Casualties unknown

2003-07-29: KAMAN AEROSPACE CORPORATION K-1200 (HB-ZEH) — Frutigen, BE, CH

Frutigen, BE, CH

On July 29, 2003, a KAMAN AEROSPACE CORPORATION K-1200 (registration HB-ZEH) was involved in an aviation accident near Frutigen, BE, CH. Investigators recorded the probable cause as: The accident is with a very high degree of probability attributable to an uncontrolled opening of the lower cargo hook because of its defective design. This summary draws on records from the Swiss Transportation Safety Investigation Board (STSB / SUST).

Sourcesthe Swiss Transportation Safety Investigation Board (STSB / SUST)Primary reportUpdated 1785034239Data APIEditorial standards

On 29 July 2003, a Kaman K-1200 K-MAX helicopter (HB-ZEH) was logging near Frutigen, Switzerland, when the lower cargo hook opened uncontrollably, dropping tree trunks that fatally struck a third party. The investigation attributed the accident to defective hook design and cited contributing factors including inadequate certification, understaffing, and communication issues.

Accident Overview

On Tuesday, 29 July 2003, at approximately 08:42 local time, a Kaman K-1200 K-MAX helicopter (registration HB-ZEH) operated by Eagle Helicopter AG was performing logging operations in the “Trute” area near Frutigen, Switzerland, about 45 km SSE of Berne. The helicopter was transporting tree trunks from the forest to a drop zone on a central landing area using a longline with a lower cargo hook. During the fifth approach of the day, while carrying two tree trunks suspended vertically, the pilot was given height information by the company flight assistant. The flight assistant warned the pilot over the radio about a fence and advised him to pull left. The two trunks impacted forcefully on the ground, gouging approximately 30 cm into the terrain and breaking in two. Subsequently, the lower cargo hook opened in an uncontrolled manner, causing the two trunk sections still suspended to fall. An assistant on the ground was struck by a tree trunk section and later died from his injuries. The pilot stated that he had not operated the cargo release.

Aircraft and Equipment

The helicopter was a single-seat Kaman K-1200 K-MAX, serial number A94-0014, powered by a Textron Lycoming T5317A-1 turbine engine. It was equipped with a belly cargo hook with a weighing system and used a Canam C60 lower cargo hook (serial number 6097) mounted on a longline approximately 50 m long. The Canam C60 was designed for loads up to 6000 lbs (2721 kg) and could be released manually or electrically via a solenoid. It featured an interlock mechanism with a hinged closure, safety catch, load beam, and a protective cage. The aircraft’s mass and center of gravity were within prescribed limits, and the helicopter itself was not damaged in the accident.

Personnel Information

The pilot, a Swiss citizen born in 1963, held a commercial helicopter pilot license issued by the Federal Office for Civil Aviation (FOCA) on 10 August 1989, valid until 4 March 2004. He had a total flying experience of 6651:45 hours, with 246:38 hours on the K-1200 type. His last medical examination on 14 July 2003 found him fit to fly. The flight assistant involved in the accident was a Swiss citizen born in 1980 with no flying experience.

Injuries and Damage

A third party on the ground was fatally injured by a falling tree trunk. The assistant who was struck was not employed by the helicopter company or the forestry company and was not wearing a safety helmet. The helicopter sustained no damage. Minor damage occurred to cultivated land.

Investigation and Probable Cause

The investigation was conducted by the Swiss Aircraft Accident Investigation Bureau (AAIB) together with the Berne cantonal police. The probable cause, as stated in the final report, is that the accident is with a very high degree of probability attributable to an uncontrolled opening of the lower cargo hook because of its defective design. The following factors were found to have contributed to the accident:

  • The cargo hook certification process was not suitable for the flight operation requirements.
  • The landing area was undermanned, with one flight assistant from the company.
  • Organisation on the landing area was made more difficult and impossible to oversee for the flight assistant because of external helpers.
  • Communication was made difficult for the external assistants because of the lack of radio equipment.

Certification Background

The Canam C60 cargo hook was certified by the manufacturer under US Federal Aviation Regulations (FAR) Part 27.865ff, which primarily focuses on the safety of the helicopter in external load operations. The hook was accepted on 29 November 2001 after passing static load, electrical, cycle, and vibration tests. However, the investigation noted that the certification process was not adapted to the operational demands encountered during flight.

Investigation report by the Swiss Transportation Safety Investigation Board (STSB / SUST). Original record: https://www.sust.admin.ch/inhalte/AV-berichte/1921_e.pdf. This page is a structured re-presentation; facts and quotes are in the Swiss Transportation Safety Investigation Board (STSB), Switzerland.