# SDR AALA202601068771

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: December 26, 2025
- Submitted: January 6, 2026
- Operation: Air carrier
- Aircraft: [N993AN](https://openairdocs.org/aircraft/N993AN), registered now
- Make and model: Airbus A321-231
- Registry model: [Airbus A321-231](https://openairdocs.org/model/airbus-a321-231) (OpenAirDocs)
- Aircraft serial: 7188
- Aircraft time: 27,843 hours, 11,130 cycles
- Engine: Iae V2533A5
- Engine time: 32,034 hours, 14,424 cycles
- System (JASC): [7200 · Engine (Turbine/Turboprop)](https://openairdocs.org/jasc/7200)
- Part: Bleed Valve
- Part number: 5950041108
- Part serial: 2972
- Condition: Defective
- Location: Zone 400
- Part time: 32,034 hours, 14,424 cycles
- Component: Engine, Iae, V2533A5
- Component part number: V2533A5
- Stage of operation: CR
- How discovered: V
- Nature of condition: J, M
- Precautionary procedure: A, O
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/AALA202601068771

## Discrepancy

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO PHL DUE TO THE FLIGHT CREW REPORTING THAT ENGINE 2 EGT OVERTEMP FOLLOWED BY COMPRESSOR STALL DURING THE EXECUTION OF ECAM PROCEDURES FOR MULTIPLE ECAM MESSAGES / FAULTS RECIEVED FOR THAT ENGINE WHILE AT CRUISE. THE AIRCRAFT LANDED SAFELY AT PHL AND TAXIED TO THE GATE UNDER ITS OWN POWER. **ORIGINAL REPORT WAS AALA202512303589 SUBMITTED 12/30/2025 BY TUL** MAINTENANCE REPLACED 7TH STAGE BLEED VALVE SOLENOID, 10TH STAGE BLEED VALVE (AALA202601068771) AND 10TH STAGE BLEED VALVE SOLENOID (AALA202601063002) PER AMM 75-32-51, AMM 75-32-53 AND AMM 75-32-54. A SATISFACTORY LEAK / OPERATIONAL CHECK WAS ACCOMPLISHED WITH NO ISSUES NOTED.

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