What is the limit for sustained G-forces during aerobatic maneuvers in the T-6?

The limit for sustained G-forces during aerobatic maneuvers in the T-6 is +6 to -3 Gs. This range is critical for maintaining structural integrity and ensuring pilot safety during aerobatic flight. Exceeding these limits can lead to excessive strain on the aircraft's airframe, potentially resulting in structural failure. The upper limit of +6 Gs allows for the necessary maneuverability and performance in aerobatic situations, ensuring the aircraft can handle a range of flight scenarios without compromising safety. Similarly, the lower limit of -3 Gs helps maintain control and prevents excessive negative loading, which could lead to a loss of control or other flight issues. This tolerance is established based on extensive testing and engineering considerations specific to the T-6's design and operational capabilities.