Honeywell

Gas Turbine

ENGINE LOG BOOK ENGINE, GAS TURBINE

PART NO. 3~0080'f- -I MOD EL NO. ~"""-=--"""""'"'15....=..o__;mc..__L.___ __ _ SERIAL NO. -'--P----"-~""'---~--=-c_• ____ _

Engine Data

MODEL NO. GTC f Sb- 150 CL QEC NO.

SERIAL NO.

DELIVERY DATE

APPLICABLE INSTRUCTION MANUALS

OPERATOR

OMB Control No. 2120-0018 0913012007

1. Approving National Aviation 2. AUTHORIZED RELEASE CERTIFICATE 3. Form Tracking Number: Authority/Country: 890000406008Y15

FAA/United States FAA Form 8130-3, AIRWORTHINESS APPROVAL TAG 303173411

-:. Organization Name and Address: Honeywell International Inc Repair Station 5. Work Order/ContracUlnvoice Number:

1944 E Sky Harbor Circle ZN3R030M 0553983 PHOENIX AZ 85034 Page 1 of 1 •

6. Item: 7. Description: 8. Part Number: 9. Eligibility:' 10. Quantity: 11 . Serial I Batch Number: 12. Status I Work:

001 ENGINE GTCP36-150[CL] 3800804-1 NIA 1 P-299C REPAIRED

13 . Remarks :

THE SERVICE SPECIFIED HAS BEEN ACCOMPLISHED IN ACCORDANCE WITH:

CMM 49-24 -74 Rev 0, NOV/30/2005

MM 49 - 24-75 Rev 0, FEB/2 5/ 2005

Additional Information

Modified GTCP36 - 100E P/N 3800050 - 5-1 TO GTCP36-150CL P/N 38 00804 - 1

PER SB 49-7885 .

TSN 5232.00

CSN N/ A

SEE ATTACHED DOCUMENTS AS APPLICABLE FOR WORK PERFORMED HONEYWELL CERTIFIES THAT THE WORK SPECIFIED IN BLOCKS 12/13 WAS CARRIED OUT IN ACCORDANCE WITH EASA PART 145 AND, WITH RESPECT TO THAT WORK, THE COMPONENT IS CONSIDERED READY FOR RELEASE TO SERVICE UNDER EASA PART 145 APPROVAL NUMBER: EASA 145.4136

~emm'""'"''"'ed1~ 19. ~ 14 CFR 43.9 Return to Service [81 Other regulation specified in Block 13

D Ap design data and are in a condition for safe operation. Certifies that unless otherwise specified in Block 13, the work identified in Block 12 and described in Block13 was accomplished in accordance with TiUe 14, Code of Federal D Non-approved des1 ta specified in Block 13. Regulations, part 43 and in respect to that work, the i tems are approved for return to service.

15. A"~ori'ed Slgoat"'"________---> ~ONO 20. Authorized Signa~ 21. Approva l/Certificate No.:

/f/rcc;rc? ~ ZN3R030M

1~rinted): 18. Date (m d y):

~ 22. Name (Typed or Printed): 23. Date (m d y):

Nongnooch Mercer JAN 29 2009

. . . . . User / Installer Responsibilities . . . It 1s important to understand that the existence of this document alone does not automatically constitute authority to inst·ill the part/component/assembly. Where the user/Installer performs work in accordance with national regulations of an airworthiness authority different than the airworthiness authority of the country specified in Block1 it is'essential that the user/installer ensures that his/her airworthiness authority accepts parts/components/assemblies from the airworthiness authority of the country specified in Block1 . Statements in Bio.ck 14 and 1g do not constitute installation certification. In all cases, aircraft maintanance records must contain an installation certification issued in accordance with the national regulations by the user/installer before the aircraft may be flown.

- - . . .. - - -FAA form 8130 3 (6 01 ) Installer must cross check eligibility w ith applicable technical data NSN . 0052 00 012 9005 Paperwork Reduction Act Statement: . . . . . . . . . .

-----------!!!!! ------------­!!!!!

