BROUGHT

FORWARD

DEC 15 1989

AIR TIME AND

DAILY

TOTAL

TOTAL AIR

TIME SINCEMFG.

HPS. MIN. MRS. MIN.

auRs-

LOGJ

ENGINEERING RECORD

NOTE: USE BOTH PAGES AND AS MANY LINES AS REQUIRED FOR COMPLETE

•: .-•r;.;X'/EWASRE

WINDSOR LOCKS. CT.0^

- 7

Oo— ~o

CARRIED FORWARD

ENGINEERING RECORD

INSPECTION. REPAIRS & REPLACEMENT

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

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REPAIR STATION

vTAT'Siie

iRir, nOMPANY REPAIR

STATION. GERTlPlGAlE NO. 3098

SIGNATURELICENCE

NUMBER

BROUGHT

FORWARD

MAR 0 1 1991

AIR TIME AND

DAILY

TOTAL

TOTAL AIRTIME SINCE

MFC.

HRS. MIN. HRS. MIN.

ENGINEERING RECORDNOTE: USE BOTH PAGES AND A3 MANY LINES AS REQUIRED FOR COMPLETE

ICfRTIFV THAT THIS 'eyCiT^r

^ iN^prrrinMAND WAS DETFRMiTiED TO BF IN AN AlRV/ORIHYCONDITION.

K-CAVI^ON.INC. CRSQK2R112L APPlETO^l54315

CARRIED FORWARD

ENGINEERING RECORD

INSPECTION. REPAIRS & REPLACEMENT

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

S.N..^//>/.r #2S.N. P /

"VA.TvTntl airportSoRLOCKS^nnseD

INSPECTIOMS REOUIRED'bY F¥9rdn HAVP RFCM m\i\m BY FAR 91.411 PARAGRAPH A-2pfrfpr',;ed ih aSd^ havf ref.n performed in acgordancc withappendix F ' far 43 appendix eparagraphT

SYSTEM //

ERVICE.

prnT,^,.:MT nFTAILsjf THE REPAIR ARE ON FILE AT THIS AGENCYUNDErSERWEWE 'J /5'Aht:^ FOfl

SIGNATURELICENCE

NUMBER

MACvTENAu'CE

FDEDAT AVIATION FTEC'.L-ATiONS ANin'.VO:TTHY FOR RFTURTl lO SERVICE

ITH CL'RRENT

Logbook SupplementTexaco Inc.

N1620 S/N: 3025TT:- 3017,1 LOGS: 2001

KC AVIATIOM, INC.FAA Repair Station QK2R112L

301 Discovery DriveAppleton, WI 54915

March 1, 1991

Performed a 3000 hour, operation 2 inspection in accordance with TexacoInc. inspection program FAR 91.409(E)(F)(3) using Canadair PSP601-5Time Limits and Maintenance checks. Reference attached sheet foradditional customer supplied CAMP codes accomplished.

Complied with the following:SB601-1070 - thrust reverser upper pylon cascades special check

carried out and reworked per pt. C.SB601-0304 - elevator control levers stress corrosion inspection pt.

A carried out and no defects noted at this time.SB601-1065 - auto throttle retarder control cable protection clamp

installation carried out on It. side only.SB601-1056 - exhaust nozzle fairings - installation of new bolts and

bushings carried out.SB601-1075 - thrust reverser blocker door link housing covers

modification carried out.SB601-1061 - thrust reverser blocker doors improved retention carried

out on rt. side only.SB601-0153 - forward engine mount retention bolts modification

carried out on It. engine only.SB601-0322 - ADG restow pump addition of warning placard carried out.SB601-1042R1 - thrust reverser blocker doors special check carried

out and no defects noted at this time (next due inspection at5417.1 flight hours).

SB601-1054 - throttle controls^ auto throttle retarder cable assemblypartial compliance by installation of spiral wrap only carriedout.

SB601-1066 - thrust reverser torque box drainage modification carriedout on It. side only.

