Casualties unknown

2014-06-22: AGUSTA S.P.A. AW109SP (HB-ZRU) — Brissago, TI, CH

Brissago, TI, CH

On June 22, 2014, an AGUSTA S.P.A. AW109SP (registration HB-ZRU) was involved in an aviation accident near Brissago, TI, CH. Investigators recorded the probable cause as: The serious incident was caused by insufficient pedal travel for directional control about the vertical axis during a steep descent with rapidly increasing speed in a right turn, combined with an inappropriate control input, leading to temporary loss of… 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
Aircraft registered HB-ZRU
Aircraft registered HB-ZRU. Photo: NAC / CC BY-SA 4.0, via Wikimedia Commons

On 22 June 2014, an AgustaWestland AW109SP helicopter experienced a temporary loss of control during a steep descending right turn, leading to an overspeed of the main rotor. The helicopter was flown near or possibly outside the certified flight envelope.

Background

On 22 June 2014, an AgustaWestland AW109SP helicopter, registration HB-ZRU, operated by the Swiss Air Rescue Guard (Guardia aerea svizzera di soccorso), was involved in a serious incident near Cortaccio, in the municipality of Brissago, Switzerland. The helicopter was crewed by a pilot, a Helicopter Emergency Medical Services crew member, and a doctor.

Sequence of Events

During a steep descent with rapidly increasing speed in a right turn, the pilot applied pedal inputs for directional control about the vertical axis. The available pedal travel became insufficient to maintain control. In combination with an inappropriate control correction, the helicopter temporarily became uncontrollable. As a consequence, the maximum permissible rotor speed was exceeded.

Contributing Factors

The investigation determined that the helicopter was being flown near or possibly outside the certified flight envelope at the time of the incident.

Cause

The serious incident was caused by insufficient pedal travel for directional control about the vertical axis during a steep descent with rapidly increasing speed in a right turn, combined with an inappropriate control input, leading to temporary loss of control. Subsequently, the maximum permissible rotor speed was exceeded. A contributing factor was that the helicopter was flown near or possibly outside the certified flight envelope.

Probable cause

The serious incident was caused by insufficient pedal travel for directional control about the vertical axis during a steep descent with rapidly increasing speed in a right turn, combined with an inappropriate control input, leading to temporary loss of control. Subsequently, the maximum permissible rotor speed was exceeded. A contributing factor was that the helicopter was flown near or possibly outside the certified flight envelope.

Investigation report by the Swiss Transportation Safety Investigation Board (STSB / SUST). Original record: https://www.sust.admin.ch/inhalte/AV-berichte/2301_i.pdf. This page is a structured re-presentation; facts and quotes are in the Swiss Transportation Safety Investigation Board (STSB), Switzerland.