3. Fault Confirmation
__________________
A. Test
(1) Open the circuit breakers 14WH, 15WH, 17WH and 18WH, wait for approx. 10 s and close again, wait for a minimum of 30 s before you start the test.
(2) Do the operational test of the cargo compartment smoke detection (Ref. AMM TASK 26-16-00-710-001).
4. Fault Isolation
_______________
A. If the test gives a different maintenance message:
- Do the trouble shooting procedure related to the maintenance message.
B. If the test gives the maintenance message SMK DET FWD LDCC (XWH) CONTAMINATION, (XWH = FIN of the related smoke detector):
- replace the FWD LDCC smoke-detector (Ref. AMM TASK 26-16-15-000-001) and (Ref. AMM TASK 26-16-15-400-001).
C. Do the test given in para. 3.
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 : 106-149, 301-399, 401-499, ∞∞26-16-00∞∞∞∞∞∞∞∞∞∞Page 214
Aug 01/05 CES CAN Bus Problem FWD LDCC Smoke-Detection
1. Possible Causes
_______________
- wiring
- FWD LDCC smoke detector
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 26-16-00-710-001 Operational Check of Cargo-Compartment
Smoke-Detection by PTT
AMM 26-16-15-000-001 Removal of the Cargo Smoke Detectors
AMM 26-16-15-400-001 Installation of the Cargo Smoke Detectors
ASM 26-16/02
3. Fault Confirmation
__________________
A. Test
(1) Open the circuit breakers 14WH, 15WH, 17WH and 18WH, wait for approx. 10 s and close again, wait for a minimum of 30 s before you start the test.
(2) Do the operational test of the cargo compartment smoke detection (Ref. AMM TASK 26-16-00-710-001).
4. Fault Isolation
_______________
A. If the test gives a different maintenance message:
- Do the trouble shooting procedure related to the maintenance message.
B. If the test gives the maintenance message WRG: CAN BUS X / SMK DET FWD LDCC (XWH), (XWH = FIN of the related smoke detector):
- do a check and repair the wiring between the CIDS DIR 1 (101RH) and the FWD LDCC smoke detector XWH (Ref. ASM 26-16/02).
(1) If the fault continues: do a check and repair the wiring between the CIDS DIR 2 (102RH) and the FWD LDCC smoke detector XWH (Ref. ASM 26-16/02)
(2) If the fault continues:
- replace the FWD LDCC smoke detector XWH (Ref. AMM TASK 26-16-15-000-001) and (Ref. AMM TASK 26-16-15-400-001).
「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 : 106-149, 301-399, 401-499, ∞∞26-16-00∞∞∞∞∞∞∞∞∞∞Page 215
Aug 01/05 CES
C. Do the test given in para. 3.
5. Close-up
________
A. Put the aircraft back to its initial configuration.
CAN Bus A or CAN Bus B Failure
1. Possible Causes
_______________
- wiring
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
AMM 26-16-00-710-001 Operational Check of Cargo-Compartment
Smoke-Detection by PTT
ASM 26-16/02
3. Fault Confirmation
__________________
A. Test
(1) Deactivation of the CIDS Directors
(a) On the circuit breaker panel 49VU, open the circuit breakers 15WH and 18WH, then open the circuit breakers 150RH and 157RH.
(b) On the circuit breaker panel 121VU, open the circuit breakers 17WH and 14WH, then open the circuit breakers 151RH and 156RH.
(2) Reactivation of the CIDS Directors
(a) After a minimum of 5 s from power-down, on circuit breaker panel 121 VU, close the circuit breakers 151RH and 156RH.
(b) On circuit breaker panel 49VU, close the circuit breakers 150RH and 157RH. 中國航空網 www.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：A320 Trouble Shooting Manual 排故手冊 FIRE PROTECTION 防火(79)
