DOC AIRBUS | TSM A320FFailure of the Two Engines
TASK 72-00-00-810-805-A
Failure of the Two Engines
1. Possible Causes
A. Referenced Information
3. Fault Confirmation
Subtask 72-00-00-710-058-A ** ON A/C NOT FOR ALL
Subtask 72-00-00-810-054-A ** ON A/C NOT FOR ALL
[Rev.8 from Aug 2018]
2026.04.04 04:35:09 UTC
Failure of the Two Engines
1. Possible Causes
- snow ingestion
- Water projections to the radio altimeter antenna
- significant presence of water or presence of snow on the runway
A. Referenced Information
| REFERENCE | DESIGNATION |
|---|---|
| TSM TASK 72-00-00-810-806-A | Failure of Engine 1 |
| TSM TASK 72-00-00-810-807-A | Failure of Engine 2 |
Subtask 72-00-00-710-058-A ** ON A/C NOT FOR ALL
A. Test
(1) Not applicable, the confirmation can cause damage to the engine.
4. Fault Isolation(1) Not applicable, the confirmation can cause damage to the engine.
Subtask 72-00-00-810-054-A ** ON A/C NOT FOR ALL
A. There is no known engine related problem that would cause the ECAM warning ENG DUAL FAILURE to come into view.
(a) During use of the thrust reverser at low speed on snow-covered runway.
The engine failure was most likely caused by snow ingestion .
The reversion of the radio-altitude to NCD (non-computed data) can occur and cause the removal of the inhibition of the reported ECAM warnings by the Flight Warning Computer. Refer to TFU 34-42-00-013.
(c) During taxiing (or when the aircraft is stopped) on a wet or snow-covered runway.
These conditions can cause disturbance of the radio altimeter signal:
Subtask 72-00-00-710-059-A ** ON A/C NOT FOR ALL NOTE: Do the trouble shooting of individual engine per TSM procedure for ENG 1(2) FAIL ECAM warning:
(1) No trouble shooting is required if the fault has occured on wet or snow-covered runway: - for engine 1 (Ref. TSM TASK 72-00-00-810-806),
- for engine 2 (Ref. TSM TASK 72-00-00-810-807).
(a) During use of the thrust reverser at low speed on snow-covered runway.
The engine failure was most likely caused by snow ingestion .
- Make sure that the air intake and fan blades are free from ice or snow accumulation before the next flight.
The reversion of the radio-altitude to NCD (non-computed data) can occur and cause the removal of the inhibition of the reported ECAM warnings by the Flight Warning Computer. Refer to TFU 34-42-00-013.
(c) During taxiing (or when the aircraft is stopped) on a wet or snow-covered runway.
These conditions can cause disturbance of the radio altimeter signal:
- Water projections to the radio altimeter antenna by main landing gears
- Reflections of emitted signals due to significant presence of water or presence of snow on the runway .
Refer to TFU 34-42-00-003.
B. No additional maintenance action is required if the fault is not confirmed.
(1) Repeat the fault isolation procedure if the fault continues.
(1) Repeat the fault isolation procedure if the fault continues.