What are the G limits for symmetric clean configuration in the T-6A?

The G limits for the T-6A in a symmetric clean configuration are indeed between -3.5 to 7.0 Gs. This range indicates the aircraft’s ability to withstand forces during maneuvers while maintaining structural integrity. The lower limit of -3.5 G allows for maneuverability during negative G operations, which could occur in certain aerobatic or fast-paced flight situations. The upper limit of 7.0 G accounts for high-performance maneuvers and aggressive turns where the aircraft is subjected to significant positive G forces. This G limit ensures that pilots can operate the aircraft effectively within safe parameters, avoiding structural damage while maintaining control during dynamic flight scenarios. Understanding these limits is crucial for both safety and performance management in flight. Other choices present limits that fall outside the verified range for a symmetric clean configuration, indicating lower operational thresholds that do not correspond with the T-6A's certified capabilities.