1 fatality

1988-11-01: Cessna 421A Golden Eagle I (N3385Q) — Hubert G. Toll — Cabazon, United States of America

Cabazon, United States of AmericaLanding (descent or approach)

On November 1, 1988, a Cessna 421A Golden Eagle I (registration N3385Q) operated by Hubert G. Toll was involved in an aviation accident near Cabazon, United States of America during landing or approach. One person was killed. Investigators recorded the probable cause as: The pilot's poor decision and misjudgement of distance. The separation of the cylinder, failure of the propeller to feather, and impact with wires and a residence were factors in the accident. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A).

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781214725Data APIEditorial standards

A pilot was killed after losing power in the right engine, attempting an interstate highway landing, and striking electrical transmission lines and a residence. The accident resulted from a fatigued cylinder head and the pilot's poor decisions.

Accident Summary

The pilot of a single-engine aircraft contacted an air route surveillance control (ARSA) controller after losing power in the right engine while flying over an air force base. The controller informed the pilot that his position was near a civilian airport with limited maintenance facilities and an air force base. The pilot stated his intention to continue to a larger civilian airport along his route where maintenance could be obtained. Subsequently, the pilot reported difficulty seeing the ground and an inability to maintain altitude because the propeller did not feather.

Emergency Landing Attempt

The aircraft overflew a small civilian airport, and the pilot informed the unicom operator that he would attempt to land on an interstate highway. After overflying the highway, the aircraft struck an electrical transmission line and then collided with a residence. The pilot, who was the sole occupant, was killed.

Post-Accident Inspection

A post-accident inspection revealed that the right engine's No. 3 cylinder head had fractured, allowing the head to displace outward by 3/8 inch. The fracture resulted from fatigue in the threaded area between the head and the cylinder. Functional testing of the propeller governor after the accident showed it operated normally.

Probable Cause

The official probable cause of the accident was the pilot's poor decision and misjudgment of distance. Contributing factors included the separation of the cylinder, the failure of the propeller to feather, and impact with wires and a residence.