What was found
(CAN) EIR PT6A 2009-030 FIRST STAGE COMPRESSOR BLADE FAILURE.
- Difficulty date
- April 20, 2009
- Submitted
- June 16, 2009
- Operation
- General aviation
- Engine
- Pwa PT6A41
- System (JASC)
- 7230 · Turbine Engine Compressor Section
- Part
- Blades
- Condition
- Damaged
- Location
- Compressor
- Stage of operation
- NR
- How discovered
- 9
- Nature of condition
- O
- Precautionary procedure
- O
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.