Casualties unknown

2006-06-15: Bell 206L (N265SH) — Vernal, UT

Vernal, UT, US

On June 15, 2006, a Bell 206L (registration N265SH) was involved in an aviation accident near Vernal, UT. Investigators recorded the probable cause as: The loss of tail rotor effectiveness during an attempted precationary landing after a takeoff over uneven, sloping, brush-covered terrain. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive; 8 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 helicopter departed from a high-altitude landing zone with density altitude over 10,000 ft. The pilot used incorrect performance data, leading to insufficient climb capability. During a precautionary landing, the tail rotor failed, causing a spin and descent.

Background

Prior to takeoff from a landing zone characterized by uneven, sloping, brush-covered terrain, the pilot computed the helicopter's takeoff and hover performance. The conditions resulted in a density altitude exceeding 10,000 feet. The pilot referenced the Hover Ceiling In Ground Effect chart, which indicated that the helicopter could safely depart the landing zone.

Flight

After liftoff, the pilot began moving the helicopter forward. However, the aircraft could not out-climb the up-sloping terrain. Recognizing the insufficient performance, the pilot decided to make a precautionary landing on a nearby road.

Landing Attempt

During the landing attempt, the helicopter's tail rotor lost its effectiveness. The aircraft spun around once and then descended into the terrain.

Analysis

The pilot should have used the Hover Ceiling Out of Ground Effect chart for the takeoff calculation, given the terrain. That chart would have indicated the helicopter did not have the necessary performance to safely depart the landing zone.

Outcome

The helicopter descended into the terrain after the loss of tail rotor effectiveness. The source does not specify injuries, damage, or other consequences.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20060711X00917. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.