!!!!! --

An agency may not conduct or sponsor. and a person is not required to respond to. a collection of information unless it di<plays a currently valid OMB control number associated with this collection of information 1s 2120-0018. Comments concerning the accuracy of this burden and suggestions for reducing the burden should be directed to the FM at: 800 Independence Ave. SW, Washington, DC 20591, Attn: Information Collection Clearance Officer. ABA-20.

36-150[CL] ACCEPTANCE TEST DATA SHEET

PAGE 1 OF 2 DATE: 01/28/09 DSC-3800804

USED WITH: TI-3800804 REV . c --ATP 31-17049 REV . L

UNIT OUTLINE: 38oo8o't-1 MODEL NO: 36-150[CL] SERIAL NO: P- 299

TEST CELL NO: Dl09 REPAIR ORDER NO =.3.tJ.t'f-pJ.2.71£37 PRODUCTION RELEASE NO: wA OI L USED: MIL-PRF - 23699

AIRFLOW MEASURING SEC NO: 6 x 3 . 0 FUEL USED: ASTM - D-1655

ECU PART NO: 2119584 ECU SERIAL NO: 75-Toool ECU LAB SLAVE; YES 0 NO D ECU SOFTWARE VERSION: .1. 11.1 ENGINE WEIGHT: MJ4 ITEM ATP SECTION UNITS REQUIRED RECORD

TOTAL NUMBER OF STARTS DURING ATP - NUMBER 3 TO 100 't-TOTAL OPERATION TIME DURING ATP - HOURS 1.0 TO 25 .2:q') AUTOMATIC START TIME 3.2.6 SECONDS 40 MAX 2')

UNIT STATUS: ACCEPTED ~ REJECTED D REMARKS:

TECHNICIAN: ~ ~/ [pl DATE: 01/28_/o_'j_ ;f

=~z~ 1 J

SUPERVISOR: DATE: ~ t 8 ~~ro . QUALITY ASSURANCE: DATE : JAN t 8 Z009

PAGE 2 OF 2

DSC-3800804A

36-150[CL) ACCEPTANCE TEST DATA SHEET

DATE: 01 / 28 / 09

USED WITH : TI-3800804

ATP 31-17049

REV. (;

REV. _8_

UNIT OUTL INE: 3800804 MODEL NO: 36-150[CL) SERIAL NO : P- 299 TEST CELL NO: Dl09

BAROMETRIC PRESSURE

AVERAGE INLET TEMPERATURE

FUEL INLET PRESSURE

OIL PRESSURE

OIL TEMPERATURE (MAX)

UNIT EXHAUST GAS TEMP

EXHAUST GAS TEMP

ORIFICE INLET PRESSURE

ORIFICE INLET TEMPERATURE

ORIFICE DELTA PRESSURE

BLEED AIRFLOW

BLEED TOTAL PRESSURE

BLEED TOTAL TEMPERATURE

FUEL CONSUMPTION

SHAFT POWER

APU SPEED

UNIT VIBRATION

DI GITAL DATA SCAN

ACTUAL

CORRECTED *

ACTUAL

CORRECTED *

ACTUAL

CORRECTED*

ACTUAL

CORRECTED*

ACTUAL

CORRECTED*

ATP SEC.

