ON FINAL APPROACH THE NR 2 ENGINE EXPERIENCED A FLAME OUT CONDITION AND THE PILOT WAS ABLE TO LAND THE AIRCRAFT SAFELY WITH ONLY POWER FROM THE #1 ENGINE. A GENERAL VISUAL INSPECTION OF THE FIRST STAGE COMPRESSOR SECTION REVEALED NO DAMAGE. A GENERAL VISUAL INSPECTION OF THE THIRD STAGE TURBINE WHEEL REVEALED DAMAGE. A BORESCOPE OF THE HOT SECTION ALSO REVEALED DAMAGE. A GENERAL VISUAL INSPECTION OF THE FUEL NOZZLES REVEALED NO DAMAGE OR UNUSUAL WEAR. A GENERAL VISUAL INSPECTION OF THE ENGINE INLET REVEALED NO DAMAGE. DAMAGE TO THE THIRD STAGE TURBINE WHEEL WAS LIKELY CAUSED BY DEBRIS FROM THE HOT SECTION, HOWEVER; NO DEFINITIVE CAUSE FOR THE DAMAGE IDENTIFIED IN THE HOT SECTION WAS DETERMINED.
| Incident date | April 3, 2026 |
|---|---|
| Airline | CALA |
| Flight | NR2 |
| Aircraft | AIRBUS A319131 |
| Registration | N835UA |
| Affected area | Engine |
| Event type | Fumes or Odor |
| Verification | Official |
Sources
- FAA SDR: CALA fumes or odor report on 2026-04-03 (external.apic4e.faa.gov)
- FAA SDR: SWAA fumes or odor report on 2026-04-01 (external.apic4e.faa.gov)
- FAA SDR: BJNA fire report on 2026-04-05 (external.apic4e.faa.gov)
- FAA SDR: JIKA fire report on 2026-04-04 (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.