^nnnniMmr cnT,, ,j)[| |uipur ' PERFORMED IN ACCORDANCE ... · icertify that the transponder tests and inspections rfqiiibfd by far !^h4i3 have been performed in accordance with far

BROUGHT

FORWARD

liAR 0 5 1996

DAILY

TOTAL

AIR TIME AND

TOTAL AIR

engineering record

I NOTE; USE BOTH PACES AND AS MANY LINES AS REQUIRED FOR COMPLETEH RS* MIN •

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REQUIRED BY FAR 91.411 have BEEN PFRmPMcn PERFORMED IN ACCORDANCE WITHIM ^nnnniMmr cnT,, ,j)[| |uipur " 'rESTAlTITUPg 5-^ TEST ALTITUDE-g^/TO>1 AIR nm Kfjg74>//f^7 n.Tr ?- >. 4A. glS.N. $£>I0/£^92. #2

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CARRIED FORWARD

INSPECTION. REPAIRS 6 REPLACEMENT

ENTRIES. DRAW A DIAGONAL LINE THROUGH ANY UNUSED LINES IN DATE AND TIME COLUMNS.

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I CERTIFY THAT THE TRANSPONDER TESTS ANDINSPECTIONS RFQIIIBFD BY FAR !^H4I3 HAVE BEENPERFORMED IN ACCORDANCE WITH FAR 43APPENDIX F.

K-CAVIATI0N.1NC. CBSIiminL. APPLETGH.W154915

ll/tnlin inMl '

HAS BEEN INSPECTED IN ACCORDANCE WITH

CONDITION.

TcMnoiuiir

SIGNATURE

BABOVE LISTED MAINTEriANCEWA

LICENCE

NUMBER

DERAL AVIATION REGULATIONS AND WAS FOUND

Operator: Texaco Inc.Reg. No.: N1620Model: CL 600-2A12

K-C AVIATION, INC.301 Discovery DriveAppleton, WI 54915

LOGBOOK SUPPLEMENT

11: 5379.1LOGS: 3061S/N: 3025

Performed a 5400 hour inspection to include 100/300/600 hour inspections inaccordance with Canadair Time Limits and Maintenance Checks, PSP 601-5,revision 22 dated 9/15/95.

Complied with the following:Performed the following eddy current inspection in accordance with Canadair

NOT Manual, part 6 and PSP 601-5 Airworthiness Limitations chapter 5-10-00:

57-30-08 - left and right lower center wing plank, WS 65.0, stringer 14& 15

57-30-09 - left and right lower wing plank, WS 65.057-30-10 - left and right lower wing plank, WS 45.0, stringer 1057-30-20 - Access panel areas 540EB, FB, 640FB, 6B and 650AB78-30-05 - left and right main track attachment fitting

Corrosion noted on wing tank access panel rebate areas, 57-30-10. Corrosionblend repaired in accordance with Canadair REG 601-57-30-218 dated 2/28/96.No other defects noted.

Performed visual inspections of the following areas in accordance withCanadair NOT manual, part 9 and PSP 601-5 Airworthiness Limitations chapter5-10-00:VC52-10-03 - left and right main landing gear door hingesVC53-30-01 - structures adjacent to overboard lavatory servicesVC53-10-11 - lower sill F.S. 209VC56-10-01 - left and right side window glazing prism checkVC57-30-06 - left and right lower wing plank, WS 45.0, stringer 10VC57-30-09 - left and right lower center wing plank, WS 65.0VC57-30-10 - left and right lower center wing plank, WS 65.0VC57-30-13 - left and right lower wing plank WS 88.0VC57-30-41 - fuel tank water drain holesVC57-30-45 - wing fuel access holesVC78-30-04 - left and right thrust reverser main track aft lugsVC78-30-05 - left and right thrust reverser main track attachment fittingNo defects noted.

AD 86-10-02R1 dated 2/9/90 - inspection of elevator and aileron flutter dampercarried out and no defects noted.Dampers are due reinspection as per AD as follows:Left aileron 3/4/97 or A/C IT: 5679.1Right aileron 3/4/97 or A/C TT: 5679.1Left elevator outboard N/A to P/N 600-75142-3Left elevator inboard 9/4/96 or A/C TT: 5579.1Right elevator outboard 9/4/96 or A/C TT: 5579.1Right elevator inboard 3/4/97 or A/C TT: 5679.195-22-01 dated 12/4/95, ALC Information Bulletin No. 90-001 dated 9/15/92 -cabin fluorescent lighting inspection carried out. Upgraded the existingALC lighting system by complying with the following:

Replaced existing fluorescent lamps with new series 12 units P/N: AL1235.Replaced lamp connectors P/N: AL-5113 and wiring from lamps to power units.Replaced power supplies in the following locations to complete aircraftprotected power supply installation:

LOCATION P/N OFF S/N OFF P/N ON S/N ONL/H VALANCE TR992 15831 AL5112 19409R/H VALANCE TR992 15850 AL5112 19410LOCATION P/N OFF S/N OFF P/N ON S/N ONL/H VALANCE TR992 15811 AL5112 19408R/H VALANCE TR992 15833 AL5112 20147L/H VALANCE TR992 15798 AL5112 20148R/H VALANCE TR992 15819 AL5112 19407L/H VALANCE TR992 15800 AL5112 20146R/H VALANCE TR992 15823 AL5112 20149GALLEY TR992 14487 AL5117 1047GALLEY TR992 14509 AL5117 1124LAV TR992 14511 AL5117 1109Above upgrade constitutes terminating action for recurring inspectionrequirements of AD 95-22-01, paragraph (b). Revised wiring manual.

