Ground loop during landing at Great Falls

Casualties unknown • Great Falls, MT, US

A tail-wheel aircraft experienced a loss of directional control and a ground loop during the landing roll at Great Falls.

What happened

During the landing phase on runway 03, the pilot was operating a tail-wheel equipped airplane. Shortly after touchdown, while the aircraft was in its roll-out, the pilot manually unlocked the tail wheel. Following the release of the tail-wheel lock, the pilot lost directional control of the aircraft.

The resulting ground loop caused substantial damage to the right wing of the aircraft. At the time of the accident, a METAR observation at Great Falls reported winds from 070 degrees at 6 knots. The occupants were not injured.

The investigation

An investigation of the aircraft revealed no mechanical malfunctions or failures that contributed to the event.

Probable cause

The loss of directional control occurred after the pilot manually unlocked the tail wheel during the landing roll.

Frequently asked questions

What happened in the 2001-07-21 Pilatus PC-6/B2-H4 accident near Great Falls, MT?

A tail-wheel aircraft experienced a loss of directional control and a ground loop during the landing roll at Great Falls.

What aircraft was involved and where did it happen?

The accident on 2001-07-21 involved a Pilatus PC-6/B2-H4, registration N2TS, operated by Thomas M. Siebel, at Great Falls, MT.

What was the probable cause of the accident?

The loss of directional control occurred after the pilot manually unlocked the tail wheel during the landing roll.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20010724X01499. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.

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