A320 Trouble Shooting Manual 排故手册飞行操纵 2(109)_航空信息_民用航空_通用航空

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A. Get access to the PREVIOUS LEGS REPORT in the EFCS1 MENU page.
(1) In the Previous Legs Report, retrieve the maintenance message linked to one of the following items:
- SFCC

- Radio Altimeter

- Pedal Position from ELACs

R (2) Associate to this message the F/CTL maintenance status (refer to a R maintenance message to found the associated trouble shooting R procedure) and repair.
(3) In the Post Flight Report, retrieve the maintenance message linked to the warning ALTN LAW.

(4) Associate to this warning the maintenance message. Do the trouble shooting procedure related to this maintenance message.

CONTROL INPUTS INTERFACE AND POWER SUPPLY - FAULT ISOLATION PROCEDURES
______________________________________________________________________
TASK 27-92-00-810-803
Failure of the Accelerometer 1
1. Possible Causes
_______________
- ACCLRM-1 (12CE1)

- wiring of the power supply signal from the accelerometer 1 (12CE1) to the first terminal block

2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 27-92-16-000-001 Removal of the Flight Control Accelerometer (12CE1,12CE2,12CE3,12CE4) AMM 27-92-16-400-001 Installation of the Flight Control Accelerometer (12CE1,12CE2,12CE3,12CE4) R AMM 27-96-00-740-001 BITE Test of the EFCS (Ground Scanning) ASM 27-92/24
3. Fault Confirmation
__________________
A. Test
(1) Do the BITE test of the EFCS (ground scanning) (Ref. AMM TASK 27-96-00-740-001).
4. Fault Isolation
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A. If the BITE test gives the maintenance message:
ACCLRM 1 12CE1:

- replace the ACCLRM-1 (12CE1), (Ref. AMM TASK 27-92-16-000-001) and (Ref. AMM TASK 27-92-16-400-001).
(1) If the fault continues:
- do a check and repair the wiring of the power supply signal from the accelerometer 1 (12CE1) to the first terminal block, (Ref. ASM 27-92/24).
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 ∞∞27-92-00∞∞∞∞∞∞∞∞∞∞Page 201
Aug 01/99 CES Failure of the Accelerometer 2

1. Possible Causes
_______________
- ACCLRM-2 (12CE2)

- wiring of the power supply signal from the accelerometer 2 (12CE2) to the first terminal block

- replace the ACCLRM-2 (12CE2), (Ref. AMM TASK 27-92-16-000-001) and (Ref. AMM TASK 27-92-16-400-001).
(1) If the fault continues:
- do a check and repair the wiring of the power supply signal from the accelerometer 2 (12CE2) to the first terminal block, (Ref. ASM 27-92/24).
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 ∞∞27-92-00∞∞∞∞∞∞∞∞∞∞Page 202
Aug 01/99 CES Failure of the Accelerometer 3

1. Possible Causes
_______________
- ACCLRM-3 (12CE3)

- wiring of the power supply signal from the accelerometer 3 (12CE3) to the first terminal block

2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 27-92-16-000-001 Removal of the Flight Control Accelerometer (12CE1,12CE2,12CE3,12CE4) AMM 27-92-16-400-001 Installation of the Flight Control Accelerometer (12CE1,12CE2,12CE3,12CE4) R AMM 27-96-00-740-001 BITE Test of the EFCS (Ground Scanning) ASM 27-92/24
　
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