UNITS

PSIA

op

PSIG

PSIG

PSIA

PSID

LB/MIN

LB/MIN

PSIA

PSIA

LB/HR

LB/HR

HP

HP

RPM

IN/SEC

TIME

DATE

4 .2

103F BLEED ONLY

REQUIRED RECORD -- 14. 20

~ 66 -- 32

35-55 45

275 219 -- 1194

1230 MAX 1216 -- 42 .3 -- 426 - 2 .1 -- 90.6

78.4 MIN 82.4 -- 52.4

51. l MIN 52 . 6

~ 448

~ 484 -- 180 . 8 -- 171. 4 -- .0 -- . 0 -- 61980

0.60 MAX .33 -- 18:31

~ 01/28

*CORRECTED TO 103°F , UNINSTALLED, SEA LEVEL CONDITIONS

4.3

103F COMBINATION

REQUIRED RECORD

~ 14 .20

~ 65

~ 33

35- 55 45

275 227

~ 1189

1230 MAX 1216

~ 49.1

~ 427

~ 1. 5

~ 82.9

70.2 MIN 74 .4

~ 56 . 3

54.8 MIN 56.4

~ 449

~ 485

~ 193. 1

~ 183 .2

~ 47.4

47.3 MIN 4 9.0

~ 61970

0.60 MAX .20

~ 1 8:46

~ 01/28

JOB/EQU: 320-0840 VER: 1.05 REV: 09/10/07 IDMS:320-2052 VER: 4.55 REV: 06/16/05

4 .4

SHAFT ONLY

REQUIRED RECORD - 14.20 - 65 - 33

35-55 45

275 227 -- 5 36 -- 571 ---- ----------------- -- --- --- 103 .5 -- 107.1 -- 47.4

47.3 MIN 49.0 - 61970

0.60 MAX .23 -- 18 : 53 -- 01 /28

DATE .\ CC l i!\lll- ACCl ' \-IU-LATED L\TED

E'IG INE ENG INE HOliRS CYCLES

1/29/2009 TSN CSN

5.232 .00 Ni i\

R EMARKS, INSPECTIONS, REPAIRS, AND r\DJllSTMENTS

APll P/N 3800804- 1 SIN P-299C

Model GTCP36-l 50CL

DESCRIPTION OF WORK PERFORMED

ENGINE DISASSEM BLED AS NECESSARY TO PERFORM 36- 100 TO 36-150 MODIFICATION. INSPECTED. MODIFIED AND TESTED IAW \'1AN UFACTURER'S MANUAL AN D CUSTOMER INSTRUCTIONS. TSR/CSR-0-ALL WORK WAS ACCOMPLISHED IN ACCORDANCE WITH:

MM 49-24 -75 Rev : 0

CMM 49-24-74 Rev: 0 SER\ICE BULLETINS COM PLIED WITH: SEE SERVICE BULLETIN LIST

PARTS REPAIRED OR REPLACED TH IS VISIT: SEE TRACE fNPUT PAGE

'IDC I LIFE LIMITED PARTS: SEE SERIALIZED COMPONENTS INSTALLED AND LIFE LIMITED/ROTATfNG PARTS INSTALLED LISTS . (LIFE LIMITED/ROTATING PARTS LIST ONLY PROVIDED IF WHEELS EXPOSED) THIS ITEM. AS SUPPLIED BY THE CUSTOMER. HAS BEEN SERVICED IN ACCORDANCE WITH THE CURRENT REGULA rIONS OF THE FEDERAL AVIATION ADM INISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. PERTINENT DETAILS ARE ON FILE AT THIS AGENCY _ UNDER REPAIR ORDER NUMBER 2009-303172874-00 I INSPECTOR:

IH l"l l· 'i WH .L .\l · l<<>SJ' ,\l'I · .'\ l· lt V ICl·S l< t · l' ,\I~ \ N I>()\. H <llAI 1L Hl-: l'A IR STAT I0,'14 / .. '111lll11JM

~=-==-========================================~=====:================== ==;====-=;================ = =::::::: === ===:::::=~==============

LOGBOOK INTERVAL CHECKLIST REPAIR ORDE 5002279537 ENGlNE YIODEL: 36-ISOCL SN: P-299C CUSTOMER: 3 18850 DATE: I- l 7-2009 OCTLLNE NO. 3800804-1

C0.\1PO:\E:-lT NA.\1E INTERV . .\L STA.\.1P 'EXT DL1E HRS/MO.

. -~ T- ROTOR REPLACEMENT IOO<XJ 1' 2.12 . /

<"OMPO:-l ENT NAME INTER VAL STAMP 'J EXT Dl lE HR Sl.\10.

jp--=c;

Fut:! Sy;.1em Co mponents 500 ( __ 57.12

f'/F DELTA P INDICATOR 500 ~' I .' 71 2 COMPRESSOR ROTOR 20000 ~ ~5~ :-l~

COMP HOUSING SHROUD . .\T ACCESS ~~ .\T .\CCESS . ' I

.--..!.

