# SDR AUS20020012

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: January 2, 2002
- Submitted: February 5, 2002
- Operation: General aviation
- Make and model: Piper PA-36-285
- Registry model: [Piper PA-36-285](https://openairdocs.org/model/piper-pa-36-285) (OpenAirDocs)
- Engine: Pwa PT6A20
- Propeller: Hartzl HCB3TN3
- System (JASC): [5510 · Horizontal Stabilizer Structure](https://openairdocs.org/jasc/5510)
- Part: Bolt
- Part number: 9735500
- Condition: Cracked
- Location: Horizontal Stab
- Component: Horizontal Stab, Piper, LIFTSTRUT
- 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/AUS20020012

## Discrepancy

(AUS) TAILPLANE LIFT STRUT CLEVIS BOLT CRACKED IN AREA OF FIRST THREAD ON THE HEAD END OF THE BOLT.

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.
