Landing Gear Collapse During Final Approach

Casualties unknown • Gulfport, MS, US

A scheduled domestic passenger flight experienced a complete landing gear collapse during touchdown after multiple extension attempts failed, resulting in an emergency evacuation.

What happened

The aircraft was operating a Part 135 scheduled domestic passenger flight when the incident occurred during the final approach phase. The pilot noticed that the nose landing gear had failed to fully extend. In an effort to resolve the issue, the pilot cycled the landing gear controls, but the system again failed to achieve full extension. Following this unsuccessful attempt, the pilot activated the emergency gear extension procedure. Despite these efforts, the landing gear did not deploy correctly.

The approach was continued to touchdown. Upon contact with the runway, the entire landing gear assembly collapsed. The aircraft slid along the runway surface before coming to a complete stop. All passengers were safely evacuated from the aircraft using the emergency exits.

The investigation

Post-incident examination of the aircraft revealed that the right main landing gear actuator end cap had failed. This failure was attributed to fatigue, which allowed hydraulic pressure and fluid to leak from the system, preventing proper gear operation.

Probable cause

The failure of the right main landing gear actuator end cap due to fatigue, which caused a loss of hydraulic pressure and prevented the landing gear from extending.

Frequently asked questions

What happened in the 1987-11-06 Beech 99 accident near Gulfport, MS?

A scheduled domestic passenger flight experienced a complete landing gear collapse during touchdown after multiple extension attempts failed, resulting in an emergency evacuation.

What aircraft was involved and where did it happen?

The accident on 1987-11-06 involved a Beech 99, registration N6724D, operated by Air New Orleans, at Gulfport, MS.

What was the probable cause of the accident?

The failure of the right main landing gear actuator end cap due to fatigue, which caused a loss of hydraulic pressure and prevented the landing gear from extending.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001213X32576. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.

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