I 1. Country 2

UNITED STATES FAA FORM 81 30-3

AIRWORTHINESS APPROVAL TAG U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

3. System Tracking

S97/310141 ,

4. Organization

&liedsignal A E R O S P A C E

AlliedSignal Singapore (Pte) Limited 161 Gul Circle Singapore 629619

5. Workorder, Contract or Invoice Numt

611341-000 ASC, SHANGHAI BRANCH

I

6 Item 7 Descr~pt~on 8 Part No 9 Ellglblllty0 10 Quant~ty 11 Ser~al I Batch No. 12 Status I Work

1. GTCPIJI-9D APU 3800592- 1 HD-90 1 Pi066 INSPKCTKD HODIFIKD RKPA I RED

'urchase Order No.: 97YWD90-608SG Order Kntry No. : 109190-001

13. Remarks

THIS CEITIPICATE IS RELEASED IN CONJUNCPIOf WITH AAC-038 FORH. RKPBR TO PORN GTCP131-9D-G04-RO FOR DETAILS OF ALL LIP1 LIHITED PARTS ALL A1 RWORTHINKSS DIRECTIVES A N D ALKRT SBRVICK BULLETINS WIRE REVIKWBD AND POUND PRKVIOUSLY COHPLIBD/NOT APPLICARLK UNIT TKSTID 1.A.W. COHPONKNT HAINTsNANCK HANUAL REPORT NO:49-26-77R3 APU TSN 686 CSR 00 CSR 503 CSR 00 SHIPPED LESS SURGK VALVE

Lim~ted life oarts must be accom~anied bv maintenance historv includino total bme / total cvcles /time since new.

19. Return to Service in Accordance with FAR 43.9

Certifies that the work specified in block 13 (or attached) above was carried out in accordance with FAA airworthiness regulations and in respect to the work performed the part(s) is (are) approved for return to service.

15. Signature 16 FAA Au!hnzatron No 20 Author~zed Stgnature 21 Certlf~cate Number

FT4Y 192H -

17. Name (tvoed or minted) 1 18. Date 1 22. Name (Typed or Prfnted) / 23. Date ~ ,.

~ C H A R L K S C H A W NAN W B N G ( 26 NOV 1997 FAA FORM 81 30-3 (07t94) '(Optional) Installer must cross check elig~bility with applicable technical data. CUSTOMER

&lliedSignal A E R O S P A C E

AlliedSignal Singapore (Pte) Limited

TURBINE ACCEPTANCE TAG & TRACEABILITY INPUT

PARTNO : 3800592-1

SERIAL NO : P1066

WIO NO : 611341

CHANGES : NIL

DESCRIF'TION

STARTER FUEL CONTROL UNIT IGNITION UNIT IGV. ACTUATOR FAN ASSEMBLY OIL-COOLER OIL PUMP

TSO I TSN : - I686

CSO I CSN: - 1503

17 SERIES :

NDC COMPONENTS:

PART NO.

2704482-3 3883600-2 3888000-7T 38861 88-2 3616140-4 160492- 1 4131010-2

DESCRIPTION PART NO.

1 ST TURBINE WHEEL 3840 160- 1 2NDTURBINEWHEEL 3840 165-4 IMPELLER (LIC) 3822400-4 IMPELLER 3822391-7 TURBINE SHAFT 3822398-4

SERIAL NO.

TRACEABLE PARTS:

LOT NO

DATE: 25th NOV. 1997

CUSTOMER: CASC

GTCP 1 3 1 -9D MODEL:

SERIAL NO.

SHIPPED LESS: SHIPPED LESS SURGE VALVE ASSEMBLY

SERIES CHGNO

TSN CSN

INSPECTOR'S SIGNATURE & STAMP: - 4

ACCEPTANCE TEST DATA SHEET

131-9 [Dl APU

I CUSTOMER : CASC ENGINE PART N O : 3800592-1 DATE

MODEL GTCP 131-9[D] ENGINE SERIAL N O : PI066 WORK ORDER N O : 611341

ECU PIN

PARAMETER

PB

WB

EGT

21 18848-1 SIN OR SLAM* : SLAVE (SIN: D8)

INDICATED LABORATORY SLAM OR ECU SIN AS APPLICABLE.

