What happened
On July 26, 2008, a Bell 206L-3 helicopter was conducting sightseeing flights for a corporate anniversary at an industrial site in Westendorf, Germany. The aircraft was performing its fifth flight of the day, carrying seven occupants, including two pilots.
At approximately 14:47 local time, the helicopter lifted off from a turnaround area surrounded by harvested grain fields. During the takeoff, the aircraft rotated 180 degrees to the left while still in a low hover. As the crew transitioned from a stationary hover to forward flight, the aircraft experienced a loss of lift. Due to a pre-existing left lateral tilt and the low altitude of the hover, the front of the left skid made contact with the ground. This contact triggered a dynamic rollover, causing the helicopter to capsize onto its right side. The tail boom separated from the fuselage, and the rotor head was torn from the mast. All seven occupants were able to exit the wreckage on their own; however, one person sustained serious injuries and two others sustained minor injuries. The aircraft was destroyed.
The investigation
The BFU examined the wreckage and analyzed video footage of the accident and preceding flights. The investigation confirmed that the aircraft was properly maintained, with its last annual inspection completed in February 2008. The takeoff weight and center of gravity were found to be within permissible limits, and no technical malfunctions were identified in the flight controls or engine systems. The investigation also reviewed meteorological data, noting visibility of over 10 km and a light wind from 100 degrees.
Findings
- The primary cause of the accident was a pilot error during the transition from hover to forward flight.
- The pilot failed to provide sufficient power to compensate for the loss of lift during the transition from ground effect to forward flight.
- The presence of a left crosswind, combined with the lateral thrust from the tail rotor, required the pilot to maintain a left bank to prevent drifting right.
- The low altitude maintained during the initial hover and the rapid nature of the takeoff procedure contributed to the skid making ground contact.