COCKPIT MOUNTED PILOT RELIEF TUBE



FAA 2008-12-01 POWER PLANT - INSPECT FOR MISSING FIREWALL SEALANT BETWEEN THE AFT FIREWALL ASSEMBLY AND SEAL ASSEMBLY



FAA 2010-12-01PARA (F)(1)

VISUALLY INSPECT LEFT AND RIGHT THRUST ATTENUATOR PADDLE ASSEMBLIES


MTH 29-Oct-2018 A/RMANDATORY

N/AFAA 2010-12-01PARA (F)(5)

REPLACE BOTH THRUST ATTENUATOR PADDLES



FAA 2010-12-01 DETECT AND CORRECT LOOSE AND DAMAGED FASTENERS, AND CRACKS IN THRUST ATTENUATOR PADDLES



0:0225-Sep-2019125:48AIR COND

0:2825-Sep-2019265324:25ENG 2

0:2825-Sep-2019265324:25ENG 1

0:2825-Sep-2019265324:25AIRCRAFT


Last ActualDate


HB-VTBReg No:

30-Sep-2019 5:15AM

23-Jun-2017


Print Date:

Airworthiness:

Aircraft Serial:


Unit:

525-0947


(ENG) DUE 2

(ENG) DUE 1


City Part Serial No


C/W Time 2 + or -

Adj. TBO 1

TBO 2 TSO 2

TSO 1

Remains

RemainsDescription


Item Code

Mod Lvl

MTH 29-Oct-2018 N/A N/AE1

FAA 1997-01-05 TO PREVENT POSSIBLE HIGH PRESSURE TURBINE (HPT) DISK BLADE RETENTION POST SEPARATIONS


MTH 29-Oct-2018 N/A N/AE2

FAA 1997-01-05 TO PREVENT POSSIBLE HIGH PRESSURE TURBINE (HPT) DISK BLADE RETENTION POST SEPARATIONS


MTH 29-Oct-2018 A/R N/AE1

FAA 1999-07-04 TO PREVENT HIGH PRESSURE TURBIBE (HPT) DISK RIM FAILURE (P/N 55291)


MTH 29-Oct-2018 A/R N/AE2

FAA 1999-07-04 TO PREVENT HIGH PRESSURE TURBIBE (HPT) DISK RIM FAILURE (P/N 55291)


MTH 29-Oct-2018 -SUPERSEDED N/A

FAA 2009-24-13 DETECT AND CORRECT LOOSE AND DAMAGED FASTENERS AND CRACKS IN THE THRUST ATTENUATOR PADDLES - SUPERSEDED BY AD 2010-12-01



Documents

Maintenance Inspections 10.pdf · 05nr08 renewal of insurance certificate mth 12 29-sep-2019 -1 d over due 05nr09 renewal of aircraft radio licence mth 18-oct-2018 120 mth 28-sep-2018