Casualties unknown

2007-07-17: Robinson R22 (N707WH) — Leading Edge Aviation — Bend, OR

Bend, OR, US

On July 17, 2007, a Robinson R22 (registration N707WH) operated by Leading Edge Aviation was involved in an aviation accident near Bend, OR. Investigators recorded the probable cause as: The pilot's failure to maintain adequate rotor rpm during a simulated power-off autorotation, which resulted in an excessive descent rate and substantial damage to the helicopter upon impact with the ground. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive; 14 related events involving the same aircraft type or operator are linked below.

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

A pilot conducting simulated autorotations allowed descent rate to become excessive during a final attempt, leading to substantial damage upon impact with an asphalt surface.

What happened

The flight involved a series of practice maneuvers designed to simulate power failure scenarios. The pilot had previously executed five or six successful simulated power-off autorotations without incident. During the subsequent maneuver, the pilot initiated another autorotation sequence. However, during this specific attempt, the helicopter's vertical descent rate increased beyond safe operational limits.

Although the pilot recognized the developing situation and attempted to apply corrective inputs to arrest the descent, the actions were not executed in sufficient time. The aircraft impacted an asphalt surface with significant force. This impact resulted in substantial damage to the helicopter's airframe structure.

The investigation

The investigation focused on the mechanics of the final autorotation attempt. Examination of the flight data and physical evidence confirmed that the primary issue was the excessive vertical speed at the moment of touchdown. No mechanical failures were identified as contributing factors to the loss of control or the subsequent impact.

Probable cause

The pilot's failure to maintain adequate rotor rpm during a simulated power-off autorotation, which resulted in an excessive descent rate and substantial damage to the helicopter upon impact with the ground.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20070808X01143. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.