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<p>The vertical tail of an aircraft typically consists of a fixed vertical stabilizer or fin on which a movable rudder is mounted. A trim tab may similarly be mounted on the rudder. Together, their role is to enable trim in the <a href="page.php?w=Aircraft_principal_axes">yaw</a> direction (compensate moments in yaw generated by any asymmetry in <a href="page.php?w=thrust">thrust</a> or <a href="page.php?w=Drag_%28physics%29">drag</a>), enable the aircraft to be controlled in yaw (for example, to initiate side slip during a <a href="page.php?w=crosswind_landing">crosswind landing</a>),</p><p>
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