FIELD: transport; dynamic air cushion crafts. SUBSTANCE: landing gear has stub wing leading-edge sweep, flaps and plates, engines with rotatable nozzles mounted on pylon secured in front of the wing on craft body. Longitudinal axis of symmetry of each nozzle is parallel to diametral plane of craft. Device has at least two additional engines with rotatable nozzles arranged inside craft body symmetrically relative to its diametral plane and at an angle to diametral plane in horizontal plane. Axis of symmetry of nozzle of each additional engine is arranged at angle to diametral plane of craft found from following equation: 
where l - wing span; Bb - craft body width; S - distance between exit of additional engine rotatable nozzle and wing nose rib in plane of craft body side; χ - sweepback angle at leading edge. EFFECT: enhanced reliability. 2 dwg
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