# SDR USAA2009042790984

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: April 24, 2009
- Submitted: April 27, 2009
- Operation: Air carrier
- Aircraft: N624AW
- Make and model: Airbus A320-231
- Registry model: [Airbus A320-231](https://openairdocs.org/model/airbus-industrie-a320-231) (OpenAirDocs)
- Aircraft serial: 55
- Aircraft time: 62,520 hours, 28,219 cycles
- System (JASC): [7532 · Compressor Bleed Valve](https://openairdocs.org/jasc/7532)
- Part: Bleed Valve
- Part number: AC69924
- Part serial: MY292
- Condition: Faulty
- Location: Nr 1 Engine
- Part time: 53,128 hours, 31,009 cycles
- Stage of operation: CL
- How discovered: O
- Nature of condition: R, J
- Precautionary procedure: A
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/USAA2009042790984

## Discrepancy

FLT 79 - PHX-SEA - RETURN TO FIELD - NR 1 ENGINE COMPRESSOR STALLED AFTER ROTATION.  ENGINE 1 EGT 611+HIGH FUEL FLOW+HIGH OIL PRESS 301 PSI+.  AFTER REDUCING POWER (LEVELED FLIGHT) ENGINE PARAMETERS WERE NORMAL.  CREW ELECTED TO RETURN TO PHX AND NO EMERGENCY WAS DECLARED.  MAINTENANCE REMOVED AND REPLACED THE 7C BLEED VALVE.

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