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

The correct answer reflects the operational limits of the T-6A in an asymmetric clean configuration, which is crucial for ensuring both safety and aircraft integrity during various flight maneuvers. In this context, the G limits are defined as the allowable range of positive and negative G-forces the aircraft can safely endure while maintaining its performance and structural integrity.

In this case, the range of -1.0 to 4.7 Gs indicates that while the aircraft can handle some negative Gs (which can occur during specific flight conditions or maneuvers), it has a maximum positive limit that is essential for operations, particularly during aerobatic maneuvers or abrupt changes in flight direction. This parameter is critical because exceeding these limits can lead to loss of control due to structural failure or aerodynamic issues.

The other choices do not accurately represent the G limits for asymmetric clean configuration in the T-6A; they either exceed known thresholds or fall below necessary performance measures, which could lead to unsafe conditions. Thus, understanding the operational limits helps pilots maintain control and ensure the longevity of the aircraft while performing under various flight scenarios.