The system splits logically into pitch–yaw (tailplane and rudder) and roll (aileron) control runs respectively. Figure 3 shows a simplified three dimensional schematic of the Hawk 200 flight control and levers -which is indicated in red circles- used in the control system. These standards exceed the military specifications that govern aircraft flight control cables. Our quality assurance procedures and personnel are relentless, ensuring that our aircraft flight control cables meet the highest standards possible. Push-pull rods get their name from the way they transmit force. McFarlane Aviation flight control cables offer quality that is second to none in the aircraft industry. In the push-pull control rod system, metal push-pull rods are used as a substitute for the cables. Movement of the cockpit controls transfers force through the cable to the bell crank, which moves the control surface. The bell crank is connected to the control surface. In the cable and pulley system, cables are connected from the control in the cockpit to a bell crank or sector. These are push-pull control rod systems and cable and pulley systems. There are presently two main methods of connecting the pilot’s controls to the rest of the flight control system. Other more sophisticated flight control systems may use electrical or hydraulic power to provide. A simple flight control system may be all mechanical that is, operated entirely through mechanical linkage and cable from the control stick to the control surface.
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