What was found
ENGINE REMOVED DUE TO CRACKED EXHAUST COLLECTOR. COMPRESSOR REPAIRED DUE TO BROKEN VANE STUD. INSPECTION OF COMPRESSOR PARTS REVEALED STEP WEAR IN EXCESS OF NO-GO GAUGE LIMITS ON AFT END SPLINES. INSTALLED A NEW SPUR GEAR SHAFT.
- Difficulty date
- May 19, 1999
- Submitted
- March 26, 2000
- Operation
- General aviation
- Aircraft
- N2133X
- Make and model
- Bell 206L1
- Aircraft serial
- 45634
- Engine
- Allsn 250C28B
- System (JASC)
- 7230 · Turbine Engine Compressor Section
- Part
- Adapter
- Part number
- 23056634
- Condition
- Worn
- Location
- Spur Gear
- Part time
- 676 hours
- Component
- 23033193
- 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.