# SDR AALA202604082751

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: April 4, 2026
- Submitted: April 8, 2026
- Operation: Air carrier
- Aircraft: [N126AN](https://openairdocs.org/aircraft/N126AN), registered now
- Make and model: Airbus A321-231
- Registry model: [Airbus A321-231](https://openairdocs.org/model/airbus-a321-231) (OpenAirDocs)
- Aircraft serial: 6313
- Aircraft time: 36,343 hours, 12,377 cycles
- Engine: Iae V2533A5
- System (JASC): [7532 · Compressor Bleed Valve](https://openairdocs.org/jasc/7532)
- Part: Bleed Valve
- Part number: EB101729C
- Part serial: TCA471
- Condition: Failed
- Location: Nr 2 Engine
- Part time: 26,596 hours, 10,584 cycles
- Stage of operation: CR
- How discovered: O
- Nature of condition: J
- Precautionary procedure: O
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/AALA202604082751

## Discrepancy

AIRCRAFT WAS GROUNDED: ENGINE 2 STALL ECAM OCCURED 4-5 TIMES IN FLIGHT. FLIGHT CREW REPORTED SPEED 310, ALTITUDES 10000-15000 APPROXIMATELY, ALL ENGINE INDICATIONS NORMAL WITH NO INDICATIONS OF COMPRESSOR STALL AT ALL.  ECAM INDICATION ALWAYS WENT AWAY EACH TIME BEFORE WE RAN ANY ECAM ACTIONS AT ALL. MAINTENANCE FOUND THE #2 ENGINE STAGE 7A BLEED VALVE HAD FAILED, REPLACED BLEED VALVE PER AMM 75-32-52 AND AACOMPLISHED A SATISFACTORY OPERATIONAL CHECK WITH NO FAULTS NOTED.

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