ENGINE 2 FIRE ON TAKE OFF. SHUT ENGINE DOWN AND FIRE ALERT WENT AWAY. SPARKS AND SMOKE REPORTED SEEN BY FAS AND PASSENGERS. PERFORMED INSPECTION AFTER ENGINE WINDMILLING ON ENG#2 AFTER ENGINE IN-FLIGHT SHUTDOWN AND FOUND HARNESS CONNECTOR DAMAGE ON CONNECTORS P105, P110, 401VC, 405VC, 404VC, 454VC AND 4108VC. FUEL RETURN LINE P/N AE1002-624-AS1072, AIR OIL HEAT EXCHANGER BELOW SEAL P/N 5323415, FIRE HARNESS CONNECTOR FIN WCOS P/N 1020890-2 ENG # PEDAL CABLES FIN 4002XV, 4003XV, 4004XU AND 4005XV MANIFOLD HOSE TUBER I/B AT 10 & 7 OCLOCK POSITION REQUIRED REPLACMENT. IAW AMM 05-51-34-200-001-A / AMM 72-00-00-210-814. AIRCRAFT WAS RETURNED TO SERVICE.
| Incident date | October 16, 2025 |
|---|---|
| Airline | F3LA |
| Flight | AE1002 |
| Aircraft | AIRBUS A321271NX |
| Registration | N671FR |
| Affected area | Engine |
| Event type | Fire |
| Verification | Official |
Sources
- FAA SDR: F3LA fire report on 2025-10-16 (external.apic4e.faa.gov)
This entry summarizes publicly reported information and links to the original reporting or official record. Details can change as authorities and operators release additional information.