Probable cause
The total loss of engine power due to a fracture in the oil filter adapter housing. Contributing to the accident was the lack of suitable terrain for the forced landing.
NTSB analysis
While in cruise flight the propeller's rpms unexpectedly increased to approximately 2,900. After an attempt to reduce the rpms via the propeller governor failed, the pilot was successful by reducing the engine throttle. Seconds later the engine began to make a "knocking noise" before complete engine power was lost. The pilot performed a forced landing to a rough field, resulting in a hard landing. The pilot was able to exit the airplane unassisted. Moments later the airplane caught fire and was fully engulfed in flames. An examination of the engine revealed that the oil filter adapter housing contained a fracture that allowed the engine oil to escape, resulting in oil starvation and a subsequent engine seizure. Reportedly this was the first flight since the airplane's annual inspection and the last oil filter change. Due to thermal damage to the oil filter adapter and oil filter, the reason for the fractured oil filter adapter could not be determined.
Text from the NTSB. Open the NTSB docket for CEN09LA014 for the full record.
Event
- Date
- Oct 8, 2008
- Type
- Accident
- Place
- Houston, Texas
- Highest injury
- None
- Weather
- Visual (VMC)
- Light
- Night, dark
Beech A36
- N-number
- N703KP
- Category
- Airplane
- Damage
- Destroyed
- Operating rule
- Part 91 (general aviation)
- Purpose of flight
- Personal
From the NTSB aviation accident database: N-registered aircraft, events since 2008, data through Oct 28, 2026. The file is published monthly, so the latest weeks are incomplete and recent records can change. The official source is the NTSB aviation investigation search. CheckAero is independent and not affiliated with the NTSB.