What was found
THE REPORT SUGGEST THAT THE LPT3 BLADE HAD FRACTURED IN HIGH CYCLE FATIGUE THAT HAD PROPAGATED FROM AN INTERGRANULAR CRACK ON THE AIRFOIL T/E.
- Difficulty date
- September 9, 2009
- Submitted
- March 5, 2010
- Operation
- General aviation
- Engine
- Rroyce TAY65015
- System (JASC)
- 7250 · Turbine Section
- Part
- Turbine Blades
- Part number
- JR28904
- Condition
- Fractured
- Location
- Engine
- Stage of operation
- IN
- How discovered
- 9
- Nature of condition
- O
- Precautionary procedure
- K
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.