SB 601-0329R2 dated 12/14/90 - replacement of left and right main landing geardoor hinge fasteners part A carried out.

SB 601-0396 dated 9/15/94 - indicating/recording - modification - auralwarning system - take-off configuration warning back up carried out.Relocated radio master bypass circuit breakers B-164, B-165, B-166 and B-167 from circuit breaker panel B to below circuit breaker panel to abracket fabricated similarly to existing brackets. Rerouted existingcircuit breaker wiring as necessary to new location.

SB 601-0405R1 dated 3/31/95 - modification - fuel tank water drains -improved protective finish, part B carried out.

SB 601-0428 dated 3/15/95 - electrical power/flight controls - specialcheck/rework - shielded wire - wire insulation carried out per BombardierTechnical Support Fax dated 2/28/96.

SB 601-0429 dated 1/14/94 - modification - fuel control unit - introductionof part No. 6078T55P05 carried out.

SB 601-0435 dated 1/31/95 - modification - wing tank fuel access panels, P/N601R10906-17 and conductive gasket, P/N 600-10910-3 carried out.

SB 601-0440 dated 3/31/95 - modification - flap actuators attachment boltreplacement carried out.

SB 601-0441R1 dated 3/31/95 - modification - standby and APU fuel pumpassemblies - sealing external surfaces/replacement of anti-noise filterpart B carried out.

SB 601-0459 dated 11/30/95 - modification - rear fuselage frame assemblyinstall doublers for APU hoist carried out.

SB 601-1053R2 dated 4/01/87 - power plant - special check/modification - upperaccess cowl - clearances parts B and C verified by inspection to bepreviously satisfied.

SB 601-1084 dated 7/14/95 - special check/modification - thrust reverser -blocker doors and sound attenuating material panels parts A and B carriedout.

Dowty SB DALG 7200-32-3 dated 3/29/94 - nose landing gear drag brace corrosionin upper link subassembly carried out.

Allied Signal SB 85020-21-94087R4 dated 11/15/95 - air conditioning - waterseparator - add epoxy coating to interior surfaces to improved corrosion

resistance carried out.FAR 91.411 and FAR 91.413 - altimeter and transponder certification carried

out.

Performed torque check of both cooling turbines per Canadair MaintenanceManual 21-51-00. Breakaway torque value for both units, 17 ozs.

Replaced TCAS control P/N: 071-01502-4402 installing a tested and certified unitby AlliedSignal Avionics, S/N off: 1209, on: X1236.

HF receiver/exciter P/N: 064-1015-01, S/N: 25588 repaired by AlliedSignalAvionics. Cleaned and applied Nolux paste to bonding straps on both PAcouplers.

Replaced avionics bay aft inverter P/N: AL-0581 installing an overhauled unitby Aerospace Lighting Corporation, S/N off: 6843, on: 7103.

Replaced #2 HF indicator lamp for selcal.Replaced left wing, right wing and APU fuel boost pump EMI filters P/N: 160-

151501 installing new units supplied by Bombardier Inc., left S/N off: unk,on: 9441114; right S/N off: unk, on: 9441120; APU S/N off: unk, on: 9441105.

Replaced left main landing gear down lock harness P/N: 601-57788-15 installinga new unit supplied by Bombardier, Inc., S/N off: unk, on: 138.

Replaced right main landing gear down lock harness installing a new unit suppliedby Learjet, P/N off:600-85080-971, S/N: unk; P/N on: 601-57788-17, S/N: 5A.

Replaced #4 brake assembly installing an overhauled unit supplied by BombardierInc., P/N off: 600-85123-63, S/N: JUL86-0045; P/N on: 600-85123-81, S/N: 0CT90-

268.Replaced all left cabin windows installing new units supplied by Bombardier,

Inc., P/N off: 600-31066-1, P/N on: 601R31056-17, S/N's as listed below:S/N off: S/N on:

#1 0243 4751#2 0249 4752#3 unk 4753#4 0242 4755#5 0240 4756#6 0239 4757

Replaced aft equipment bay oxygen gage P/N: 171007 installing a new unit suppliedby AMR Combs.

Replaced co-pilots Davtron battery P/N: 8118 installing new battery withmanufacture date of 1-96.

Replaced jumpseat circlip found missing.Replaced #1 hydraulic accumulator gauge lens.Repaired eight pylon panel bonding plates in accordance with Canadair Structural

Repair Manual chapter 51-61-14, pages 1-3.Repaired chafe damaged left aileron access panel P/N; 600-13031-49 in accordance

with Bombardier Canadair REG 601-57-51-009 dated 2/29/96.Removed existing baggage door service light in left lower pylon panel installing

new door service light per K-C Aviation, Inc. Drawing No. CL600-33-90-244,rev. G, sheet 3. Reference one FAA field approved 337 dated 3/4/96 fordetails. Electrical manual revised.

Installed access panels in left and right wing tip fairings for access of strobelight power supplies and navigation lights in accordance with K-C Aviation,Inc. Drawing No. CL600-52-90-401, rev. A, sheet 8. Reference one FAA form337 dated 3/4/96 for details.

Reswaged #1 hydraulic T fitting P/N: D10023-060406 in aft bay and checked withgo-no-go gauge and found within limits.

Replaced damaged APU hoist intercostal in aft bay installing new unit P/N: 601-97111-1 per Structural Repair Manual 51-42-11.

Replaced nose gear drag brace center pivot pin assembly P/N: 200814624 installinga new unit supplied by Dowty, S/N off: unk, on: DCL493. Replaced thefollowing associated hardware: Pin assembly P/N: 200814206; P/N: 200814205and lock pin P/N: 200814707.