" PERFORMANCE DATA HAVE BEE MJUSTEDTO S.L, 103 'F. INSTALLED CONMTIONS.

" CORRECTED EGT AND FUEL FLOW ARE ALSO CORRECTEDTO MlNMUM BLEED PRESSURE.

%PACK STD. ECS MODE "

DESCRIPTION

BLEED PRESSURE. PSlA

BLEED AIRFLOW. LBllllN

EXHAUST GAS TEMPERATURE. OFm

FUEL FLOW. LBMHR " I

CELL PRESSURE. PCELL =

APU INLET TEMPERATURE. T2 =

MES MODE "

14.64 prla

91.0 'F

AUTOMATIC STARTS CHECK : X I = 36 SEC; m = 36 SEC; #3= 3 6 SEC:

TOTAL NUMBER OF STARTS (MIRING ATP): 8

TOTAL OPERATING TIME (WRING ATP): 2 HRS 1 5 MlNS -

UNIT STATUS :

REQUIRED

49.6 WIN)

145.0 C N )

1180.0

CAW

195.0 w

ACCEPT REJECT

REWIRED

55.0

WIN,

NR

1205.0

NR

I WE CERTIFYTHE ABOVE DATA ARETRUE AND CORRECT, AND THE UNIT HAS SUCCESSFULLY MET ALL OTHERS TESTS REWIREMEWS

SPEUFIED IN THE LATEST REVlSlON OF THE APPUCABLE TEST SPECIFICATION INDICATED ABOVE.

MEASURED

49.5

148.8

1035.0

276.0

MEASURED

56.0

156.6

1055.0

290.0

CORRECTED

50.1

149.1

1114.1

286.4

FORM I J I S D - 7 - 0 5 REV 0 (DDMMW 201296)

CORRECTED

55.1

153.2

1119.9

348.6

TECHNICIAN

QUALITY ASSURANCE

STAMP DATE

@ $ 6 NOV 191

GTCP131=9[D] PERFORMANCE DATA SHEET

WIO NO : 61 1341 ENGINE PIN 3860582-1 DATE

MODEL : GTCP 131-9[D] ENGINE SIN P I 066 CUSTOMER CASC 1 MANUAL : CMM 49-26-77 REVISION NO : 3 ENGINE STATUS : WRC

I I I I

QUANTITY

BAROMETRIC PRESSURE

FUEL INLET PRESSURE

GEARBOX PRESSURE 1 "Hz0 1 16.00 1 10.00 1 10.a I

OIL PUMP DISCHARGE PRESSURE

EGT TOTAL TEMPERATURE (LAB)

PSlA

PSlG

BLEED AIRFLOW

OIL TEMPERATURE OF 1 89 191 1 IS0 I PSlG 68.0 I 68.0 I

BLEED AIR TOTAL PRESSURE

1 4.64

29.0

68.0

BLEED AIR TOTAL TEMPERATURE

FUEL CONSUMPTION

14.64

28.0

I

SPECIFICATION MIN. BLEED AIRFLOW LBSlMlN

14.64

27.0

REQUIREMENTS 1 MIN. BLEED PRESSURE I PSlA 1 49.6 rnin - 50.1 1 55.0 rnin - 55.5 1

I MAX EGT I O F 1 1180 1 1205 1

(CORRECTED)

I I 1 I I

DATA CORRECTED TO INDICATED T2 AND INSTALLED SEA LEVEL CONDITIONS. - L-

,IJ,~

TEST TECHNICIAN : b QUALITY ASSURRANCE :

MAX FUEL FLOW

DATE

PPH 295

25-Nov-97 DATE 2 6 HOV 1997 FORM 13143D-T-04 REV 0 (DDMMYY 201296)