# SDR 06FDEA04015

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: November 15, 2006
- Submitted: November 20, 2006
- Operation: Air carrier
- Aircraft: N805FD
- Make and model: Airbus A310-324
- Registry model: [Airbus A310-324](https://openairdocs.org/model/airbus-industrie-a310-324) (OpenAirDocs)
- Aircraft serial: 456
- Aircraft time: 52,030 hours, 10,335 cycles
- System (JASC): [2750 · Trailing Edge Flap Control System](https://openairdocs.org/jasc/2750)
- Part: Computer
- Condition: Malfunctioned
- Location: Te Flaps
- Stage of operation: AP
- How discovered: O
- Nature of condition: J
- Precautionary procedure: R
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/06FDEA04015

## Discrepancy

FLAPS STUCK, BOTH FLAPS 1 AND FLAPS 2 HAD FAULT ON OVHD HYD PANEL.  ECAM SHOWED SAME, SPFI HAD NO INDICATION.  FOUND BOTH SFCC'S FAULTING FLAP JAM FOUND RT TORQUE LIMITER IN WHEEL WELL FAULTED, FOUND NR 1 SCREW JACK  TORQUE LIMITER FAULTED, RESET BOTH TORQUE LIMITERS PER MM 27-54-19-2, LWR FLAPS INSPECTED ALL RT WING FLAP TRACKS AND JACK SCREWS NO DEFECTS NOTED, CHECKED SERVICING ON ALL RT WING CREW JACK ASSEMBLIES, ALL CHECKED GOOD EXCEPT NR 1 SCREW JACK REQUIRED APPROX 50 CC'S OF 5606 HYD FLUID.  OPS CK'D FLAPS PER MM 27-54-00.  NO FAULTS NOTED.

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