Turbine engine (110) having a nacelle (126) comprising, upstream, an air intake fairing (126a) and an element (140) for deflecting foreign objects which defines with said fairing an air intake flow path for supplying air to two coaxial flow paths, namely a radially inner and a radially outer flow path, said outer flow path being defined by a hub housing (152) and scoops, said hub housing (152) and said scoops (144) being installed downstream of the element (140) for deflecting objects, characterised in that each scoop comprises two independent portions, namely an upstream portion (144a) borne by the hub housing (152) and a downstream portion (144b) borne by the nacelle (162).