W DOC AIRBUS | TSM A320F

Loss of the IDG2 Temperature Indication

TASK 24-21-00-810-819-A
Loss of the IDG2 Temperature Indication

1. Possible Causes
2. Job Set-up Information
 A. Referenced Information
REFERENCE
DESIGNATION
ASM 242101
AMM 24-21-51-000-040
Removal of the Integrated Drive Generator - IDG 1(2)
AMM 24-21-51-400-040
Installation of the Integrated Drive Generator - IDG 1(2)
ASM 242203
AMM 24-22-33-000-001
Removal of the EGIU-1(2)
AMM 24-22-33-400-002
Installation of the EGIU-1(2)
AMM 24-22-34-000-001
Removal of the GCU-1(2)
AMM 24-22-34-400-001
Installation of the GCU-1(2)
AMM 24-41-00-861-002
Energize the Aircraft Electrical Circuits from the External Power
AMM 24-41-00-862-002
De-energize the Aircraft Electrical Circuits Supplied from the External Power
ASM 315403
AMM 31-60-00-860-001
EIS Start Procedure
AMM 31-60-00-860-002
EIS Stop Procedure
3. Fault Confirmation
Subtask 24-21-00-860-058-A
A. Job Set-up
   (1) Aircraft Maintenance Configuration
     (a) Energize the aircraft electrical circuits
AMM 24-41-00-861-002.
     (b) Do the EIS start procedure (lower ECAM DU only) AMM 31-60-00-860-001.
Subtask 24-21-00-710-079-A
B. Test
ACTION
RESULT
1.On the ECAM control panel:
  • push the ELEC key to get the ELEC page.
If on the lower ECAM DU:
  • amber crosses replace the oil temperature indication of the IDG2,
    do the trouble shooting given in Para. 4.A.
4. Fault Isolation
Subtask 24-21-00-810-074-B ** ON A/C NOT FOR ALL
A. If the test confirms the fault:
   (1) If the fault continues:
   (2) If the fault continues:
  • do a check and repair the wiring between ASM 242101:
    . the pin AB/7 of the IDG2 (4000XU) and the pin AA/8A of the GCU2 (1XU2)
    . the pin AB/8 of the IDG2 (4000XU) and the pin AA/9B of the GCU2 (1XU2)
    . the pin AB/9 of the IDG2 (4000XU) and the pin AA/9A of the GCU2 (1XU2)
  • do a check and repair the wiring between ASM 242203:
    . the pin AB/9A of the GCU2 (1XU2) and the pin AA/4C of the EGIU2 (22XU2)
    . the pin AB/9B of the GCU2 (1XU2) and the pin AA/4D of the EGIU2 (22XU2)
    . the pin AB/9C of the GCU2 (1XU2) and the pin AA/5A of the EGIU2 (22XU2). Then make sure that the ground wire is correctly connected to the pin AA/5C of the EGIU2 (22XU2).
  • do a check and repair the wiring between ASM 315403:
    . the pin AA/1A of the EGIU2 (22XU2) and the pin AE/10C of the SADC1 (1WV1)
    . the pin AA/1B of the EGIU2 (22XU2) and the pin AE/10D of the SADC1 (1WV1)
    . the pin AA/1C of the EGIU2 (22XU2) and the pin AE/10C of the SADC2 (1WV2)
    . the pin AA/1D of the EGIU2 (22XU2) and the pin AE/10D of the SADC2 (1WV2)
   (3) If the fault continues:
Subtask 24-21-00-810-074-D ** ON A/C NOT FOR ALL
A. If the test confirms the fault:
   (1) If the fault continues:
  • do a check and repair the wiring between ASM 242101:
    . the pin AB/7 of the IDG2 (4000XU) and the pin AA/9C of the GCU2 (1XU2)
    . the pin AB/8 of the IDG2 (4000XU) and the pin AA/9D of the GCU2 (1XU2)
    . the pin AB/9 of the IDG2 (4000XU) and the pin AA/10C of the GCU2 (1XU2)
  • do a check and repair the wiring between ASM 315403:
    . the pin AA/8F of the GCU2 (1XU2) and the pin AE/10C of the SADC1 (1WV1)
    . the pin AA/7F of the GCU2 (1XU2) and the pin AE/10D of the SADC1 (1WV1)
    . the pin AA/8J of the GCU2 (1XU2) and the pin AE/10C of the SADC2 (1WV2)
    . the pin AA/8H of the GCU2 (1XU2) and the pin AE/10D of the SADC2 (1WV2)
   (2) If the fault continues:
Subtask 24-21-00-710-080-A
B. Do this test to make sure that the system operates correctly:
ACTION
RESULT
1.On the ECAM control panel:
  • push the ELEC key to get the ELEC page.
On the lower ECAM DU:
  • the oil temperature indication of the IDG2 comes into view.
5. Close-up
Subtask 24-21-00-860-059-A
A. Put the aircraft back to its initial configuration.
   (1) Do the EIS stop procedure AMM 31-60-00-860-002.
   (2) De-energize the aircraft electrical circuits
AMM 24-41-00-862-002.
[Rev.8 from Aug 2018] 2026.04.04 04:39:30 UTC
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