# SDR AALA202601063589

- 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): [7532 · Compressor Bleed Valve](https://openairdocs.org/jasc/7532)
- Part: Solenoid Valve
- Part number: AC69572
- Part serial: EKV129
- Condition: Defective
- Location: Nr 2 Eng
- Part time: 32,034 hours, 14,424 cycles
- Component: Engine, Iae
- Stage of operation: CR
- How discovered: O
- Nature of condition: M, J
- Precautionary procedure: A
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/AALA202601063589

## 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. 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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