What was found
(CAN) EXCESSIVE DAMAGE TO SPLINES OF ADAPTER AND INNER SPLINES OF THE COMPRESSOR TO TURBINE COUPLING SHAFT. IN SOME CASEA SPLINE TOOTH IS COMPLETELY SHEARED OFF.
- Difficulty date
- May 2, 2000
- Submitted
- January 19, 2001
- Operation
- General aviation
- Engine
- Allsn 250C20B
- System (JASC)
- 7250 · Turbine Section
- Part
- Adapter
- Part number
- 689784
- Condition
- Damaged
- Location
- Outer Spline
- Part time
- 323 hours
- 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.