R (b) If the DRIVE ASSY-TACHOMETER is not damaged and there is no
R report of brake temperature differences:
R - replace the SEC-3 (1CE3) (Ref. AMM TASK 27-94-34-000-001) and
R (Ref. AMM TASK 27-94-34-400-001).
「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 ∞∞27-94-00∞∞∞∞∞∞∞∞∞∞Page 243
Feb 01/03 CES
R (c) If the DRIVE ASSY-TACHOMETER is not damaged and there is a report
R of brake temperature differences:
R - replace the TACHOMETER-WHEEL (Ref. AMM TASK 32-42-57-000-001)
R and (Ref. AMM TASK 32-42-57-400-001).
Loss of the Accelerometer 1 Signal for the SEC 1
1. Possible Causes
_______________
- SEC-1 (1CE1)
- ACCLRM-1 (12CE1)
- wiring of the ANI 4-1 signal from the SEC 1 (1CE1) to the accelerometer 1 (12CE1)
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:
SEC1 OR WIRING FROM ACCLRM1 12CE1
- replace the SEC-1 (1CE1), (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-1 (12CE1), (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 1 (1CE1) to the accelerometer 1 (12CE1) SEC 1 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 245
Feb 01/03R CES
Loss of the Accelerometer 2 Signal for the SEC 1
1. Possible Causes
_______________
- SEC-1 (1CE1)
- ACCLRM-2 (12CE2)
- wiring of the ANI 4-1 signal from the SEC 1 (1CE1) to the accelerometer 2 (12CE2)
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:
SEC1 OR WIRING FROM ACCLRM2 12CE2
- replace the SEC-1 (1CE1), (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-2 (12CE2), (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 1 (1CE1) to the accelerometer 2 (12CE2) SEC 1 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 246
Feb 01/03R CES
