What is the maximum Gs limit in an asymmetrical clean configuration?

In the T-6 aircraft, the maximum Gs limit in an asymmetrical clean configuration is established to ensure structural integrity and maintain safe flight operations. The correct answer of 4.7 Gs reflects the aircraft's design limits, which account for the stresses that can be placed on the airframe during maneuvers.

Asymmetrical clean configuration refers to a state where the aircraft has no external stores and is not symmetrically loaded, meaning the wings may not be carrying the same amount of weight or aerodynamic forces. This configuration increases the risk of exceeding G limits during aggressive maneuvers due to uneven load factors, hence the specification of a conservative limit of 4.7 Gs for safe operations.

Understanding this operational limit is crucial for pilots as it ensures they do not inadvertently exceed the aircraft's design capabilities, which could lead to structural failure or loss of control.