W DOC AIRBUS | TSM A320F

Internal Failure of the ECU on Engine 2


TASK 73-20-81-810-881-A
Internal Failure of the ECU on Engine 2


1. Possible Causes
  • ECU [4000KS]
  • ECU air cooling system
  • anti-ice system ducts
2. Job Set-up Information
 A. Referenced Information
REFERENCE
DESIGNATION
AMM 30-21-49-210-001
Visual Inspection of the Anti-Ice System Tubes, Ducts, and Hoses
AMM 30-21-49-210-040
Visual Inspection of the Anti-Ice System Hoses, Tubes and Ducts
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)
AMM 73-29-00-710-040
Operational Test of the FADEC on the ground (with Engine Motoring)
AMM 75-24-49-210-040
Visual inspection of the ECU Air Cooling Tubes and Ducts
AMM 75-24-49-210-042
Visual Inspection of the ECU Air Cooling Tubes and Ducts
3. Fault Confirmation
Subtask 73-20-81-710-129-A ** ON A/C NOT FOR ALL
A. Do the operational test of the FADEC 2B on the ground (with engine non motoring) AMM 73-29-00-710-040.
4. Fault Isolation
Subtask 73-20-81-810-129-A ** ON A/C NOT FOR ALL
A. If the test gives the maintenance message ECU (OVERTEMP):
   (1) Remove the ECU [4000KS] AMM 73-21-60-000-001.
   (2) Do a check of the ECU air cooling system to make sure that the inlet and outlet ports are not clogged AMM 75-24-49-210-042.
   (3) Do a check for leakage on the anti-ice system ducts AMM 30-21-49-210-040.
   (4) Install the new ECU (4000KS) AMM 73-21-60-400-001.
Subtask 73-20-81-810-129-B ** ON A/C NOT FOR ALL
A. If the test gives the maintenance message ECU (OVERTEMP):
   (1) Remove the ECU [4000KS] AMM 73-21-60-000-001.
   (2) Do a check of the ECU air cooling system to make sure that the inlet and outlet ports are not clogged AMM 75-24-49-210-040.
   (3) Do a check for leakage on the anti-ice system ducts AMM 30-21-49-210-001.
   (4) Install the new ECU (4000KS) AMM 73-21-60-400-001.
[Rev.8 from Aug 2018] 2026.04.04 04:35:40 UTC