Right Main Landing Gear Collapse During Go-Around

Casualties unknown • Denver, CO, US

An aircraft experienced a right main landing gear collapse during a go-around after an intermittent unsafe indication occurred during the landing roll.

What happened

Following takeoff, the right main landing gear failed to retract. After reviewing available procedures, the crew elected to continue the flight to their destination.

Upon arrival, the pilots selected the landing gear to the down position. All landing gear indicated down and locked, and the captain visually verified that the right main gear was in place. During the landing roll, as the aircraft passed through approximately 60 knots, the indication for the right main landing gear provided an intermittent unsafe signal. In response, the pilot flying applied power to initiate a go-around. During this maneuver, the right main landing gear collapsed. The aircraft slid and rolled to a stop on the runway, and all occupants were not injured during an uneventful evacuation.

The investigation

An examination of the right main landing gear assembly revealed that the extension/retraction actuator had failed at the spherical bearing. A metallurgical examination determined that the spherical bearing had suffered a fatigue failure, with evidence of wear and binding in certain positions. The component was found to be dry, with no evidence of lubrication. A review of the aircraft's maintenance records and procedures indicated that all required inspections and maintenance had been completed according to applicable directives.

Probable cause

The fatigue failure of the spherical bearing in the landing gear extension/retraction actuator due to wear, binding, and a lack of lubrication.

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Frequently asked questions

What happened in the 1996-05-02 Beech 1900D accident near Denver, CO?

An aircraft experienced a right main landing gear collapse during a go-around after an intermittent unsafe indication occurred during the landing roll.

What aircraft was involved and where did it happen?

The accident on 1996-05-02 involved a Beech 1900D, registration N154ZV, operated by Mesa Airlines, Inc., at Denver, CO.

What was the probable cause of the accident?

The fatigue failure of the spherical bearing in the landing gear extension/retraction actuator due to wear, binding, and a lack of lubrication.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001208X05744. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.

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