Oil Filter Clogged on Engine 1
TASK 79-00-00-810-820-A
Oil Filter Clogged on Engine 1
1. Possible Causes
A. Referenced Information
3. Fault Confirmation
Subtask 79-00-00-710-088-A ** ON A/C NOT FOR ALL
Subtask 79-00-00-810-076-A ** ON A/C NOT FOR ALL
[Rev.8 from Aug 2018]
2026.04.04 04:38:22 UTC
Oil Filter Clogged on Engine 1
1. Possible Causes
- oil scavenge filter element
- engine
- SW-OIL FILTER DIFF PRESS [4001EN]
- aircraft wiring
- main oil supply filter
A. Referenced Information
| REFERENCE | DESIGNATION |
|---|---|
| AMM 71-00-00-710-003 | Engine Automatic Start |
| AMM 71-00-00-710-004 | Engine Manual Start |
| AMM 71-00-00-710-006 | Minimum Idle Check |
| AMM 71-00-00-710-028 | Engine Shutdown |
| AMM 79-00-00-281-002 | Check of the Electrical Master Chip Detector (EMCD) for Particles |
| AMM 79-00-00-281-003 | Check of FWD Sump, AFT Sump, AGB, and TGB Scavenge Screens |
| AMM 79-21-10-000-003 | Removal of the Lube Supply and/or Common Scavenge Filters |
| AMM 79-21-10-210-001 | Check Supply and Scavenge Filters Clogging Indicator Position |
| AMM 79-21-10-210-002 | Check of the Lubrication Unit Magnetic Plugs and Scavenge Screens |
| AMM 79-21-10-400-003 | Installation of the Lube Supply and/or Common Scavenge Filters |
| AMM 79-21-10-920-002 | Remove and Discard Supply Filter |
| AMM 79-35-15-000-003 | Removal of the Oil Filter Differential Pressure Switch |
| AMM 79-35-15-000-040 | Removal of the Oil Filter Differential Pressure Switch |
| AMM 79-35-15-400-003 | Installation of the Oil Filter Differential Pressure Switch |
| AMM 79-35-15-400-040 | Installation of the Oil Filter Differential Pressure Switch |
Subtask 79-00-00-710-088-A ** ON A/C NOT FOR ALL
A. Test
(1) Start the engine 1 by the normal engine automatic start procedure AMM 71-00-00-710-003 or the normal engine manual start procedure AMM 71-00-00-710-004.
(2) When the oil temperature is more than 40 deg. C (104 deg. F) and the engine is at stabilised idle conditions, check if the ENG OIL FILTER CLOG indication is displayed on the ENGINE page lower display unit.
4. Fault Isolation(1) Start the engine 1 by the normal engine automatic start procedure AMM 71-00-00-710-003 or the normal engine manual start procedure AMM 71-00-00-710-004.
(2) When the oil temperature is more than 40 deg. C (104 deg. F) and the engine is at stabilised idle conditions, check if the ENG OIL FILTER CLOG indication is displayed on the ENGINE page lower display unit.
NOTE: If the warning is triggered temporarily during engine start with low engine oil temperature (lower than 40 deg. C or 104 deg. F) no maintenance action is required. Check for correct operation after the next start with oil temperature above 40 deg. C (104 deg. F).
(3) Do a shutdown of the engine 1 AMM 71-00-00-710-028. Subtask 79-00-00-810-076-A ** ON A/C NOT FOR ALL
A. The ECAM warning is triggered if a clogging of the oil scavenge filter element is detected.
(3) If the fault continues:
(a) Do a check of the aircraft wiring between the oil filter differential pressure switch (4001EN) and SDAC1/SDAC2 for short to ground:
Subtask 79-00-00-810-076-B ** ON A/C NOT FOR ALL NOTE: If the warning is triggered temporarily during engine start with low engine oil temperature (lower than 40 deg.C (104 deg.F)), no maintenance action is required. Check for correct operation after next start with oil temperature above 40 deg.C (104 deg.F).
(1) Do the following checks: - do a check of the lubrication unit magnetic plugs and screens AMM 79-21-10-210-002,
- do a check of the lube supply and common scavenge filters clogging indicators AMM 79-21-10-210-001.
(3) If the fault continues:
- replace the SW-OIL FILTER DIFF PRESS [4001EN] AMM 79-35-15-000-040 and AMM 79-35-15-400-040.
(a) Do a check of the aircraft wiring between the oil filter differential pressure switch (4001EN) and SDAC1/SDAC2 for short to ground:
- repair or replace the wiring as required.
- if the fault continues contact CFM PSE for further inspection recommendation.
A. The ECAM warning is triggered if a clogging of the main oil supply filter is detected.
(3) If the fault continues:
(a) Do a check of the aircraft wiring between the oil filter differential pressure switch (4001EN) and SDAC1/SDAC2 for short to ground:
Subtask 79-00-00-710-089-A ** ON A/C NOT FOR ALL NOTE: If the warning is triggered temporarily during engine start with low engine oil temperature (lower than 40 deg.C (104 deg.F)), no maintenance action is required. Check for correct operation after next start with oil temperature above 40 deg.C (104 deg.F).
(1) Do the following checks: - Do a check of the Electrical Master Chip Detector for particles AMM 79-00-00-281-002,
- Do a check of FWD, AFT Sump, AGB, and TGB scavenge screens AMM 79-00-00-281-003.
(3) If the fault continues:
- Replace the SW-OIL FILTER DIFF PRESS [4001EN] AMM 79-35-15-000-003 and AMM 79-35-15-400-003.
(a) Do a check of the aircraft wiring between the oil filter differential pressure switch (4001EN) and SDAC1/SDAC2 for short to ground:
- Repair or replace the wiring as required.
- If the fault continues contact CFM PSE for further inspection recommendation.
B. Do a minimum idle leak check AMM 71-00-00-710-006.
(1) No additional maintenance action is required if the fault is not confirmed.
(2) Repeat the fault isolation procedure if the fault continues.
(1) No additional maintenance action is required if the fault is not confirmed.
(2) Repeat the fault isolation procedure if the fault continues.