# SDR 7AA2008F00000

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: December 13, 2007
- Submitted: January 10, 2008
- Operation: Air carrier
- Aircraft: [N310SA](https://openairdocs.org/aircraft/N310SA), registered now
- Make and model: Cessna 310R
- Registry model: [Cessna 310R](https://openairdocs.org/model/cessna-310r) (OpenAirDocs)
- Aircraft serial: 310R1565
- Engine: Cont IO520*
- System (JASC): [5510 · Horizontal Stabilizer Structure](https://openairdocs.org/jasc/5510)
- Part: Bolt
- Part number: AN56A
- Condition: Sheared
- Location: Horizontal Stab
- 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/7AA2008F00000

## Discrepancy

WHILE PREPARING AIRCRAFT FOR HORIZONTAL STABILIZER REMOVAL, THE 4 BOLTS THAT ATTACH THE HORIZONTAL STABILIZER TO THE AFT FUSELAGE ALL SHEARED WITH MINIMAL EFFORT WHEN THEY WERE BEING REMOVED.  THERE ARE STANDARD AIRCRAFT BOLTS, AN5-6A.  (K)

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