# SDR 2026FA0000231

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: March 24, 2026
- Submitted: March 27, 2026
- Operation: General aviation
- Aircraft: [N206FR](https://openairdocs.org/aircraft/N206FR), registered now
- Make and model: Airbus A320-214
- Registry model: [Airbus A320-214](https://openairdocs.org/model/airbus-a320-214) (OpenAirDocs)
- Aircraft serial: 48589
- Aircraft time: 23,664 hours, 48,589 cycles
- Engine: Cfmint CFM565B43
- Engine time: 10,541 hours, 13,827 cycles
- System (JASC): [5753 · Trailing Edge Flaps](https://openairdocs.org/jasc/5753)
- Part: Computer
- Condition: Faulted
- Location: Flap System
- Stage of operation: CL
- How discovered: O
- Nature of condition: F
- Precautionary procedure: A
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/2026FA0000231

## Discrepancy

AFTER TAKE OFF FLAPS LOCKED.  IAW AMM 27-51-00-740-002-A BITE TEST SLAT AND FLAP CONTROL COMPUTER, IAW AMM 27-50-00-869-006-A  RESET OF WING TIP BRAKE  WAS PERFORMED, SATISFACTORY, IAW AMM 31-36-00-000-001-A  PCMCIA MEMORY CARD WAS DOWNLOADED.  IAW TSM TASK 27-51-00-810-855-A WTB/POB TEST PERFORMED UNSUCCESSFULLY OR TEST ABORTED.  AND AMM 27-51-00-710-001-A / 27-51-00-810-855-A REV 76 REV DATE 01 FEB 2026 WAS PERFORMED . THE SFCC 2 WAS REPLACED. NO HELP, BITE TEST AND W.T.B/ P.O.B OF TWO SYS FLAP AND SLATS WERE PERFORMED SEVERAL TIMES TO CONFIRM FAULT. THE WTB FLAP LT WERE FOUND WITH FOLLOW MESSAGE FLP LT WTB YEL SOLENOID 33CV FAULT AND  FLP LT WTB BLUE SOLENOID 33CV FAULT. PENDING REPLACED OF THE WTB FLAP LH 33CV AND MANAGE THE COMPONENT SFCC COMPUTER.  IAW AMM 27-51-51-000/400-001-A THE WING-TIP BRAKE (33CV) WAS REMOVED AND REPLACED.TEST SATISFACTORY.

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