What is the maximum aileron deflection in degrees for the T-6A?

The maximum aileron deflection for the T-6A is ±20 degrees. This limit is critical for maintaining the aircraft's stability and control during flight maneuvers. Ailerons, which control roll, are designed to provide adequate responsiveness while ensuring the aircraft remains within safe operational parameters. The ±20 degrees deflection serves to optimize roll rate without compromising safety or risking adverse aerodynamic effects, such as adverse yaw or excessive bank angles. Understanding and adhering to this limit is essential for pilots in order to operate the aircraft effectively and safely, especially during training exercises and advanced maneuvers.