What is the minimum torque requirement for an aileron roll?

The minimum torque requirement for an aileron roll in the T-6A is 80%. This means that when performing an aileron roll, the aircraft must have at least 80% of its maximum available torque to ensure sufficient power for the maneuver. The reason for this requirement is tied to maintaining the aircraft's performance during the roll, specifically ensuring that the roll is executed safely and effectively without risking a stall or loss of control.

In practical terms, having adequate torque allows the aircraft to perform the roll with the necessary speed and energy, which is particularly important as the maneuver involves a change in orientation and can impose additional aerodynamic loads on the airframe. With less than 80% torque, the roll may be sluggish or could result in an incomplete maneuver, potentially compromising safety.

Understanding this requirement is essential for pilots to ensure they have the required power available for performing dynamic flight maneuvers, such as the aileron roll, while maintaining control and safety of the aircraft.