I' I 5712 .\11\GNETIC CHIP 500 . ~-

CONTAINMENT RING AT ACCESS ,'" _":'; 7 AT ACCESS

,, . -1 nl:\2 <>IL FILTER ELEMENT l \){XI

.... ~ I' _.: TURBINE HOUSING .-\T .-\CCESS . ~ . ~ ,... , AT ACCESS DISC.-\IW Lill I lXXJ 02.12

EXHAlJST NOZZLE AT REMOVAL ~l ·\T REMOVAL

1-···-rr 1'.'JLET DUCT SCREEN 1) ()1) I / . I

r·=ry n712

IGl'>ITER PLLG 2U< XJ 72.12

ST .\f<TER MOTOR 2500 ~ 7712

I -~ K2.12 LOWER INLET DUCT ."1000

--~

UPPER INLET DUCT ."1 000 J ~232

DRAINS INSPECTION 11100 8232

i ·OPERATORS PARTICIPATING IN SPECTRO.'vlETERIC OIL AND FILTER ANALYSIS PROGRAM !SOAP) SHALL CHANG OIL AND FILTER ELEMENT AS DIRECTED IN SIL APU-49. HO:-.IEYWELL M:ROSPACE SERVICES PHOE:-llX REPAIR AND OVERHAUL FACILITY CERIFY THl\TTHIS ENGINE I COMPONENT HAS REEN INSPECTED IN .\CCORDANCE WITH MAINTENANCE :VIAN UAL INSPECTION I CHECK TAflLE oOI REQUIREMENTS. INSPECTIONS ACCOMPLISHED ARE LISTED AflOVE .

. .\PU TSN 5232.0 __ _

STAMP IN 1 ::-:::::1 ) INDICATES COMPLIANCES, OR ENTER CODE AS APPLICABLE.

NCW =NOT COMPLIED WITH. ND= NOT DISASSEMBLED. NA= NOT APPLICABLE TO PIN OR SIN r NR = NOT RECEI VED

ANALYST SIGNATURE: ;)____~cc ( ! c "\,,_ DATE: 1- 17-2009 _____ _

SERVICE RECORD ENGINE MODEL: GTCP36-150CL

ENGINE SERIAL NUMBER: P-299C TRACEABILITY PARTS REWORKED OR REPLACED

1 CUSTOMER: MIDCOAST AVIATION INC

REPAIR ORDER: 2009-303172874-001

PART :'liA\'IE MOTOR START

POWER SECTION ASSY COMPRESSOR ROTOR

TURBINE ROTOR

HOUSING ASSY

HOUSING SET

SENSOR PRESS !NL

IGNITION UN IT APU

FUEL CONTROL

VALVESURGE

VAL VE SHUTOFF

PART "ill'\IBER 2704458-1

3801340- 1

3822632-1

3842368-1

3862069-3

3862083-2

3876225-1

3876280-4

3883964-3

3884538-6

3885091-4

METER ASSY 3888033-5

WIRING HARNESS 3888524-3

SIN

2302

0812003

08-03160-00200

08-01345-08005

NIA

SET4P-12071

08-20219-09766

081121406592

080218092715

33629

1961

0465

NIA

08-16226-19460

LOT CONDITION 'iBR NIA New

NIA New

NIA New

08P351 New

303000044 Overhauled

302689052 Overhauled

NIA New

N/A New

NIA New

NIA New

NIA New

NIA New

NIA New

NIA New

i BULB TEMP MS28034-1 163527 NIA New

HONEYWEU. INTERNATIONAL INSPECTOR SIGNATURE d r -~~d, REPAIR STATION# ZN3R030M Nongnoo& Mercer

I

QTY

1

1

1 1 1 1

1 1

1 1 1 1 1

DATE: 01 12912009

Page I of I

DOC NBR

49-23-99

DAT E

AC Cutvl ll ­LATED ENGIN E HOURS

ACC l lf\1l i­LATEO

ENGINE CYCLES

REM,\RJ(S. INSPECTIO NS. REPAJR S. AND ADJ USTM ENTS SIGNAT URE

,,,,) M1 DCOA S T MAINTENANCE RECORD A .I CT A \.' tAT i O N C O t-!PA N Y

DATE: March 4, 2009 AlRCRAFT MAKE I MODEL: Challenger CL-601-3A AIRCRAFT REGISTRATION NUMBER: N953FA AIRCRAFT SERIAL NUMBER 5041 APU MODEL: GTCP-36-ISO(CL) APU SERIAL NUMBER: P-299C DESCRIPTION OF WORK PERFORMED:

