Bell 212 experiences power settling during takeoff from remote Peruvian helipad

Casualties unknown • PE

A Bell 212 helicopter operated by AVIASUR sustained major damage after experiencing a sudden loss of rotor RPM during a takeoff from a remote helipad in Cusco.

What happened

On January 16, 2008, a Bell 212 helicopter, registration OB-1850, was performing a scheduled flight for a client at the KP-50 remote helipad in the La Convención district, Cusco. The flight was part of a series of operations involving the transport of personnel near a gas pipeline.

After picking up two passengers, bringing the total number of occupants to 11, the crew prepared for takeoff. The flight plan involved a vertical takeoff into a hover at two meters, followed by a lateral movement to clear nearby obstacles before climbing. During the climb, at an altitude of approximately 25 to 30 meters and a distance of about 90 meters from the takeoff point, the aircraft experienced a sudden descent. The rotor RPM (NR) dropped sharply from 100% to nearly 80%, triggering the low RPM warning siren.

Recognizing the loss of altitude and the proximity of trees, the pilot attempted an emergency landing in a nearby clearing. The aircraft struck three trees and crashed on its left side. While the crew and passengers were able to evacuate, the impact resulted in two fatalities and several serious injuries among the passengers and crew.

The investigation

The CIAA investigation focused on the aerodynamic performance of the aircraft and the environmental conditions at the remote site. Investigators examined the aircraft's maintenance records, weight and balance calculations, and the meteorological conditions at the time of the accident.

Key elements of the investigation included the lack of a windsock at the remote helipad, which prevented the crew from accurately assessing wind direction and intensity. Furthermore, the investigation noted that the aircraft was not equipped with a Flight Data Recorder (FDR), a requirement for helicopters of this maximum takeoff weight under Peruvian regulations. The absence of this data limited the investigators' ability to analyze the specific flight parameters leading up to the loss of rotor RPM.

Probable cause

The primary cause of the accident was the inadequate flight planning by the crew, specifically regarding a takeoff from a remote helipad surrounded by trees while experiencing a tailwind component. This led to the aerodynamic phenomenon of **power settling** (vortex ring state) when the aircraft failed to maintain the minimum required climb rate.

Frequently asked questions

What happened in the 2008-01-16 aircraft accident near PE?

A Bell 212 helicopter operated by AVIASUR sustained major damage after experiencing a sudden loss of rotor RPM during a takeoff from a remote helipad in Cusco.

What aircraft was involved and where did it happen?

The accident on 2008-01-16 involved a aircraft, registration OB-1850, at PE.

What was the probable cause of the accident?

The primary cause of the accident was the inadequate flight planning by the crew, specifically regarding a takeoff from a remote helipad surrounded by trees while experiencing a tailwind component. This led to the aerodynamic phenomenon of **power settling** (vortex ring state) when the aircraft failed to maintain…

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