# SDR 2003F00407

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: June 27, 2003
- Submitted: July 11, 2003
- Operation: Air carrier
- Aircraft: [N464TA](https://openairdocs.org/aircraft/N464TA), registered now
- Make and model: Airbus A320-233
- Registry model: [Airbus A320-233](https://openairdocs.org/model/airbus-a320-233) (OpenAirDocs)
- Aircraft serial: 1353
- Engine: Iae V2527EA5
- System (JASC): [7230 · Turbine Engine Compressor Section](https://openairdocs.org/jasc/7230)
- Part: Blade
- Condition: Bent
- Location: Compressor
- Stage of operation: CL
- How discovered: O
- Nature of condition: R, J
- Precautionary procedure: E, A
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/2003F00407

## Discrepancy

DURING CLIMB, TWO COMPRESSOR STALLS AND LOSS OF POWER ON ENGINE NR 1 WERE EXPERIENCED.  THE ENGINE WAS SHUTDOWN IN FLIGHT AND THE AIRCRAFT WAS RETURNED TO SAL STATION.  ON GROUND TECHNICIANS PERFORMED HPC BOROSCOPE INSPECTION PER AMM 72-00-00.  THE 6TH WAS FOUND WITH BENT BLADES.  THE ENGINE WAS REPLACED AND TESTED AS PER AMM 71-00-20.  ALL TEST RESULTS WERE NORMAL AND THE AIRCRAFT RETURNED TO NORMAL OPERATION.  (M)

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