1. Complied with General Inspection. 2. Complied with Pre-Install ati on Inspection . 3. Install ed Customers Q.E.C. Kit. 4 . Installed Engine onto Aircraft. 5. Serviced Engine with BP 2380 . 6. Complied with Engine Run and Leak Check.

AIRCRAFT TIME: AIRCRAFT LANDINGS:

APU HOURS: APU CYCLES:

7852.5 3572 5232.0 Not Applicable

All Maintenance, Operational, Functional and Leak checks were complied with in accordance with current revi sion of CL-60 J Aircraft Maintenance Manual and GTCP-36-150(CL) Maintenance manual

Foe moce ;nfonn'('.on op ' ck pecfo ed~cefe&ce Wock Ocdec No. M 11 3 81 on file alth;s fac;1;cy.

inspector Sign : _J , Date: March 4. ?009 JA' ON KlRK.PATRJCK

Midcoast Aviat on, Inc., CRS R03R822L, 6400 Curtiss-Steinberg Drive, Cahokia, IL 62206-1445 (s504 I .APU Log-02) (MC-RSM-0 I 3C (Revision 3, 11 /06))

DATE

ACCUMU­LATED ENGINE HOURS

r\CCl lMll ­LATEO ENGINE CYCLES

REMARKS, INSPECTIONS, REP AIRS. AN O ADJUSTMENTS

BOMBARDIER Aircraft Model Airc raft Serial # Aircraft Registration APU Model APU Serial#

Com lied with the followin Ins ections: 500 Hour MSG-3 Ins ection

c f t ks r d "th th f II omp 1e WI e o owmg mspec ion as : Code No.

49-90-00-202 APU - Discard of the APU oil

CL-600-2816 5041 N953FA GTCP36-150(CL) P-299C

APU LOG ENTRY

Description

49-90-03-202 APU - Discard of the auxiliary power unit oi l filter element

Date Aircraft Time Aircraft Cycles APUTime

SIGNATllRF.

February 1, 2011 839 l.5 3744 5578

I certify that this APU has been inspected in accordance with the instructions and procedures for an inspection program required by FAR 9!.409(f)(3), and is approved for return to service. Work orde~458

Date February 1, 2011 Signed (__:<~·~=~,.__...:::::~_,,::::::::::~-==---"==---FOR Fort Lauderdale Se Learjet Inc. 4 100 S.W. I Ith Terrace Fort Lauderdale, FL 3331 5 CRS: LN4R342M

ACCUMU- ACClli\1ll-

LATED LATED

DATE ENG INE ENGINE REM/\Rl-:S. INSPECTIONS. REPAIRS. AND i\DJUSTMENTS SIGNATURE

HOURS CYCLES

BOMBARDIER Aircraft Registration I

Serial Number I Aircraft Model I Nl70FL 5041 CL-600-2B 16

Page I of I

Tota l Time I

Total Landings I

Date 8811.6 3963 November 29'", 2012

APU Model

I APU SIN

I APU TSN

I GTCP36-150(CL) P-299C 6015.5

Auxilia ry Power Unit Logbook Entry

The Following Serialized Parts Were Instulled: Part Name P/NOll' SIN Off PIN On S/NOn Sta tus

APU Load Control Va lve 388509 1-4 0455 388509 1-4 0542 (Butternv Va lve)

Repaired

The 'Following Non-Serialized Parts Were Insta lled:

Part Name I PIN Off I Part Name I PIN On l Status Low Oil Pressure Switch I 387600 1-8 I Low Oil Pressure Switch I 387600 1-8 I New

The above described maintenance is certified airwo11hy and a detailed record is on file under work order: 162512 (\

Salvatore I I I l Tornatore \{'Q\j~ Date: November 29'", 2012 FAA CRS LN4R342 M

LEARJET INC. FORT LAUDERDALE SERVICE CENTER. 4 100 SW! Ith TERRACE FORT LAUDERDALE FLOR IDA 333 15

FAA CRS LN4R342M

ACCUMU- ACCll111l 1-LATED LATEIJ

DATE ENGINE ENGI NE REM r\RhS, INS PECTI ONS. REPAIRS. AN IJ ADJ USTMENTS SIGNATUR E HOURS CYCLES - CHALLENGE AIRCORP INC.

