Casualties unknown

1996-04-27: Beech B55 (N1580W) — Lynchburg, VA

Lynchburg, VA, US

On April 27, 1996, a Beech B55 (registration N1580W) was involved in an aviation accident near Lynchburg, VA. Investigators recorded the probable cause as: The pilot's failure to maintain directional control during the landing roll, which resulted in an inadvertent ground loop/swerve and landing gear collapse. A related factor was the strong crosswind. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive.

Sourcesthe U.S. National Transportation Safety Board (NTSB) historical archivePrimary reportUpdated 1781061362Data APIEditorial standards

A pilot reported that after a preflight inspection revealed a flat right main landing gear strut, a mechanic inflated it. During landing with 18-knot crosswinds, the aircraft veered left, exited the runway, and collapsed the main landing gear.

Incident Overview

A pilot experienced a landing gear collapse after his aircraft veered off the runway during the landing roll. The incident occurred when the nosewheel touched down on runway 21, causing the aircraft to turn left. Despite applying full right rudder and brake, the pilot was unable to correct the deviation, and the aircraft exited the runway.

Preflight Inspection

Before departure, the pilot completed a preflight inspection and noticed that the right main landing gear strut was flat. A mechanic subsequently inflated the strut, after which the pilot proceeded with the takeoff.

Landing and Ground Loop

During the landing roll, as the nosewheel contacted the runway surface, the aircraft began to veer to the left. The pilot attempted to counter this by applying maximum right rudder and brake inputs. However, the aircraft continued its leftward movement, departing the runway surface. The forces generated during the subsequent ground loop caused the main landing gear to collapse. The pilot reported that no mechanical malfunction occurred and that the gear collapse resulted solely from side loads during the ground loop.

Wind Conditions

The pilot indicated that the wind was from 240 degrees at 18 knots at the time of the landing.

Postaccident Examination

A postaccident examination of the aircraft revealed no evidence of any preimpact anomaly or mechanical failure.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001208X05593. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.