![]() ![]() Primary Flight Control Aileron Control System Ailerons are mounted on the trailing edge of each wing near the wingtips, and move in opposite directions. Action Push / pull rod or cableĪn Elevator Control System of a Commercial Aircraft Primary Flight Control Elevator Control System Drive or climb Rotate around lateral axis Forward and aft. Many aircraft use a stabilator - a moveable horizontal stabilizer - in place of an elevator. This makes the wings fly at a higher angle of attack which generates more lift and more drag. Raised elevators push down on the tail and cause the nose to pitch up. Pushing the stick forward causes the elevators to go down. When the pilot pulls the stick backward, the elevators go up. Primary Flight Control Elevator Control System An elevator is mounted on the back edge of the horizontal stabilizer on each side of the fin in the tail. ![]() They can be divided into three main groups: - Primary flight control - Secondary flight control - Auxilliary flight control Aircraft engine controls are also considered as flight controls as they change speed. Introduction Aircraft flight control systems consist of flight control surfaces, the respective cockpit controls, connecting linkages, and the necessary operating mechanisms to control an aircraft's direction in flight. ![]() Outline of Presentation Introduction Primary flight control - Elevator Control System - Aileron Control System - Rudder Control System Secondary flight control - Elevator Trim Tab System - Rudder and Aileron Trim Tab System Auxilliary flight control - Flap Control System - High Lift Devices ![]()
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