??In the recent times, the aerospace industry is moving toward the development of more electric aircraft. This shift involves a transition from an hydraulic to an electric type of actuation. Conversion that promises to reduce the overall weight of the aircraft while increasing the efficiency of the system. However, the use of electric-type actuators called EMAs is currently limited to non-safety critical functions given the still basic insight into the behavior of these systems. ??To compensate for the lack of confidence in the EMAs systems, the use of prognostic techniques has found ample opportunity. The model-based approach described is intended to reproduce the behavior of an actuation characterized by reaction times that fall somewhere between those of a primary and a secondary flight control system.