What was found
BLADE SEPARATION FROM 3RD STAGE COMPRESSOR WHEEL, FATIGUE FAILURE.
- Difficulty date
- September 10, 2010
- Submitted
- January 4, 2011
- Operation
- Air carrier
- Make and model
- Bell 206B
- Aircraft time
- 11,748 hours
- Engine
- Allsn 250C20
- System (JASC)
- 7230 · Turbine Engine Compressor Section
- Part
- Compressor Blade
- Part number
- 23060432
- Condition
- Separated
- Location
- 3rd Stage
- Part time
- 10,780 hours
- Stage of operation
- CL
- How discovered
- O
- Nature of condition
- R
- Precautionary procedure
- A
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.