W DOC AIRBUS | TSM A320F

Internal Failure of the ECU on Engine 1


TASK 73-20-81-810-874-A
Internal Failure of the ECU on Engine 1


1. Possible Causes
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 732510
AMM 73-29-00-710-040
Operational Test of the FADEC on the ground (with Engine Motoring)
3. Fault Confirmation
Subtask 73-20-81-710-122-B ** ON A/C NOT FOR ALL
A. Do the operational test of the FADEC 1B on the ground (with engine non motoring) AMM 73-29-00-710-040.
4. Fault Isolation
Subtask 73-20-81-810-122-B ** ON A/C NOT FOR ALL
A. If the test gives the maintenance message ECU (ARINC OUT):
  • do a check for a short to ground at the wiring and connectors between the ECU (4000KS) and the test receptacle of the aircraft computers:
    . EIU1 (1KS1) - DMC1 (1WT1)
    . DMC2 (1WT2) - DMC3 (1WT3)
    . FMGC1 (1CA1) - FWC1 (1WW1)
    . FWC2 (1WW2) - DMU (1TV)
    ASM 732510.
   (1) If there is a short to ground:
  • repair the defective wiring.
   (2) If there is no short to ground:
[Rev.8 from Aug 2018] 2026.04.04 04:35:39 UTC