Landing gear collapse during landing of aircraft

No fatalities • West Jordan, United States of America • Landing (descent or approach)

An aircraft experienced a landing gear collapse and separation during its landing roll after the pilot reported a lack of a green down-and-locked indication for the left main gear.

What happened

Following the deployment of parachutists from the aircraft, the pilot returned to the airfield and observed that the left main landing gear lacked a green down-and-locked indication. In response to this indication, the pilot performed emergency protocols and conducted two fly-bys of the runway to assess the situation. While ground staff noted that the landing gear appeared to be properly extended and locked, the aircraft experienced a lateral slide during the landing roll. During this sliding motion, the right main landing gear collapsed and eventually detached from the airframe. The left main gear subsequently collapsed as the aircraft slid to a halt.

Findings

An inspection of the wreckage revealed that the upper torque knee on the left main landing gear had sustained a break. The specific mechanism or mode that led to the failure of this upper torque knee remained undetermined.

Probable cause

The failure mode of the broken upper torque knee on the left main landing gear was not identified.

Frequently asked questions

What happened in the 1997-04-19 Beechcraft 90 King Air accident near West Jordan, United States of America?

An aircraft experienced a landing gear collapse and separation during its landing roll after the pilot reported a lack of a green down-and-locked indication for the left main gear.

Were there any fatalities in the 1997-04-19 Beechcraft 90 King Air accident?

No fatalities were recorded in this accident.

What aircraft was involved and where did it happen?

The accident on 1997-04-19 involved a Beechcraft 90 King Air, registration N616AS, operated by Fayard Enterprises, at West Jordan, United States of America.

What was the probable cause of the accident?

The failure mode of the broken upper torque knee on the left main landing gear was not identified.

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