What was found
(CAN) POWER LOSS/IFSD UPON APPLYING POWER FOR T/O, A LOUD NOISE WAS HEARD. THE ENGINE WAS SHUTDOWN AND THE ACFT TAXIED BACK TO THE GATE. POST EVENT INSPECTION REVEALED THAT THE FRACTURE OF THE 2ND STAGE POWER TURBINE BLADES.
- Difficulty date
- April 19, 2011
- Submitted
- September 14, 2015
- Operation
- General aviation
- Make and model
- Cndair CL6002D24
- Engine
- Pwa PT6A67D
- System (JASC)
- 7250 · Turbine Section
- Part
- Blades
- Condition
- Fractured
- Location
- Turbine
- Stage of operation
- TO
- How discovered
- O
- Nature of condition
- Z
- Precautionary procedure
- E, C
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.