- make sure that there is no continuity between pins AA/6G, 6H, between pins AA/6H, 6J and between pins AA/6G, 6J of the rack connector.
(1) If there is no continuity:
- install a new ADIRU1 (Ref. AMM TASK 34-12-34-400-001).
(2) If there is continuity:
- get access to the ADM-L TOTAL PRESSURE (19FP1) (Ref. AMM TASK 34-11-17-000-001) (Para. 2.B.)
- disconnect the electrical connector of the ADM1 and make sure that there is no continuity between pins A/A, C, between pins A/C, E and between pins A/A, E of the ADM1.
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1R EFF : 001-049, 101-105, 151-199, 201-210, ∞∞34-11-00∞∞∞∞∞∞∞∞∞∞Page A236
301-399, 401-499, Aug 01/05 CES
(a) If there is continuity:
- replace the ADM1 (Ref. AMM TASK 34-11-17-000-001) and (Ref. AMM TASK 34-11-17-400-001)
- install the ADIRU1.
(b) If there is no continuity:
- get access to the ADM-R STATIC PRESSURE (19FP4) and the ADM-L STATIC PRESSURE (19FP5) (Ref. AMM TASK 34-11-17-000-001) (Para. 2.B.)
- disconnect the electrical connector of the ADM4 and make sure that there is no continuity between pins A/A, C, between pins A/C, E and between pins A/A, E of the ADM4.
1_ If there is continuity:
- replace the ADM4 (Ref. AMM TASK 34-11-17-000-001) and (Ref.
AMM TASK 34-11-17-400-001)
- connect the electrical connector of the ADM1
- install the ADIRU1.
2 If there is no continuity:
_
- disconnect the electrical connector of the ADM5 and make sure that there is no continuity between pins A/A, C, between pins A/C, E and between pins A/A, E of the ADM5.
a If there is continuity:
_
- replace the ADM5
- connect the electrical connector of the ADM1 and 4
- install the ADIRU1.
b If there is no continuity:
_
- do a check and repair the aircraft wiring between ADIRU1 pins AA/6G, 6H, 6J and the related LRU (Ref. ASM 34-13/03)
- connect the electrical connector of the ADM
- install the ADIRU1.
B. Do the test given in Para. 3.
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1R EFF : 001-049, 101-105, 151-199, 201-210, ∞∞34-11-00∞∞∞∞∞∞∞∞∞∞Page A237
301-399, 401-499, Aug 01/05 CES
Failure of the ADM Power Supply of the ADIRU2
1. Possible Causes
_______________
- ADIRU-2 (1FP2)
- ADM-R TOTAL PRESSURE (19FP2)
- ADM-R STATIC PRESSURE (19FP6)
- ADM-L STATIC PRESSURE (19FP7)
- aircraft wiring
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 34-11-17-000-001 Removal of the Air Data Module (19FP1,19FP2,19FP3,19FP4,19FP5,19FP6, 19FP7,19FP8) AMM 34-11-17-400-001 Installation of the Air Data Module
(19FP1,19FP2,19FP3,19FP4,19FP5,19FP6, 19FP7,19FP8) AMM 34-12-34-000-001 Removal of the ADIRU (1FP1, 1FP2, 1FP3) AMM 34-12-34-400-001 Installation of the ADIRU (1FP1, 1FP2, 1FP3) AMM 34-13-00-740-002 INTERFACE TEST of the ADR ASM 34-13/03
3. Fault Confirmation
__________________
A. Test Do the Interface test of the ADR (system 2) (Ref. AMM TASK 34-13-00-740-002).
4. Fault Isolation
_______________
A. If the test gives the maintenance message ADM2 (19FP2)/ ADM6 (19FP6)/ ADM7 (19FP7):
- remove the ADIRU-2 (1FP2) (Ref. AMM TASK 34-12-34-000-001)
- make sure that there is no continuity between pins AA/6G, 6H, between pins AA/6H, 6J and between pins AA/6G, 6J of the rack connector.
(1) If there is no continuity:
- install a new ADIRU2 (Ref. AMM TASK 34-12-34-400-001).
(2) If there is continuity:
- get access to the ADM-R TOTAL PRESSURE (19FP2) (Ref. AMM TASK 34-11-17-000-001) (Para. 2.B.)
- disconnect the electrical connector of the ADM2 and make sure that there is no continuity between pins A/A, C, between pins A/C, E and between pins A/A, E of the ADM2.
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1R EFF : 001-049, 101-105, 151-199, 201-210, ∞∞34-11-00∞∞∞∞∞∞∞∞∞∞Page A238
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本文鏈接地址：A320 Trouble Shooting Manual 排故手冊 導航 NAVIGATION 1(50)