Aircraft Model Number: CL600-2B 16 Date: 3 April, 2013

Aircraft Serial Number: 5041 Aircraft Time: 8901 .6

Aircraft Registration: N l 70FL Aircraft Cycles : 4000

APU Model Number: GTCP 36-150 (CL) APU Hours: 6083.6

APU Serial Number: P-299C

Performed 500 Hour MSG-3 APU Inspection

The work identified above was performed and inspected in accordance with current regulations of the Federal

A 'iation Administration, and is appro,ed foe cotum to sm~~ock ocdec: 135

Date: 3 April, 2013 Signed: Gino Giorgi~~ ~ Lie: A&P 2886697 """' e---

DATE

ACCUMU­LATED ENGINE HOURS

ACCI lf\1l 1-

LATED ENGINE CYCLES

REMi\Rh:S. INSPECTIONS. REPAIRS. AND ADJUSTMENTS

BOMBARDIER Aircraft Registration I

Serial Number l Aircraft Model Nl70FL 5041 CL-600-2816

Total Time Total L1ndings 9003.1 4063

APU Model APU Serial Number GTCP-36-lSO(CL) P-299C

Auxiliary Power Unit Logbook Entry

Complied With The Followin2 1000 Hour TLMC MSG-3 Chapter 5 Inspection Tasks:

Code: Descriotion:

49- 10- 10-201 Operational Test of the APU Enclosure Drains 49-43-04-201 Ooerational Test of the APU External Remote Switch 49-80-00-204 Detailed Insoection of the APU Exhaust Svstem 49-81-00-201 Detailed Insoection of the APU Exhaust Shield and Visor Assemblv

49-90-00-202 Discard of the APU Oil 49-90-03-202 Discard of the APU Oil Filter Element

SIGNATURE

l Page 1 of 1

Date November 7, 2013

APUTSN 6214.0

I ceiiify that this APU has been inspected in accordance with the instructions and procedures for an inspection program required by far 91.409 (I) (3 ), and is approved for return to service. Work Order# 167516

Steve Gann

LEARJET INC, FORT LAUDERDA FAA CRS LN4R342M

Date: November 7, 2013 FAA CRS LN4R342M

FORT LAUDERDALE FLORIDA 33315

ENG INE MODEL: GTCP36- I SOCL ENGINE SERI AL NUMBE R: P-299C CUSTOMER: l'vlIDCOAST AV IATION INC REPA IR ORDER: 2009-303172874-00 I

SE RVI CE Bl iLLETIN

REV

SERVICE RECORD SERVICE BULLETIN COMPLIANCE

DESCRIPTION

-19-7885 0 CONVERSION OF ENGINE GTCPJ6- I DOE, PN 3800050-1 /-2/-3/-4/-5 . TO GTCP36-1 50CL. PN 3800804- 1

HONEYWELL INTERNATIONAL

REPA IR STATION # ZNJROJOM

WHERE ACC0:\1P

Pl-IX

DATE: 1/29/2009

Page I of I

WHE:--1 ACCO MP I /29/2009

Engines & Systems Acceptance Tag

Honeywell

I n t e r n a t i o n a I I n c.

· Engines & Systems

OUTLINE I KIT P/N REV. SEIUAL NO.

380 1340-1 A 0812003

SERIES CHANGES

NONE

NDC PART

NUMBER

380 1340- 1

NONE

NOMENCLATURE

PWRSECT

LOOSE ITEMS PART UMBER NOMENCLATURE

SERIAL NUMBER

08 12003

SERIAL NUMBER

Page 1 of 1

ACCEPTANCE TAG Certificate of Conformance

CUSTOMER

C USTOMER NAME MODEL CODE

CODE

HONEYWELL 36-150CL

AIRLINE SERVICES ASD POWER NIA

SECTION SlllPPER NO. ALLOCATION SALES ORDER NO.

