Aircraft Rudder

Aircraft rudders are a type of airframe structural component that belongs to the supply class Airframe Structural Components in the supply group Aerospace Craft And Structural Components.

The rudder is a movable control surface located at the trailing edge of the vertical stabilizer (also known as the fin) of an aircraft. It is typically hinged and can be deflected to the left or right to control the yaw motion of the aircraft. Yaw refers to the rotation of the aircraft around its vertical axis.

The primary function of the rudder is to provide directional control during flight. By deflecting the rudder, the pilot can induce a yawing moment, which helps the aircraft turn left or right. This is particularly important during takeoff, landing, and maneuvering.

Aircraft rudders are typically made of lightweight yet strong materials such as aluminum or composite materials. They are designed to withstand the aerodynamic forces and loads experienced during flight.

In addition to the rudder, other airframe structural components in the supply class Airframe Structural Components may include wings, fuselage sections, stabilizers, control surfaces, and other structural elements that contribute to the overall strength and stability of the aircraft.

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