Casualties unknown

2000-10-14: Bell 206L-1 (N2233F) — Classic Lifeguard Aeromedical — Grand Canyon, AZ

Grand Canyon, AZ, US

On October 14, 2000, a Bell 206L-1 (registration N2233F) operated by Classic Lifeguard Aeromedical was involved in an aviation accident near Grand Canyon, AZ. Investigators recorded the probable cause as: The pilot's in-flight loss of control during liftoff due to his improper planning and decisions. Related factors were the high density altitude and helicopter weight condition, and the lack of a suitable takeoff area. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive.

Sourcesthe U.S. National Transportation Safety Board (NTSB) historical archivePrimary reportUpdated 1781061362Data APIEditorial standards

During a patient evacuation, a helicopter's tail rotor lost effectiveness after takeoff from a tree-surrounded clearing, leading to uncontrolled yaw and a forced landing into trees due to high density altitude and heavy weight.

Incident Overview

A helicopter conducting an aeromedical evacuation of a seriously injured patient attempted to take off from a clearing that was surrounded by trees and high-elevation terrain. On board were the pilot, a paramedic, and a flight nurse. According to crewmembers, as the helicopter climbed between 80 and 100 feet above the terrain, no tree branches were closer than 8 to 20 feet from the aircraft.

Sequence of Events

After takeoff, the pilot initiated a turn into the light wind. During this maneuver, the tail rotor lost effectiveness, causing the helicopter to yaw uncontrollably in a clockwise direction. Concurrently, the aircraft experienced a lack of climb performance due to the high density altitude—approximately 8,850 feet—and the heavy weight condition resulting from the patient, crew, and equipment.

Forced Landing

Unable to maintain controlled flight, the pilot executed a forced landing into the underlying terrain. During the landing, the helicopter impacted trees. The source does not specify further details about the outcome of the impact or the condition of those on board.

Factors

The incident involved a combination of environmental and operational conditions, including high elevation, surrounding trees, light wind, and the weight of the helicopter. The tail rotor's loss of effectiveness and reduced climb performance were noted as central to the event.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001212X22192. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.