What was found
(CAN) DURING TAKEOFF ROLL, THE ENGINE LOST POWER. TAKEOFF WAS ABORTED AND AC RETURNED TO THE RAMP. INVESTIGATION BY MFG REVEALED FRACTURED COMPRESSOR TURBINE BLADES AND A FRACTURED FUEL BYPASS LINE. (TC NR 20080116016)
- Difficulty date
- November 26, 2007
- Submitted
- January 21, 2008
- Operation
- General aviation
- Make and model
- Dhav DHC6300
- Engine
- Pwa PT6A27
- System (JASC)
- 7250 · Turbine Section
- Part
- Turbine Blades
- Condition
- Fractured
- Location
- Engine
- Stage of operation
- TO
- How discovered
- O
- Nature of condition
- R, J
- Precautionary procedure
- C, E, D
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.