# SDR FDEA201401230187

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: January 23, 2014
- Submitted: January 24, 2014
- Operation: Air carrier
- Aircraft: [N653FE](https://openairdocs.org/aircraft/N653FE), 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: 736
- Aircraft time: 28,146 hours, 14,733 cycles
- System (JASC): [2780 · Leading Edge Slat Control System](https://openairdocs.org/jasc/2780)
- Part: Computer
- Part number: 4909505
- Part serial: 1030664
- Condition: Faulted
- Location: Slat System
- Stage of operation: TO
- How discovered: O
- Nature of condition: J
- Precautionary procedure: A
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/FDEA201401230187

## Discrepancy

AT TAKEOFF CAPTAIN RECEIVED A FLASHING, SPD LIM,  WARNING ON PFD NEXT TO SPEED TAPE.  ALL SPEED LIMIT INFO WAS LOST ON CAPTAIN'S PFD.  UPON RETRACTING SLATS, RECEIVED SLATS SYS 1 FAULT.  CYCLED SLATS IAW QRH BUT FAULT REMAINED, REPEAT WU.  SFCC NR 1 FAULTED, SFCC NR 2 FAULTED.  LT RETRACT SWITCH ALSO CHECKED SLAT TORQUE LIMITERS, NEITHER  TRIPPED.  WILL CONTINUE TO TROUBLE SHOT.  FOUND NR 2 SFCC UNIT FAULTED.  R & R NR 2 DUE TO FAULT & NR 1 SFCC PRECAUTIONARY IAW AMM A300 27-51-18.  OPERATIONS CHECKED GOOD.  .

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