Casualties unknown

Hard Landing After Loss of Tail Rotor Effectiveness During Sight-Seeing Flight (N39122)

Telluride, CO, US

On June 20, 1999, a Bell BH-206B (registration N39122) operated by Walter Duraur was involved in an aviation accident near Telluride, CO. Investigators recorded the probable cause as: The pilot-in-command allowed the helicopter to slow and enter a high sink rate, and in attempting to recover, loss of tail rotor effectiveness occurred. 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 2026-07-04Data APIEditorial standards

During approach, the helicopter slowed and entered a high sink rate. The recovery attempt caused loss of tail rotor effectiveness and a spin. The safety pilot regained control, but the helicopter landed hard.

Accident Overview

A helicopter on a sight-seeing flight with two pilots and two passengers experienced a hard landing during approach. The incident occurred when the pilot-in-command allowed the aircraft to slow down and enter a high sink rate at an altitude of 100 to 150 feet above ground level. Contributing conditions included high gross weight, high-density altitude, and low wind.

Sequence of Events

While approaching to land, the helicopter's speed decreased, leading to a high sink rate. The pilot-in-command attempted to recover from the sink rate. During this recovery, the helicopter experienced a loss of tail rotor effectiveness (LTE), causing it to begin spinning. The safety pilot then took control and successfully stopped the spin. Despite the recovery, the helicopter landed hard.

Probable Cause

The pilot-in-command allowed the helicopter to slow and enter a high sink rate. In attempting to recover, loss of tail rotor effectiveness occurred, leading to a spin and subsequent hard landing.

Frequently asked questions

What happened in the 20 Jun 1999 Bell BH-206B accident near Telluride, CO?

During approach, the helicopter slowed and entered a high sink rate. The recovery attempt caused loss of tail rotor effectiveness and a spin. The safety pilot regained control, but the helicopter landed hard.

What aircraft was involved and where did it happen?

The accident on 20 Jun 1999 involved a Bell BH-206B, registration N39122, operated by Walter Duraur, at Telluride, CO.

What was the probable cause of the accident?

The pilot-in-command allowed the helicopter to slow and enter a high sink rate, and in attempting to recover, loss of tail rotor effectiveness occurred.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001212X18983. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.