# SDR 08FDEA01272

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: April 3, 2008
- Submitted: April 3, 2008
- Operation: Air carrier
- Aircraft: N455FE
- Make and model: Airbus A310-222
- Registry model: [Airbus A310-222](https://openairdocs.org/model/airbus-industrie-a310-222) (OpenAirDocs)
- Aircraft serial: 331
- Aircraft time: 33,213 hours, 15,029 cycles
- System (JASC): [2750 · Trailing Edge Flap Control System](https://openairdocs.org/jasc/2750)
- Part: Flap System
- Condition: Malfunctioned
- Location: Te Flaps
- Stage of operation: AP
- How discovered: O
- Nature of condition: J
- Precautionary procedure: L
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/08FDEA01272

## Discrepancy

WHEN SELECTED FLAPS 15 ON APPROACH SFPI SHOWED FLAPS LIGHT AND FLAPS WOULD NOT EXTEND, RE-CYCLED FLAPS AND ON SECOND ATTEMPT FLAPS EXTENDS NORMALLY.  PERFORMED WIRING CHECK HIGH SPEED SOL V/V, ENABLE V/V AND RETRACT SOL V/V ALL RESISTANCE VALUE WITHIN LIMIT.  CHECKED BOTH TORQUE LIMIT ARE NO FAULTS NOTED, ALL SCREW JACK TORQUE LIMITER NO JAM NOTED.  RAN NR 2 ENG AGAIN AND FLAP/SLAT SYS OPS CHECKED ALL IND SYS WORKS OK.  CARRIED OUT BITE CHK OF SFCC NR1/NR 2, NO FAULT NOTED PER AMM 27-50-00-0/5, JRH CHAP 5.

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