# SDR AWXA200401338

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: November 24, 2004
- Submitted: November 26, 2004
- Operation: Air carrier
- Aircraft: [N662AW](https://openairdocs.org/aircraft/N662AW), registered now
- Make and model: Airbus A320-232
- Registry model: [Airbus A320-232](https://openairdocs.org/model/airbus-a320-232) (OpenAirDocs)
- Aircraft serial: 1274
- Aircraft time: 16,397 hours, 6,302 cycles
- System (JASC): [2780 · Leading Edge Slat Control System](https://openairdocs.org/jasc/2780)
- Part: Actuator
- Part number: 830C000001
- Part serial: 0852
- Condition: Malfunctioned
- Location: Flap/Slats
- Part time: 16,397 hours, 6,302 cycles
- Stage of operation: AP
- How discovered: O
- Nature of condition: F, J
- Precautionary procedure: O
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/AWXA200401338

## Discrepancy

UPON PREPARING FOR LANDING PILOTS REPORTED SELECTING FLAP LEVER TO 1, WITH A SPEED OF 210 KTS AND RECEIVED A SLAT/FLAP ECAM FAULT.  FLAPS OPERATED NORMAL, SLATS REMAINED AT ZERO.  LANDING WAS UNEVENTFUL.  MAINTENANCE REMOVED AND REPLACED 6079CM ROTARY ACTUATOR IAW AMM 27-84-49-04. OPERATIONAL TEST OF SYSTEM GOOD.  BOTH FCC'S SELF TEST GOOD.  WTB/POB TEST GOOD ON BOTH SIDES. VENDORS FUNCTIONAL TEST OF ROTARY ACTUATOR S/N 20852 CONFIRMED REASON FOR REMOVAL, UNIT FAILED LOW TEMPERATURE TEST. RESHIMMED UNIT AND REACCOMPLISHED FUNCTIONAL TEST IAW CMM 27-82-14, REV. 4.

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