What is the maximum nose-up pitch attitude during a takeoff for the T-6?

The maximum nose-up pitch attitude during a takeoff for the T-6 is 12.5 degrees. This limit is established to ensure safe takeoff performance and to maintain appropriate aerodynamic characteristics of the aircraft. Exceeding this pitch attitude can result in a stall, especially at lower airspeeds during the critical phase of flight just after takeoff. Adhering to this limit helps ensure that airflow over the wings remains effective, facilitating optimal lift and stability.

Understanding this limit is essential for pilots to manage the aircraft's ascent safely. It also helps in preventing excessive drag, which could hinder the climb performance. The specific figure of 12.5 degrees reflects a careful consideration of the aircraft’s design and operational performance characteristics.