Casualties unknown

2007-10-25: Bell 206L-1 (N412KK) — Ramona, CA

Ramona, CA, US

On October 25, 2007, a Bell 206L-1 (registration N412KK) was involved in an aviation accident near Ramona, CA. Investigators recorded the probable cause as: The pilot's failure to maintain control and correct a descent and a loss of tail rotor effectiveness while maneuvering at a low altitude and reduced airspeed. 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 1781061362Data APIEditorial standards

During a low-altitude damage assessment flight, a helicopter experienced airspeed loss, control resistance, and yaw, leading to a precautionary landing that resulted in a tree impact and rollover.

Incident Overview

A helicopter conducting a low-altitude survey of utility equipment damaged by a recent wildfire encountered handling difficulties that culminated in a precautionary landing and collision with trees. The pilot reported that the helicopter was flying at an altitude of approximately 100 feet above ground level (AGL) at speeds between 40 and 60 knots while assessing wildfire damage.

Sequence of Events

While rolling out of a turn at 100 feet AGL, the pilot noticed a reduction in airspeed. As he applied forward cyclic and raised the collective to regain desired airspeed and altitude, he felt resistance on the controls. The helicopter responded by assuming a nose-high attitude. The pilot stated that a high power setting was required to maintain altitude. Subsequently, the helicopter began to yaw to the right, which the pilot attributed to the onset of loss of tail rotor effectiveness (LTE).

In response to the yaw, the pilot reduced power. The helicopter then started to descend. The pilot decided to execute a precautionary landing. During the landing, the helicopter impacted trees and came to rest on its left side.

Post-accident Examination

An FAA inspector responded to the accident site and examined the wreckage. The inspection revealed no mechanical anomalies with the helicopter or its control system.

Conclusion

The investigation did not identify a specific mechanical failure or other causal factor. The pilot's actions in response to the perceived loss of tail rotor effectiveness and the subsequent precautionary landing resulted in the helicopter striking trees.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20071127X01859. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.