# SDR FDEA201503060701

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: March 6, 2015
- Submitted: March 9, 2015
- Operation: Air carrier
- Aircraft: [N667FE](https://openairdocs.org/aircraft/N667FE), 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: 771
- Aircraft time: 268 hours, 14,503 cycles
- System (JASC): [2750 · Trailing Edge Flap Control System](https://openairdocs.org/jasc/2750)
- Part: Pcu
- Part number: 579B000005
- Part serial: 00121
- Condition: Failed
- Location: Te Flap Sys
- Part time: 7,739 hours, 4,297 cycles
- Stage of operation: LD
- How discovered: O
- Nature of condition: F
- Precautionary procedure: O
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/FDEA201503060701

## Discrepancy

FLAPS BINDING AT APPROX 35 DEGREES ON APPROACH.  COMPLIED WITH ECAM & QRH & LANDED.   CREW STATED NO ASYMMETRY FAULTS RECEIVED & ACFT HAD NO ABNORMAL FLIGHT CHARACTERISTICS.  VISUALLY  INSPECTED FLAPS & SLATS FROM THE GROUND, NO ABNORMALITIES NOTED.  INTERROGATED SFCC'S, NR 1 SFCC HAD KRUGER NOTCH FLAP EXTENSION & RETRACTION SWITCHES FAULT & NR 2 SFCC HAD FLAP BINDING FAULT.    REMOVED AND REPLACED FLAPS POWER CONTROL UNIT IAW MM 27-54-11-04,   OPS CHECKED FLAPS WITH ENGINE RUNNING. OPS CHECKED NORMAL.

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