1 fatality

Single-Engine Airplane Crashes After Takeoff from Nikiski Airfield (N6469H)

Nikiski, United States of AmericaTakeoff (climb)

On August 7, 1979, a Cessna 207 Skywagon/Stationair (registration N6469H) operated by Butler Aviation was involved in an aviation accident near Nikiski, United States of America during takeoff. One person was killed. Investigators recorded the probable cause as: Engine failure during initial climb and subsequent collision with trees due to powerplant failure for undetermined reasons. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A).

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 2026-06-12Data APIEditorial standards

A single-engine airplane failed to gain height after takeoff from Nikiski Airfield, struck trees, and crashed in flames. The pilot was killed and another occupant seriously injured. Investigation cited engine failure and multiple contributing factors.

Accident

A single-engine airplane departed from Nikiski Airfield. Shortly after takeoff, it failed to gain altitude, struck trees, and crashed in a wooded area. The impact resulted in a fire. The pilot was killed, and the second occupant sustained serious injuries.

Investigation

The official investigation examined the circumstances surrounding the accident. The aircraft had been loaded 340 lbs over its maximum takeoff weight. The runway was described as set and soft. The pilot had not used the flaps correctly or had failed to use them, and preflight preparation was deemed inadequate. The aircraft encountered high obstructions during departure. A momentary power reduction occurred before the collision.

Probable Cause

The probable cause of the accident was engine failure during initial climb and subsequent collision with trees due to powerplant failure for undetermined reasons. Contributing factors included: failed to see and avoid objects or obstructions, inadequate preflight preparation, misused or failed to use flaps, set and soft runway, improperly loaded aircraft, high obstructions, momentary power reduction, and 340 lbs over maximum takeoff weight.