Removed and treated minor fuel sump corrosion per Structural Repair Manual.Repaired miscellaneous interior discrepancies. Recovered crew coat closet hanger

pole with new fabric. Materials used meet the requirements of FAR 25.853 asapplicable and are DER approved on FAA form 8110-3.

Adjusted lav dump cable.Rigged right flight spoiler proximity switch.Repaired as necessary forward and aft fuselage tank shroud leaks.#1 INS battery P/N: CA154~1, S/N: 9003645 bench checked, capacity checked, deep

cycled and repaired per Marathon manual BA-89.Replaced #1 hydraulic system poly flow drain line.Replaced miscellaneous interior and exterior lamps.Performed a post maintenance preflight inspection.ICERIIfy THAT THE AIR DATA GOMPUTER SYSTEM ICERTIFY THATTHE ALTIMETER AND STATIC SYSTEM ICERTIFY THAT THISSTATIC SYSTEM AND AUTOMATIC Vtit IDF TESTS AND INSPECTIONS REQUIRED BY FAR 91.411 HAS BEEN INSPECTED IN ACCORDANCE WITHREPORTING EQUIPMENT TESTS AND INSPECTIONS HAVE BEEN PERFORMED IN ACCORDANCE WITH .MCOFrnnij

oHrr-tHuiAL TEST ALTITUDE FEET. CONDITION.

K-CAVIATION.INC. CRSQK2!11ia APPLETON.WiSISIS

IN ACCORDANCE WITH FAR 43 APPEND XL ^ crrrHrr-tHuiA L ALTITUDE nra FEET. CONDITION.

TEST ALTITUDE FEET i,i ^h g£^9/oSS K-CAVIATIOH.IHC. Zmmm APPLETOH.WIS

#1 AIR DATA .S.[j.g2fZ2.?^Z.i)ATE_£Vzf£_ MAVlATiOH.lNG. CKQK2^L APPIHON.WI 54315#2AIRDATAS.H.g^ô7VgnATE _DATEJz£z££1^3ALTIMETERS.N. qatf Mtf /*93 runr

IH}AVIAT1I)N.INC. CfiSQR2R112l APPl£rON.WIS4915 I CERTIFY THAT THE TRANSPONDER TESTS AND MAINTENANCE RELEASEm, <i~' /J INSPECTIONS REQUIRED BY FAR 91.413 HAVE BEEN THE ABOVE LISTED MAlfiTENANCE WAS FERFORHEO

/ 7^ ^ ^ PERFORMED IN ACCORDANCE WITH FAR 43 AND INSPECTED IN ACCORDANCE WITH CURRENTUtO^ /093 naTF APPENDIX F. FEDERAL AVIATION REGULATIONS AND WAS FOUND• //1S.N. #2SN AIRWORTHYFORRETURJITOSERVICE,

K-CAVIAUOH.INC. CRS^R112UAPPmON.W154915 Ci!S^FI^lL^LETQ3. K) 54315

/£>93 naTF .

/D93

WQ.^ /093 nftTc

m

FAA Repair Station No. QK2R112L

REPORT OF NONDESTRUCTIVE TESTING

NDT METHOD: ET X MT

CL601

301 Discovery Dr. \ 414735-7000Appleton,WI 54915 \

VT X

Customer: Texaco Incorporated

Aircraft Registration Number: N162Q

Aircraft Serial -Number: 3025

Technique Number (AD, SL, SB): See Below

Type of Inspection: 5400 Hour

Technician: M. Weiter, T Haak Level: H, II

Date: February 28, 1996 Work Order: 01093

Accept: Reject: See Below: X

Performed eddy current inspection in accordance with Canadair Challenger NDT manual

part 6, on the following areas;

57-30-08, Left and right lower center wing plank, WS 65.0, stringers 14 & 15.

No defects noted

Signature:.Form 20273

KC Aviation isanEqual Oppomintty Employer

REPORT OF NONDESTRUCTIVE TESTING fCQNT

78-30-05, Left and right main track attachment fitting. No defects noted.

Performed visual inspection of the following are^^-in accordance with Canadair

Challenger NDT manual part 9;

52-10-03, Left and right main landing gear door hinges. No defects noted.

53-30-01, Structures adjacent to overboard lavatory services (external). No defects

noted.

53-10-11, Lower sill FS 209.0, No defects noted. ^

56-10-01, Left and right side window glazing prism check. No defects noted.

57-30-06, Left and right lower wing plank, WS 45.0, stringer 10. No defects noted.

57-30-09, Left and right lower center wing plank WS 65.0. No defects noted.

57-30-10; Left and right lower center wing plank WS 65.0. No defects noted.

57-30-13, Left and right lower wing plank WS 88.0. No defects noted.

78-30-04, Left and right thrust reverser main track aft lugs. No defects noted.

78-30-05, Left and right thrust reverser main track attachment fitting. No defects

noted.

BROUGHT

FORWARD

DAIl_Y

TOTAL

AIR TIME AND

TOTAL AIR

I engineering recordNOT_E: USE BOTH PASES AND AS MANY LINES AS REQUIRED FOR COMPLETE

HRS. MIN. HRS. MIN.

55b 1.3.

carried FORWARD

is e.

ENGINEERING RECORD

INSPECTION, REPAIRS a REPLACEMENT

ENTRIES. DRAW A DIAGONAL LINE THROUGH ANY UNUSED LINES IN DATE AND TIME COLUMNS.

CERTIFY THkT THE STATIC SYSIEM MAINTENAMCE KELEASu

K-C AVIATjD:L irlQ. CitS Qr/Ein2L APPLET0N,W154915CRSC':;2r.ii2L

SIGNATURELICENCE

N UMBER

A —V

OPERATOR: Texaco Inc.

