# SDR 06FDEA1568

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: April 22, 2006
- Submitted: April 24, 2006
- Operation: Air carrier
- Aircraft: [N675FE](https://openairdocs.org/aircraft/N675FE), registered now
- Make and model: Airbus A300 B4-605R
- Registry model: [Airbus A300 B4-605R](https://openairdocs.org/model/airbus-industrie-a300-b4-605r) (OpenAirDocs)
- Aircraft serial: 789
- Aircraft time: 12,391 hours, 6,671 cycles
- System (JASC): [2750 · Trailing Edge Flap Control System](https://openairdocs.org/jasc/2750)
- Part: Computer
- Part number: 4909505
- Part serial: 01146
- Condition: Malfunctioned
- Location: Flap/Slats
- Stage of operation: CL
- How discovered: O
- Nature of condition: F
- Precautionary procedure: A
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/06FDEA1568

## Discrepancy

FLAP SYS 2 FAULT LIGHT ILLUMINATED ON OVERHEAD PANEL WITH ASSOCIATED FLAP FAULT ON ECAM.  FOLLOWED QRH.  F/O HAD NO HOOK INDICATION.  COULD NOT RECOVER SYSTEM.  EMERGENCY DECLARED.  FOUND NR 2 SFCC FLAP FAULT SHOWING 5 FAULT BALLS = BAD SFCC.  PART NIS RDU.  RESET C/W.  CYCLED FLAPS UP DOWN SEVERAL TIMES, CHECKED GOOD.  TEST PER MM 27-51-0  0-5 GOOD.  PLACED NR 2 SFCC ON MEL.  COMPUTER REMOVED AND REPLACED THE NR 2 SFCC PER A300-600 MM 27-51-18-4, OPS CHECKS GOOD PER A300-600 MM 27-51-00-5, SYSTEM OK FOR SERVICE.

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