Aircraft accident at Hooper Bay, Alaska

No fatalities • Hooper Bay, United States of America • Landing (descent or approach)

An aircraft sustained substantial damage after crashing short of the runway threshold during an approach to Hooper Bay, Alaska.

What happened

During an approach under visual meteorological conditions, an aircraft crashed while attempting to land on runway 13 at Hooper Bay, Alaska. The impact occurred approximately 1,320 feet before reaching the runway threshold. The plane struck hard-packed snow and ice in a location situated roughly 700 feet from the shoreline of the Bering Sea. While the aircraft suffered substantial damage, no fire was reported following the impact.

The accident resulted in eight individuals—comprising the two pilots and six passengers—sustaining serious injuries.

Findings

Investigations concluded that the primary factor in the accident was the flightcrew's failure to accurately calculate and understand the aircraft's weight and balance. Specifically, the crew operated the aircraft with a center of gravity located significantly behind its permitted limit, which led to a loss of control during the landing sequence.

Probable cause

The flightcrew failed to properly calculate weight and balance, resulting in an aft center of gravity that caused a loss of control during landing.

Frequently asked questions

What happened in the 1982-05-16 De Havilland DHC-6 Twin Otter accident near Hooper Bay, United States of America?

An aircraft sustained substantial damage after crashing short of the runway threshold during an approach to Hooper Bay, Alaska.

Were there any fatalities in the 1982-05-16 De Havilland DHC-6 Twin Otter accident?

No fatalities were recorded in this accident.

What aircraft was involved and where did it happen?

The accident on 1982-05-16 involved a De Havilland DHC-6 Twin Otter, registration N103AQ, operated by Gifford Aviation, at Hooper Bay, United States of America.

What was the probable cause of the accident?

The flightcrew failed to properly calculate weight and balance, resulting in an aft center of gravity that caused a loss of control during landing.

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