Casualties unknown

2000-12-28: Hughes 369HS (N9186F) — Pierce, ID

Pierce, ID, US

On December 28, 2000, a Hughes 369HS (registration N9186F) was involved in an aviation accident near Pierce, ID. Investigators recorded the probable cause as: While maneuvering, clearance from an object was not maintained. A tree was a factor. 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

A helicopter conducting an aerial survey at low altitude struck a dead tree on a ridge, resulting in an inverted crash. The passenger reported no mechanical anomalies before the impact, and post-crash inspection found no evidence of failure.

Flight Maneuvers

During an aerial survey flight, the helicopter was maneuvering to position for another run along a contour line in mountainous terrain. The flight elevation along the contour was reported to be about 150 feet above ground level. The terrain was covered with deciduous and coniferous trees varying in height to about 50 feet.

Passenger Account

The surviving passenger, seated directly behind the pilot on the left side, reported that the helicopter was making a descending right turn when he suddenly felt a jolt. He saw the pilot's head jerk up as the helicopter pitched straight up, then fell backwards and collided with the terrain in an inverted and nose low attitude at the base of a dead tree located on an outcropping along a ridge. This tree was taller than any of the surrounding trees and the top was broken off. The snag was dark in coloration and void of branches. Plexiglas fragments and two rivets were found embedded in the section that broke off.

Impact Damage

Structural impact signatures noted that the helicopter came in contact with the tree on the right side lower fuselage section with rearward crushing damage through the anti-torque pedals and traveling aft to the cyclic control stick socket. Wood particles were embedded within the deformed fuselage structure and also to the forward section of the landing skids.

Post-Crash Inspection

The passenger reported that he did not detect any mechanical anomalies prior to the jolt, nor did the pilot indicate any problems over the headset prior to the collision. Post-crash inspection of the wreckage did not reveal evidence of a mechanical failure or malfunction.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20010104X00011. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.