# SDR AWXA200401012

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: September 10, 2004
- Submitted: September 13, 2004
- Operation: Air carrier
- Aircraft: [N651AW](https://openairdocs.org/aircraft/N651AW), registered now
- Make and model: Airbus A320-232
- Registry model: [Airbus A320-232](https://openairdocs.org/model/airbus-a320-232) (OpenAirDocs)
- Aircraft serial: 866
- Aircraft time: 22,736 hours, 8,708 cycles
- Engine: Iae V2527A5
- Engine time: 22,389 hours, 8,954 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: R, J
- Precautionary procedure: C
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/AWXA200401012

## Discrepancy

ON TAKEOFF AT ORD EN ROUTE FOR PHX, WHEN FLEX THRUST APPLIED HEARD A LOUD BANG WITH MOMENTARY STALL INDICATED ON ECAM, REJECTED TAKEOFF AND UPON CLEARING RUNWAY NOTICED NR 1 ENGINE N2 VIB AT 7.4, SHUTDOWN ENGINE AND RETURNED TO GATE.  MAINTENANCE PERFORMED A VISUAL INSPECTION OF INLET AND EXHAUST AREAS AND FOUND NO APPARENT DAMAGE.  INSPECTED 7TH AND 10TH STAGE BLEED VALVES AND FOUND METAL SHAVINGS IN 7TH STAGE AT THE 1 O'CLOCK AND 7 O'CLOCK POSITIONS.  REMOVED AND REPLACED NR 1 ENGINE IAW T/C R5M71302, OPERATIONAL CHECK WAS GOOD.

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