Single-engine fatal accident involving DHC-6 Twin Otter

1 fatality • Washington-Dulles, United States of America • Takeoff (climb)

A de Havilland Canada DHC-6 Twin Otter crashed during its initial climb following a maintenance inspection, resulting in one fatality.

What happened

Following a recent maintenance inspection, a DHC-6 aircraft departed on its first flight. During the takeoff roll on runway 19L, observers noted that the flaps were in the full down position. Shortly after liftoff, the aircraft entered an extremely steep climb, reaching a pitch attitude of approximately 60 degrees. As the plane reached an altitude between 200 and 500 feet, it experienced a stall and began a nose-down descent while executing a left turn. The aircraft impacted the ground roughly 2000 feet beyond the runway and 300 feet to the left of the centerline. The pilot, who was the only person on board, was killed in the crash.

Findings

Investigations into the accident identified several critical errors regarding aircraft configuration and pilot performance. Post-accident examination confirmed that the flaps remained in the full down position, a setting that is explicitly prohibited for takeoff according to the flight manual; the manual instead prescribes a 10-degree setting. Additionally, evidence indicated that the flight control lock may have been engaged during the takeoff phase, restricting necessary control movements. The investigation also noted that the pilot's checklist was found at the beginning of the takeoff sequence, suggesting it was not properly utilized. Contributing factors included the failure to adjust the flaps, inattention to procedures, and the failure to remove the gust lock.

Probable cause

The accident was caused by an improper flap configuration and the likely presence of a flight control lock, which led to an excessive pitch attitude and a subsequent stall.

Frequently asked questions

What happened in the 1988-07-20 De Havilland DHC-6 Twin Otter accident near Washington-Dulles, United States of America?

A de Havilland Canada DHC-6 Twin Otter crashed during its initial climb following a maintenance inspection, resulting in one fatality.

Were there any fatalities in the 1988-07-20 De Havilland DHC-6 Twin Otter accident?

The accident was fatal, resulting in 1 fatality.

What aircraft was involved and where did it happen?

The accident on 1988-07-20 involved a De Havilland DHC-6 Twin Otter, registration N7267, operated by Fairways Corporation, at Washington-Dulles, United States of America.

What was the probable cause of the accident?

The accident was caused by an improper flap configuration and the likely presence of a flight control lock, which led to an excessive pitch attitude and a subsequent stall.

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