REG NO: N1620

MODEL: CL 600-2A12

K-C AVIATION, INC.301 Discovery DriveAppleton, WI 54915

LOGBOOK SUPPLEMENT

IT: 5501.2

LOGS: 3112

S/N: 3025

Performed a 144 month airframe inspection to include a 6/12/24/36/72 monthinspections in accordance with Canadair Time Limits and Maintenance Checks,PSP 601-5 Rev. 23 dated 02/15/96.

Complied with the following:S/B 601-0460 dated 02/29/96. Modification - APU Bleed Air Duct - Check Valve

Reliability Improvement. APU check valve modified in accordance with Figure1 sheets 1 & 2. APU check valve part number changed from 3202072-2-1 to K600-97018-5, S/N: P-355C.

S/B 601-0471 dated 12/15/95. Special Check / Rework - Wing Anti Icing - Coupling/Boot - Cover position at FS 559.00. Installed new boot assembly P/N: 600-97074-25.

S/B 601-0472 dated 04/04/96. Special Check / Modification - MLG Door Mechanism -Possible Fouling Between Crank and Door Strut Link. Accomplished paragraph 2Aand figure 2.

Accomplished the following:Repaired left and right hand main landing gear door links and crank assemblies

by blending damage per PSP 607-51-52-00 and touch up per PSP 607-51-58-138/42A028 in accordance with Canadair Tech Support REO # 601-32-30-006 dated05/23/96.

Replaced the pilots oxygen mask P/N: MClO-13-03 with a overhauled unit by ScottS/N off: 15550, S/N on: 25840.

Replaced the copilots oxygen mask P/N: MClO-13-03 with a overhauled unit by ScottS/N off: 21254, S/N on: 25821.

The following items were hydro tested, serviced and function checked by C & MMarine, Inc. Outboard main oxygen bottle P/N: 89501015, S/N: 282-1068. Inboardmain oxygen bottle P/N: 89501015, S/N: 282-1065, Cockpit portable oxygen bottleP/N: 176965SMB3, S/N: 084840. Next hydrostatic test date due on 05/21/2001.

Replaced emergency exit handle Beta Light P/N: CANAC7B with a new unit S/N:4123, S/N on: 9493.

Replaced #1 brake assembly P/N: 600-85123-63 with a overhauled and modified unitby Aircraft Braking Systems Corporation. S/N off: Feb. 82-252, S/N on: Jan 83-585.

Replace #1 wheel assembly P/N: 5009029-1 with a overhauled unit by FlightpathServices, Inc. S/N off: Mar 90-0189, S/N on: Mar 90-0195. #1 tire P/N: 256K43-3, S/N off: 40480360, S/N on: 42080565.

Repaired #1 hydraulic line by installing new perma swaged fittings P/N's: D-10036-04, D-10036-06 and D-10023-060406 on the Tee fitting of the #1, #4#6 hydraulic 1ines.

TCAS Processor P/N: 066-50000-0108, S/N: 2949 modified and repaired by AlliedSignal.

Up dated #I & #2 FMS Data Bases with world wide and extended disks #1344-1 x1344-E dated 05/23/965 to 06/19/96. ^

Minor modification to forward fuselage upper electrical bay access doors

Recessed the left and right door locks to fit flush with the access doorsouter exterior using the existing door locks and hardware.

URDC AMPS 500 battery P/N: 171BS101-1, S/N: 602R was bench checked and repaired.Replaced battery assembly with 1 ea. battery pack P/N: 171BS104-2, S/N: 3425,charged and inspected i n accordance with URDC AMPS 500 Maintenance Manual171UM110.

Main SAFT battery P/N: 4078-3, S/N: 01806 was bench checked, capacity checked,deep cycled, thermostat operating parameters checked, charged, adjustedelectrolyte level and inspected in accordance with SAFT Maintenance ManualDC3-0I-78-3176-5B.

The following Grimes Emergency Light Batteries P/N: 60-1321-1 were repaired byK-C Aviation, Inc. reference FAA forms 8130-3's dated 05/24/96 for details ofrepairs.

Location

Under floor FS 280Under floor FS 320R/H LavatoryBaggage area

S/N:12996

14500

11927

10526

Bench checked, repaired, chargedBench checked, repaired, chargedBench checked, repaired, chargedBench checked, repaired, charged

The above Grimes batteries P/N: 60-1321-1 had battery packs P/Nreplaced with new units. All work was performed in accordanceOverhaul Manual 33-50-42.

Accomplished miscellaneous minor interior discrepancies.Performed a post maintenance preflight inspection.

& inspected& inspected& inspected& inspected55-2198-1

with Grimes

J CERTIFY THAT ml STATIC PRESSURE SYSIEMTESTS REQUIRED BY FAR 91.411 PARAGRAPH A-2HAVE BEEN PERFORMED IN ACCORDANCE WITHFAR 43 APPENDIX EPARAGRAPH A.

SYSTEM

K-GAVIflTIQfJ.h'lC. CRSmi2L APPl£rON,Vn54915

DV /M IJlr(jf -

MAINTENANCE RELEASETHE ABOVE LISTED MAIflTENANCE WAS PERFORMEDAND IflSPECTEO IN ACCORDANCE WITH CURRENTFEDERAL AVIATION REGULATICL'S AND WAS FOUNDAIRWORTHY FOR RETURNTO SERVICE.

K-CAVLTICN.IHC. CRSflWRIlEL fiF?lETOIU'l S45iS

W.0..j2.£3o

I CErri'.-v irL" '•'••••

70L:i:;anaikvôothycc;.:;".;:-:.

