FIFE, WA, USA
N8794G
Cessna 150F
The Subaru Legacy powered Cessna 150 experienced a partial loss of engine power about 30 minutes after takeoff. Soon thereafter, the engine lost all power, and the pilot executed a forced landing in a nearby field. Although the touchdown was successful, the nose gear dug into the soft terrain as the pilot applied brakes to stop short of an upcoming ditch. After the nose gear dug into the terrain, the aircraft flipped over onto its back. A teardown of the engine revealed that the head had fractured off one of the exhaust valves in the forward left cylinder, resulting in the destruction of the piston.
On February 24, 1998, approximately 1430 Pacific standard time, an experimental Cessna 150F, N8794G, nosed over during the landing roll following a forced landing after a loss of engine power near Fife, Washington. The private pilot and his passenger were not injured, but the aircraft, which was owned and operated by the pilot, sustained substantial damage. The 14 CFR Part 91 flight, which departed Auburn Municipal Airport, Auburn, Washington, about 30 minutes earlier, was being operated in visual meteorological conditions. No flight plan had been filed, and there was no report of an ELT activation. According to the pilot, the aircraft, which was registered in the Experimental Exhibition category, was powered by a modified Subaru Legacy automobile engine. He said that while demonstrating the aircraft to an acquaintance, the engine experienced a partial power loss. Soon thereafter, the engine lost all power, and the pilot elected to land in a nearby farm field. He said that his touchdown on the soft terrain was successful, but as he applied brakes to stop prior to an upcoming ditch, the nose wheel dug into the soft terrain and the aircraft nosed over. Although the owner, who was the individual that modified the engine for aviation use, was quite sure that a camshaft gear locating pin had failed, an engine teardown revealed that was not the case. Instead, it was found that the head on one of the two exhaust valves in the forward left cylinder had broken off of its stem and fallen into the cylinder. The piston itself had been torn into numerous small pieces and much of it was found laying in the cylinder. The piston pin was still in the end of the connecting rod, but none of the piston was still attached to the pin.
The fracture separation of an exhaust valve head, followed by the total failure of the associated piston. A factor was the soft terrain at the location of the forced landing.
Source: NTSB Aviation Accident Database
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