What is the range of acceleration limits for asymmetric clean configuration in Gs?

The correct response indicates that the range of acceleration limits for an asymmetric clean configuration is between -1.0 to 4.7 Gs, which accounts for both negative and positive accelerations in this specific configuration.

This range reflects the aerodynamic and performance characteristics of the aircraft in an asymmetric clean configuration, which typically includes an optimal configuration for performance without significant drag. The negative limit highlights the aircraft's ability to experience downward acceleration, which can occur during certain maneuvers or situational responses. The upper limit of 4.7 Gs suggests a considerable positive acceleration threshold that the aircraft can safely handle under these conditions, ensuring that it remains within acceptable operational limits during flight.

Understanding this range is critical for pilots as it directly relates to the aircraft's performance envelope and handling capabilities, ensuring safe flight operations within the defined limits.