SB601-0216R1 - pressure fuel line and N2 filter harness compatibilitywith ceco fuel pump modification carried out on It. engine only.

SB601-0320 - primary ejector pump and fuel feed tube connectorassembly modification carried out.

SB601-0361 - auxiliary tank fuel lines, elimination of possiblechafing modification carried out.

SB601-1068R1 - exhaust nozzle fairing fire sensing cable modificationcarried out to both sides.

SB601-0238 - use of CF34-3A at 3A power settings on CL601-1A aircraftmodification carried out.

SB A601-0309 - engine fire protection system wiring and fireextinguisher bottle squib wiring special check/modificationcarried out.

SB601-0360 - increased MTOW to 45,100 lbs modification carried out.

SB601-0334 - pitot static system drain modification carried out.SB601-0371 - tail tank float switch bracket modification carried out

to include RNIEO's #5, #13 and #14.SB601-0310R2 - air conditioning unit - introduction of water

extractor carried out. Replaced It. and rt. ACU heat exchangersinstalling repaired and/or modified units by AiresearchManufacturing, It. P/N off:191486-1, S/N: 91-392; P/N on: 191486-2, S/N: 108-133 ; rt. P/N off: 191486-1, S/N; 91-402, P/N on:191486-2, S/N: 71-730. Replaced It. cooling turbine installing anoverhauled unit by Garrett, P/N off: 586110-3, S/N: 19-298, P/Non: 586110-8, S/N: 30-605C. Installed new water extractors P/N:2340666-1, It. S/N: 50-237, rt. S/N: 79-161.

SB601-0262R2 - tail fuel tank addition modification to includeRNIEO's #53, #54, #55, #63, #72 and #86 carried out removing tailcone P/N: 600-21062-45 and installing tank P/N: 601-21001-1001/01,S/N: 0039; added aux tank float switches P/N: 88-5475, S/N: 0100and S/N: 0098. Replaced fuel quantity indicator installing a newunit, P/N off: 478-286-102, S/N: 146, on: 478-286-105, S/N: 433.Installed new signal conditioner P/N: 473382-01, S/N: 0208.Installed the following new fuel valves P/N: 601-62900-1: 3B pumparea S/N: N54423, aft bay refuel S/N: 137, gravity feed line S/N:143, shut-off S/N: 141. Installed vent system check valve P/N:7F2R-200000, S/N: 047. Replaced the following tail tank switches:upper float switch installing new unit, P/N off: 88-5475, S/N:0271, P/N on: 86-4086, S/N: 1271, rt. 4QD P/N off: 88-5475, S/N:0209, P/N on: 86-4086, S/N: 1269; It. 5QD P/N off: 88-5475, S/N:0281, P/N on: 86-4086, S/N: 1266. Added switch P/N: 86-4086, S/N:1262. Replaced the following aux tank switches: S3QD P/N off: 88-5475, S/N 0100, P/N on: 86-4086, S/N: 1272; S16QC P/N off: 88-5475, S/N: 0100, P/N on: 86-4086, S/N: 1268. Added It. aux tankswitch P/N: 86-4086, S/N: 1263. Reference 337 dated February 22,1991 for details.

Allied-Signal SB126758-78-1487 - pneumatic drive actuator replacementof plug and filter with vented plug carried out

Bombardier Alert Wire TA600-0612-034 - air driven generator outputwiring harness special check carried out and no defects noted

Service letter 600L-8409 - tail tank fittings visual check fortightness and sealant carried out

AD86-10-02R2 dated 2/9/90 - aileron and elevator flutter damper fluidlevel check carried out. Next inspection due 3217.1 hours or8/28/91.

Replaced APU fire extinguisher cartridge P/N: 897776 installing a newunit, S/N off: 4-84, on: 1-90.

Replaced It. and rt. fuel collector tank ejector pumps P/N: 2780602-104installing new units,It. S/N off: 0518, on: 0817; rt. S/N off: 0505,on: 0840.

