# SDR 20010416CW010

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: March 13, 2001
- Submitted: April 16, 2001
- Operation: General aviation
- Aircraft: N414JK
- Make and model: Cessna 414A
- Registry model: [Cessna 414A](https://openairdocs.org/model/cessna-414a) (OpenAirDocs)
- Aircraft serial: 414A0626
- Engine: Cont TSIO520*
- System (JASC): [2750 · Trailing Edge Flap Control System](https://openairdocs.org/jasc/2750)
- Part: Control Cable
- Part number: 500000863
- Condition: Broken
- Location: Te Flaps
- Part time: 6,160 hours
- Stage of operation: IN
- How discovered: V
- Nature of condition: O
- Precautionary procedure: K
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/20010416CW010

## Discrepancy

CABLE SNAPPED BY FIRST PULLEY OUTBOARD OF FLAP MOTOR,  RIGHT SIDE.  NO EVIDENCE OF WEAR OR CORROSION.  PULLEY WAS TURNING FREE.  FAILURE CAUSED SPLIT FLAPS ON LANDING.

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