3. Fault Confirmation
__________________
A. Test
ADIRS Start ProcedureADIRS Stop ProcedureRemoval of the Air Data Module (19FP1,19FP2,19FP3,19FP4,19FP5,19FP6, 19FP7,19FP8)Installation of the Air Data Module (19FP1,19FP2,19FP3,19FP4,19FP5,19FP6, 19FP7,19FP8)INTERFACE TEST of the ADR
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 3) (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-STBY TOTAL PRESSURE (19FP3) (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-STBY STATIC PRESSURE (19FP8) (Ref. AMM TASK 34-11-17-000-001) and (Ref. AMM TASK 34-11-17-400-001)
「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 ∞∞34-13-00∞∞∞∞∞∞∞∞∞∞Page A279
May 01/05 CES
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 A280
Feb 01/05R
CES Loss of the FCU Inputs on the ADIRU1
1. Possible Causes
_______________
- FCU (2CA)
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 22-81-12-000-001 Removal of the FCU (2CA) AMM 22-81-12-400-001 Installation of the FCU (2CA) AMM 34-13-00-740-002 INTERFACE TEST of the ADR
3. Fault Confirmation
__________________
A. Test Do the Interface test of the ADR (system 1) (Ref. AMM TASK 34-13-00-740-002).
4. Fault Isolation
_______________
A. If the BITE test gives the maintenance message FCU (3CA):
- replace the FCU (2CA) (Ref. AMM TASK 22-81-12-000-001) and (Ref. AMM TASK 22-81-12-400-001).
B. Do the test given in Para. 3.
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞34-13-00∞∞∞∞∞∞∞∞∞∞Page A281
Feb 01/05R
CES Loss of the FCU Inputs on the ADIRU2
1. Possible Causes
_______________
- FCU (2CA)
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 22-81-12-000-001 Removal of the FCU (2CA) AMM 22-81-12-400-001 Installation of the FCU (2CA) AMM 34-13-00-740-002 INTERFACE TEST of the ADR
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 BITE test gives the maintenance message FCU (3CA):
- replace the FCU (2CA) (Ref. AMM TASK 22-81-12-000-001) and (Ref. AMM TASK 22-81-12-400-001).
B. Do the test given in Para. 3.
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞34-13-00∞∞∞∞∞∞∞∞∞∞Page A282
Feb 01/05R
CES TASK 34-13-00-810-943 Loss of the FCU Inputs on the ADIRU3
1. Possible Causes
_______________
- FCU (2CA)
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 22-81-12-000-001 Removal of the FCU (2CA) AMM 22-81-12-400-001 Installation of the FCU (2CA) AMM 34-13-00-740-002 INTERFACE TEST of the ADR
3. Fault Confirmation
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 導航 NAVIGATION 1(108)