BD 2128 REL) BD DRY WEIG llT F.T. DATE

NONE LBS.

TRACEABLE PARTS SERIES PART NUMBER SERIAL NUMBER LOT

HOURS NUMBER

NONE 3822632- 1 08-03160-00200 NONE 00:00 3842365-1 08-19914-24467 NONE 00:00 .....

~1_842366-.? 08- 1 99 14-1 ~506 NONE 00:00 3842368-1 08-01345-08005 08P351 00:00

3846564-1 NONE 08-27843-00:00 SERIES 324

3846779-1 NONE 08P346 00:00

This certifies that the materials and/or articles noted hereon were procured and/or manufactured under a Quality Assurance System acceptable to the Government and that all applicable certificates and records

arc on file and available for review by authorized customer representatives

PX2310-l

https://aeroserialctrl.honeywell.com/acctag/servlet/ AcptTagFCopy?onumbe1= 3801340- 1. .. 12/24/2008

ULTIMATE LIFE PART CARD

PART NAME Compressor Rotor

SERIAL NUMBER 08-03160-00200

Honeywell

TIME ON PART THIS INSTALLATION

CYCLE HOURS

00:00 00:00

PART NUMBER

ASSY. PART NUMBER 3822632-1 ~~~~~~~~~~~~-!

TOTAL TIME ON THIS PART

CYCLE HOURS

00:00 00:00

Honeywdl International Inc. Engines & Systems P.O. Box 52181 Phoeni x. Arizona 85072-21 81

REMARKS

AX6167-2B

~N. 08P35 e ULTIMATE LIFE PART CARD

PART NAME Turbine Rotor

SERIAL NUMBER 08-01345-08005

Honeywell

TIME ON PART THIS INSTALLATION

CYCLE HOURS

00:00 00:00

PART NUMBER

ASSY. PART NUMBER 3842368-1

TOTAL TIME ON THIS PART

CYCLE HOURS

00:00 00:00

Honeywell International Inc. Engines & Systems P.0.Box52181 Phoenix. Arizona 85072-21 81

REMARKS

AX6167-2B

ENGINE MODEL: GTCP36-I 50CL ENGINE SERIAL NUMBER: P-299C CUSTOMER: MIDCOAST A. YIATION INC REPA IR ORDER: 2009-3 03 172874-00 1

PAR I :'llAME PARI :'I/UM BER 'v10TOR ST ART 2704458-1

IGN ITION L"NIT APU 3876280-4

FUEL CONTROL 3883964-3

VAL YES URGE 3884538-6

VAL VE SHUTOFF 388509 1-4

METER ASSY 3888033-5

WIRING HARNESS 3888524-3

ENGINE MODEL: GTCP36- l 50CL ENGINE SERIAL NUMBER: P-299C CUSTOMER: MIDCOAST AVIATION INC RE PAIR ORDER: 2009-303 172874-00 I PART 'IA"IE PART !'HIMBER

: COMPRESSOR ROTOR 3822632- 1

3842368- 1

SERVICE RECORD SERIALIZED COMPONENTS INSTALLED

~ ERIAL NUM BER C'ONDlTTO 2302 N~w

1)802 180927 15 New

33629 :--Jew

196 1 New

0465 :--Jew

NIA New

08- 16226- 19460 New

SERVICE RECORD LIFE LIM ITED/ROTATING PARTS INSTALLED

P.\ RT SIN TSN

08-03160-00200 0.0

08-01345-08005 00

REFE R TO THE ACCOMPANYING TRACEAB ILITY REPORT ( IF APPLICABLE) FOR PARTS REPAJRED/REPLACED DURING THIS VISIT

HONEYWELL t:'l/TERNATIONAL

REPAIR STATION# ZN3 R030M

l'agc I of I

Page: I of I

CSN

0.0

0.0