What was found
(CAN) THE NR4 ENGINE SHUTDOWN DURING THE TAKEOFF ROLL AT ABOUT 90 KNOTS. INSPECTION REVEALED 16 SECOND STAGE BLADES HAD FRACTURED.
- Difficulty date
- September 9, 1997
- Submitted
- March 26, 2000
- Operation
- General aviation
- Engine
- Pwa PT6A66
- System (JASC)
- 7250 · Turbine Section
- Part
- Blades
- Condition
- Fractured
- Location
- 2nd Stage
- Part time
- 1,437 hours
- Stage of operation
- TO
- Nature of condition
- Y
- Precautionary procedure
- O
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.