Casualties unknown

1995-08-12: AEROSPATIALE AS 350 B2 (HB-XVT) — Mittel Stafel Schlattalp, GL, CH

Mittel Stafel Schlattalp, GL, CH

On August 12, 1995, an AEROSPATIALE AS 350 B2 (registration HB-XVT) was involved in an aviation accident near Mittel Stafel Schlattalp, GL, CH. Investigators recorded the probable cause as: The accident resulted from an uncoordinated takeoff attempt where the pilot's sudden control inputs caused the rotor blades to strike the ground, compounded by a lack of clear communication regarding pilot responsibilities during the flight. 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

A private flight involving an AS 350B2 ended in a fatal accident near Mittel Stafel after an uncoordinated takeoff attempt caused the rotor blades to strike the ground.

What happened

On August 12, 1995, an AS 350B2 helicopter, registration HB-XVT, was conducting a private transport mission in the Klöntal region of Switzerland. The flight involved a private pilot and an experienced second pilot acting as a safety observer. After landing on a small, grassy alpine meadow at Mittel Stafel to deliver passengers and pick up cargo, the second pilot exited the aircraft to assist with the load.

As the cargo was being brought to the helicopter, the pilot attempted a sudden takeoff. During this maneuver, the aircraft experienced a sharp nose-down movement and a significant pitch change. The main rotor blades struck the rising terrain, causing the helicopter to spin 90 degrees and crash. The pilot sustained fatal injuries during the impact.

The investigation

The investigation focused on the sequence of events during the takeoff and the communication between the crew members. Investigators examined the aircraft's technical condition, the landing site, and the flight logs of the involved pilots. The wreckage showed that the main rotor blades had been sheared off at the head due to the impact with the ground.

Physical evidence at the site confirmed that the landing area, while relatively small and slightly sloped, was otherwise unobstructed. The investigation also reviewed the pilot's flight experience, noting discrepancies in reported flight hours, and examined the lack of clear operational agreements between the individuals involved in the flight organization.

Findings

  • The primary cause of the accident was an uncontrolled and uncoordinated takeoff maneuver.
  • The pilot likely inadvertently pushed the cyclic control forward, causing the rotor disk to tilt toward the rising slope.
  • The pilot reacted to perceived vibrations by pulling the collective pitch lever aggressively and without coordination.
  • There was a lack of clear and complete communication between the involved parties before and during the flight, leading to confusion regarding command authority.
  • The pilot was not wearing a protective flight helmet; investigators concluded that the fatal head injuries likely could have been avoided if a helmet had been worn.
  • No technical defects or mechanical failures were found in the aircraft's systems or components.

Probable cause

The accident resulted from an uncoordinated takeoff attempt where the pilot's sudden control inputs caused the rotor blades to strike the ground, compounded by a lack of clear communication regarding pilot responsibilities during the flight.

Investigation report by the Swiss Transportation Safety Investigation Board (STSB / SUST). Original record: https://www.sust.admin.ch/inhalte/AV-berichte/1634.pdf. This page is a structured re-presentation; facts and quotes are in the Swiss Transportation Safety Investigation Board (STSB), Switzerland.