# SDR RJEF20201204001

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: December 4, 2020
- Submitted: December 7, 2020
- Operation: Air carrier
- Aircraft: [N686TA](https://openairdocs.org/aircraft/N686TA), registered now
- Make and model: Airbus A320-214
- Registry model: [Airbus A320-214](https://openairdocs.org/model/airbus-a320-214) (OpenAirDocs)
- Aircraft serial: 5238
- Aircraft time: 26,925 hours, 10,062 cycles
- System (JASC): [2780 · Leading Edge Slat Control System](https://openairdocs.org/jasc/2780)
- Part: Controller
- Part number: 200301E00000206
- Part serial: 200301E00000
- Condition: Malfunctioned
- Location: Slat/Flap System
- Part time: 23,287 hours, 17,951 cycles
- Stage of operation: AP
- 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/RJEF20201204001

## Discrepancy

AIRCRAFT HAD F/CTL SYS 2 FAULT DEFERRED ON DEC-04, THEN ON THE SAME DAY ON FLIGHT AV310 SAL-MIA SYSTEM 1 FAILS AND AIRCRAFT EMIT THE F/CTL FLAPS FAULT ECAM WARNING, WHICH LEADS THE CREW TO DECLARE EMERGENCY FOR LANDING.  ONCE THE AIRCRAFT WAS ON GROUND TSM 27-81-00-810-804-A AND 27-51-00-810-836-A WERE FOLLOWED.  SFCC 2 WAS REPLACED, TEST TO BOTH SFCC WERE OK AND RESTRICTED CONDITION F/CTLS FLAPS FAULT WAS CORRECTED.  AIRCRAFT RETURNED TO SAL WERE SFCC 1 WAS REPLACED TO ELIMINATE THE POSSIBLITIES TO THE FAULT OCCURS AGAIN.

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