Loss of the Accelerometer 3 Signal for the SEC 2
1. Possible Causes
_______________
- SEC-2 (1CE2)
- ACCLRM-3 (12CE3)
- wiring of the ANI 4-1 signal from the SEC 2 (1CE2) to the accelerometer 3 (12CE3)
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)
AMM 27-94-34-000-001 Removal of the SEC (1CE1,1CE2,1CE3)
AMM 27-94-34-400-001 Installation of the SEC (1CE1,1CE2,1CE3)
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:
SEC2 OR WIRING FROM ACCLRM3 12CE3
- replace the SEC-2 (1CE2), (Ref. AMM TASK 27-94-34-000-001) and (Ref. AMM TASK 27-94-34-400-001).
(1) If the fault continues:
- replace the ACCLRM-3 (12CE3), (Ref. AMM TASK 27-92-16-000-001) and (Ref. AMM TASK 27-92-16-400-001).
(2) If the fault continues:
- do a check and repair the wiring of the ANI 4-1 signal from the SEC 2 (1CE2) to the accelerometer 3 (12CE3) SEC 2 COM part and MON part (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 ∞∞27-94-00∞∞∞∞∞∞∞∞∞∞Page 247
Feb 01/03R CES
Loss of the Accelerometer 4 Signal for the SEC 2
1. Possible Causes
_______________
- SEC-2 (1CE2)
- ACCLRM-4 (12CE4) R - wiring of the ANI 4-2 signal from the SEC 2 (1CE2) to the accelerometer 4 R (12CE4)
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)
AMM 27-94-34-000-001 Removal of the SEC (1CE1,1CE2,1CE3)
AMM 27-94-34-400-001 Installation of the SEC (1CE1,1CE2,1CE3)
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:
SEC2 OR WIRING FROM ACCLRM4 12CE4
- replace the SEC-2 (1CE2), (Ref. AMM TASK 27-94-34-000-001) and (Ref. AMM TASK 27-94-34-400-001).
(1) If the fault continues:
- replace the ACCLRM-4 (12CE4), (Ref. AMM TASK 27-92-16-000-001) and (Ref. AMM TASK 27-92-16-400-001).
(2) If the fault continues:
- do a check and repair the wiring of the ANI 4-2 signal from the SEC 2 (1CE2) to the accelerometer 4 (12CE4) SEC 2 COM part and MON part (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 ∞∞27-94-00∞∞∞∞∞∞∞∞∞∞Page 248
Feb 01/04 CES Loss of the Blue Hydraulic Pressure Switch Signal for the SEC 1
1. Possible Causes
_______________
- SEC-1 (1CE1)
- wiring of the LOW BLUE PRESS signal from the SEC 1 (1CE1) COM and MON parts to the first terminal block
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION
-------------------------------------------------------------------------------
AMM 27-94-34-000-001 Removal of the SEC (1CE1,1CE2,1CE3)
AMM 27-94-34-400-001 Installation of the SEC (1CE1,1CE2,1CE3)
AMM 27-96-00-740-001 BITE Test of the EFCS (Ground Scanning)
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本文鏈接地址：A320 Trouble Shooting Manual 排故手冊 飛行操縱 3(101)
