What was found
(CAN) SUSPECT POSSIBLE SEPARATION OF FIRST STAGE STATOR BLADES CAUSING EXTENSIVE DAMAGE TO COMPRESSOR AND TURBINE AND ENGINE FAILURE. PART TC: 6,604.
- Difficulty date
- July 4, 1996
- Submitted
- March 26, 2000
- Operation
- Air carrier
- Make and model
- Bell 206B
- Engine
- Allsn 250C20
- System (JASC)
- 7230 · Turbine Engine Compressor Section
- Part
- Compressor
- Part number
- 6853337
- Condition
- Cracked
- Location
- Axial Stage
- Part time
- 10,269 hours
- Stage of operation
- IN
- Nature of condition
- O
- Precautionary procedure
- K
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.