What was found
ENGINE WOULD NOT PRODUCE TAKEOFF POWER AND WOULD HAVE A TORQUE SURGE WITH POWER LEVER IN MAXIMUM POSITION. BOV GUIDE PIN BUSHING WAS FOUND WORN. BOV DIAPHRAGM WAS FOUND TORN. C/W SB 1581 FOR CORRECTIVE ACTION.
- Difficulty date
- January 6, 2000
- Submitted
- March 26, 2000
- Operation
- Air carrier
- Aircraft
- N95NA
- Make and model
- Cessna 208B
- Aircraft serial
- 208B0666
- Engine
- Pwa PT6A114A
- System (JASC)
- 7532 · Compressor Bleed Valve
- Part
- Valve
- Part number
- 312124803
- Condition
- Failed
- Location
- Compressor
- Part time
- 750 hours
- Stage of operation
- NR
- Nature of condition
- O
- Precautionary procedure
- O
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.