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(d) Stop the engine (Ref. AMM TASK 71-00-00-710-028).
(e) If you find an oil leakage from the IDG drain, change the IDG (4000XU) (Ref. AMM TASK 24-21-51-000-040) (Ref. AMM TASK 24-21-51-400-040).
5. Close-up
________
A. Put the aircraft back to its initial configuration.
(1) Do the EIS stop procedure (Ref. AMM TASK 31-60-00-860-002).
(2) De-energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-862-002).
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CES TASK 24-21-00-810-818
Loss of the IDG1 Temperature Indication
1. Possible Causes
_______________
- EGIU-1 (22XU1)
- GCU-1 (1XU1)
- IDG (4000XU)
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 24-21-51-000-040 Removal of the Integrated Drive Generator -IDG 1(2),(4000XU) AMM 24-21-51-400-040 Installation of the Integrated Drive Generator -IDG
1(2),(4000XU) AMM 24-22-33-000-001 Removal of the EGIU-1(2) (22XU1, 22XU2) AMM 24-22-33-400-002 Installation of the EGIU-1(2) (22XU1, 22XU2) AMM 24-22-34-000-001 Removal of the GCU-1(2) (1XU1, 1XU2) AMM 24-22-34-400-001 Installation of the GCU-1(2) (1XU1, 1XU2) AMM 24-41-00-861-002 Energize the Aircraft Electrical Circuits from Engine
1(2) AMM 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied
from the Engine 1(2) AMM 31-60-00-860-001 EIS Start Procedure AMM 31-60-00-860-002 EIS Stop Procedure ASM 24-21/01 ASM 24-22/02 ASM 31-54/03
3. Fault Confirmation
__________________
A. Job Set-up
(1) Aircraft Maintenance Configuration
(a) Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
(b) Do the EIS start procedure (lower ECAM DU only) (Ref. AMM TASK 31-60-00-860-001).
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CES B. Test
-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1. On the ECAM control panel: If on the lower ECAM DU:
- push the ELEC key to get the - amber crosses replace the oil
ELEC page. temperature indication of the IDG1, do the trouble shooting given in Para. 4.A.
4. Fault Isolation
_______________
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 301-399,
A. If the test confirms the fault:
- replace the EGIU-1 (22XU1) (Ref. AMM TASK 24-22-33-000-001) and (Ref. AMM TASK 24-22-33-400-002).
(1) If the fault continues:
- replace the GCU-1 (1XU1) (Ref. AMM TASK 24-22-34-000-001) and (Ref. AMM TASK 24-22-34-400-001).
(2) If the fault continues:
- do a check and repair the wiring between (Ref. ASM 24-21/01): . the pin AB/7 of the IDG1 (4000XU) and the pin AA/8A of the GCU1 (1XU1) . the pin AB/8 of the IDG1 (4000XU) and the pin AA/9B of the GCU1 (1XU1) . the pin AB/9 of the IDG1 (4000XU) and the pin AA/9A of the GCU1 (1XU1)
- do a check and repair the wiring between (Ref. ASM 24-22/02): . the pin AB/9A of the GCU1 (1XU1) and the pin AA/4C of the EGIU1 (22XU1) . the pin AB/9B of the GCU1 (1XU1) and the pin AA/4D of the EGIU1 (22XU1) . the pin AB/9C of the GCU1 (1XU1) and the pin AA/5A of the EGIU1 (22XU1). Then make sure that the ground wire is correctly connected to the pin AA/5C of the EGIU1 (22XU1).
- do a check and repair the wiring between (Ref. ASM 31-54/03): . the pin AA/1A of the EGIU1 (22XU1) and the pin AB/10G of the SADC1 (1WV1) . the pin AA/1B of the EGIU1 (22XU1) and the pin AB/10H of the SADC1 (1WV1) . the pin AA/1C of the EGIU1 (22XU1) and the pin AB/10G of the SADC2 (1WV2) . the pin AA/1D of the EGIU1 (22XU1) and the pin AB/10H of the SADC2 (1WV2)
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本文鏈接地址：A320 Trouble Shooting Manual 排故手冊(cè) 電源 2(111)