AIR TIME AND

'"• •• I |̂ M^lllhl^^ViLlM T- rgg '̂ations of the Federal•ervlce. Pertinent ^ 'S/aie upprouud fui latuiii toeni oetaiis ef the caliâtion are on fila dthlj J&LiMûmli. Wu.K U,Ll„ .a

Data - ?//</% -•

-nm ,?n-' < T^^.. ,DECISION COMPASS CALIBRAS4'i^c''nigKWB'« '̂a.'"

carried

ENGINEERING RECORD

INSPECTION. REPAIRS & REPLACEMENT

ENTRIES. DRAW A DIAGONAL LINE THROUGH ANY UNUSED LINES IN DATE AND TIME COLUMNS.SIGNATURE

K-OAVlATIOnmLoqbook Attachment

Date: 26 JULY. 1996Model: CL600-2A12AFTT: 5620.5

A/C: N1620

S/N: 3025

LNDS: 3158

LICENCE

NUMBER

Removed nllots windshield P/N 600-33030-19 S/N 1259 and installed a repaired/modified windshield P/N 600-33030-25S/N 1789R wlndshleW by Sierracin/Syimar Corp FAA CRS #U03R900L under work orter #20758.Reference FAA Form 8130-3 dated 5/24/96 for details. Windshield pressure/ operational checKed satisfactoniy.D HO- I k^nHHinnpr P/N 601-50910-9 S/N 038720. Installed a serviceable/tested signal conditioner P/N 601-S f sX 7S. rXn™ .»« -liWM »7 ~ FAA CJS ,E3DR»»Ji s".;: X„°. FAA F0,m 8130-! d.Bd 3!MS Idrd.l.iB. Opd..l,D.«l dO.dk! g.od.All work was accomplished in accordance with: PSP 601-2 Maintenance Manual,The aircraft, airframe, engine, or appliance identified above is ap^ return to service for the wortr perfonmed inaccordance with current regulations of the Federal Aviation Administration.

Mechanic:

ReferencedK-C Aviation inc. Work Order # A0169_Inspector, fjo/ Tv •

ÂMIATiOHhlC., 33 Elise Street, Westfield. MA 01085FAA CRS LEGR039G

•Kofatt ha® t»en inepected In aijoofdsnoo^^hwInipoctinn prrr]! ivi' r' hy l-JittlJfli"

' M. O P) Is ooprovod for;«turn towivloe.;fliljlt iuoMllly"^teeen in with Tffmgp inOi.

it/C' Iotal T[ni9

Precision Compass CalibratorsPfv tuK\1

kcvv-1P O Box 9221 Phoenix, A2 85068FAA Repair Station No KP3R639L

[lie attached c^t^jieet contains the re.'̂ ilts ol acompass swing icalibriilioii) ol the compass svsicms on your aircrall A/Zr^rOn Iins work w..' Cur Work Order No applies to this swing The upper portion ol'this data sheet iPC( \. contains data lor PCC relative to values either measured or used Irom previous swings in order to simulate electroinaaneticalK a hiah accuracvrotation ol the aircralt on a compass rose. For those interested, abriel explanation ol" these terms isas follows.

P '̂idfil'̂ nnined hearing which allow.s u.. k. align the MONTTOR ( a Magnetic Reterence transil like inslrument) parallel to an earth reference line which i-

oRRFCT^nv " MOXnOR INDEX is the hearing ol the eanh reference line a.s mea.sured al the Monitor location and this i.s corrected bv the TfRXT Vbl 1n,-.onv h^ f magnetic hearing for the line a. each aircraft llox \ahc location. With AlRCR.VI-f .AIJGXMEXT to the line vvc no« have an accurate iniliainidgnetic heading fortheaircraft al eachflux valve location a^wurau n.iuai

M&E2 are relative voltage values for the NS and EW components ol the electromagnetic lields reiimred tt. simulate the local earth's magnetic field in the Flux \ alve These numl'crIII sars with location and lalitiide being lower al high latitudes where the directional componenl ofthe earth's magnetic field becomes weaker.

El CK &E2 CK are sensitivitx coeflicienls which relate El and i:2 voltage values to our MONITOR. These numbers are acoastant and peculiar to each Mux v.iKc Thes ar.ill cpen em o atitu t and when used with ARE.A COMR allow us to eslahlish the correct El E2 voltages for suhsetiiienl swings without having to remove the flux va|\ c

AlXO and A27() are corrective circuit senings which are aconstant lor an\ Flux Valve and are independent oflatilude.

There are some other standards and abbreviations used by PCC. These are as follows:.ainipass Svstem tt] - Our standard is to designate the Flux \'alvc in the left wing as being associated with the =1 compass sv.stem. In most cases this will control the headun,in.strumems on the pilot's side of the instrument panel but there are exceptions. We will note these hv designating the in-strumenLs as =1 (pilot side! or -2 (copilot side) The •Mundards will apply to Compass Sx-stem =2 (ftux valve in right wing). For aircraft where the lliix valve is not mounted in the wing (C650 and Helicopters), we will use manufacturer's

R;^ -Radio Magnetic Indicator. The majority ofour work is with the Sperrx (Hone>\xel!) C9. Clft and Cll Compa.ss .System.s These use the Spcrrv Cft Indicator a.s the K.MI and wûse the C6 de^gnatiori|on our sheets The C6 indicator is also aM.VS'flvR IXDIC.VfOR I'or the system and has 2or 3Heading Transmiller.s which feed heading inlomvo.'.n to oihc^-onip,menus. These transmitters are designated us C\l. CX2 and CX.'̂ Our ct|uipmem can read these outputs in "minutes ofarc" where fU)' (miiuilcs) is ci|ual to ]'. Ucrecord the eirot'i t ic indicator or transmitter a.s or depending upon whether it is over tir under the input heading. Thus a" -1" "error in an indicator at an input heading of 27(j me ms that theIndicatorwillindieate27l''toflvacourseof27f) n.c.ui. u. ne

