What is the maximum weight of the T-6 with a forward CG?

The maximum weight of the T-6 with a forward center of gravity (CG) is established at 6,500 lbs. This figure is critical because it ensures that the aircraft operates within safe limits for stability, control, and performance. The forward CG affects the aircraft's handling characteristics, making it more stable but also requiring more control input from the pilot, especially during landing and takeoff phases.

Understanding the implications of exceeding this weight limit is vital for safe flight operations. Being over the maximum weight can lead to a degradation in performance, including longer takeoff distances, higher stall speeds, reduced climb rates, and challenges in controlling the aircraft effectively.

Knowing these limitations allows pilots to properly assess their load and ensure they maintain safe operations. The weight limits, including those for different CG positions, help in calculating performance metrics and balance, ensuring the aircraft remains easy to control and safely operable.