9 fatalities

2021-07-08: De Havilland DHC-2 Beaver (SE-KKD) — Kalle David Flyg — Örebro, Sweden

Örebro, SwedenTakeoff (climb)

On July 8, 2021, a De Havilland DHC-2 Beaver (registration SE-KKD) operated by Kalle David Flyg was involved in an aviation accident near Örebro, Sweden during takeoff. 9 people were killed. Investigators recorded the probable cause as: Control of the aircraft was likely lost in connection with the wing flaps being retracted in a situation where the stick forces were high due to an abnormal elevator trim position, while the aircraft was unstable due to being tail-heavy and abnormally… This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A).

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781190006Data APIEditorial standards

A parachute jump flight crashed after a steep descending turn, killing all nine on board. The probable cause included flap retraction, abnormal trim, tail-heavy condition, and multiple safety slips.

Flight Details

The flight was intended to drop eight parachutists from an altitude of 1,500 metres. It was the twelfth and planned final flight of the day. Weather conditions were good. The parachutist bench to the right of the pilot had been replaced with a pilot's seat to distance the parachutists from the pilot as a Covid-19 precautionary measure. The pilot had no ability to perform a mass and balance calculation with the available information.

Accident Sequence

After take-off, the aircraft climbed to an altitude of 400 to 500 feet above ground before changing course 180 degrees to the left. The aircraft turned around quickly in a descending turn with a high bank angle. During the final phase, the aircraft dived steeply and then slightly levelled off before impact. Upon impact, the landing gear was teared off, after which the aircraft skidded on its belly 48 metres straight ahead and caught fire. All nine persons on board sustained fatal injuries.

Probable Cause

Control of the aircraft was likely lost in connection with the wing flaps being retracted in a situation where the stick forces were high due to an abnormal elevator trim position, while the aircraft was unstable due to being tail-heavy and abnormally trimmed. The low altitude was not sufficient to regain control of the aircraft. The cause of the accident was that several safety slips occurred in the operation, which resulted in that the safety margin was too small for a safe flight.