What was found
(CAN) COMPRESSOR TURBINE BLADE FRACTURED CAUSING COMPLETE ENGINE FAILURE AT APPROX. 40KNOTS FORWARD AIRSPEED, PILOT CARRIED OUT EMERGENCY LANDING.ENGINE REMOVED FOR EXAMINATION BY PWC.
- Difficulty date
- July 17, 2003
- Submitted
- September 4, 2003
- Operation
- General aviation
- Make and model
- Bell 212
- Aircraft time
- 7,337 hours
- Engine
- Pwa PT6T3
- System (JASC)
- 7230 · Turbine Engine Compressor Section
- Part
- Blade
- Part number
- 3031801
- Condition
- Fractured
- Location
- Compressor
- Stage of operation
- CL
- How discovered
- O
- Nature of condition
- Y, J
- Precautionary procedure
- A
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.