# SDR AU000449

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: June 5, 2000
- Submitted: July 4, 2000
- Operation: General aviation
- Make and model: Cessna 208B
- Registry model: [Cessna 208B](https://openairdocs.org/model/cessna-208b) (OpenAirDocs)
- System (JASC): [5320 · Fuselage Miscellaneous Structure](https://openairdocs.org/jasc/5320)
- Part: Bracket
- Part number: 26111446
- Condition: Failed
- Location: Fuselage
- Part time: 4,215 cycles
- Component: Fuselage Miscell, Cessna
- Stage of operation: DE
- How discovered: O
- Nature of condition: F
- Precautionary procedure: O
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/AU000449

## Discrepancy

(AUS) FLAP MOTOR SUPPORT BRACKETS PN 2611144-6 AND PN 2611144-7 TORN FROM FUSELAGE STRUCTURE.

---
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.