# SDR AU961207

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: January 19, 1996
- Submitted: March 26, 2000
- Operation: General aviation
- Make and model: Saab 340B
- Registry model: [Saab 340B](https://openairdocs.org/model/saab-340b) (OpenAirDocs)
- Engine: Ge CT79B
- Propeller: Rotol R3754123F21
- System (JASC): [7230 · Turbine Engine Compressor Section](https://openairdocs.org/jasc/7230)
- Part: Compressor
- Part number: 6058T86G01
- Condition: Fod
- Location: Turbine Engine
- Component: Ge, CT79B
- Stage of operation: CR
- Nature of condition: R
- Precautionary procedure: E, C
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/AU961207

## Discrepancy

(AUS) LH ENGINE COMPRESSOR DAMAGED DUE TO FOD - INSPECTION FOUND ONE 1ST STAGE BLADE BENT FORWARD AND SEVERAL OTHER BLADES DAMAGED -SUSPECT DUE TO ICE INGESTION - MID FRAME DESWIRL CONE RING ALSO  CRACKED AND DAMAGED

---
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.