FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering. Aircraft comprises fuselage with nose and tail ends, wings, system of fuel tanks, power plant and undercarriage arranged to wings and/or fuselage. Fuselage has control cabin, cargo and/or manned compartment, and outer empennage. Said fuselage houses skin stiffness elements and structural floor. Aircraft is equipped with onboard systems and equipment. Manned compartment skin is composed of inner untight part and outer tight part. Manned compartment inner skin is made of high-strength synthetic reinforced composite, for example, coal-plastic to rest on outer skin via resilient flexing supports.
EFFECT: reduced takeoff weight.
3 dwg
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