FIELD: aeronautical engineering; transportation of aircraft fuselages in cargo compartment of flying vehicle. SUBSTANCE: device for tie-down of fuselage 1 of aircraft has compression strut 2 mounted on front undercarriage leg 3, ears mounted on main undercarriage legs 5 and bracing wires 6 secured on load-bearing floor 7 at one end and on compression strut 2 and in ears at other end. Device is provided with pivot units 8, additional bracing wires 9 and cross-pieces; each cross-piece is provided with fork and roller. Each pivot unit 8 is made in form of shaft. EFFECT: enhanced reliability and improved service characteristics.
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