- The messages show during aircraft electrical power up at the power up test or the CFDIU test.
- The FDU gives the messages during each flight until the aircraft
operation is fully stopped. Airbus supplies a new FDU that corrects R this fault. For more information refer TFU 26.13.00.001.
(1) To prevent the FDU to give messages on power up:
(a) When the Electric Ground Supply energizes the aircraft:
- Do not operate switches in this order: MAINT BUS -> "ON", BAT 1+2 -> "ON" and EXT PWR -> "ON"
- Operate switches in this order: MAINT BUS -> "ON", EXT PWR -> "ON" and BAT 1+2 -> "ON".
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞26-13-00∞∞∞∞∞∞∞∞∞∞Page 201
May 01/05 CES (b) When the APU energizes the aircraft:
- Do the 'Operational Test of the APU Fire and Overheat Detection with the CFDS' after the APU starts (Ref. AMM TASK 26-13-15-710-051).
- If FWC and FDU are connected and all other systems operate satisfactorily, the unwanted message(s) clear(s). No maintenance work is necessary.
- If FWC and FDU are not connected or another system has a failure, the message stays. Maintenance work is necessary.
B. Do the operational test of the APU fire and overheat detection system (Ref. AMM TASK 26-13-00-710-001).
4. Fault Isolation
_______________
R
R A. If the test gives a different maintenance message:
R - Do the trouble shooting procedure related to the maintenance message.
B. If the test gives the maintenance message:
CHECK APU FIRE LOOP A,
and/or
CHECK FDU APU LOOP A WARN CKT
- replace the DETECTOR-APU FIRE (LOOP A) (21WG) (Ref. AMM TASK 26-13-15-000-001) and (Ref. AMM TASK 26-13-15-400-001).
(1) If the fault continues:
- replace the FDU-APU (13WG) (Ref. AMM TASK 26-13-34-000-001) and (Ref. AMM TASK 26-13-34-400-001).
(2) If the fault continues:
- do a check and repair the wiring between the: FDU (13WG) connector A/K and DETECTOR (21WG) connector A/A, FDU (13WG) connector A/J and DETECTOR (21WG) connector A/E (Ref. ASM 26-13/01).
C. If the test gives the maintenance message:
CHECK APU FIRE LOOP B
and/or
CHECK FDU APU LOOP B WARN CKT
- replace the DETECTOR-APU FIRE (LOOP B) (22WG) (Ref. AMM TASK 26-13-15-000-001) and (Ref. AMM TASK 26-13-15-400-001).
(1) If the fault continues:
- replace the FDU-APU (13WG) (Ref. AMM TASK 26-13-34-000-001) and (Ref. AMM TASK 26-13-34-400-001).
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞26-13-00∞∞∞∞∞∞∞∞∞∞Page 202
May 01/05 CES (2) If the fault continues:
- do a check and repair the wiring between the: FDU (13WG) connector B/K and DETECTOR (22WG) connector A/A, FDU (13WG) connector B/J and DETECTOR (22WG) connector A/E (Ref. ASM 26-13/01).
D. If the test gives the maintenance message FDU APU:
- replace the FDU-APU (13WG) (Ref. AMM TASK 26-13-34-000-001) and (Ref. AMM TASK 26-13-34-400-001).
(1) If the fault continues:
- do a check and repair the wiring between the: FDU (13WG) connector A/A and C/B (1WG), FDU (13WG) connector B/A and C/B (2WG), FDU (13WG) connector A/B and GND, FDU (13WG) connector B/N and GND, FDU (13WG) connector B/B and GND (Ref. ASM 26-13/01).
E. Do the test as given in the Para. 3.A.
5. Close-up
________
A. Put the aircraft back to its initial configuration.
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞26-13-00∞∞∞∞∞∞∞∞∞∞Page 203
May 01/05R
CES APU Loop A and/or Loop B Fire Warning Signal Output
1. Possible Causes
_______________
- FDU-APU (13WG)
- wiring
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
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本文鏈接地址：A320 Trouble Shooting Manual 排故手冊 FIRE PROTECTION 防火(65)
