# SDR 04FDEA02047

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: July 12, 2004
- Submitted: July 12, 2004
- Operation: Air carrier
- Aircraft: N427FE
- Make and model: Airbus A310-203
- Registry model: [Airbus A310-203](https://openairdocs.org/model/airbus-industrie-a310-203) (OpenAirDocs)
- Aircraft serial: 362
- Aircraft time: 42,976 hours, 18,559 cycles
- System (JASC): [2780 · Leading Edge Slat Control System](https://openairdocs.org/jasc/2780)
- Part: Computer
- Condition: Malfunctioned
- Location: Nr 2 Sfcc
- Stage of operation: CL
- 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/04FDEA02047

## Discrepancy

AFTER TAKEOFF NR 1 SYSTEM FAULT, FLAPS RETRACTED NORMAL FROM 20/20.  NEXT RETRACTION GOT BOTH SYSTEM 1 & 2 FAULT.  SLATS LOCKED AT 15 DEG.  FOLLOWED QRH PROCEDURES, RECYCLED AND NO HELP.  SET UP FOR SLATS 15 STUCK LANDING.  SFCC NR 2 WAS REMOVED AND REPLACED DUE TO HARD FAULT AT BLOCK-IN REF A310 AMM 27-51-18-4.  TROUBLESHOT BOTH SFCC COMPUTERS AND FOUND THE NR 2 SFCC WOULD CONTINUALLY FAULT THE RT KRUEGER.  REPLACED THE RT KRUEGER FLAP RETRACT SWITCH IN REF TO AIRBUS AMM A310-20 0 27-51-18-4, 27-89-00-6.  SYSTEM OPERATES AND CHECKS NORMAL.

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.