Casualties unknown

2009-11-24: COSTRUZIONI AERONAUTICHE GIOVANNI AGUSTA S.P.A. A109K2 (HB-XWM) — Wilderswil, BE, CH

Wilderswil, BE, CH

On November 24, 2009, a COSTRUZIONI AERONAUTICHE GIOVANNI AGUSTA S.P.A. A109K2 (registration HB-XWM) was involved in an aviation accident near Wilderswil, BE, CH. Investigators recorded the probable cause as: The accident was caused by the fracture of two swashplate attachment bolts, rendering the helicopter nearly uncontrollable. 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 24 November 2009, an Agusta A109K2 helicopter (HB-XWM) became uncontrollable after two swashplate attachment bolts fractured. Incomplete maintenance documentation from the manufacturer was identified as contributing to the bolt failure.

Background

On 24 November 2009, an Agusta A109K2 helicopter, registered HB-XWM, was involved in an accident on the former Interlaken airfield in the canton of Bern, Switzerland. The Swiss Accident Investigation Board (SUST) conducted the investigation and published its final report (No. 2153).

Accident Sequence

During the flight, two bolts securing the swashplate (plateau cyclique) fractured. This allowed the swashplate to be displaced by the main rotor, rendering the helicopter nearly uncontrollable. The pilot lost control of the aircraft, leading to the accident.

Investigation Findings

Metallurgical examination of the failed bolts revealed that the fractures originated from fatigue cracks. The investigation traced the root cause to incomplete maintenance documentation provided by the manufacturer, AgustaWestland, and used by the maintenance organization, Agusta Aerospace Services SA (AAS). The documentation lacked critical instructions, which led to improper maintenance procedures that initiated the bolt failures.

Causes

According to the investigation, the accident was caused by the fracture of two swashplate attachment bolts, resulting in a loss of control. The incomplete maintenance documentation published by the manufacturer and used by the maintenance organization was at the origin of the bolt failure.

Probable cause

The accident was caused by the fracture of two swashplate attachment bolts, rendering the helicopter nearly uncontrollable. The incomplete maintenance documentation published by the manufacturer and used by the maintenance organization was at the origin of the bolt failure.

Investigation report by the Swiss Transportation Safety Investigation Board (STSB / SUST). Original record: https://www.sust.admin.ch/inhalte/AV-berichte/2153_d.pdf. This page is a structured re-presentation; facts and quotes are in the Swiss Transportation Safety Investigation Board (STSB), Switzerland.