# SDR FDEA201710112906

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: October 11, 2017
- Submitted: October 13, 2017
- Operation: Air carrier
- Aircraft: [N689FE](https://openairdocs.org/aircraft/N689FE), 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: 875
- Aircraft time: 14,356 hours, 7,958 cycles
- System (JASC): [2750 · Trailing Edge Flap Control System](https://openairdocs.org/jasc/2750)
- Part: Solenoid Valve
- Part number: 500A000003
- Part serial: 12789
- Condition: Inoperative
- Location: Slat / Flap Sys
- Stage of operation: AP
- How discovered: O
- Nature of condition: J
- Precautionary procedure: O
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/FDEA201710112906

## Discrepancy

SLATS & FLAPS SYSTEM 1 AND 2 FAULTED WHEN THE HANDLE WAS SELECTED TO 15/20.  FLAPS WOULD RETRACT TO 0 WHEN SELECTED, BUT ONLY EXTEND TO 15/15 WITHOUT A FAULT INDICATION.   REPLACED A FAULTY SOLENOID MM 27-54-33-04.  OPERATED FLAPS AND SLATS FOR 6 CYCLES WITH BOTH ENGINES RUNNING, NO FAULTS ON EITHER SFCC, OR ON OVERHEAD AND NO ASSYMETRY LOCKOUT.  SYSTEM OPS CHECKED NORMAL.

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