Rudder Trim Tab

Rudder Trim Tabs are a type of airframe structural component that falls under the supply class Airframe Structural Components in the supply group Aerospace Craft And Structural Components.

Rudder Trim Tabs are small, movable surfaces attached to the trailing edge of the rudder on an aircraft. They are used to adjust the trim or balance of the aircraft during flight. By deflecting the rudder trim tab, the pilot can counteract any imbalances or asymmetrical forces that may affect the aircraft's stability.

The purpose of the rudder trim tab is to reduce the amount of control force required by the pilot to maintain the desired flight path. By adjusting the trim tab, the pilot can achieve a neutral or balanced rudder position, which helps in reducing the workload on the pilot and improving the overall handling characteristics of the aircraft.

Rudder trim tabs are typically controlled by a separate trim control mechanism, which allows the pilot to make small adjustments to the trim tab position. These adjustments can be made either manually or electrically, depending on the aircraft's design.

Overall, rudder trim tabs play a crucial role in maintaining the stability and control of an aircraft during flight, ensuring a smooth and efficient flying experience for the pilot and passengers.