FIELD: aeronautical engineering; manufacture of vertical takeoff and landing aircrafts. SUBSTANCE: airbus includes at least two fuselages connected by means of transversal beams of aerodynamic profile. Two stages of wings together with two rows of gas-turbine engines mounted in front of them form thrust lift complexes. Wings are secured between fuselages by means of cantilevers for turn about their longitudinal axes. Rear thrust lift complex is located above front one. EFFECT: extended ranged of service characteristics of airbus. 2 cl, 2 dwg
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