What was found
AXIAL BLADE SEPARATION AT BLADE ROOT AREA - ENGINE FAILURE. INVESTIGATION ONGOING. CORRECTIVE ACTION IN PROGRESS.
- Difficulty date
- March 26, 1998
- Submitted
- March 26, 2000
- Operation
- General aviation
- Engine
- Lyc LTS101650B1
- System (JASC)
- 7230 · Turbine Engine Compressor Section
- Part
- Axial Rotor
- Part number
- 410100641
- Condition
- Separation
- Location
- Blade Root
- Part time
- 787 hours
- Component
- 410102050
- 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.