- swap back the CPC 1 (11HL) and the CPC 2 (12HL) (Ref. AMM TASK 21-31-34-000-001) and (Ref. AMM TASK 21-31-34-400-001).
- replace the CONTROLLER-CABIN PRESSURE 2 (12HL) (Ref. AMM TASK 21-31-34-000-001) and (Ref. AMM TASK 21-31-34-400-001).
(2) If the fault does not move with the CPC 2:
- swap back the CPC 1 (11HL) and the CPC 2 (12HL) (Ref. AMM TASK 21-31-34-000-001) and (Ref. AMM TASK 21-31-34-400-001).
- do the INTERFACE test of the ADR system (Ref. AMM TASK 34-13-00-
740-002). R
R (a) If the test gives a different maintenance message refer to the R Fault Symptom List.
「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 ∞∞21-31-00∞∞∞∞∞∞∞∞∞∞Page 240
May 01/05 CES (b) If the fault continues:
- do a check and repair the wiring of the signal DATA BUS #2 from the ADIRS 2 (1FP2) to the CPC 2 (12HL) (Ref. ASM 21-31/03) and (Ref. ASM 21-31/03).
C. If the test with the CPC 2 (12HL) gives the maintenance message NO DATA FROM ADIRS 3 (21):
- swap the CPC 1 (11HL) and the CPC 2 (12HL) (Ref. AMM TASK 21-31-34-000-001) and (Ref. AMM TASK 21-31-34-400-001).
(1) If the fault moves with the CPC 2:
- swap back the CPC 1 (11HL) and the CPC 2 (12HL) (Ref. AMM TASK 21-31-34-000-001) and (Ref. AMM TASK 21-31-34-400-001).
- replace the CONTROLLER-CABIN PRESSURE 2 (12HL) (Ref. AMM TASK 21-31-34-000-001) and (Ref. AMM TASK 21-31-34-400-001).
(2) If the fault does not move with the CPC 2:
- swap back the CPC 1 (11HL) and the CPC 2 (12HL) (Ref. AMM TASK 21-31-34-000-001) and (Ref. AMM TASK 21-31-34-400-001).
- do the INTERFACE test of the ADR system (Ref. AMM TASK 34-13-00-
740-002). R
R (a) If the test gives a different maintenance message refer to the R Fault Symptom List.
(b) If the fault continues:
- do a check and repair the wiring of the signal DATA BUS #4 from the ADIRS 3 (1FP3) to the CPC 2 (12HL) (Ref. ASM 21-31/03) and (Ref. ASM 21-31/03).
D. Do the test as given in the Para. 3.A.
5. Close-up
________
A. Put the aircraft back to its initial configuration.
TASK 21-31-00-810-816
EIU Signal Replaced
1. Possible Causes
_______________
- wiring
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 73-25-34-710-040 Operational Test of the Engine Interface Unit
(1KS1,1KS2)
ASM 21-31/02
3. Fault Confirmation
__________________
A. Not applicable, you cannot confirm this fault on the ground.
NOTE : In the flight phases 4 and 5 the maintenance message EIU SIGNAL
____
REPLACED shows that:
- during the take-off at least one of the throttle levers was not set to take-off power >70%.
4. Fault Isolation
_______________
A. If the CPC 1 (11HL) and/or CPC 2 (12HL) CLASS 3 FAULTS gives the maintenance messsage EIU SIGNAL REPLACED (17) caused in flight phase 7 or 8, no other maintenance action is necessary.
NOTE : The fault is caused by LDG IbouncingI or by a hard landing.
____
B. If the CPC 1 (11HL) CLASS 3 FAULTS gives the maintenance messsage EIU SIGNAL REPLACED (17) caused in flight phase other than 7 or 8 and, the take off was performed with the minimum max. climb setting (throttle levers set at 70%):
- do the operational test of the engine interface unit (Ref. AMM TASK 73-
25-34-710-040). R
R (1) If the test gives a different maintenance message refer to the Fault R Symptom List.
(2) If the fault continues:
- do a check and repair the wiring between: CPC 1 (11HL) AB/7D and EIU 1 (1KS1) AB/G1, CPC 1 (11HL) AB/8D and EIU 2 (1KS2) AB/G1 (Ref. ASM 21-31/02).
「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 ∞∞21-31-00∞∞∞∞∞∞∞∞∞∞Page 242
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320 Trouble Shooting Manual 排故手冊 AIR CONDITIONING 空調1(104)
