Loss of directional control during the take-off roll led to a runway excursion and a landing gear collapse in the runway safety zone.
On final approach for runway 10R, deviations from standard operating procedures led to aircraft collision with the localizer antenna mast system for runway 28L.
Following an aborted take-off the pilot attempted to bring the glider back for landing at the runway. During the final turn towards the runway, the left wing stalled, and the glider entered a spin fro ...
After disconnecting from the tow aircraft, the pilot deployed the speed brakes and felt the curtains close (disillusioned). The glider crashed approximately 240 m short of Gørløse (EKGL) runway 28 thr ...
On approach to Vamdrup (EKVD), two aircraft flew on conflicting opposite tracks at approximately same altitude leading to a risk of collision.
During landing, approximately 5 meters above the runway, the flap handle released from a positive flap position and moved to a negative flap position.
During the landing roll on runway 07, the left wing of the glider collided with the rudder of a parked glider.
During the start-up sequence of engine no. 2, a breaker bar and a socket ejected from the MR head, and the breaker bar penetrated the leading edge of a moving rotor blade.
During a sling operation, the loss of pilot external visual cues led to pilot spatial disorientation and partly loss of control of the helicopter.
During the landing roll on a private grass airstrip, the left main landing gear collapsed, and the pilot lost directional control (in Danish only).