HM •Horizontal Situation Indicator. Apart of the Flight Director System, wc read crror.s to the nearest '. The same tolerance applies to RMl or C6 indicators.

iil or Flux Valve. The errors of the flux valve are measured in "minutes of arc". They appear under ORIGIXAI. ERRORS. On reswings this information will not appearRTT or Raw Flux Valve. Tbis is used to designate the errors of the flux valve when mounted in the aircraft with no compensation. These errors when compared with the tlux salve errorv5>ve a measureof the magneticdisturbances at the flux valve location. The errorswill he tn minutes of arc.

- Directional Gno. Drift tests of the gxro (no slaving). These tests are done only on Sperrx- C9. ClO. C11 and CI2 compass systems. Other systems do not have the oualits Bnt<where this test can he done in a static condition. '

XA - NotApplicable NC-No Change

Original Errors System #1

I'ltix Valve Spec. Flux Valve OK? Yes No

COMMENTS.

A/-5 '3'

COMMENTS - Final System Errors

o/tr

COMMENTS - DG Performance or SlavingSystem

~S, y/ry/Aj.

Coriolis Navig. Lights pj Strobes

OTHER COMMENTS:

PCC Work Order No. Aircraft

Original Errors System #2

Flux Valve Spec. ' Flux Valve OK? Yes y iVo

COMMENTS:

A/S .^-CO '

COMMENTS - Final Svstem Errors

COMMENTS -DG Performance or Slav'ing System 5Vau€ ^

Coriolis /i/W Navig. Lights av CroK..Strobes

OTHER COMMENTS:

Owner/Operator

Target Bearing

I IumtableCorrection -s I Corrected Index

ni -vrt E1CK_53r:2 -yn ^^9 E2CK

= i SYSTEM ORIGINAI. ERRORS

HDG RFV

COMIASS#! TYPE

= ^ CO Indie, or

Comnensalor/ Remote Compensator S/N

hnal Svstem Errors

hdgI

0

PRECISION COMPASS CALIBRATORS

Monitor Index —-V'

Area Comp,

^ 180

A 270 y-

E.W y.

Transmission Error

Magn. A/Aif Dm a//)

HDGl

180

195

#2 Turntable Correction

ti2 Corrected Index

EICK y>l3

H2 VP. E2 CK Vro

#2 SYSn-:M ORIGINAL ERRORS

HDG I I RFV

COMl'ASS n TYPE

# c? C6 Lidic. or# t>? Remote Compensator S/N

Final Svsiem Errors

pl'c form :

R«TO«d 2'<»4

Aircraft Alignment /

Area Comp ♦y/^

I ransmission l.rror

Magn /i/yf iJir /i//l

IF DIFFERRSCE

PERFECTIF

PEKKEC1

n FF RENCE

/Hr. corrected tor latitude

Î Flux Valve P/N

Aircraft T>pe

EC CWork Order No. Pô2:

Hrceision Compass Calibrators

S/N

S/N

l -U Repair Sution No. KP3R639LPhoenix. AZ

Calibrated By

Where Done

#2 Flux Valve P/N

Owner/Operator "7^

Inspected By

Aniluiiuud Sigiirttiiic

°/Hr. corrected lor laliiudc

AuUiunzod Sipmnite

BROUGHT

FORWARD

D All_Y

TOTAL

AIR TIME AND

TOTAL AIR

engineering RECORD

I NOTE; use BOTH PAOES AND AS MANY LINES AS REQUIRED FOR COMPLETEMRS, MIN. MRS. MIN.

^ ' 2. L. : 2,1^0 ATTAcH<^t:^

engineering record

inspection. REPAIRS ft REPLACEMENTENTRIES. DRAW ADIAGONAL LINE THROUGH ANY UNUSED LINES IN DATE AND TIME COLUMNS.

A cc<^^Pt-t C>

f':: s was fti'J'«0

SIGNATURELICENCE

NUMBER

K-C AVIATION. INC.301 Discovery DriveAppleton, U1 54915

OPERATOR: TexacoREG NO: N1620MODEL: CL500-2A12

IT: 5671.2LOGS: 3180

S/N: 3025

Performed aircraft evaluation per customer request. Reference attached list foradditional CAMP codes accomplished at this time.

Complied with the following:AD 86-10-02 R1 dated 2-9-90. Flutter Damper Inspection. Next due at: 5871.2

hours TT or 5-1-97 for L/H and R/H aileron, L/H elevator inboard, R/H elevatoroutboard; 5971.2 hours TT or 11-1-97 for R/H elevator inboard. AD notapplicable to L/H elevator outboard due to part number.

AD 95-17-14 dated 9-12-95. (SB A601-0443). Horizontal Stabilizer Trim ActuatorCheck. Next due at 5771.2 hours TT.

