What is the deflection angle of the flaps in LDG position?

The deflection angle of the flaps in the LDG (Landing) position for the T-6A is indeed 50 degrees. This flap position is specifically designed to increase the lift coefficient during landing, which allows the aircraft to fly at lower speeds without stalling. The increased deflection enhances the camber of the wing, thereby improving lift and allowing for safer approach and landing configurations.

By having the flaps deflected to this angle, the aircraft is able to maintain better control and stability during descent and takeoff rolls, which is crucial for flight safety, especially in training scenarios involving student pilots. This specific deflection is a key aspect of the aircraft's performance characteristics, particularly during the critical phases of landing and takeoff.