The forces acting on the aircraft structure could lead to the occurrence of change of shape or structure of the failure as a case that is often found on one of the components of the outboard ground spoilers on the actuator housing. So to find out the limit of the power structure it needs to be done analysis by doing modeling, see where the voltage value and calculate maksimuk crisis margin of safety. Modeling and analysis done on the structure of housing outboard ground spoiler actuator using software CATIA V5R20. Methods of analysis conducted is static analysis method by utilizing facilities generative structural analysis on CATIA V5R20 softwere. The imposition on the research style lift and drag on models of outboard housing ground spoiler actuator that is different based on the type of connection in software CATIA V5R20 i.e. fastened connection, rigid connection and pressure fittings connection.
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