Casualties unknown

2011-04-23: Piper PA-23-250 Aztec (N40267) — Virgin Gorda Airport, British Virgin Islands, GB

Virgin Gorda Airport, British Virgin Islands, GB

On April 23, 2011, a Piper PA-23-250 Aztec (registration N40267) was involved in an aviation accident near Virgin Gorda Airport, British Virgin Islands, GB. Investigators recorded the probable cause as: The left main landing gear was not fully locked down, which resulted in the actuator being subjected to excessive loads that caused it to fail. The investigation did not determine why the left landing gear was not fully locked down. This summary draws on records from the UK Air Accidents Investigation Branch (AAIB).

Sourcesthe UK Air Accidents Investigation Branch (AAIB)Primary reportUpdated 1785658417Data APIEditorial standards

On 23 April 2011, a Piper PA-23-250 Aztec (N40267) experienced a left main landing gear collapse during landing at Virgin Gorda Airport. The pilot reported selecting gear down with three green lights, but the gear was not fully locked, causing actuator failure. No injuries.

Introduction

On 23 April 2011, at 1815 hours UTC, a Piper PA-23-250 Aztec, registration N40267, sustained damage during a landing accident at Virgin Gorda Airport, British Virgin Islands. The aircraft was operated on a commercial air transport (non-revenue) flight with a single pilot and no passengers. The pilot, holding a Commercial Pilot's Licence with 4,500 hours total experience (200 on type), was uninjured.

Event

The pilot selected the landing gear down and observed three green landing gear position lights, indicating that all gear appeared down and locked. A normal landing was performed on Runway 03. As the aircraft decelerated, the landing gear warning horn sounded. The aircraft subsequently rolled to the left until its left wing and propeller contacted the runway surface. The aircraft skidded for a further 100 feet before coming to rest on the left side of the runway. The pilot shut down the engine and vacated the aircraft without injury.

Damage

The damage comprised the underside of the left wing, left flap, landing gear doors, left propeller, left main landing gear, and its actuator.

Investigation

Examination revealed that the left main landing gear actuator had failed in overload. It is likely that the left main landing gear was not fully locked down before landing, which resulted in the actuator being subjected to excessive loads that caused it to fail. The investigation did not determine why the left landing gear was not fully locked down.

Probable cause

The left main landing gear was not fully locked down, which resulted in the actuator being subjected to excessive loads that caused it to fail. The investigation did not determine why the left landing gear was not fully locked down.