No fatalities

Helicopter Encounters Severe Turbulence, Tailrotor Drive Shaft Separates (N999DW)

Nederland, CO, US

On June 8, 2002, a Bell 47G-3B-1 (registration N999DW) was involved in an aviation accident near Nederland, CO. No fatalities were reported. Investigators recorded the probable cause as: the pilot's inadvertent in-flight encounter with severe turbulence, which resulted in main rotor-tailboom contact and the separation of the tailrotor drive shaft. 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

A helicopter in mountainous terrain encountered severe turbulence, causing the tailrotor drive shaft to be severed by the main rotor blades. The pilot regained control and autorotated to sloping terrain without further incident.

Weather and Flight Conditions

Prior to the flight, the pilot obtained a weather forecast that indicated winds from the southwest at 30 mph with gusts up to 40 mph. The helicopter departed and was in cruise flight at an altitude of 9,000 feet (700 feet above ground level). At that time, it experienced a 20-25 knot headwind and light turbulence.

Severe Turbulence Encounter

While in cruise, the flight encountered severe turbulence. The pilot stated that the helicopter went up and down violently for a period of 2-3 seconds. During this event, the tailrotor drive shaft was severed by the main rotor blades. Subsequently, the helicopter experienced a right yaw that could not be corrected by full application of left pedal. The engine and rotor rpm increased beyond their upper limits. However, the pilot was able to bring both the engine and rotor rpm back within limits and regain control of the helicopter.

Autorotation Landing

After regaining control, the pilot performed an autorotation to sloping terrain, which was completed without further incident.

Witness Observation

A witness who was fishing on a lake approximately 4 miles from the accident site reported observing water spouts between 2 and 8 feet tall and high swirling winds near the time of the accident.

Frequently asked questions

What happened in the 8 Jun 2002 Bell 47G-3B-1 accident near Nederland, CO?

A helicopter in mountainous terrain encountered severe turbulence, causing the tailrotor drive shaft to be severed by the main rotor blades. The pilot regained control and autorotated to sloping terrain without further incident.

Were there any fatalities in the 8 Jun 2002 Bell 47G-3B-1 accident?

No fatalities were recorded in this accident.

What aircraft was involved and where did it happen?

The accident on 8 Jun 2002 involved a Bell 47G-3B-1, registration N999DW, at Nederland, CO.

What was the probable cause of the accident?

the pilot's inadvertent in-flight encounter with severe turbulence, which resulted in main rotor-tailboom contact and the separation of the tailrotor drive shaft.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20020612X00856. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.