What was found
UPON REMOVAL OF THE COMPRESSOR CASE FOUND 2 6TH STG STATOR VANES MISSING. THE VANES HAD BROKEN OFF NEAR THE BLADE ROOT, AT APPROX THE LEVEL OF THE COMPRESSOR CASE PLASTIC COATING. THE COMPRESSOR CASE HAD BEEN O/H 366.6 HRS PRIOR.
- Difficulty date
- September 2, 2010
- Submitted
- September 17, 2010
- Operation
- General aviation
- Engine
- Allsn 250C20B
- System (JASC)
- 7230 · Turbine Engine Compressor Section
- Part
- Stator Vane
- Condition
- Broken
- Location
- Eng Compressor
- Stage of operation
- IN
- How discovered
- V
- Nature of condition
- O
- Precautionary procedure
- K
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.