What was found
AXIAL CRACK 30CM LONG BEGINNING IN A HOLE AFTER THE THREAD AND GOING FROM THE REAR OF THE SHAFT AND DEFORMATION OF THE SHAFT. PARTS CURRENTLY UNDER SNECMA/CFMI INVESTIGATION.
- Difficulty date
- January 12, 1997
- Submitted
- March 26, 2000
- Operation
- General aviation
- Engine
- Ge CFM565A
- System (JASC)
- 7250 · Turbine Section
- Part
- Shaft
- Part number
- 3360097040
- Condition
- Cracked
- Location
- Lpt
- Part time
- 2,365 hours
- 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.