Casualties unknown

2004-02-18: Bell 206B (N16MV) — U.s. Forestry Services — Decatur, TX

Decatur, TX, US

On February 18, 2004, a Bell 206B (registration N16MV) operated by U.s. Forestry Services was involved in an aviation accident near Decatur, TX. Investigators recorded the probable cause as: The rear portion of the helicopter's right main skid contacted the ground during lift-off from soft uneven terrain, resulting in a dynamic rollover. 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 experienced a dynamic rollover during takeoff from soft uneven terrain after the rear of the right main skid contacted the ground. The pilot reported clumpy, lumpy terrain with grass ruts 1 to 2 feet high.

Accident Summary

During lift-off from soft, uneven terrain, the rear portion of the helicopter's right main skid contacted the ground, initiating a dynamic rollover. The event occurred as the pilot attempted to depart from an area described as clumpy and lumpy with grass ruts approximately 1 to 2 feet in height.

Pilot Report

The pilot reported making a slow ascent after lifting the helicopter off the ground. When the skids were about 1 foot above the terrain, the helicopter momentarily stopped as if something had caught the right side, followed by a slight lateral roll to the right. The pilot recognized the situation too late and applied full left cyclic while lowering the collective. By that time, the helicopter had exceeded the critical angle of bank into the low skid, making recovery impossible. The helicopter subsequently rolled 90 degrees to the right.

Terrain Conditions

The departure area consisted of soft, uneven ground with clumps and ruts of grass 1 to 2 feet high. This uneven surface contributed to the skid contacting the ground during the lift-off.

Dynamic Rollover Mechanism

The Rotorcraft Flying Handbook (FAA-H-8083-21) describes dynamic rollover as pivoting around a skid or landing gear wheel that causes the helicopter to reach its critical rollover angle. Beyond this point, main rotor thrust continues the roll and recovery is impossible. In this event, the skid contact led to such a scenario.

No mechanical deficiencies with the engine or airframe were noted. The pilot's actions, including the late application of corrective controls, were consistent with the dynamics described in the handbook.

Probable cause

The rear portion of the helicopter's right main skid contacted the ground during lift-off from soft uneven terrain, resulting in a dynamic rollover.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20040302X00255. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.