At what speed will full rudder deflection exceed the limits of the rudder control system, in KIAS?

Full rudder deflection exceeding the limits of the rudder control system generally occurs at a specified speed, beyond which the aerodynamic forces on the rudder surfaces become too great for the control system to handle effectively. In typical aircraft operations, this threshold is usually determined by the design limits of the rudder and the control system itself, ensuring that the aircraft can be maneuvered safely without risking structural or control system failure.

In this case, the choice of 150 KIAS (Knots Indicated Airspeed) reflects a common design safety limit established for many aircraft, where full deflection of the rudder is still controllable without exceeding structural limits. This typically marks a critical speed where pilots need to be cautious with inputs to the rudder, as pushing beyond this limit could lead to diminished effectiveness or even potential control issues.

Understanding this limit is crucial for pilots to ensure they are flying within safe parameters, especially during operations that may require significant use of the rudder, such as during crosswind landings or while executing certain maneuvers.