Casualties unknown

2006-08-12: Bell 206L-1 (N601GM) — Silver State Helicopters — Ozona, TX

Ozona, TX, US

On August 12, 2006, a Bell 206L-1 (registration N601GM) operated by Silver State Helicopters was involved in an aviation accident near Ozona, TX. Investigators recorded the probable cause as: The pilot's selection of an unsuitable terrain for landing. A contributing factor was the lack of suitable 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
Aircraft registered N601GM
Aircraft registered N601GM. Photo: Tony Hisgett from Birmingham, UK / CC BY 2.0, via Wikimedia Commons

A helicopter performing long-line external load operations in support of seismic activities slid backward after the pilot exited to re-hook a load bag, causing the tail rotor to strike a rock outcrop. The tail rotor gear box and aft tailboom separated.

Incident Details

The operator reported that the helicopter was conducting long-line external load operations in a remote area to support seismic activities. The pilot landed the helicopter on an uphill rocky slope. After landing, the pilot rolled the throttle to idle and checked the controls to assess the stability of the landing surface.

Pilot Experience

The commercial pilot held a total flight experience of 1,263 hours, with 48 hours accumulated in the same make and model of helicopter.

Sequence of Events

The pilot exited the helicopter to re-attach another external load bag. While the pilot was outside, the helicopter began to slide backward. In an attempt to stop the slide, the pilot pushed down on the toe of one of the landing gear skids. However, the helicopter continued to slide until the tail rotor blades made contact with a large rock outcrop.

Post-Impact Actions

The pilot re-entered the helicopter and retarded the engine. The impact caused the tail rotor gear box and the aft portion of the tailboom to separate from the tailboom. Both tail rotor blades sustained structural damage but remained attached to the tail rotor gear box. The helicopter remained upright, and there was no fire.

Weather Conditions

The pilot reported that at the time of the mishap, weather conditions were clear, with winds from the southeast at 10 to 15 knots and a temperature of 90 degrees Fahrenheit.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20060815X01173. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.