- replace the ACCLRM-3 (12CE3), (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 3 (12CE3) 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 203
Aug 01/99 CES Failure of the Accelerometer 4
1. Possible Causes
_______________
- ACCLRM-4 (12CE4)
- wiring of the power supply signal from the accelerometer 4 (12CE4) 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
_______________
A. If the BITE test gives the maintenance message:
ACCLRM 4 12CE4
- replace the ACCLRM-4 (12CE4), (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 4 (12CE4) 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 204
Aug 01/99 CES Failure of the Accelerometers 3 and 4
1. Possible Causes
_______________
- ACCLRM-3 (12CE3)
- ACCLRM-4 (12CE4)
- wiring of the power supply signal from the accelerometer (12CE3) to the first terminal block
- wiring of the power supply signal from the accelerometer (12CE4) 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
_______________
A. If the BITE test gives the maintenance messages:
ACCLRM 3 12CE3
ACCLRM 4 12CE4
- replace the ACCLRM-3 (12CE3) and the ACCLRM-4 (12CE4), (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 (12CE3) to the first terminal block and the wiring of the power supply signal from the accelerometer (12CE4) 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 205
Aug 01/99 CES Failure of the Accelerometers 1 and 2
1. Possible Causes
_______________
- ACCLRM-1 (12CE1)
- ACCLRM-2 (12CE2)
- wiring of the power supply signal from the accelerometer 1 (12CE1) to the first terminal block
- wiring of the power supply signal from the accelerometer 2 (12CE2) to the first terminal block 中國(guó)航空網(wǎng) m.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：A320 Trouble Shooting Manual 排故手冊(cè) 飛行操縱 2(110)
