R **ON A/C 001-049, 051-099, 101-105, 151-199, 201-299,
5. Close-up
________
A. Put the aircraft back to its initial configuration.
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1R EFF : 001-049, 051-099, 101-105, 151-199, ∞∞26-17-00∞∞∞∞∞∞∞∞∞∞Page 216
201-299, May 01/05 CES
Smoke Detector(s) Wiring Fault
1. Possible Causes
_______________ R - wiring
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 31-32-00-860-005
ASM 26-16/01 ASM 26-17/01 ASM 26-17/01 ASM 26-17/01
3. Fault Confirmation
__________________
A. TestProcedure to Get Access to the SYSTEM REPORT/TEST FIRE PROT Page
(1) On one MCDU get the SYSTEM REPORT/TEST SDCU menu page (Ref. AMM TASK 31-32-00-860-005).
(2) On the MCDU:
- push the line key adjacent to the <WIRING REPORT indication.
4. Fault Isolation
_______________
A. If the SDCU WIRING REPORT page gives the maintenance message NO FAILURE, no other maintenance action is necessary.
B. If the test gives the maintenance message TEST OK, no other maintenance action is necessary.
R C. If the SDCU WIRING REPORT page gives the maintenance message(s):
WIRING DEFECT BETWEEN SDCU (10WQ) AND SMOKE DET LAV X (XWQ), and/or
WIRING DEFECT BETWEEN SMOKE DET LAV X (XWQ) AND SMOKE DET LAV X (XWQ),
and/or
WIRING DEFECT BETWEEN SMOKE DET LAV X (XWQ) AND SDCU (10WQ) (X =
RESP.LAV)
WIRING DEFECT BETWEEN SMOKE DETECTOR (XWH) FWD (OR AFT) LDCC AND
SMOKE DETECTOR (XWH) FWD (OR AFT) LDCC.
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1R EFF : 001-049, 051-099, 101-105, 151-199, ∞∞26-17-00∞∞∞∞∞∞∞∞∞∞Page 217
201-299, May 01/05 CES 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1R EFF : 001-049, 051-099, 101-105, 151-199, ∞∞26-17-00∞∞∞∞∞∞∞∞∞∞Page 218
R R R R - Check and repair if necessary the wiring between the SDCU and the related smoke detector or - Check and repair if necessary the wiring between the related smoke detectors which is shown in the SDCU WIRING REPORT (Ref. ASM 26-17/01) , (Ref. ASM 26-17/01), (Ref. ASM 26-17/01) and (Ref. ASM 26-16/01).
D. Do the test given in para. 3.
5. Close-up________
A. Put the aircraft back to its initial configuration.
201-299, May 01/05 CES
Pin Programming Configuration Fault
1. Possible Causes_______________
R R - SDCU (10WQ) - PIN PROGRAMMING
2. Job Set-up Information______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 26-17-34-000-001
AMM 26-17-34-400-001
AMM 31-32-00-860-005
ASM 26-17/01
3. Fault Confirmation
__________________
A. Test
Removal of the Smoke-Detection Control Unit (SDCU)
(10WQ)
Installation of the Smoke-Detection Control Unit
(SDCU) (10WQ)
Procedure to Get Access to the SYSTEM REPORT/TEST
FIRE PROT Page
R (1) - Open the circuit breakers 11WQ and 12WQ R - Wait 20 seconds R - Close the circuit breakers and wait again 1 minute before start of R the next test.
R (2) Get access to the MCDU/SDCU menu page (Ref. AMM TASK 31-32-00-860-
005): R - Push the line key adjacent to the <ON GROUND FAULTS indication. R The MCDU shows the fault message. If there is no fault, the MCDU R shows NO FAILURE. R
4. Fault Isolation
_______________
R A. If the test gives a different maintenance message:
R - Do the trouble shooting procedure related to the maintenance message.
R
B. If the test gives the maintenance message TEST OK, no other maintenance action is necessary.
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1R EFF : 001-049, 051-099, 101-105, 151-199, ∞∞26-17-00∞∞∞∞∞∞∞∞∞∞Page 219
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：A320 Trouble Shooting Manual 排故手册 FIRE PROTECTION 防火(88)
