(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 34-13-00-740-002 INTERFACE TEST of the ADR
3. Fault Confirmation
__________________
A. Test
Not applicable, you cannot confirm this fault on the ground.
4. Fault Isolation
_______________
A. If the fault only occurs during the flight:
- do the Interface test of the ADR (system 1) (Ref. AMM TASK 34-13-00-740-002).
(1) If the test gives a maintenance message: R - do the trouble shooting procedure related to the maintenancee R message. R
(2) If the test is OK:
- no maintenance action is necessary.
B. If the fault continues on the ground:
- replace the ADM-L TOTAL PRESSURE (19FP1) (Ref. AMM TASK 34-11-17-000-001) and (Ref. AMM TASK 34-11-17-400-001)
- do the ADIRS start procedure (Ref. AMM TASK 34-10-00-860-002).
(1) If the fault continues:
- replace the ADM-R STATIC PRESSURE (19FP4) (Ref. AMM TASK 34-11-17-000-001) and (Ref. AMM TASK 34-11-17-400-001)
- do the ADIRS start procedure.
(a) If the fault continues:
- replace the ADM-L STATIC PRESSURE (19FP5).
5. Close-up
________
A. Do the ADIRS stop procedure (Ref. AMM TASK 34-10-00-860-005).
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞34-13-00∞∞∞∞∞∞∞∞∞∞Page A276
Feb 01/05R
CES Loss of the ADM Data to the ADR2
1. Possible Causes
_______________
- ADM-R TOTAL PRESSURE (19FP2)
- ADM-R STATIC PRESSURE (19FP4)
- ADM-R STATIC PRESSURE (19FP6)
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 34-10-00-860-002 ADIRS Start Procedure
AMM 34-10-00-860-005 ADIRS Stop Procedure
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 34-13-00-740-002 INTERFACE TEST of the ADR
3. Fault Confirmation
__________________
A. Test
Not applicable, you cannot confirm this fault on the ground.
4. Fault Isolation
_______________
A. If the fault only occurs during the flight:
- do the Interface test of the ADR (system 2) (Ref. AMM TASK 34-13-00-740-002).
(1) If the test gives a maintenance message: R - do the trouble shooting procedure related to the maintenance R message. R
(2) If the test is OK:
- no maintenance action is necessary.
B. If the fault continues on the ground:
- replace the ADM-R TOTAL PRESSURE (19FP2) (Ref. AMM TASK 34-11-17-000-001) and (Ref. AMM TASK 34-11-17-400-001)
- do the ADIRS start procedure (Ref. AMM TASK 34-10-00-860-002).
(1) If the fault continues:
- replace the ADM-R STATIC PRESSURE (19FP4) (Ref. AMM TASK 34-11-17-000-001) and (Ref. AMM TASK 34-11-17-400-001)
- do the ADIRS start procedure.
(a) If the fault continues:
- replace the ADM-R STATIC PRESSURE (19FP6).
5. Close-up
________
A. Do the ADIRS stop procedure (Ref. AMM TASK 34-10-00-860-005).
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞34-13-00∞∞∞∞∞∞∞∞∞∞Page A278
Feb 01/05R
CES Loss of the ADM Data to the ADR3
1. Possible Causes
_______________
- ADM-STBY TOTAL PRESSURE (19FP3)
- ADM-STBY STATIC PRESSURE (19FP8)
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 34-10-00-860-002
AMM 34-10-00-860-005
AMM 34-11-17-000-001
AMM 34-11-17-400-001
AMM 34-13-00-740-002
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本文鏈接地址：A320 Trouble Shooting Manual 排故手冊 導航 NAVIGATION 1(107)
