No fatalities

18 Nov 2009: BELL 206B — Leading Edge Aviation Inc. — Lyons, OR

Lyons, OR, United States

On 18 Nov 2009, a BELL 206B operated by Leading Edge Aviation Inc. was involved in an aviation accident near Lyons, OR. No fatalities were reported. Investigators recorded the probable cause as: The pilot's inadvertent encounter with a vortex ring state (settling with power) condition while he was descending, and his improper initial remedial action. This summary draws on records from NTSB; 12 related events involving the same aircraft type or operator are linked below.

SourcesNTSBPrimary reportUpdated 1778583330Data APIEditorial standards

A helicopter settling with power during Christmas tree relocation resulted in a hard landing, bending the tailboom. The pilot reported no mechanical malfunctions.

Accident Details

The pilot of the helicopter was engaged in relocating Christmas trees to a nearby drop site. Over a duration of about 15 minutes, he had completed several loads. While maneuvering to the drop site with another load, the helicopter began to settle with power, according to the pilot. In response, he applied more collective pitch in an attempt to arrest the descent, but the helicopter continued to descend. He then attempted to reduce collective and maneuver forward. The helicopter touched down hard on the heels of the skids, and its nose came to rest in a pile of Christmas trees. The tailboom was bent as a result of the hard landing.

Mechanical Condition

The pilot stated that there were no preimpact mechanical malfunctions or failures with the airframe or engine.

Background on Settling with Power

The Rotorcraft Flying Handbook, FAA-H-8083-21, Chapter 11, discusses vortex ring state, also known as settling with power. It notes that a combination of conditions is likely to cause this phenomenon: a vertical or nearly vertical descent of at least 300 feet per minute, the rotor system using 20 to 100 percent of available engine power, and horizontal velocity slower than effective translational lift. The handbook warns that when recovering from settling with power, a pilot's tendency to first try to stop the descent by increasing collective pitch only results in increasing the stalled area of the rotor, thus increasing the rate of descent. Since inboard portions of the blades are stalled, cyclic control is limited. Recovery is accomplished by increasing forward speed and/or partially lowering collective pitch. In a fully developed vortex ring state, the only recovery may be to enter autorotation to break the vortex ring state, after which cyclic authority is regained and forward airspeed can be increased.

Contributing factors

PilotDescent rate — Not attained/maintained