Aircraft control locking apparatus

B - Operations – Transporting – 64 – C

Patent

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Details

B64C 13/14 (2006.01)

Patent

CA 2068305

ABSTRACT OF THE DISCLOSURE An aircraft control locking apparatus for a control yoke on a control shaft extending from an instrument panel in an aircraft is provided. The aircraft control locking apparatus utilizing a pair of elastic shock cords, a first mechanism for connecting an upper end of each of the elastic shock cords in a spaced apart relationship to the control yoke and a second mechanism for connecting a lower end of each of the elastic shock cords in a spaced apart relationship to a fixed point on the instrument panel below the control shaft. The control lock retains the control yoke in a neutral position, keeping the control surfaces of the aircraft from moving freely, thereby preventing damage to the aircraft stored outdoors during periods of strong gusty winds in severe weather. -8-

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