Post on 30-Mar-2021
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)