W DOC AIRBUS | TSM A320F

Loss of Outputs 1 and 2 on Engine 2 J3 Connector

TASK 73-29-00-810-919-A
Loss of Outputs 1 and 2 on Engine 2 J3 Connector

1. Possible Causes
  • J3 connector
  • 5CA1
  • 5CA2
  • harness J3
  • ECU [4000KS]
2. Job Set-up Information
 A. Referenced Information
REFERENCE
DESIGNATION
AMM 73-21-60-000-001
Removal of the Electronic Control Unit (ECU)
AMM 73-21-60-400-001
Installation of the Electronic Control Unit (ECU)
ASM 732512
AMM 73-29-00-710-040
Operational Test of the FADEC on the ground (with Engine Motoring)
3. Fault Confirmation
Subtask 73-29-00-710-232-A ** ON A/C NOT FOR ALL
A. Do the operational test of the FADEC 2B on the ground (with engine motoring) AMM 73-29-00-710-040.
4. Fault Isolation
Subtask 73-29-00-810-215-A ** ON A/C NOT FOR ALL
A. If the test gives the maintenance message J3:
  • do a check for loose J3 connector at the ECU 2 ASM 732512.
   (1) If the fault continues:
  • make sure that the pins are not bent and that the pins and sockets have not moved into the J3 ECU 2 connector ASM 732512.
   (2) If the fault continues:
  • do a check for open circuit in the harness J3 between the pins J3/6, 31 ASM 732512.
     (a) If the fault continues:
  • replace the 5CA1
  • replace the 5CA2
  • replace the harness J3 .
     (b) If there is no fault:
Subtask 73-29-00-810-215-B ** ON A/C NOT FOR ALL
A. If the test gives the maintenance message J3 (INSTINCT DISC):
  • do a check for loose J3 connector at the ECU 2 ASM 732512.
   (1) If the fault continues:
  • make sure that the pins are not bent and that the pins and sockets have not moved into the J3 ECU 2 connector ASM 732512.
   (2) If the fault continues:
  • do a check for open circuit in the harness J3 between the pins J3/6, 31 ASM 732512.
     (a) If the fault continues:
  • replace the 5CA1
  • replace the 5CA2
  • replace the harness J3 .
     (b) If there is no fault:
Subtask 73-29-00-710-233-A ** ON A/C NOT FOR ALL
B. Do the test given in Para. 3.A.
[Rev.8 from Aug 2018] 2026.04.04 04:36:03 UTC
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