Incident Overview

Date: Saturday 25 April 2015
Aircraft Type: Dassault Falcon 20D
Owner/operator: Cobham Aviation Services
Registration Number: G-FRAK
Location: 37 km S of Portland Bill – ÿ United Kingdom
Phase of Flight: Manoeuvring (airshow, firefighting, ag.ops.)
Status: Substantial, repaired
Casualties: Fatalities: 0 / Occupants: 3
Component Affected: The leading edge of the wing.The leading edge of the wing.
Investigating Agency: AAIBAAIB
Category: Accident
An aircraft was recovering a military target during target towing operations over the English Channel. A turbine-powered winch accelerated rapidly, causing the target to strike the leading edge of the wing before detaching. While the launcher and droop leading edge were damaged, the aircraft landed safely. The acceleration was attributed to the winch’s overspeed due to a faulty closed limit switch.An aircraft was recovering a military target during target towing operations over the English Channel. A turbine-powered winch accelerated rapidly, causing the target to strike the leading edge of the wing before detaching. While the launcher and droop leading edge were damaged, the aircraft landed safely. The acceleration was attributed to the winch’s overspeed due to a faulty closed limit switch.

Description

The aircraft was undertaking target towing operations for a military exercise and was recovering the target whilst flying in an assigned danger area over the English Channel. With the target approximately 40 m from the aircraft, the target winch accelerated rapidly and the target struck the leading edge of the wing before detaching and travelling over the wing. Although, the launcher and the droop leading edge on the wing were damaged, the aircraft landed safely. The target winch is powered by a turbine, and the speed of the turbine is controlled by vent doors. The target winch had oversped due to a fault with the closed limit switch on the vent doors which prevented the doors from closing. The target accelerated during the latter stages of its recovery, causing it to strike the aircraft. The acceleration was probably due to an overspeed of the target winch as a result of the failure of the vent door closed limit switch preventing the vent doors from closing when commanded. The turbine would then have spooled up, increasing the torque and resulting in the winch accelerating.

Primary Cause

Faulty closed limit switch on the vent doors of the target winch caused the winch to accelerate.Faulty closed limit switch on the vent doors of the target winch caused the winch to accelerate.

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