91-10-0592-16-1594-19-06

I Airworthiness Directives areat this time:

Air Cruisers Life RaftsNickel Cadmium BatteriesLeigh Systems ELTAPU Turbine Hub SeparationLockheed Digital FDRNarco ELT BatteryELT Lithium DioxidePacific Scientific BuckleEON Corp. Seat BeltsJET Power SuppliesFairchild CVRArtex ELT BatteriesSwitlick Life VestsKing Radio Fit. ComputersSperry AHRSCollins VOR/ILS ReceiverBendix King DMESwitlick Vest InflatorsTracor Omega/VLFTexas InstrumentsCircuit Breakers02 Corp. Lanyard PinsPortable 02 BottlesPuritan Bennett 02 Masks

not applicable due to equipment not

71-21-10 Hicrodot CVR74-18-15 Leigh Systems ELT74-24-07 ELT Battery Packs75-05-07 King Radio Nav System76-07-09 Collins RMI78-14-09 Pyrotector Fire

Detectors

80-05-02 Hamil Seat Belts80-12-15 Rosemount Probes80-19-19 JET RNAV Systems81-08-04 Puritan Bennett 02 Masks82-18-09 Tygothane Tubing85-22-10 Collins HSI/ADl86-05-02 United Inst. Altimeter86-22-10 Collins DME87-04-19 EON Seat Belt Buckle89-03-01R1 Goodyear Tires90-01-03 Honeywell AHRS/AHRU90-06-13 Honeywell Vertical Gyros91-08-04 Shoulder Harnesses

91-08-51 Honeywell FMS Data Base91-15-15 DuPont Breathing Equip.94-06-04 Eros 02 Mask Pin Failure

Performed corrosion inspection on L/H and R/H main landing gear shock struts andside actuator attach pins. No defects noted. Reassembled and serviced inaccordance with Canadair Maintenance Manual.

Performed corrosion inspection on nose landing gear shock strut and dragbrace.Removed and treated light corrosion in lower I.D. of nose gear bore inaccordance with Canadair Maintenance Manual 32-20-03. Replaced lower housingbearing P/N: CRS59-18-3 installing new unit. Reassembled and serviced inaccordance with Maintenance Manual.

Replaced #2 brake accumulator P/N: 2770571-103 installing repaired unit fromParker Hannifin. S/N off: 0855A S/N on: 1311A.

Replaced L/H flight spoiler proximity switch P/N: 8-405-04 installing new unit.S/N off: 22019 S/N on: 44100.

Replaced L/H and R/H outboard flap inboard leading edge rollers in accordancewith Maintenance Manual 27-50-11.

Serviced L/H inboard flutter damper and reinstalled in accordance with CanadairMaintenance Manual 27-33-11. No leaks noted.

Replaced L/H thrust reverser blocker door bushings and hardware at 11 o'clockposition. Replaced R/H thrust reverser blocker door bushings and hardware at9, 12, 1, and 5 o'clock positions.

Inspected and checked rigging of main cabin door in accordance with MaintenanceManual 52-12-00 and found to be rigged properly.

Performed visual inspection of L/H cockpit windshield frame, outboard side, 4thfastener downward from top T-plate. Blemish is a slight scratch only.

Replaced R/H motive flow lines P/N; 600-62257-5 and 600-62257-9 installing new.Tightened clamps at FS 556, WLllO for fuel shroud vent lines.R/H air conditioning duct assembly P/N: 601-95015-5 repaired by Bombardier

Aviation Services.Replaced wiring terminals on R/H air conditioning duct temperature sensorReplaced gasket P/N: 600-97106-1 at L/H ACU duct.

Replaced R/H engine core cowl seal P/N: 228-50196-101 and two seal capsP/N: 228-50196-103 installing new.

Repaired erosion on L/H engine nacelle inlet leading edge in accordance withStructural Repair Manual 51-51-03.

Repaired floor support angle at FS 621, L/H and R/H side, in accordance withCanadair Structural Repair Manual PSP 607 Chapter 53-15-08. Angle materialand fastener substitutions in accordance with Service Engineerino Letter dated10-25-96.

Existing four place divan reconfigured in accordance with Arkansas ModificationCenter Inc. SIC #SA4708SW, floor plan drawing 2700-3610, belted for threeplaces. Weight and balance change negligible, aircraft loading schedulerevised. Reference FAA Form 337 dated 11-06-96 for details.

Exterior placards redone as required in accordance with Canadair MaintenanceManual 11-20-00.

Installed new "No Smoking" placard at lavatory door.

Repaired fuel quantity indicator P/N: 601-50921-1 S/N: 433 by replacing lampassembly P/N: 220-355111-000 with new unit.

Repaired pilot's audio select panel P/N: M1045-FLAL-GQU7 S/N: 840858.Repaired cockpit flight phone controller P/N: 400-0138-005 S/N: 1085.#1 main battery P/N: 4078-3 S/N: 01806 capacity checked, deep cycled, and

charged in accordance with Saft Maintenance Manual.Fuel panel battery P/N: CA-125 S/N: 9200888 capacity checked, deep cycled, and

charged in accordance with Marathon Maintenance Manual.

Complied with miscellaneous minor interior and exterior discrepancies includingreplacing bad hardware and light bulbs as required.

Performed post maintenance preflight check. fiAirjiEWANCSreleaseTHE ABOVE LISTED MAiTsOErLMTCE WAS PERFORMEDAnO INSPECTED l!J ACCORD.'.'iCE V.'ITH CU-IREfiTFED"',I av!At;o:i REGi'Ui:c:;s and was foundAIRWORTHY EOT; DETC.Ji lO SERVICE.

