# SDR 07FDEA02290

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: June 27, 2007
- Submitted: June 27, 2007
- Operation: Air carrier
- Aircraft: [N722FD](https://openairdocs.org/aircraft/N722FD), registered now
- Make and model: Airbus A300 B4-622R
- Registry model: [Airbus A300 B4-622R](https://openairdocs.org/model/airbus-a300-b4-622r) (OpenAirDocs)
- Aircraft serial: 479
- Aircraft time: 39,140 hours, 21,493 cycles
- System (JASC): [2750 · Trailing Edge Flap Control System](https://openairdocs.org/jasc/2750)
- Part: Computer
- Part number: 4909505
- Part serial: 01174
- Condition: Faulted
- Location: Nr 2
- Part time: 15,009 hours, 8,095 cycles
- Stage of operation: CL
- How discovered: O
- Nature of condition: J
- Precautionary procedure: A
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/07FDEA02290

## Discrepancy

ATB - AFTER T/O - ECAM AND OVH SYS 2 FLAP FAULT.  UNABLE TO CLEAR FAULT.  FOUND NR 2 SFCC FAULTING MAIN CONTROL VALVE UPON ARRIVAL.  RESET SFCC AND RAN FLAPS, AGAIN FAULTED MAIN CONTROL VALVE.  BOTH TIMES NR 2 FLAP SYS FAULT LIGHT ON OVERHEAD CAME ON AND WOULD NOT RESET.  SWAPPED NR 2 AND NR 1 SFCC AND RAN FLAPS.  FLAP SYS NR 1 BEGAN FAULTING.  PUT BOXES BACK IN ORIGINAL POSITION.  PLACING BOX ON ORDER.  RAN NR 2 ENG AND TIMED FLAPS WITH NR 2 SFCC BREAKERS PULLED PER AMM 27-54-00-5.  ALL TIMES WERE WITHIN LIMITS AND FLAPS MOVED SYMMETRICALLY ON SYSTEM NR 1.  REPLACED NR 2 SFCC FLAP/SLAT SYSTEM TEST OK PER MM 27-51-18-4 27-51-00-5.

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