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SENARBET Wiring adds a considerable amount of weight to an aircraft; therefore, researchers are exploring implementing fly-by-wireless solutions. The biggest benefits are weight savings, the possibility of redundant power circuits and tighter integration between the aircraft flight control systems and its avionics systems. All benefits of digital fly-by-wire are retained since the power-by-wire components are strictly complementary to the fly-by-wire components. The power circuits power electrical or self-contained electrohydraulic actuators that are controlled by the digital flight control computers. This system is used in the Lockheed Martin F-35 Lightning II and in Airbus A380 backup flight controls. To accomplish this, it uses an existing standard that defines a suitable physical layer and medium access control, through which the desired performance can be met, and it adds to it a convergence layer to merge both architectural efforts. The absence of hydraulics greatly reduces maintenance costs.|But what's beyond these Basic Controls?