Hydraulic Leakage Leads to Landing Gear Collapse in Piper PA-23

Casualties unknown • Shoreham Airport, West Sussex, GB

A Piper PA-23-250 experienced a left main landing gear collapse during landing at Shoreham Airport due to internal hydraulic leakage within the power pack.

What happened

On 18 December 1998, a Piper PA-23-250, registration G-BATX, was performing a private flight at Shoreham Airport, West Sussex. Following a series of low approaches and go-arounds, the pilot executed a normal approach and landed the aircraft. After touchdown and a significant reduction in speed, the left main landing gear leg began to collapse slowly. The pilot immediately shut down both engines, disconnected electrical services and fuel, and evacuated the two passengers.

During the subsequent salvage operation to clear the runway, airport management and fire services used an air bag to lift the left wing. While attempting to manually extend the left gear, the right main leg inadvertently retracted, causing the aircraft to fall onto the ground and resulting in damage to the right wing and the left propeller.

Probable cause

Internal leakage within the hydraulic power pack caused the loss of residual pressure in the landing gear extension line, allowing the downlock to become unseated and the gear to collapse.

Frequently asked questions

What happened in the 1998-12-18 Piper PA-23-250 accident near Shoreham Airport, West Sussex, GB?

A Piper PA-23-250 experienced a left main landing gear collapse during landing at Shoreham Airport due to internal hydraulic leakage within the power pack.

What aircraft was involved and where did it happen?

The accident on 1998-12-18 involved a Piper PA-23-250, registration G-BATX, at Shoreham Airport, West Sussex, GB.

What was the probable cause of the accident?

Internal leakage within the hydraulic power pack caused the loss of residual pressure in the landing gear extension line, allowing the downlock to become unseated and the gear to collapse.

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