# SDR 2024FA0000897

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: March 25, 2023
- Submitted: November 27, 2024
- Operation: General aviation
- Aircraft: [N80GE](https://openairdocs.org/aircraft/N80GE), registered now
- Make and model: Cessna 208B
- Registry model: [Cessna 208B](https://openairdocs.org/model/cessna-208b) (OpenAirDocs)
- Aircraft serial: 208B0585
- Aircraft time: 7,189 hours
- Engine: Pwc PT6A42A
- Engine time: 4,023 hours, 4,668 cycles
- Propeller: Hartzl HCE4N3
- System (JASC): [7230 · Turbine Engine Compressor Section](https://openairdocs.org/jasc/7230)
- Part: Compressor Blade
- Part number: 312313102
- Condition: Fractured
- Location: Zone 400
- Part time: 4,023 hours, 3,049 cycles
- Component: Rotor Assy, Pwc
- Component part number: 305414101
- Stage of operation: CR
- How discovered: O
- Nature of condition: O
- Precautionary procedure: A
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/2024FA0000897

## Discrepancy

CT BLADE SEPARATED FROM ENGINE WITH ENGINE ONLY 3049 HRS AND 3090 CYCLES  SINCE OEM REPAIR ON COMPRESSOR.  AIRCRAFT WAS ON A CROSS COUNTRY FLIGHT OVER MOUNTAINS WHEN CT BLADES SEPARATED.

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