Replaced ITT indicator installing new unit, P/N off: 418-101-104, S/N:296, P/N on: 418-101-120, S/N: 518,

Replaced It. aft bay temperature control valve P/N: 979558-8 installinga repaired unit by Canadair, S/N off: P-340, on: P-378. Replaced rt.aft bay temperature control valve P/N: 979558-8 installing a new unitsupplied by Canadair, S/N off: P-405, on: P-428.

Replaced It. engine power drive lock unit P/N: 126758-6-2 installing arepaired unit by Garrett, S/N off: P-115C on: 290C. Replaced shut-off and regulation valve P/N: 3214090-4-1 on It. PDU installing a newunit, S/N off: P-630C, on: 569,

Replaced #2 brake assembly installing an overhauled unit by AircraftBraking Systems Corp., P/N off: 600-85123-57, S/N: DEC 81-157; P/Non: 600-85123-63, S/N: FEB 84-721.

Replaced #2 wheel assembly installing an overhauled unit by FlightpathServices, P/N off: 5009815, S/N: JUN 88-0016, P/N on: 5009029-R-l,S/N: JUN 85-00488.

Replaced engine oil pressure indicator P/N: 418-106-106 installing arepaired unit by Canadair, S/N off: 416, on: 675.

The following fuselage fairings repaired by MIC Composites: center 3Aand 3B area, aft 3A and 3B area, 3A It. fairing and 3B rt. fairing.

Replaced It. thrust reverser emergency stow switch installing new unit.Replaced rt. engine IDG chip detector installing new unit.Replaced laser nav filters installing new units.Rebushed as necessary It. and rt. thrust reverser blocker doors.Replaced both water separator sock springs with new units.Replaced It. and rt. ground spoiler link rods and two bolts installing

new units.

Replaced It. outboard flap roller bearing installing new unit.Repositioned oxygen rack lower frame supports to provide clearance for

tail tank fuel lines installed for SB601-262R2.Accomplished the following listed FAA field approved form 337's dated

March 1, 1991 in conjunction with avionics installations andmodifications:1. The previously installed Fairchild AlOO Cockpit Voice Recorder has

been modified to comply with FAR 25.1457. Both Baker audio panelsP/N: M1045-FLAL-GQV7, S/N: 840858 and S/N: 840857 updated to mod11 by baker electronics. CVR rendered inoperative pending flightevaluation and FAA approval.

2. Installed Matrix terminal strips in the under floor avionics bayto centralize all tie points and fabricated a junction box tohouse relays and other similar components. Reworked Data Navinterface to permit display of FMS-1, FMS-2 or INS. Modifiedcenter cockpit pedestal by raising the aft end of the pedestal byapproximately 5.00 inches to a more horizontal plane, providing amore flat surface for crew visibility. The external lightingpanel located in the center pedestal has been modified to includeNAV and wing light positions on the Logo light switch. Added toadditional warning lights test switches, one on each pilotsvertical side panels which is paralleled from existing test switchlocated in center pedestal. Added two Master Specialties Series90K Annunciators at main cabin door to alert flight attendant ofcabin door and baggage door status and whether or not main cabindoor is secured properly. This indication is paralleled fromsimilar indication found in cockpit.

3. Replaced the two Collins VIR-30A VHF Nav Receivers, P/N: 622-0876-001, with two Collins VIR-32, VHF Nav Receivers, P/N: 622-6137-001. #1 S/N off: 22690, on: 6594; #2 S/N off: 22200, on: 10543.Replaced the two Collins DME-40 Receiver/Transmitters, P/N: 622-

1233-001 with two each Collins DME-42 Receiver/Transmitters, P/N:622-6263-003. ^1 S/N off: 8963, on: 9378; #2 S/N off: 15639, on:9413. Modified existing Colt CD-7000 cabin display system whichrequired the CD-7010, S/N: 037 cabin display interface to bemodified by Colt Electronics.

4. The previously installed Canadian Marconi SDS-776 Status DisplaySystem S/N: 103 was modified and repaired by Canadian MarconiCompany to account for the CF-34-3A engine type. P/N changed from100-478801-022 to -023. System inoperative pending STCapproval.

