# SDR JGVR20200218001

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: February 18, 2020
- Submitted: February 18, 2020
- Operation: General aviation
- Aircraft: [N91FP](https://openairdocs.org/aircraft/N91FP), registered now
- Make and model: Cessna 510
- Registry model: [Cessna 510](https://openairdocs.org/model/cessna-510) (OpenAirDocs)
- Aircraft serial: 5100001
- Aircraft time: 3,667 hours, 3,010 cycles
- System (JASC): [2710 · Aileron Control System](https://openairdocs.org/jasc/2710)
- Part: Bellcrank
- Part number: 70611215
- Condition: Wrong Part
- Location: Rt Wing Aileron
- Part time: 3,667 hours, 3,010 cycles
- Stage of operation: IN
- How discovered: V
- Nature of condition: W
- Precautionary procedure: K
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/JGVR20200218001

## Discrepancy

DURING A DOCUMENT 16 INSPECTION FOUND AILERON WING CABLES TO BE WORN REQUIRING REPLACEMENT.  AFTER THE REPLACEMENT OF THE AILERON WING CABLES AND DURING THE RIGGING OF THE R/H AILERON IT WAS FOUND THAT THE AILERON COULD NOT BE RIGGED TO THE REQUIRED 2 DEGREES UP WITHOUT EXCEEDING THE WITNESS HOLES FOR THE R/H AILERON PUSH/PULL ROD.  AFTER FURTHER INVESTIGATION IT WAS FOUND THAT THE R/H AILERON WING SECTOR WAS THE INCORRECT P/N.  THE P/N INSTALLED (7061121-5) WAS FOR THE L/H SIDE.  AS FAR AS ANYONE CAN DETERMINE THIS COME FROM THE FACTORY.  THE AIRCRAFT WAS IN EXPERIMENTAL CATEGORY DURING CERTIFICATION AND WAS EVENTUALLY REMOVED FROM EXPERIMENTAL AND SOLD.

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