No fatalities

Helicopter Tail Rotor Damaged During Autorotation Training (N58431)

North Las Vegas, NV, US

On August 8, 2005, a Hughes 369D (registration N58431) was involved in an aviation accident near North Las Vegas, NV. No fatalities were reported. Investigators recorded the probable cause as: the pilot's improper use of the cyclic flight control and the flight instructor's inadequate supervision of the flight. 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 a full touchdown autorotation training exercise, a helicopter's tail rotor and stinger were damaged when the cyclic was not moved forward sufficiently during the deceleration flare.

Incident Overview

During a 120-day recurrent training session, an instructor pilot and a commercial pilot were performing their fifth full-down autorotation in a helicopter. Both pilots were on the controls throughout the maneuver. As the helicopter decelerated and flared, the instructor pilot advised the commercial pilot to push the cyclic forward. However, the commercial pilot did not move the cyclic far enough, causing the stinger to contact the ground first, followed by the tail rotor.

Damage

The tail rotor sustained substantial damage and required replacement. The stinger was also damaged in the sequence of ground contacts. No other components were reported as damaged beyond the tail rotor and stinger.

Prior Mechanical Condition

No mechanical problems were reported with the helicopter prior to the training event. The incident was attributed solely to the control input during the autorotation maneuver.

Training Context

The autorotation was part of a routine recurrent training program. The instructor and commercial pilot were both controlling the helicopter at the time of the incident. The instructor's guidance to push the cyclic forward was intended to manage the flare, but the execution was insufficient to prevent ground contact.

Frequently asked questions

What happened in the 8 Aug 2005 Hughes 369D accident near North Las Vegas, NV?

During a full touchdown autorotation training exercise, a helicopter's tail rotor and stinger were damaged when the cyclic was not moved forward sufficiently during the deceleration flare.

Were there any fatalities in the 8 Aug 2005 Hughes 369D accident?

No fatalities were recorded in this accident.

What aircraft was involved and where did it happen?

The accident on 8 Aug 2005 involved a Hughes 369D, registration N58431, at North Las Vegas, NV.

What was the probable cause of the accident?

the pilot's improper use of the cyclic flight control and the flight instructor's inadequate supervision of the flight.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20050908X01418. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.