Casualties unknown

1999-08-26: Bell 47G-2 (N11VH) — Beightol, Steven, L. — Benton City, WA

Benton City, WA, US

On August 26, 1999, a Bell 47G-2 (registration N11VH) operated by Beightol, Steven, L. was involved in an aviation accident near Benton City, WA. Investigators recorded the probable cause as: A loss of power for undetermined reasons and the failure of the pilot to maintain adequate rotor RPM following the power loss. Contributing factors were the pilot's lack of certification and total experience. 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 non-certificated pilot with limited flight experience crash-landed a homebuilt helicopter after reporting engine issues. Witnesses heard a popping sound followed by silence and smoke.

Accident Overview

A non-certificated pilot, who had been constructing the helicopter over several years, was operating the aircraft when it descended steeply and impacted terrain. The wreckage was confined to a small area, and a post-crash fire heavily damaged the center portion of the helicopter, including the engine and transmission.

Pilot Experience

The pilot had accumulated 5 hours of flight experience in 1988 and an additional 10 hours between July 19 and August 24, 1999. Although all flights were logged as 'dual,' family members reported that several of the eight flights conducted in 1999—all in the accident helicopter—were flown solo.

Witness Accounts

An ear witness reported hearing the helicopter depart, followed by a 'popping' sound and then silence. Shortly after, the witness observed a plume of smoke.

Mechanical Issues

A mechanic stated that the pilot had reported engine problems and borrowed a used carburetor. The pilot's logbook contained an entry dated August 16, 1999, with the remark: 'flight test changed carb running good.'

Damage and Indicators

The rotor blades exhibited minimal leading-edge damage. The engine/rotor RPM indicator displayed 0 RPM for the engine and 170 RPM for the rotor at the accident site.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001212X19655. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.