# SDR FDEA201609073130

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: September 7, 2016
- Submitted: September 7, 2016
- Operation: Air carrier
- Aircraft: [N690FE](https://openairdocs.org/aircraft/N690FE), registered now
- Make and model: Airbus A300 F4-605R
- Registry model: [Airbus A300 F4-605R](https://openairdocs.org/model/airbus-industrie-a300-f4-605r) (OpenAirDocs)
- Aircraft serial: 876
- Aircraft time: 13,156 hours, 7,229 cycles
- System (JASC): [2750 · Trailing Edge Flap Control System](https://openairdocs.org/jasc/2750)
- Part: Solenoid Valve
- Part number: 500A000003
- Condition: Malfunctioned
- Location: Te Flap
- Stage of operation: AP
- How discovered: O
- Nature of condition: O, F
- Precautionary procedure: A
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/FDEA201609073130

## Discrepancy

CONFIGURING FOR APPROACH, FLAPS STUCK AT ZERO.  CYCLED WITH NO HELP.  FLAPS UP LANDING.  SLATS MOVED NORMALLY.  FLIGHT DIVERTED.  INTERROGATION OF NR 1 SFCC SHOWS MAIN CONTROL VALVE FAULT.  NR 2 SFCC SHOWS SFCC FAILED.  RESET AND OPERATED ON GREEN SYS WITH NO SFCC  FAULTS.  REMOVED AND REPLACED SFCC'S 1 & 2 REF AMM 27-51-18-04.  SLAT FLAP BITE TEST IS NORMAL.  RAN ENGINES PER JRH AND FLAPS OPERATED NORMAL.  REF SDR GMM 12-7-600 NR 1 SFCC, P/N 49-095-05, S/N 1221 & NR 2 SFCC, P/N 49-095-05, S/N 639.  SEE WRI 27-50-8260 FOR  FLAP/EXT SOLENOID R&R.

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