# SDR AWXA200401033

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: September 17, 2004
- Submitted: September 20, 2004
- Operation: Air carrier
- Aircraft: [N626AW](https://openairdocs.org/aircraft/N626AW), registered now
- Make and model: Airbus A320-231
- Registry model: [Airbus A320-231](https://openairdocs.org/model/airbus-industrie-a320-231) (OpenAirDocs)
- Aircraft serial: 65
- Aircraft time: 48,374 hours, 21,664 cycles
- Engine: Iae V2500A1
- Engine time: 39,857 hours, 18,248 cycles
- System (JASC): [7320 · Fuel Controlling System](https://openairdocs.org/jasc/7320)
- Part: Fmu
- Condition: Malfunctioned
- Location: Nr 2 Engine
- Stage of operation: DE
- How discovered: O
- Nature of condition: R, Y, J
- Precautionary procedure: E
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/AWXA200401033

## Discrepancy

ON DESCENT INTO LAS EN ROUTE FROM ORD AT APPROXIMATELY 17,000 FT, RECEIVED ECAM MESSAGE NR 2 ENGINE VANE FAILURE, ENGINE THEN SPOOLED DOWN AND ECAM INDICATED NR 2 ENGINE FAILED.  FOLLOWED ECAM INSTRUCTIONS AND SECURED NR 2 ENGINE; DECLARED EMERGENCY AND LANDED WITHOUT FURTHER EVENT.  MAINTENANCE PERFORMED ELECTRICAL CHECKS PER TSM 75-30-00-810-806; VARIABLE STATOR VANE (VSV) AND LINKAGE CHECK PER AMM 75-32-42-06, MAGNETIC CHIP DETECTOR INSPECTION PER T/C I5M72314, AND WINDMILL INSPECTION OF BLADES, NO DEFECTS NOTED.  A/C MX FERRIED TO PHX, REMOVED AND REPLACED NR 2 ENGINE FUEL METERING UNIT (FMU) IAW T/C R5M73306, AND FUEL PUMP IAW T/C R5M73304.

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