What was found
(CAN) ENGINE UNABLE TO ACHIEVE TAKEOFF POWER/TORQUE DUE TO BLEED VALVE NOT CLOSING FULLY. COMPRESSOR BLEED VALVE DIAPHRAM FOUND RUPTURED.
- Difficulty date
- March 14, 2005
- Submitted
- May 2, 2005
- Operation
- General aviation
- Make and model
- Beech C90
- Aircraft time
- 8,294 hours
- Engine
- Pwa PT6A21
- Propeller
- Hartzl HCB3TN3
- System (JASC)
- 7532 · Compressor Bleed Valve
- Part
- Diaphragm
- Part number
- 310082903
- Condition
- Ruptured
- Location
- Bleed Valve
- Stage of operation
- TO
- How discovered
- O
- Nature of condition
- O
- Precautionary procedure
- C
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.