The split flaps on the T-6A are controlled and operated in what manner?

The correct answer is that the split flaps on the T-6A are electrically controlled and hydraulically operated. This means that the pilot uses electrical inputs to signal the flaps to move, while the actual motion is executed through a hydraulic system.

In aircraft design, using electric control with hydraulic operation allows for precise and responsive flap adjustments, improving the handling characteristics during critical flight phases such as takeoff and landing. The electrical control system can ensure that adjustments can be made quickly and efficiently, while the hydraulic system provides the necessary power to move the flaps against the aerodynamic forces they face during flight.

This is distinct from purely mechanical or manual systems, which may not offer the same level of responsiveness or reliability under varying flight conditions. The T-6A's design leverages the benefits of both electrical and hydraulic systems for enhanced performance and safety.