# SDR AU000815

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: September 12, 2000
- Submitted: October 3, 2000
- Operation: General aviation
- Make and model: Cessna U206B
- Registry model: [Cessna U206B](https://openairdocs.org/model/cessna-u206b) (OpenAirDocs)
- Engine: Cont IO520A
- Propeller: Mcauly D3A34C404
- System (JASC): [5711 · Wing Spar](https://openairdocs.org/jasc/5711)
- Part: Angle
- Part number: 07214003
- Condition: Corroded
- Location: Wing Spar Struct
- Part time: 12,154 cycles
- Component: Wing Spar Struct
- 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/AU000815

## Discrepancy

(AUS) LEFT WING UPPER SPAR CAP ANGLE CONTAINED EXFOLIATION CORROSION.  (X)

---
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.
