Casualties unknown

1987-05-28: Hiller UH-12E (N28875) — Olympic Air, Inc. — Shelton, WA

Shelton, WA, US

On May 28, 1987, a Hiller UH-12E (registration N28875) operated by Olympic Air, Inc. was involved in an aviation accident near Shelton, WA. Investigators recorded the probable cause as: Exceeding the normal flight envelope for the aircraft, resulting in mast bumping and separation of the main rotor. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive; 2 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 properly certificated pilot's first commercial flight as sole pilot ended with main rotor separation after mast bumping, likely from exceeding the aircraft's normal flight envelope during high-speed flight in turbulent conditions.

Incident Summary

A commercial helicopter flight ended with the main rotor separating in flight after the aircraft experienced mast bumping, a phenomenon associated with teetering rotor systems. The separation occurred as the aircraft was returning to base following a round-trip passenger flight, after passengers had disembarked. The accident happened during high forward speed in strong but intermittent wind conditions.

Pilot Background

The pilot was properly certificated for the flight. However, due to operator insurance restrictions, all prior commercial flights had required the aircraft's owner/operator to accompany this pilot. Consequently, this flight was the pilot's first commercial operation as the sole pilot in command.

Flight Conditions and Observations

Witnesses observed the aircraft proceeding at high forward speed in strong but intermittent wind conditions. Earlier during the same route, passengers had remarked about turbulence encountered during the flight.

Investigation Findings

Examination revealed that the main rotor separated in flight due to mast bumping. Mast bumping is a condition associated with teetering rotor systems, and the investigation determined that the envelope exceedance induced the event. Specifically, the aircraft exceeded its normal flight envelope, leading to the mast bumping and subsequent rotor separation.

Probable cause

Exceeding the normal flight envelope for the aircraft, resulting in mast bumping and separation of the main rotor.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001213X31041. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.