In this paper fluid dynamic analysis and pressure distribution analysis is performed using finite element method for the Remote Controlled (RC) aircraft wing. The attachment joints are inevitable in any large structure like an airframe. The wings are the most important lift-producing part of the aircraft. Wings vary in design depending upon the aircraft type and its purpose. Remote controlled airplane models are of great importance in the present era. They are used by scientific,government and military organizations for experiments,gathering weather readings,aerodynamic modelling and testing,and as drones or spy planes. Finally,it is concluded that the selection of airfoil,choosing the right thrust,wing dimensions,calculation of lift and drag forces a wing which is optimum for a small,slow flying RC airplane. © 2016,International Journal of Pharmacy and Technology. All rights reserved.