What was found
(CAN)ENGINE SHUTDOWN FOLLOWING AN INCREASE IN ITT. AS THE POWER LEVER WAS BEING RETARDED, DRBRIS WAS SEEN TO BE COMING FROM THE EXHAUST. INITIAL REPORT INDICATE THIS TO BE A COMPRESSOR TURBINE BLADE FRACTU RE.
- Difficulty date
- April 3, 1996
- Submitted
- March 26, 2000
- Operation
- General aviation
- Make and model
- Beech B200
- Engine
- Pwa PT6A41
- System (JASC)
- 7250 · Turbine Section
- Part
- Blade
- Condition
- Fractured
- Location
- Comp Turbine
- Part time
- 4,629 hours
- Stage of operation
- CR
- Nature of condition
- Y
- Precautionary procedure
- A
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.