# SDR FDEA200810084278

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: October 8, 2008
- Submitted: December 15, 2008
- Operation: Air carrier
- Aircraft: [N650FE](https://openairdocs.org/aircraft/N650FE), 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: 726
- Aircraft time: 21,906 hours, 11,330 cycles
- System (JASC): [2750 · Trailing Edge Flap Control System](https://openairdocs.org/jasc/2750)
- Part: Limiter
- Part number: 532A000003
- Part serial: N148
- Condition: Malfunctioned
- Location: Flap Torque
- Stage of operation: CL
- How discovered: O
- Nature of condition: F, J
- Precautionary procedure: A
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/FDEA200810084278

## Discrepancy

FLAPS STUCK AT 20 DEG WOULD NOT RETRACT.  FOLLOWED RED TABS FLAPS DID EXTEND TO 30/40 ON LANDING FLAPS RETRACTED AFTER LANDING.  BOTH SYS 1 AND SYS  2 FLAP FAULT LIGHT ON IN FLIGHT.  PERFORMED SERVICING OF RT WING JACKSCREWS AND TORQUE LIMITER PER AMM 12-13-27-0.  ALL FLUIDS CLEAN WITH MINIMAL SERVICING REQUIRED.  REMOVED AND REPLACED FLAP TORQUE LIMITER IAW MM 27-54-12-4.  PERFORMED OPERATIONAL TEST OF FLAP SYSTEM AND NO  DEFECTS FOUND.  REINSTALLED INBD NR 1 JACKSCREW ACCESS PANEL.  PER VERBAL, MTSI STEP 4 FLAP SYSTEM LUBE ACCOMPLISHED BY EMP NR 175004.  PER STEP 1 PERFORMED VISUAL INSPECTION OF ALL CARRIAGES,  BEARINGS, ROLLERS, JACKSCREWS, TRACKS, NO DEFECTS FOUND.

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