FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, particularly, to VTOL aircraft. Aircraft comprises airframe with wing 1, two spaced apart lengthwise beams 2, horizontal and vertical fins 3, 4. Wing 1 is connected with lengthwise beams 2. Power plants including engines and propellers 5 are arranged at the ends of said beams. Horizontal fins 3 can be arranged both at nose section and at tail section. Payload is arranged in detachable container 7 secured to pylon 9 under wing 1.
EFFECT: simplified transfer of out-of-gage cargoes.
6 cl, 10 dwg
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