No fatalities

Touch-and-Go Landing Ends with Engine Failure and Off-Airport Landing (G-OFRL)

Bournemouth-Hurn, United KingdomTakeoff (climb)

On May 15, 1984, a Cessna 414 Chancellor (registration G-OFRL) operated by Flight Refuelling was involved in an aviation accident near Bournemouth-Hurn, United Kingdom during takeoff. No fatalities were reported. Investigators recorded the probable cause as: A safe climb out could not be achieved following the complete loss of power from one engine just when the aircraft became airborne at a speed of about 80 knots with full flap extended. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A); 2 related events involving the same aircraft type or operator are linked below.

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 2026-06-11Data APIEditorial standards

During a touch-and-go landing training exercise, the aircraft suffered a complete loss of power on one engine after rotation with full flaps, leading to an off-airport landing with no injuries.

Incident Description

During a training flight, the crew performed a touch-and-go landing on Runway 17. The final approach was described as steep, flown with full (45°) flap. After a short ground roll, the pilot under training advanced the throttles and rotated the aircraft at about 80 knots, with the flaps still at the full 45-degree setting.

Sequence of Events

Shortly after becoming airborne, a loss of power occurred, accompanied by vibration or buffeting. The aircraft yawed and rolled to the right, and airspeed began to decay. The pilot under training then retracted the flaps to 30°, at which point the instructor took control, closed the throttles, and landed the aircraft on the grass on a heading of approximately 200° magnetic.

The aircraft continued across the southwestern taxiway, through the airfield perimeter fence, across a public road, where the undercarriage collapsed, and finally came to rest in an adjacent field. Both fuel tanks were ruptured by impact with fence posts, but there was no fire.

Outcome

The crew, who were uninjured, shut off the fuel cocks, switched off the electrical systems, and vacated the aircraft through the main entry door. Emergency services responded quickly and arrived at the scene by the time the crew exited the aircraft.

Probable cause

A safe climb out could not be achieved following the complete loss of power from one engine just when the aircraft became airborne at a speed of about 80 knots with full flap extended. The commander was therefore left with no alternative but to land whilst it was still possible to control the aircraft.