Casualties unknown

Hard Landing and Runway Excursion in Chevak, Alaska (N200EH)

Chevak, AK, US

On March 29, 1990, a DE Havilland DHC-6 (registration N200EH) was involved in an aviation accident near Chevak, AK. Investigators recorded the probable cause as: IMPROPER FLARE BY THE PILOT (PIC) DURING THE LANDING/FLARE. THE WEATHER CONDITION WITH FOG WAS A RELATED FACTOR. 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 2026-07-04Data APIEditorial standards

A scheduled flight from Bethel, Alaska, to Chevak landed hard after the pilot did not apply power during a high sink rate. The right main gear separated, damaging the wing strut, and the aircraft veered off the runway.

Flight Details

A scheduled flight departed Bethel, Alaska, with a weather dispatch release. Upon reaching the destination, Chevak, Alaska, the station manager (who was not a certified weather observer) advised the flight crew not to attempt a landing because the weather was not good.

Approach and Landing

According to the flight crew, the fog was not obscuring the runway, and they elected to make an approach. The pilot-in-command (PIC) reported that a high sink rate developed on short final and he did not apply power. He believed the landing flare would have arrested the sink rate. However, the aircraft landed hard on the right main gear.

Damage and Runway Excursion

The hard landing caused the right main gear to separate and damaged the right main wing strut. The right wing settled to the surface, and the aircraft yawed to the right, veered off the runway, and sustained further damage.

Load Manifest Non-Compliance

The load manifest did not comply with 14 CFR Part 135.63(c) or the company's operations manual.

Frequently asked questions

What happened in the 29 Mar 1990 DE Havilland DHC-6 accident near Chevak, AK?

A scheduled flight from Bethel, Alaska, to Chevak landed hard after the pilot did not apply power during a high sink rate. The right main gear separated, damaging the wing strut, and the aircraft veered off the runway.

What aircraft was involved and where did it happen?

The accident on 29 Mar 1990 involved a DE Havilland DHC-6, registration N200EH, at Chevak, AK.

What was the probable cause of the accident?

IMPROPER FLARE BY THE PILOT (PIC) DURING THE LANDING/FLARE. THE WEATHER CONDITION WITH FOG WAS A RELATED FACTOR.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001212X22644. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.