What is the maximum acceleration limit for asymmetric gear/flaps in Gs?

The maximum acceleration limit for asymmetric gear/flaps is designated between 0 to 2.0 Gs. This limit is defined to ensure that aircraft can safely operate under various conditions, particularly when deploying asymmetric configurations like flaps or gear, which can significantly affect the aerodynamic characteristics and overall stability of the aircraft.

In this context, 2.0 Gs represents the upper threshold of load factors that the aircraft structure can withstand without risking damage or compromising safety. The lower limit of 0 Gs indicates conditions such as weightlessness experienced during certain maneuvers. This range helps pilots maintain awareness of the performance limits of the aircraft when dealing with asymmetric configurations, thus emphasizing the importance of adhering to these operational limits during flight to ensure safety and control.