What was found
(CAN) ON TAKE-OFF ROLL, THE ENGINE SURGED, ACCOMPANIED BY FLAMES EMITTED FROM THE EXHAUST. SUBSEQUENT INVESTIGATION DETERMINED THE COMPRESSOR BLEED VALVE CLOSING POINT TO BE OUT OF LIMITS. THE BOV WAS REPLACED.
- Difficulty date
- September 22, 2005
- Submitted
- November 1, 2005
- Operation
- General aviation
- Make and model
- Pilats PC7
- Engine
- Pwa PT6A25
- System (JASC)
- 7532 · Compressor Bleed Valve
- Part
- Bleed Valve
- Condition
- Out Of Limits
- Location
- Compressor
- Stage of operation
- TO
- How discovered
- O
- Nature of condition
- D, J
- Precautionary procedure
- C
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.