Aircraft veers into ditch following landing gear malfunction

Casualties unknown • Groveland, CA, US

A pilot experienced a partial retraction of the right main landing gear and a wing strike after touching down on a runway, causing the aircraft to veer into a ditch.

What happened

While approaching the destination airport, the pilot extended the wing flaps and lowered the landing gear, confirming the deployment via three green gear lights. The aircraft floated over the 3640-foot long runway, making initial contact with the surface approximately 800 to 900 feet beyond the threshold.

Following touchdown, the right main landing gear partially retracted, and the wing made contact with the runway surface. This sequence caused the aircraft to veer off the runway and into a ditch.

The investigation

An examination of the wreckage revealed that the wing flaps were in the retracted position and had sustained damage from ground impact. Investigators determined that the landing gear system was otherwise functioning normally.

Physical evidence indicated that during the rollout, the landing gear motor was activated while weight was being applied to the left main gear. This activation caused the left gear actuator arm to bend and led to the partial retraction of the right gear.

Probable cause

The activation of the landing gear motor during the aircraft rollout while weight was on the left main gear, causing a bending of the left gear actuator arm and subsequent partial retraction of the right gear.

Frequently asked questions

What happened in the 1992-05-25 Aerospatiale TB-20 accident near Groveland, CA?

A pilot experienced a partial retraction of the right main landing gear and a wing strike after touching down on a runway, causing the aircraft to veer into a ditch.

What aircraft was involved and where did it happen?

The accident on 1992-05-25 involved a Aerospatiale TB-20, registration N2824F, operated by Paul James, at Groveland, CA.

What was the probable cause of the accident?

The activation of the landing gear motor during the aircraft rollout while weight was on the left main gear, causing a bending of the left gear actuator arm and subsequent partial retraction of the right gear.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001211X14693. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.

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