Aircraft crash near takeoff site results in one fatality

1 fatality • Östersund, Sweden • Takeoff (climb)

A twin-engine aircraft stalled and crashed shortly after departing runway 30, leading to one death and three injuries.

What happened

During the initial climb phase of flight, a twin engine aircraft experienced a loss of control while at an altitude of approximately 100 feet. After departing from runway 30, the aircraft entered a left bank and subsequently stalled. This maneuver caused the left wing to make contact with the terrain.

Following the wing strike, the aircraft became uncontrollable and impacted a wooded area situated roughly 100 meters from the initial point of contact, resulting in a post-crash fire. The accident resulted in one fatality involving the pilot, while the three passengers on board sustained injuries.

Findings

Investigations into the accident determined that the primary factor leading to the stall was the incorrect flap configuration during the takeoff sequence.

Probable cause

The aircraft stalled due to an improper flap setting during the takeoff procedure.

Frequently asked questions

What happened in the 1953-01-09 Beechcraft 18 accident near Östersund, Sweden?

A twin-engine aircraft stalled and crashed shortly after departing runway 30, leading to one death and three injuries.

Were there any fatalities in the 1953-01-09 Beechcraft 18 accident?

The accident was fatal, resulting in 1 fatality.

What aircraft was involved and where did it happen?

The accident on 1953-01-09 involved a Beechcraft 18, registration 007, operated by Swedish Air Force - Flygvapnet, at Östersund, Sweden.

What was the probable cause of the accident?

The aircraft stalled due to an improper flap setting during the takeoff procedure.

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