Casualties unknown

Eurocopter AS 350 B3 accident in Zollikofen, Switzerland (HB-ZES)

Zollikofen, BE, CH

On August 3, 2010, an EUROCOPTER AS 350 B3 (registration HB-ZES) was involved in an aviation accident near Zollikofen, BE, CH. Investigators recorded the probable cause as: The accident was due to an emergency landing following a total failure of the anti-torque rotor after a sling located under the helicopter during the landing phase became entangled in the anti-torque rotor. This summary draws on records from the Swiss Transportation Safety Investigation Board (STSB / SUST).

Sourcesthe Swiss Transportation Safety Investigation Board (STSB / SUST)Primary reportUpdated 2026-09-13Data APIEditorial standards
Aircraft registered HB-ZES
Aircraft registered HB-ZES. Photo: Hyppolyte de Saint-Rambert / CC BY-SA 4.0, via Wikimedia Commons

On 3 August 2010, a Eurocopter AS 350 B3 (HB-ZES) was heavily damaged during a commercial VFR landing in Zollikofen, Switzerland, after a sling became entangled in the tail rotor.

Overview and Aircraft Details On 3 August 2010, a Eurocopter AS 350 B3 “Ecureuil” helicopter, registered HB-ZES, was involved in an accident at “Häberlimatte,” south of Schulhausstrasse in Zollikofen, Canton of Bern, Switzerland. The location was approximately 11 km north-northwest of Bern-Belp Airport (LSZB). The aircraft was operated by Eagle Helicopter AG and owned by Fortis Lease Suisse SA. The pilot was a Swiss citizen born in 1962, holding an ATPL(H) and type rating for the AS350. ## Operational Context The helicopter was engaged in a commercial VFR operation to remove two storm-damaged spruce trees using a 60 m nylon transport sling. The operation involved a project manager, a ground crew member, and two additional helicopter riggers. The pilot had not previously used a 60 m sling of this type. ## Sequence of Events During the operation, the pilot landed on a stubble field to wait while the pickup area was reorganized. As the helicopter hovered, a sling loop on the ground became disturbed and was subsequently drawn into the tail rotor. The tail rotor stopped immediately, causing the helicopter to rotate counterclockwise. The pilot reduced collective pitch, and the aircraft made a hard landing after rotating approximately 180° in the air and an additional 45° on the ground. ## Damage and Injuries The helicopter was heavily damaged, and the operation was aborted. The pilot was not injured. No third parties were injured, and there was no third-party damage. The emergency locator transmitter was not activated.

Probable cause

The accident was due to an emergency landing following a total failure of the anti-torque rotor after a sling located under the helicopter during the landing phase became entangled in the anti-torque rotor.

Investigation report by the Swiss Transportation Safety Investigation Board (STSB / SUST). Original record: https://www.sust.admin.ch/inhalte/AV-berichte/2115.pdf. This page is a structured re-presentation; facts and quotes are in the Swiss Transportation Safety Investigation Board (STSB), Switzerland.