How many Gs can the T-6A withstand during positive maneuvers?

The T-6A has a maximum positive load limit of +6 Gs during maneuvers, making this the correct response. This is a critical aspect of the aircraft's structural integrity, as it defines the maximum amount of aerodynamic load that the airframe can safely handle without risking damage or structural failure.

Understanding this limit is essential for pilots, particularly during advanced maneuvers or in situations where strong forces are at play, such as tight turns or during aerobatic flying. Exceeding this threshold could lead to excessive strain on the aircraft’s components, potentially resulting in structural failure or catastrophic events. Thus, adhering to the maximum G-limit is vital for ensuring the safe operation of the T-6A.

The other options reflect values that surpass the aircraft's design specifications and would not be feasible or safe under typical operating conditions.