# SDR 20001013SH003

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: October 10, 2000
- Submitted: October 12, 2000
- Operation: General aviation
- Aircraft: [N810JP](https://openairdocs.org/aircraft/N810JP), registered now
- Make and model: Piper PA-34-200T
- Registry model: [Piper PA-34-200T](https://openairdocs.org/model/piper-pa-34-200t) (OpenAirDocs)
- Aircraft serial: 347670088
- Aircraft time: 4,415 hours
- System (JASC): [2740 · Stabilizer Control System](https://openairdocs.org/jasc/2740)
- Part: Control Cable
- Part number: 6270197
- Condition: Broken
- Location: Aft Fuselage
- Part time: 4,415 hours
- Stage of operation: CR
- 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/20001013SH003

## Discrepancy

STABILATOR TRIM CABLE (P/N 62701-97) BROKE AT THE ELECTRIC TRIM DRIVE WHEEL ASSEMBLY WHILE DOING STEEP TURNS IN PT FOR COMML (ME). AIRCRAFT PITCHED UP 10-20 DEGREES BUT WAS CONTROLLABLE BY SLOWING AND LOWERING FLAPS TO FIRST NOTCH FOR SLOW RETURN AND LANDING WITHOUT FURTHER PROBLEM.  ABOVE PART WAS REPLACED. SUSPECT OVER-STRESS OF TRIM CABLE (P/N 62701-73) AND THAT WAS ALSO REPLACED.  ALL CONTROL/TRIM FUNCTIONS RESTORED TO NORMAL.  FORM 337 ISSUED 11 OCT AND MAILED TO SCOTTSDALE FSDO.   (X)

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