No fatalities

Twin Otter Accident at Flotta, Orkney (G-STUD)

Flotta, United KingdomLanding (descent or approach)

On April 20, 1983, a De Havilland DHC-6 Twin Otter (registration G-STUD) operated by Air Ecosse was involved in an aviation accident near Flotta, United Kingdom during landing or approach. No fatalities were reported. Investigators recorded the probable cause as: The accident was caused by a loss of control, shortly after touchdown, following a strong lateral gust which was in excess of the maximum cross-wind capability of the aircraft. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A).

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary report: the UK Air Accidents Investigation Branch (AAIB)Updated 2026-09-03Data APIEditorial standards

A Twin Otter lost control after landing at Flotta in Orkney due to a strong lateral gust exceeding its crosswind limits. All 12 occupants escaped uninjured, but the aircraft was destroyed.

Approach and Landing Conditions Strong winds were reported at Flotta as the Twin Otter approached Orkney Island. The aircraft first contacted the airport at 11:56 and was informed that the surface wind was indicating 260°/26 knots. The pilot elected to make a straight-in approach to runway 35, preferring the crosswind to come from the left so that the left main wheel could be seen onto the runway. ## Loss of Control After Touchdown The aircraft touched down with the left main wheel first, followed by the right main wheel. As the nosewheel touched, the commander selected reverse thrust from the propellers. An audible stall warning sounded momentarily at touchdown. Shortly after reverse thrust was selected and achieved, the left wing began to rise. The captain applied full left wing-down aileron and full left rudder, then cancelled reverse thrust from the right-hand propeller and increased forward power on that engine. These actions were unable to prevent the left wing from rising further. ## Crash Sequence The right-hand wingtip contacted the ground, causing the aircraft to yaw to the right. It then fell back momentarily onto the main wheels before cartwheeling through an aerodrome boundary fence. The aircraft came to rest on its left side, with both wings detached. All 12 occupants escaped uninjured, while the airplane was damaged beyond repair.

Probable cause

The accident was caused by a loss of control, shortly after touchdown, following a strong lateral gust which was in excess of the maximum cross-wind capability of the aircraft. The lack of accurate surface wind information at the runway threshold was a contributory factor.

Frequently asked questions

What happened in the 20 Apr 1983 De Havilland DHC-6 Twin Otter accident near Flotta, United Kingdom?

A Twin Otter lost control after landing at Flotta in Orkney due to a strong lateral gust exceeding its crosswind limits. All 12 occupants escaped uninjured, but the aircraft was destroyed.

Were there any fatalities in the 20 Apr 1983 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 20 Apr 1983 involved a De Havilland DHC-6 Twin Otter, registration G-STUD, operated by Air Ecosse, at Flotta, United Kingdom.

What was the probable cause of the accident?

The accident was caused by a loss of control, shortly after touchdown, following a strong lateral gust which was in excess of the maximum cross-wind capability of the aircraft. The lack of accurate surface wind information at the runway threshold was a contributory factor.