A wire-strike system (1) including; a wire cutter with at least one pair of electrodes (5, 6), electrically insulated from each other and mounted to an outer surface of an aircraft (2). The electrodes (5, 6) being connectable to a power source (11) capable of generating an electrical potential difference between the electrodes (5, 6) and in the event of a wire-strike, supplying a short-circuit current flow through a portion of the wire connecting both electrodes (5, 6).
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