K-COITQ.ING CnSDli.IlUL APPLEiGfLWI54915

//-fe

f» • ^ * * » •• •m *

K-C Aviation Inc. Computerized Maintenance Work Order: A0634FAA Repair Station QK2R112L Code Sign-Off Record Date: 10/29/96301 Discovery Drive S/N: 3025Appleton, WI 54915 Model: CL601-1

Time: Cycles: Reg. No: N1620Sheet No:

Companv: Texaco

Code Description Code Description242114 ADG oil level and leak check 243048 Check #1 main battery

243051 Capacitance test main batte

271121 Checkleft aileron flutter damperer

273031 Check left elevator flutter damperer (outer

223041 Check left elevator flutter damperer (inner

289016

491141 APU searbox magnedc plu

575710 Check right outboard flap vane/support structure

Inspector's Signature:

249211 Deep cycle main batte

271126 Check right aileron flutter damperer

273036 Check right elevator flutter damperer (outer

273046 Check right elevator flutter damperer (inner)

289018 Deep cycle fuel panel batte

575708 Check left outboard flap vane/support structure

995245 Functional test horizontal stabilizer trim actuator brake

Date:

Note: This sheet is a supplement to work order as listed above.

\st}MBARa/ER\

w

Bombardier Inc-Canadair, Business Aircraft DivisionP.O. 50S7, Station Centre-viiieMontreal Quebec H3C 369Phone (514) 855-5(300 Telex 05-825747Fax (514) S55-7701

DATE ZS HEURE/T/ME

TELECOPIEUR/FAX

DESTINATAIRE

TELECOPIE / FACSIMILE

PAGE / DE/OF 3

ADDRESS TO

OS> A l-Tl:^

}/. (L. AUHAHeuW —EXPEDITEURI FROM

OBJETSUBJECT A'/C

hfpLe-roJ

/s -r>/£; -ro

iJnJ^ A ,

SI VOUS Ne RECEVEZ PAS TOUTES LES PAGES, VEUiLLEZ NOUS RAPPELER JIF YOU DC NOTRECEIVS AU THE PAGES, C4U US.(514)SSS-7469

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laoddns X3naodd=wodd ss=80 9b-s3-xo(

Bon bardiei'-lnc.'Câinacldir

SERVIC'E "REQUEST hUHh^HUUUUl ourrA^m^wi

CAGE CODE 88308IPHONE

i0Zi sse t-is I 'Qi

DEPT.TZ't'

jSPPSAINUMBER

iMOddnS XOnaOdd'WOdd 93'00 9G-SS-J3

OCT-22-9G 10:2e FROM:CANADAIR CHALL PROJECT

Bombardier Inc-Canadair, Business Aircraft DivisionP.O. 6087, Stn Centre-ville

ExSIz^ Montreal, Quebec H3C 3G9// llLa Pbone (514) 855-5000 Telex 05-826747

Facsimile (514) 855-7701

date -2ô^<rT^ HEURE/HAfE

TELECOPIEUR / FAX

DESTINATAIRE/TO

k-. >ôe.c((rC Arf^LfcCT^-Z!)

PAGE 1

TELECOPIE / FACSIMILE

PAGES ( DE / OF ^

APRES-VENTE / PRODUCTSUPPORT .seRvice/ oept: 729 REF.EXPEDITEUR/FFO/W ^ CTiCi^Gvsr^^

MOTCLE [ KEYWORD A/C

MESSAGE

SI VOUSNe RSCEVEZPAS TOUTES LES PACeS, VEU1LLEZ NOUSRAPPEL£R / IFYOUOO NOTRECEIVEALL7WBPAGES CALLUS($14}S5€-5I)00(S5S9)

0CT-22-9B 10 s20 PROM: CANADAIR CHALL PROJECT' ' ID=1 51 4 855 8201

Bombardier Inc.

Canadair, Business Aircraft DivisionP.O. Bm Station CsntCft-Vill^

Motttr£al. QuibM H3C 3S9

Keith Schjoeder

ChallengerProgramCoordinatorKG Aviation, Inc.301 Discovery driveAppleton, WI 54915U.S.A.

Subject: Nose Landing GearLifeLimits

22 October 1996

Ref: 601L^755

References: A. Tdq>hcme Conversation L. Gerber/K. Schroeder 22 October 96B. Time Limits/Maintenance Checks PSP 601-5 Section 5-10-10

Keith,

Further to your inquiry at Reference A, the structural life limit applicable to NoseLanding Gear 601-55002-1 post Service BulletinSB601-0280 is 14500landings inaccordance with Reference B.

Canadair recognizesthat Nose Landing Gear601-85002-1 is not currently listed insection 5-10-11 of PSP 601-5 which provides the structural life limits for parts uponincorporation erf" SB601-0280. Wcare takingaction to correct this situation. Shouldvou have an>" additional questions, please call me at 514-855-8013.

Regari

LucGeiber

Maintenance Planning EngiQeering

Distribution:

Burak M.

Gdalevitch M.

Malcolm G.

Muniigi J.Reading File

BROUGHT

FORWARD

DAIUY

TOTAL

HRS. MIN.

AIR TIME AND

TOTAL AIRTIME SIN CE

M FG. ENGINEERING RECORDNOT^: use BOTH PAGES AND AS MANY LINES AS REQUIRED FOR COMPLETE

LOG BOOK SUPPT.F.MTTNt

Date: 12/20/96

A/C hours: 5674.7

Landings: 1383

This airframe log book is being dosed at this time. Ail future log book entries can be

Sted 12^6"'̂ Log beginning with log number iOOi"™bered 001 dated

to tWs date maintenance bistoiy prior

David S. BrownA&P 222307303

engineering record

INSPECTION, REPAIRS & REPLACEMENTENTRIES. DRAW ADIAGONAL LINE THROUGH ANY UNUSED LINES IN DATE AND TIME COLUMNS.

Documents

^nnnniMmr cnT,, ,j)[| |uipur ' PERFORMED IN ACCORDANCE ... · icertify that the transponder tests and inspections rfqiiibfd by far !^h4i3 have been performed in accordance with far