1. Plane "classic biplane Biryukova" to improve safety, comprising a fuselage, two identical tandem arranged and spaced along the length of the fuselage and wings full aerodynamic control surfaces changes the direction of the flight located on wings, wherein the wings are made aerodynamically clean, aerodynamic control surfaces located on both sides of the wing surfaces and the fuselage has a fuselage aerodynamic channel formed by the bottom of the fuselage and the walls of the fuel bakov.2. Aircraft according to claim 1, characterized in that the intervals comprise fuel tanks in the form of cavities shassi.3. The aircraft according to claim 1, characterized in that the wheel motors to the chassis include acceleration and deceleration koles.4. Aircraft according to claim 1, characterized in that the gear wheels comprise a blade aerodynamic front wheels to spin posadkoy.5. Aircraft according to claim 1 characterized in that the aerodynamic control surfaces and the braking device are correct and the airplane in flight and on landing.
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