5. Reworked the previously installed single Honeywell Laser NavManagement System to include rewiring of INS, attitude sourceselection, heading source selection, pilots RMI. Replaced CA-54-1INS battery with a CA-154-1, P/N: 28656-002, S/N off: 7408023, on:9003645, Removed Global NDB- 2 Nav Data Base, P/N: 21105-2-03,S/N: 869.

6. Removed previously installed dual Global GNS-500 Series 3BVLF/Omega Nav Systems as follows: two CDU P/N: 11600-6, S/N: 2296and S/N: 643, two RCU P/N: 10050-3-3BE, S/N: 1410 and S/N: 3442,two OEU P/N: 10600-2-211, S/N: 3788 and S/N: 1942, two loopcouplers P/N: 11444-1, S/N: 3760 and S/N: 3752, two loop antennasP/N: 11455-2, S/N: 118 and S/N: 0098. Installed dual UniversalUNS-IA Compact Flight Management Systems as follows: two Super CDUP/N: 1016-1-11, S/N: 707 and S/N: 708, two Nav Computer Units P/N:1180-21-21, S/N: 525 and S/N: 528, one Data Transfer Unit P/N:140-01011, S/N: 312, two UNS-764 Omega/VLF Sensors P/N: 100-601200-003, S/N: unk and S/N: 580, two antenna coupler units P/N:418-312-001, S/N: 1432 and S/N: 1433, and two GPS antennas P/N:100-602061-000, S/N: 008 and S/N: unk.

7. Installed a Bendix/King CAS-81 TCAS-II Traffic Alert andCollision Avoidance System as follows: one TPA-81A TCAS processorP/N: 066-50000-8101, S/N: 1423, two MST-67A mode S transpondersP/N: 066-01143-0301, S/N: P1018 and S/N: P1021, one GC-362Agraphics processor P/N: 071-01505-0101, S/N: P1004, one KFS-578ATCAS/mode S control P/N: 071-01507-2001, S/N: 1013, IVA-81ATA/RA/VSI display P/N: 066-50001-1001, S/N: 1535 and S/N: 1557,two ANT-81A directional antenna P/N: 071-50001-8102, S/N: 1355 andS/N: 1354, two ANT-81A antenna adapter plate P/N: 047-50357-0003,two Sensor L-band antennas P/N: S65-5366-7L, S/N: 21047 and S/N:24325. Removed two Collins TDR-90 transponders P/N: 622-1270-001,S/N: 14770 and S/N: 15028, and one Gables G-6106-05 ATC controlS/N: 50. TCAS installation and usage pending STC issuance.Aircraft-placarded "TCAS USE PROHIBITED PENDING STC ISSUANCE".

Accomplished the following listed FAA field approved 337's datedFebruary 22, 1991:1. Removed AMC refuel/defuel control panel from cockpit center

pedestal installing new fabricated unit in same location.2. Installed two Grimes flush mounted dome lights in cockpit overhead

controlled by cockpit overhead lighting panel.3. The previously installed Lockheed Flight Data Recorder model 319

was relocated from fuselage station 760 to 745 in aft compartmentdue to tail tank installation. CVR relocated from fuselage

station 755 to 773 due to tail tank installation,4. Added a water drain system to existing lavatory water system

which when activated, drains the supply tank and purges the lineswith air supplied by existing water system air pump.

5. Removed existing water fill service fitting and associated linefrom right lower fuselage at toilet service area. Replaced toiletdump valve installing new Kaiser assembly P/N: 2651-311-3.

Installed an APU Carbon Seal Oil drain Ecology Canister in accordancewith KC Aviation STC SA1513GL. Reference 337 dated February 22,1991.

Replaced copilot altimeter indicator P/N: 4016341-904 installing arepaired and tested unit by Honeywell, S/N off: 82052767, on:87124926.

Recovered entrance and cabin headliner with new material. Replacedentryv/ay carpet with new material. Cleaned all interior softwarematerial. Repaired miscellaneous interior discrepancies. Allmaterials used meet burn test requirements of FAR 25.853 paragraph b.

