An entry speed of 160 KIAS will typically result in how much altitude gain during a power on stall?

In the context of a power-on stall in the T-6A, the entry speed significantly influences the altitude gain experienced during the maneuver. When executing a power-on stall at an entry speed of 160 KIAS, the aircraft typically generates more lift due to the higher airspeed and increased power setting, leading to a greater altitude gain before the stall condition occurs.

During power-on stalls, the aircraft’s aerodynamic characteristics dictate that while the angle of attack is increased to induce a stall, the kinetic energy is converted to potential energy more effectively at this speed, resulting in a substantial climb. The range of 1,500 to 2,000 feet is representative of this scenario, reflecting the dynamics one could expect as the aircraft transitions through the stall and begins to recover.

Understanding this relationship between entry speed and altitude gain helps pilots anticipate the aircraft's behavior during critical phases of flight and emphasizes the importance of proper stall recognition and recovery techniques.