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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