Agusta A-109-A II Tail and Landing Gear Damage During Autorotation Training

Casualties unknown • Helipuerto de La Cartuja (Sevilla), ES

An Agusta A-109-A II helicopter sustained damage to its tail structure and landing gear after an improper collective pitch adjustment during an instructional flight in Seville.

What happened

On November 13, 2000, at approximately 14:15 local time, an Agusta A-109-A II (registration EC-HBQ) was conducting a flight verification and instruction mission near the La Juliana aerodrome in Seville. The flight, which began at the Isla de la Cartuja helipad, involved a pilot and an instructor performing various emergency procedure reviews, specifically focusing on autorotation maneuvers.

During the third attempt at a low-speed autorotation maneuver, the crew attempted to transition from the descent to a controlled approach. As the pilot applied collective pitch, the aircraft experienced an excessive rate of descent. In an effort to recover, the crew attempted to exit the maneuver; however, the aircraft struck the ground with its rear landing gear and tail stabilizer before returning to flight. After maintaining a hover for several minutes to check for vibrations or flight control damage, the crew decided to return to the Isla de la Cartuja helipad due to the visible damage to the landing gear. Upon arrival, ground personnel noted the damage, and the aircraft landed on its skids.

The investigation

The investigation established that the crew was practicing specific autorotation techniques designed to reach a precise point with minimal airspeed. During the final maneuver, the pilot initiated the power application (collective pitch) while the aircraft was at a low speed. The investigation focused on the aerodynamic response of the rotor system to the sudden change in pitch during the descent phase.

Probable cause

The incident was caused by an improper increase in collective pitch during a low-speed autorotation maneuver, which led to a decay in rotor RPM and a subsequent loss of lift.

Frequently asked questions

What happened in the 2000-11-13 Agusta A-109-A II accident near Helipuerto de La Cartuja (Sevilla), ES?

An Agusta A-109-A II helicopter sustained damage to its tail structure and landing gear after an improper collective pitch adjustment during an instructional flight in Seville.

What aircraft was involved and where did it happen?

The accident on 2000-11-13 involved a Agusta A-109-A II, registration EC-HBQ, at Helipuerto de La Cartuja (Sevilla), ES.

What was the probable cause of the accident?

The incident was caused by an improper increase in collective pitch during a low-speed autorotation maneuver, which led to a decay in rotor RPM and a subsequent loss of lift.

Investigation report by the Spanish Civil Aviation Accident and Incident Investigation Commission (CIAIAC). Original record: https://www.transportes.gob.es/recursos_mfom/2000_044_in_0.pdf. This page is a structured re-presentation; facts and quotes are in the Comision de Investigacion de Accidentes e Incidentes de Aviacion Civil (CIAIAC), Spain - Ministerio de Transportes y Movilidad Sostenible.

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