What was found
ENGINE REMOVED DUE TO TURBINE OVERHAUL. UPON INSPECTION OF TURBINE PARTS NOTED THE FOLLOWING: MINOR SULFIDATION ON 1ST STAGE WHEEL BLADES. SCRAPPED 1ST STAGE WHEEL.
- Difficulty date
- May 4, 1995
- Submitted
- March 26, 2000
- Operation
- General aviation
- Aircraft
- N3905B
- Make and model
- Bell 206L1
- Aircraft serial
- 45598
- Engine
- Allsn 250C28B
- System (JASC)
- 7250 · Turbine Section
- Part
- Wheel
- Part number
- 6895801
- Condition
- Sulfidation
- Location
- 1st Stage Blade
- Part time
- 1,216 hours
- Component
- 23031899
- 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.