BAe 125

On the day of the accident the aircraft left Bristol under the command of the company's chief pilot for a flight to Edinburgh via East Midlands Airport. After conveying passengers to Edinburgh it was scheduled to position empty at Newcastle Airport to collect passengers for Bristol. Weather briefing had been obtained and a thorough flight plan covering the outward and return flights had been filed before the aircraft left Bristol in the morning. As there were no passengers on the flight from Edinburgh to Newcastle, the captain decided to make use of this sector to continue the other pilot's training for command of the HS-125. Accordingly, the trainee captain was flying the aircraft from the left hand seat. Prior to takeoff he was briefed that a failure of one of the engines (he was not told which one), would be simulated on takeoff and for the purpose of the exercise the rudder bias system would be switched 'OFF'. The pilots decided that no flap would be used for the takeoff which was started from the end of runway 13. The point where the aircraft became airborne was approximately 2,700 feet from the start of the roll, which was normal for the aircraft's weight and configuration, with both engines operating. The training captain called 'rotate' at approximately 120 knots, which was slightly faster than the calculated figure and when the aircraft had reached a height of approximately 12 feet and had accelerated to about 130 knots, he pulled back the thrust lever of the port engine to simulate a failure. He considered that the trainee pilot's reaction to the emergency was slow and was just about to apply right rudder to counteract the yaw when the trainee pilot applied considerable force to the left rudder and locked his leg in position. The captain immediately applied full right aileron and opened the port thrust lever but he was unable to prevent a high rate of roll developing to the left. Approximately 700 feet after the point where the aircraft became airborne the port wing tip struck the runway, fracturing the port fuel tank and spilling out fuel. The aircraft left the runway at an angle of approximately 30 degrees to the left and travelled across the grass, becoming partially inverted before settling back sideways on the ground on its undercarriage. The sideways movement of the aircraft pulled off the nose gear and the aircraft then gyrated across the airfield sustaining further structural damage before coming to rest on its main wheels and tail facing approximately in the opposite direction to the direction of takeoff. During the aircraft's gyrations on the ground, fuel, which was centrifuged out of the fractured port tank, ignited and a flash fire occurred. When the aircraft finally came to rest there was a small residual fire in the port wing which was very quickly extinguished by the airport fire service.

The twin engine aircraft departed Churchill Falls Airport at 1800LT on a flight to Montreal with an intermediate stop in Wabush (Labrador City). On final approach, the crew encountered poor weather conditions and failed to realize his altitude was insufficient. Out of track, the airplane struck trees then crashed on a mountainous terrain located few km from the airport. The controller at Wabush Airport informed Moncton ATC about the disappearance of the aircraft and SAR operations were initiated. All eight occupants were killed, among them Donald J. McParland, President of Churchill Falls (Labrador) Corporation, his assistant John Lethbridge, Eric Lambert and three employees of the Acres Canadian Bechtel.

The crew was engaged in a local training flight at Luton Airport. Shortly after takeoff with an engine voluntarily shut down, the airplane went out of control and crashed in flames onto a factory near the airport. The aircraft was destroyed and both crew were killed while no one on the ground was injured.

The pilot departed Miami on a private flight to Freeport with his spouse on board. He did not file any flight plan and failed to ask for a copilot. During a night approach to Freeport Airport, in dark night, the twin engine airplane struck the water surface and crashed into the sea about 7,2 km short of runway, off Pinder Point. The pilot was seriously injured while the passenger's body was not recovered.

The airplane departed Cannes at 1645LT bound for Nice and the crew was supposed to perform three low pass over the Airport of Nice-Côte d'Azur during a local Airshow. The first path was performed at low height over the runway. The crew then completed a turn to the right in an attempt to make a second low pass but on the opposite direction. Doing so, the airplane climbed to an altitude of 2,000 feet when control was lost. It went into a dive, caught fire in the air and crashed in flames into the sea some 1,5 km southwest of the airfield. The aircraft was destroyed and both pilots were killed.

During the takeoff roll, the pilot-in-command attempted to rotate when an unexpected situation was encountered. The captain decided to abort the takeoff and started an emergency braking procedure. Unable to stop within the remaining distance, the airplane overran and struck ditches before coming to rest in a field. While all four passengers were unhurt, both pilots were seriously injured. The aircraft was written off.