Casualties unknown

2015-07-14: EUROCOPTER AS 350 B3 (HB-ZIS) — Lauterbrunnen, BE, CH

Lauterbrunnen, BE, CH

On July 14, 2015, an EUROCOPTER AS 350 B3 (registration HB-ZIS) was involved in an aviation accident near Lauterbrunnen, BE, CH. Investigators recorded the probable cause as: The accident is due to loss of control of the helicopter due to instability of the external load causing oscillations of the transport cable along the fuselage causing damage in the areas of the main and tail rotors. This summary draws on records from the Swiss Transportation Safety Investigation Board (STSB / SUST).

Sourcesthe Swiss Transportation Safety Investigation Board (STSB / SUST)Primary reportUpdated 1785639345Data APIEditorial standards

An Airbus Helicopters AS 350 B3 (HB-ZIS) lost control after external load instability caused cable oscillations, damaging main and tail rotors. Excessive speed with unstable load was causal; insufficient fuel, lack of load assessment, and inappropriate attachment device contributed.

Accident Overview

On 14 July 2015, an Airbus Helicopters AS 350 B3, registration HB-ZIS, was involved in an accident on the Guggigletscher near Lauterbrunnen, Switzerland. The helicopter was conducting an external load operation when the pilot lost control. The instability of the external load caused oscillations of the transport cable along the fuselage, resulting in damage to the main and tail rotor areas.

Causal and Contributing Factors

The Swiss Transportation Safety Investigation Board (STSB) determined that the accident was caused by the loss of control due to the instability of the external load, which led to cable oscillations and subsequent rotor damage. The identified causal factor was excessive speed with an unstable load. Contributing factors included insufficient fuel reserve, the air transport company's failure to evaluate the load attachment device, and the use of an inappropriate load attachment device for the mission.

Operational Context

The flight was part of a transport operation. The helicopter was equipped with an external load system. The flight crew comprised a pilot and three flight helpers. The accident occurred during the day under visual meteorological conditions. No injuries were reported among the occupants.

Investigation Findings

Examination of the wreckage and load system revealed that the load attachment device was not suitable for the task. The transport cable showed signs of oscillation damage. The fuel level at the time of the accident was below the required reserve for the mission profile. The investigation did not find any pre-existing technical faults with the helicopter or its engine.

Safety Recommendations

The STSB issued safety recommendations aimed at improving operational procedures for external load operations, including better assessment of load attachment devices and ensuring adequate fuel reserves. However, these recommendations are not part of the causal analysis.

Probable cause

The accident is due to loss of control of the helicopter due to instability of the external load causing oscillations of the transport cable along the fuselage causing damage in the areas of the main and tail rotors. The causal factor is excessive speed with an unstable load.

Investigation report by the Swiss Transportation Safety Investigation Board (STSB / SUST). Original record: https://www.sust.admin.ch/inhalte/AV-berichte/2309_D.pdf. This page is a structured re-presentation; facts and quotes are in the Swiss Transportation Safety Investigation Board (STSB), Switzerland.