# SDR CA091110008

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: November 7, 2009
- Submitted: December 1, 2009
- Operation: General aviation
- Make and model: Beech B200
- Registry model: [Beech B200](https://openairdocs.org/model/beech-b200) (OpenAirDocs)
- Aircraft time: 1,418 hours
- Engine: Pwa PT642A
- Propeller: Hartzl HCE4N3
- System (JASC): [5311 · Fuselage Main, Frame](https://openairdocs.org/jasc/5311)
- Part: Frame
- Condition: Chafed
- Location: Fuselage
- Part time: 2,266 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/CA091110008

## Discrepancy

(CAN) WHEN PERFORMING SB 24-3939, IT WAS DISCOVERED THAT ONE OF THE WIRING HARNESS WAS CONTACTING THE FWD FRAME OF THE CO-PILOT CIRCUIT BREAKER PANEL RECESS.  CHAFING HAS NOT PENETRATED THE WIRING INSULATION.  CONTACT AREA WAS LIMITED TO THE FRAME `TAB` PROTRUDING AFT INTO THE RECESS AREA AND WAS TRIMMED TO PROVIDE ADEQUATE CLEARANCE AND THEN COVERED WITH ALIGATOR GROMMET MATERIAL TO PREVENT FURTHER DAMAGE.

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