- do a check of the wiring of K3-1 signal from the ELAC 1 (2CE1) to the first terminal block COM part and MON part (Ref. ASM 27-93/12).
(a) If there is no continuity, repair the wiring.
(b) If there is continuity:
- do a check of the wiring of the DSI-49 signal from the ELAC 1 (2CE1) to the ELAC 1 (2CE1) COM part and MON part (Ref. ASM 27-93/12).
1 If there is no continuity, repair the wiring.
_
2 If there is continuity:
_
- do a check of the wiring of the K3-1B signal from the ELAC 1 (2CE1) to the first terminal block, (Ref. ASM 27-93/12).
a If there is no continuity, repair the wiring.
_
b If there is continuity:
_
- do a check and repair the wiring of the relay (36CE2) to the ELAC 1 (2CE1) and to the THS actuator (9CE), wiring of the fault signal from the ELAC 1 (2CE1) to the first terminal block, (Ref. ASM 27-93/12).
B. Do the tests given in Para. 3.
Loss of the ADR 1 BUS 3 for the ELAC 1
1. Possible Causes
_______________
- ELAC-1 (2CE1)
- wiring of the DGI 06 signal from the ELAC 1 (2CE1) to the first terminal block
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
34-11-00-810-861 Different Angle of Attack Value on the three ADIRUs 34-11-00-810-870 Airspeed Discrepancy on the PFD or on the Standby Airspeed Indicator 34-13-00-810-998 Altitude or Airspeed Discrepancy between CAPT PFD and
F/O PFD
AMM 27-93-34-000-001 Removal of the ELAC (2CE1,2CE2)
AMM 27-93-34-400-001 Installation of the ELAC (2CE1,2CE2)
AMM 27-96-00-740-001 BITE Test of the EFCS (Ground Scanning)
ASM 27-92/50
3. Fault Confirmation
__________________
A. Test
(1) Do the BITE test of the EFCS (ground scanning) (Ref. AMM TASK 27-96-
00-740-001). R
4. Fault Isolation
_______________
A. If the BITE test gives the maintenance message:
ELAC1 COM OR BUS3 FROM ADR1
or
ELAC1 MON OR BUS3 FROM ADR1
- replace the ELAC-1 (2CE1) (Ref. AMM TASK 27-93-34-000-001) and (Ref. AMM TASK 27-93-34-400-001).
(1) If the fault continues:
- do a check and repair the wiring of the DGI 06 signal from the ELAC 1 (2CE1) to the first terminal block, COM or MON part as shown in the maintenance message (Ref. ASM 27-92/50).
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞27-93-00∞∞∞∞∞∞∞∞∞∞Page 294
Nov 01/02 CES
R (2) If the fault continues:
R - do the following trouble shooting procedures.
R (a) Airspeed Discrepancy on the PFD or on the Standby Airspeed
R Indicator (Ref. TASK 34-11-00-810-870)
R (b) Altitude or Airspeed Discrepancy between CAPT PFD and F/O PFD
R (Ref. TASK 34-13-00-810-998)
R (c) Different Angle of Attack Value on the three ADIRUs (Ref. TASK
R 34-11-00-810-861).
B. Do the test given in Para. 3.
Loss of the ADR 1 BUS 2 for the ELAC 2
1. Possible Causes
_______________
- ELAC-2 (2CE2)
- wiring of the DGI 07 signal from the ELAC 2 (2CE2) to the first terminal block
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
34-11-00-810-861 Different Angle of Attack Value on the three ADIRUs 34-11-00-810-870 Airspeed Discrepancy on the PFD or on the Standby Airspeed Indicator 34-13-00-810-998 Altitude or Airspeed Discrepancy between CAPT PFD and
F/O PFD
AMM 27-93-34-000-001 Removal of the ELAC (2CE1,2CE2)
AMM 27-93-34-400-001 Installation of the ELAC (2CE1,2CE2)
AMM 27-96-00-740-001 BITE Test of the EFCS (Ground Scanning)
ASM 27-92/52
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本文鏈接地址：A320 Trouble Shooting Manual 排故手冊 飛行操縱 3(17)
