1 fatality

Pilot Killed in Single-Engine Airplane Crash After Takeoff from Lake Hood (N90574)

Anchorage-Lake Hood, United States of AmericaTakeoff (climb)

On May 21, 1975, a De Havilland DHC-3 Otter (registration N90574) operated by Woods Air Service - Woods Air Fuel was involved in an aviation accident near Anchorage-Lake Hood, United States of America during takeoff. One person was killed. Investigators recorded the probable cause as: Inadequate preflight preparation on part of the pilot. The following contributing factors were reported: - Failed to maintain flying speed, - Lack of familiarity with aircraft, - Improperly loaded aircraft, - Incorrect trim setting, - Aircraft at least 484… This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A); 3 related events involving the same aircraft type or operator are linked below.

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

A single-engine airplane crashed shortly after takeoff from Anchorage-Lake Hood, striking a lumber stack and fence before crashing into a parking lot. The pilot, the sole occupant, was killed. The aircraft was overloaded by at least 484 lbs.

Accident Summary

A single-engine airplane crashed shortly after takeoff from the gravel airstrip at Anchorage-Lake Hood, Alaska. The pilot, who was the sole occupant, was killed in the accident. The aircraft encountered difficulties gaining altitude after departure, striking a lumber stack and a fence before crashing in flames onto a parking lot. Five cars were damaged in the crash. The flight was en route to Aniak on a cargo mission.

Probable Cause and Contributing Factors

According to official findings, the probable cause of the accident was the pilot's inadequate preflight preparation. The investigation reported several contributing factors: failure to maintain flying speed, lack of familiarity with the aircraft, improperly loaded aircraft, incorrect trim setting, and the aircraft being at least 484 pounds over its maximum gross weight.