FIELD: mechanical engineering; hatches of flying vehicles. SUBSTANCE: parallel link mechanisms are interconnected by means of shaft connecting the ends of bell cranks; shaft is located at area where main rollers are mounted for motion in guide rails mounted on fuselage perpendicularly to main rails. Guide roller is fitted on shaft of bell crank; is mounted on cover. Besides that, additional parallel link mechanism may be mounted. EFFECT: enhanced reliability. 2 cl, 1 dwg
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