FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering. Proposed section comprises wing root 7, 8 with wing 1 jointed with fuselage 2, fuselage section 3 with fuselage frame elements 11-15, 21-25 extending along aircraft lengthwise axis, and wing section 5, 6 with spars 16-19, 26-29 extending along wing span. In compliance with this invention, said spars and said fuselage frame elements make integral assembly 40 including, at least, inner wing 1 and fuselage section 3 comprises wing root sections 7, 8.
EFFECT: simplified assembly, decreased weight.
24 cl, 16 dwg
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