Helicopter crashes at Swiss mountain landing site following loss of control

Casualties unknown • Steingletscher, BE, CH

An Eurocopter EC 120 B crashed at the Hotel Steingletscher landing site after encountering a tailwind that triggered an uncontrolled rotation.

What happened

On August 13, 2003, an Eurocopter EC 120 B, registration HB-ZER, was involved in an accident at the Hotel Steingletscher mountain landing site in the Canton of Bern. After performing several practice approaches and landings from the west, the pilot and two passengers took a break. Upon returning to the aircraft approximately one hour later, the pilot attempted a takeoff.

During the initial takeoff phase, the pilot noted a light tailwind. After a brief hover to check engine performance and controls, the pilot attempted to turn the aircraft to the right to fly down-valley. However, witnesses observed the helicopter beginning to rotate rapidly to the left at an altitude of only about one meter. The pilot attempted to correct the rotation by applying full right pedal, but the leftward rotation continued to increase. To avoid further complications, the pilot decided to descend and land immediately. During the landing, the aircraft tilted onto its right side near a steep embankment, resulting in the destruction of the helicopter. The pilot sustained minor injuries, while the two passengers were uninjured.

The investigation

The investigation conducted by the Swiss Transportation Safety Investigation Board (SUST) focused on the mechanical and operational circumstances of the rotation. Technical examinations of HB-ZER revealed no mechanical failures or deficiencies in the engine or flight controls. The tail rotor, specifically the Fenestron system, was found to have been fully functional up until the moment of impact.

Investigators examined the meteorological conditions, noting that while the prevailing wind was from the west-northwest, local mountain winds were fluctuating. The investigation also reviewed manufacturer documentation regarding the specific handling characteristics of the Fenestron tail rotor system during low-speed flight and tailwind conditions.

Probable cause

The accident was caused by a loss of directional control during takeoff, triggered by a tailwind that induced a leftward rotation. The pilot's inability to immediately arrest this rotation—likely due to an insufficient application of right pedal input—led to a decision to land that resulted in the aircraft tipping over.

Frequently asked questions

What happened in the 2003-08-13 EUROCOPTER EC120 B accident near Steingletscher, BE, CH?

An Eurocopter EC 120 B crashed at the Hotel Steingletscher landing site after encountering a tailwind that triggered an uncontrolled rotation.

What aircraft was involved and where did it happen?

The accident on 2003-08-13 involved a EUROCOPTER EC120 B, registration HB-ZER, at Steingletscher, BE, CH.

What was the probable cause of the accident?

The accident was caused by a loss of directional control during takeoff, triggered by a tailwind that induced a leftward rotation. The pilot's inability to immediately arrest this rotation—likely due to an insufficient application of right pedal input—led to a decision to land that resulted in the aircraft tipping…

Investigation report by the Swiss Transportation Safety Investigation Board (STSB / SUST). Original record: https://www.sust.admin.ch/inhalte/AV-berichte/1941_d.pdf. This page is a structured re-presentation; facts and quotes are in the Swiss Transportation Safety Investigation Board (STSB), Switzerland.

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