The invention concerns a control wheel (100) for aeronautics constituted of at least two half-shells (10) assembled one to the other, said half-shells comprising reinforcing ribs (11) on their internal surface, positioning and fixing means (12) and locating holes (13) to allow the passage of electrical wires connecting electrical actuating means (20) to a control unit. The control wheel (100) includes a central opening (15) intended to be connected to a control shaft/hub. The wheel comprises an intermediate guide part (50) disposed between the half-shells (10) and positioned inside the control wheel (100), said part including at least one guide conduit (51) adapted to connect on the one hand a locating hole (13) to the central opening (15) of the control wheel (100).