Main Rotor Blade Separation Leads to Fatal Gazelle Crash in Italy

Casualties unknown • Condove (Torino) Elicottero SA341 Gazelle, IT

A structural failure of a tie bar caused a rotor blade to detach from an SA 341 Gazelle, resulting in a fatal helicopter crash in Condove.

What happened

On May 28, 2001, an SA 341 Gazelle, registration I-OLLY, was performing utility flight operations in the mountains near Condove, Italy. The aircraft was engaged in transporting personnel and materials for the construction of an electrical substation intended for the 2006 Winter Olympics.

During a takeoff from a landing site near a tool depot, the helicopter was in a hover at an altitude of approximately 15 to 20 meters. As the pilot began to transition from a hover toward the valley, one of the main rotor blades detached from the rotor head. This separation caused an immediate severe imbalance in the main rotor system, which subsequently caused the entire rotor assembly and transmission unit to detach from the fuselage. The aircraft plummeted to the ground and caught fire upon impact.

The accident resulted in two fatalities and two serious injuries. While the specialist technician was able to assist one passenger in exiting the wreckage before the fire became impassable, the pilot and the second passenger were unable to escape the intense flames.

Probable cause

The accident was caused by the structural failure of a main rotor blade tie bar due to stress corrosion and fatigue, triggered by the ingress of corrosive environmental agents through a degraded polyurethane protective coating.

Frequently asked questions

What happened in the 2001-05-28 SA341 Gazelle, accident near Condove (Torino) Elicottero SA341 Gazelle, IT?

A structural failure of a tie bar caused a rotor blade to detach from an SA 341 Gazelle, resulting in a fatal helicopter crash in Condove.

What aircraft was involved and where did it happen?

The accident on 2001-05-28 involved a SA341 Gazelle,, registration I-OLLY, at Condove (Torino) Elicottero SA341 Gazelle, IT.

What was the probable cause of the accident?

The accident was caused by the structural failure of a main rotor blade tie bar due to stress corrosion and fatigue, triggered by the ingress of corrosive environmental agents through a degraded polyurethane protective coating.

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