Casualties unknown

Turbine Shaft Failure Leads to Autorotation Water Landing (N5013F)

West Delta 105, US

On September 26, 1984, a Bell 206L-1 (registration N5013F) operated by Commercial Helicopters was involved in an aviation accident near West Delta 105. Investigators recorded the probable cause as: Frictional overheating and subsequent failure of the turbine inner shaft due to carbon buildup between the turbine-to-compressor coupling and the turbine inner shaft. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive; 1 related events involving the same aircraft type or operator are linked below.

Sourcesthe U.S. National Transportation Safety Board (NTSB) historical archivePrimary reportUpdated 2026-06-20Data APIEditorial standards

A total power loss during cruise forced a pilot to execute an autorotative water landing with emergency floats. The aircraft rolled inverted because the right float failed to fully inflate upon impact.

What happened

During a cruise phase of flight, the aircraft experienced a complete loss of power. The pilot initiated procedures for an autorotative water landing and deployed the emergency flotation system. Upon touchdown on the water, the right float did not fully inflate. This failure caused the aircraft to roll to the right, resulting in an inverted position.

The investigation

A teardown of the engine was conducted to determine the root cause of the power loss. Examination revealed significant carbon buildup located between the turbine-to-compressor coupling and the turbine inner shaft. This accumulation caused frictional overheating, which ultimately led to the failure of the shaft.

Probable cause

Frictional overheating and subsequent failure of the turbine inner shaft due to carbon buildup between the turbine-to-compressor coupling and the turbine inner shaft.

Frequently asked questions

What happened in the 26 Sept 1984 Bell 206L-1 accident near West Delta 105?

A total power loss during cruise forced a pilot to execute an autorotative water landing with emergency floats. The aircraft rolled inverted because the right float failed to fully inflate upon impact.

What aircraft was involved and where did it happen?

The accident on 26 Sept 1984 involved a Bell 206L-1, registration N5013F, operated by Commercial Helicopters, at West Delta 105.

What was the probable cause of the accident?

Frictional overheating and subsequent failure of the turbine inner shaft due to carbon buildup between the turbine-to-compressor coupling and the turbine inner shaft.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001214X41095. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.