Internal Failure of the ECU on Engine 1
TASK 76-11-00-810-811-A
Internal Failure of the ECU on Engine 1
1. Possible Causes
2. Job Set-up Information
A. Referenced Information
3. Fault Confirmation
Subtask 76-11-00-710-072-A ** ON A/C NOT FOR ALL
Subtask 76-11-00-810-064-C ** ON A/C NOT FOR ALL
[Rev.8 from Aug 2018]
2026.04.04 04:37:25 UTC
Internal Failure of the ECU on Engine 1
1. Possible Causes
2. Job Set-up Information
A. Referenced Information
| REFERENCE | DESIGNATION |
|---|---|
| AMM 31-36-34-000-001 | Removal of the Data Management Unit (DMU) |
| AMM 31-36-34-400-001 | Installation of the Data Management Unit (DMU) |
| 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 73-21-60-740-007 | Correct Time Limited Faults (Non Asterisked) of the Engine Scheduled Maintenance Report |
| ASM 732510 | |
| AMM 73-29-00-710-040 | Operational Test of the FADEC on the ground (with Engine Motoring) |
Subtask 76-11-00-710-072-A ** ON A/C NOT FOR ALL
A. Do the operational test of the FADEC 1A and 1B on the ground (with engine non motoring) AMM 73-29-00-710-040.
4. Fault IsolationSubtask 76-11-00-810-064-C ** ON A/C NOT FOR ALL
A. If the ECAM Warning "THR LEVER FAULT" is not associated with failure messages TLA SNSR, J3, ECU and TLA SNSR, J4, ECU this is most likely indicating an internal failure of the ECU. In such a case this ECAM Warning is usually displayed with other engine related ECAM Warnings.
This can be checked in the Post Flight Report (PFR) AMM 73-21-60-740-007.
(1) If the test does not give the failure messages TLA SNSR, J3, ECU and TLA SNSR, J4, ECU:
Subtask 76-11-00-710-078-A ** ON A/C NOT FOR ALL This can be checked in the Post Flight Report (PFR) AMM 73-21-60-740-007.
(1) If the test does not give the failure messages TLA SNSR, J3, ECU and TLA SNSR, J4, ECU:
- replace the ECU [4000KS] AMM 73-21-60-000-001 and AMM 73-21-60-400-001.
- replace the DMU [1TV] AMM 31-36-34-000-001 and AMM 31-36-34-400-001.
- Do a continuity and insulation check of the wiring between the ECU (ARINC OUTPUT) connector J3 (pins 11 and 24) / connector J4 (pins 11 and 24) and FWC 1 and 2 ASM 732510.
- replace or repair wiring as required.
- repeat the fault isolation procedure.
- Do the related troubleshooting procedure.
B. Do the test given in Para. 3.A.
(1) No additionnal maintenance action is required if the fault is not confirmed.
(2) Repeat the fault isolation procedure if the fault continues.
(1) No additionnal maintenance action is required if the fault is not confirmed.
(2) Repeat the fault isolation procedure if the fault continues.