Plates laminated by the mulitilayers of the composite materials show different behaviors at each layer. Coupling effects of shearing stresses at layers make it more difficult to analyze them. In this paper, three-variable simulataneous partial differential equations for anisotropic laminated plates are derived and finite difference method for analysis of them is developed. Finite difference method in this paper is used to obtain more exact responses of them in a few mesh number. It is shown that deflections, stresses at layers, and member forces of them have different distributions compared with those of orthotropic or isotropic plate. Theory and Analysis of anisotropic laminated plate proposed in this paper should be used in design of them.