Casualties unknown

1988-07-01: Piper J3 (N6868H) — Rialto, CA

Rialto, CA, US

On July 1, 1988, a Piper J3 (registration N6868H) was involved in an aviation accident near Rialto, CA. Investigators recorded the probable cause as: The engine quit due to a cracked manifold that separated above the carburetor, which led to a forced landing where wind gusts caused the aircraft to leave the road and collide with terrain. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive.

Sourcesthe U.S. National Transportation Safety Board (NTSB) historical archivePrimary reportUpdated 1781061362Data APIEditorial standards

During a local flight, an aircraft experienced engine failure while descending to the airport. The pilot executed a forced landing on a road, but wind gusts caused the plane to ground loop and collide with terrain.

What happened

The incident occurred during a local flight operation. While the aircraft was in the process of descending toward the airport, the engine ceased functioning without warning. The pilot initiated a forced landing procedure, selecting a nearby road as the landing site.

During the landing roll, environmental conditions played a critical role in the outcome. A sudden gust of wind pushed the airplane off the paved surface. As the aircraft left the road, it ground looped violently. This loss of directional control led to a collision with the surrounding terrain, causing the nose section to overturn.

The investigation

Following the accident, investigators conducted a thorough inspection of the aircraft's engine components. The examination focused on identifying the root cause of the sudden power loss. The inspection revealed significant structural failure within the engine assembly. Specifically, the manifold was found to have cracked and separated just above the carburetor. This mechanical failure prevented the engine from operating effectively.

Findings

The primary factor contributing to this accident was mechanical failure of the engine's fuel delivery system. The separation of the manifold above the carburetor directly caused the engine to quit during the descent phase. Additionally, wind gusts exacerbated the situation by pushing the aircraft off the intended landing path during the roll-out. The combination of the sudden power loss and the subsequent loss of control resulted in the ground loop and collision with terrain.

Probable cause

The engine quit due to a cracked manifold that separated above the carburetor, which led to a forced landing where wind gusts caused the aircraft to leave the road and collide with terrain.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001213X26010. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.