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As flight control actuation systems become more complex，a multidisciplinary approach is needed to understand the interactions between diverse systems including electrical，mechanical，hydraulic，and control systems. In addition，the development of flight control actuation(FCA)systems is being transformed by its integration into computer aided engineering process. This presentation explores the interactions between diverse systems including electrical，mechanical，hydraulic，control systems in a FCA system and its integration into different CAE attribute analysis like flexible multi-body analysis，stress analysis，and fatigue damage prediction.