Abstract: A helicopter cyclic control assembly for redirecting the thrust produced at a main rotor assembly includes a rotor disc control plate having arms with arm tubes therein for close, slideable insertion of slide rods, the slide rods being pivotally attached to bi-directional linear actuators, the bi-directional linear actuators being attached to the helicopter transmission casing or main truss works. The rotor disc control plate also having a neck tube with a bore which passes through the rotor disc control plate, through which an upper shaft passes and is rotatably engaged, the neck tube being perpendicular to the arm tubes.