# SDR AUS20020670

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: July 9, 2002
- Submitted: August 7, 2002
- Operation: General aviation
- Make and model: Beech B200C
- Registry model: [Beech B200C](https://openairdocs.org/model/beech-b200c) (OpenAirDocs)
- Engine: Pwa PT6A42
- Propeller: Hartzl HCD4N3A
- System (JASC): [2701 · Control Column Section](https://openairdocs.org/jasc/2701)
- Part: Stud
- Part number: AN2278B
- Condition: Fractured
- Location: Control Column S
- Component: Control Column S
- Stage of operation: IN
- Nature of condition: O, F
- Precautionary procedure: K
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/AUS20020670

## Discrepancy

(AUS) AILERON CONTROL SYSTEM STUD FRACTURED. CLAMP PNO AN737TW56-66 LOOSE AT BOTTOM OF CONTROL COLUMN ALLOWING THE CONTROL COLUMN BOOT PNO 101-54149-37 TO MOVE UNSECURED AROUND THE CONTROLCOLUMN. LH AILERON CONTROL CABLE TURNBUCKLE LOCKWIRE CAUGHT ONBRACKET PNO 50-524466-7 WHEN THE CONTROL WHEEL WAS MOVED TO THE RIGHT.

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