Many small airplanes have a non-moveable metal trim tab on the rudder. This tab is bent in one direction or the other while on the ground to apply a trim force to the rudder.
The correct displacement is determined by trial-and-error process. Usually, small adjustments are necessary until you are satisfied that the airplane is no longer skidding left or right during normal cruising flight.
Brief and clear explanations of Aircraft Weight Control. This article describes about Aircraft Weight Control as a part of Aeronautical Knowledge Handbook.
AIRCRAFT SYSTEMS - OUTSIDE AIR TEMPERATURE GAUGE AND FUEL INJECTION SYSTEMS
OUTSIDE AIR TEMPERATURE GAUGE Most airplanes also are equipped with an outside air temperature (OAT) gauge calibrated in both degrees Celsi...
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The correct name for the tail section of an airplane is empennage. The empennage includes the entire tail group, consisting of fixed su...
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The control forces may be excessively high in some airplanes, and in order to decrease them, the manufacturer may use balance tabs. They loo...
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The fuselage includes the cabin and/or cockpit, which contains seats for the occupants and the controls for the airplane. In addition,...