FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, particularly, to aircraft fuselage compartment. Method of producing fuselage compartment formed by top skin 4 and bottom skin 20 as well as by floor frame 13 consists in making thermal isolation of skin element surface and fitting service rigging systems (1-3, 10-12, 22-24) into skin element and floor frame. Then skin element and floor frame are assembled into fuselage section 32. Note here that said service rigging systems comprise electrical and hydraulic lines, air conditioning lines, electric and hydraulic devices, sanitary and bar-galley equipment.
EFFECT: simplified mounting in fuselage assembly.
9 cl, 6 dwg
