3. Fault Confirmation
__________________
A. Test After the subsequent flight, make sure that the fault does not continue.
4. Fault Isolation
_______________
A. If the failure is confirmed on the PFD 1:
- do a check of the operational test of the AFS (Ref. AMM TASK 22-96-00-710-001).
(1) If the test gives a maintenance message:
- refer to the procedure related to this message.
(2) If the test gives no maintenance message:
- replace the ADIRU-1 (1FP1) (Ref. AMM TASK 34-12-34-000-001) and (Ref. AMM TASK 34-12-34-400-001).
(a) If the fault continues:
- replace the FAC-1 (1CC1) (Ref. AMM TASK 22-66-34-000-002) and (Ref. AMM TASK 22-66-34-400-002).
「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 ∞∞22-66-00∞∞∞∞∞∞∞∞∞∞Page 290
May 01/04R CES
(b) If the fault continues:
- replace the SFCC-1 (21CV) (Ref. AMM TASK 27-51-34-000-001) and (Ref. AMM TASK 27-51-34-400-001).
B. If the failure is confirmed on the PFD 2:
- do a check of the operational test of the AFS (Ref. AMM TASK 22-96-00-710-001).
(1) If the test gives a maintenance message:
- refer to the procedure related to this message.
(2) If the test gives no maintenance message:
- replace the ADIRU-2 (1FP2) (Ref. AMM TASK 34-12-34-000-001) and (Ref. AMM TASK 34-12-34-400-001).
(a) If the fault continues:
- replace the FAC-2 (1CC2) (Ref. AMM TASK 22-66-34-000-002) and (Ref. AMM TASK 22-66-34-400-002).
(b) If the fault continues:
- replace the SFCC-2 (22CV) (Ref. AMM TASK 27-51-34-000-001) and (Ref. AMM TASK 27-51-34-400-001).
「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 ∞∞22-66-00∞∞∞∞∞∞∞∞∞∞Page 291
May 01/04R
CES R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
TASK 22-66-00-810-866
Loss of the ELAC Functions by the FAC 1
1. Possible Causes
_______________
- wiring of the ELAC OWN bus from the FAC 1 (1CC1) to the ELAC 1 (2CE1)
- wiring of the ELAC OPP bus from the FAC 1 (1CC1) to the ELAC 2 (2CE2)
- wiring of the ELAC OWN HLTY MON discrete from the FAC 1 (1CC1) to the ELAC 1 (2CE1)
- wiring of the ELAC OWN HLTY COM discrete from the FAC 1 (1CC1) to the ELAC 2 (2CE2)
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 22-91-00-710-001 Ground Scanning of the AFS
AMM 22-96-00-710-001 Operational Test of the AFS
ASM 22-68/01
ASM 22-69/01
3. Fault Confirmation
__________________
A. Test
(1) Do the Ground Scanning of the AFS (Ref. AMM TASK 22-91-00-710-001).
4. Fault Isolation
_______________
A. If the test gives the maintenance message AFS: CHK FAC1-ELAC 1/2 WRG:
- do a check of the wiring of the ELAC OWN bus from the FAC 1 (1CC1) to the ELAC 1 (2CE1)
- do a check of the wiring of the ELAC OPP bus from the FAC 1 (1CC1) to the ELAC 2 (2CE2) (Ref. ASM 22-69/01).
(1) If there is no continuity:
- repair the above wiring.
(2) If there is continuity:
- do a check of the wiring of the ELAC OWN HLTY MON discrete from the FAC 1 (1CC1) to the ELAC 1 (2CE1)
- do a check of the wiring of the ELAC OWN HLTY COM discrete from the FAC 1 (1CC1) to the ELAC 2 (2CE2)
「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, 101-149, 151-199, ∞∞22-66-00∞∞∞∞∞∞∞∞∞∞Page 292
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本文鏈接地址：A320 Trouble Shooting Manual 排故手冊 AUTO FLIGHT 自動飛行2(30)
