No fatalities

2018-04-20: McDonnell Douglas MD-83 (N807WA) — World Atlantic Airlines — Alexandria-Esler Regional, United States of America

Alexandria-Esler Regional, United States of AmericaLanding (descent or approach)

On April 20, 2018, a McDonnell Douglas MD-83 (registration N807WA) operated by World Atlantic Airlines was involved in an aviation accident near Alexandria-Esler Regional, United States of America during landing or approach. No fatalities were reported. Investigators recorded the probable cause as: The failure of the right main landing gear under normal loads due to fatigue cracking in an area subject to an FAA Airworthiness Directive that was not adequately inspected. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A).

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781191475Data APIEditorial standards
Aircraft registered N807WA
Aircraft registered N807WA. Photo: Venkat Mangudi / CC BY 2.0, via Wikimedia Commons

During landing, the right main landing gear collapsed, causing substantial lower wing skin damage. An emergency evacuation was performed; the left forward escape slide failed. Investigation uncovered a fatigue crack missed during inspections required by an Airworthiness Directive.

Accident Overview

The airplane experienced a right main landing gear collapse while landing at the destination airport. The right lower wing skin sustained substantial damage when it contacted the runway. The crew brought the airplane to a stop on the runway and initiated an emergency evacuation through three of the four available doors.

Escape Slide Malfunction

The escape slide at the left forward door failed to deploy or inflate. The failure was attributed to depletion of the gas charge in the slide's reservoir. The reservoir had been leaking through the valve assembly, and the leak was not detected during multiple inspections performed after the slide assembly was installed on the airplane.

Landing Gear Failure

The landing gear cylinder fractured under normal landing loads. Metallurgical examination revealed a fatigue crack on the forward side of the cylinder, located in an area subject to inspections mandated by an Airworthiness Directive (AD). The most recent AD inspection had been conducted 218 landings prior to the accident; at that time, the fatigue crack was large enough to be detectable. A previous AD inspection, performed 497 landings before the accident, also failed to identify the crack, which would have been marginally detectable at that point.

Probable Cause

The official finding stated the probable cause as: "The failure of the right main landing gear under normal loads due to fatigue cracking in an area subject to an FAA Airworthiness Directive that was not adequately inspected."