# SDR 2006UALA02025

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: October 18, 2006
- Submitted: October 24, 2006
- Operation: Air carrier
- Aircraft: [N472UA](https://openairdocs.org/aircraft/N472UA), registered now
- Make and model: Airbus A320-232
- Registry model: [Airbus A320-232](https://openairdocs.org/model/airbus-a320-232) (OpenAirDocs)
- Aircraft serial: 1435
- Aircraft time: 18,767 hours, 7,839 cycles
- Engine: Iae V2527A5
- Engine time: 18,767 hours, 7,839 cycles
- System (JASC): [7200 · Engine (Turbine/Turboprop)](https://openairdocs.org/jasc/7200)
- Part: Engine
- Condition: Failed
- Location: Nr 1
- Stage of operation: TO
- How discovered: O
- Nature of condition: X, J
- Precautionary procedure: C
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/2006UALA02025

## Discrepancy

NR 1 ENGINE FAILED DURING TAKEOFF RUN.     REPLACED NR 1 ENGINE.  FOUND FINE METAL SHAVINGS IN TAILPIPE.  CAPT REPORTED BURNING ODOR IN CABIN. NO SMOKE. EGT, EPR SPIKED.  FADEC MESSAGE, VSV VALVE FAILURE.  NOTHING ON PFR.  NR 1 ENGINE HAS METAL IN THE AFT FAN AIR DUCT ALSO THE RIGHT SIDE 7TH AND 10TH STAGE BLEEDS HAVE METAL IN TH E SCREENS. THE 7TH RIGHT UPPER BLEED VALVE HAS AN ACCUMULATION OF METAL APPROX 1 TABLESPOON FULL.  ACCOMPLISHED IDLE LEAK CHECK, AND EEC CHECK DUE TO ENGINE REPLACEMENT.  NO DEFECTS NOTED.

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