Left main landing gear collapse during taxi

Casualties unknown • Sand Point, AK, US

A tailwheel aircraft equipped with 29-inch tundra tires experienced a sudden veer to the right and subsequent gear collapse while slowing to taxi speed on a hard surface runway.

What happened

After landing on a hard surfaced runway, the pilot of a tailwheel airplane equipped with 29-inch tundra tires was reducing speed to taxi speed when the aircraft suddenly veered to the right. The pilot attempted to correct the deviation by applying full left rudder and left brake; however, the pilot could not straighten the aircraft before the left main landing gear collapsed.

The investigation

An examination of the tailwheel steering mechanism revealed that the anti-castoring limits were set below the break free force recommended by the manufacturer. This condition allowed the aircraft to turn to the right more freely and faster than the rudder control inputs intended to command.

Findings

Investigation into the handling characteristics of aircraft equipped with large tundra tires indicated that such aircraft are significantly more difficult to manage on hard surfaced runways compared to aircraft using conventional tires.

Probable cause

The anti-castoring limits on the tailwheel steering mechanism were below the manufacturer's recommended break free force, causing the aircraft to veer right more easily than controlled by rudder inputs, leading to the collapse of the left main landing gear.

Frequently asked questions

What happened in the 1995-06-03 Piper PA-18-150 accident near Sand Point, AK?

A tailwheel aircraft equipped with 29-inch tundra tires experienced a sudden veer to the right and subsequent gear collapse while slowing to taxi speed on a hard surface runway.

What aircraft was involved and where did it happen?

The accident on 1995-06-03 involved a Piper PA-18-150, registration N125FG, at Sand Point, AK.

What was the probable cause of the accident?

The anti-castoring limits on the tailwheel steering mechanism were below the manufacturer's recommended break free force, causing the aircraft to veer right more easily than controlled by rudder inputs, leading to the collapse of the left main landing gear.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001207X03601. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.

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