Aircraft weighed using Revere Electronic Weighing Kit S/N: 5805Acalibrated May 1990. Reference KC Aviation weighing report datedFebruary 25, 1991. Aircraft equipment list and electrical manualsrevised.

Serviced aircraft main battery S/N: 51345, and the following batterypower supplies: S/N: 12918, 7254, 11927, and 9026.

Radar indicator P/N MI-58535-1, S/N: 1205 updated to a -2 by Honeywell.Colt cabin display interface P/N: CD-7010, S/N: 037 removed and sent in

for repair.Replaced engine oil temperature guage P/N: 601-50916-3 installing a

repaired unit by Canadair, S/N off: 458, on: 499.Lockheed FDR P/N: 650/1/14040/004, S/N: 3009 repaired and function

tested by Lockheed Aircraft Service Company.Performed minor alteration of the aft tailcone Kevlar fairings. These

fairings were cut and fitted with three access panels for transferboost pump, tail strobe light power supply and the lower fuel tankaccess panel. All work performed in accordance with CanadairChallenger Maintenance Manual (PSP607), Chapter 51 and KC Aviationdrawing number CL600-52-90-401-7. All hardware used meets AN, MSand/or NAS standards.

Performed a post maintenance preflight inspection.

ICERTirr mi THIS —

HAS BEfT.' INSPECTED IN ACCORDANCF WITH

3aoe> Z. INSPECTIONAND WAS DETERI.MNED TO BF IN-AN AIRWORTHYCONDITION.

K-CAV1AOO;J.[NC, Cr.SQR2R112L tPP™.WI54915

BY

(=Z?>X DATE 3h J

) CERTIFY THAT T>!E TRANSPONDER TESTS ANDINSPECTIONS REQUIRED BY FAR 91.413 HAVE BEENPEKrPR:.:ED Hi ACCGRD.''.HCE WITH FAR 43appe:;d!>; f.

HI ''7 P/aH/R^AViADiOU.iKC. CR3ai;2::ii2L Pj?LET^V.'i54315

ivn

MAINTENANCE RELEASE

THE ABOVE LISTED MAINTENANCE WAS PERFORMEOAND INSPECTED IK ACCORDANCE WITH CURRENTFEDERAL AVIATION REGULATIONS AND WAS FOUNDAIRWORTHY FOR RETURN TO SERVICE

K-CAVIATIOK.IKC CRS0l'v2R112L APPliTOf|/fl54318

DATE 'S//M

J CERTIFY THAT THE STATIC PRESSURE SYSTEMTESTS REQUIRED BV FAR 51.411 PARAGRAPH A-2HAVE CEEm PERFORIAED IN ACCORDANCE WITHFAR 43 APrENDI): I PARAGRAPH A.

SYSTEM

K-CfiyiAHOfi.iriC. CRSGaRilZL AFPl^N.WI54315

RY

WfK 2 DATE ^/l/IA

OPERATOR: TexacoREG NO: N1620

MODEL: CL600-2A12

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

LOGBOOK SUPPLEMENT

IT: 3065.3

LOGS: 2029

S/N: 3025

The previously installed Fairchild AlOO Cockpit Voice Recorder System has beenmodified to comply with FAR 25.1457 - reference FAA form 337 dated 3/19/81 fordetails. Cockpit recordings, as well as cabin interface, has been ground checkedwith an evaluation flight performed. The CVR was removed and evaluated by thisrepair facility, K-C Aviation, Appleton, WI., CRS QK2R112L and found to beacceptable. maintenance release

THE ABOVE LISTED MAIHTENANCE WAS PERFORMEDAKO INSPECTED IN ACCORDANCE WITH CURRENT

FEDERAL AVIATION REGULATIONS AND WAS FOUNDAIRWORTHY FOR RETURN TO SERVICE.

K-C AVUTIOH, IKC. CHS 0^1121 APFLETOIi, WI i4915

W.O_^iLL£_