For asymmetrical configurations, what is the minimum Gs limit when gear or flaps are deployed?

The minimum Gs limit for asymmetrical configurations when gear or flaps are deployed is 0 Gs. This limit is established to ensure the aircraft remains safe during various flight phases, particularly when configurations such as landing gear or flaps are extended.

0 Gs indicates that the aircraft can operate without experiencing negative G forces, which is important in maintaining structural integrity and controlling the aircraft effectively. If the G forces extend into negative values, it could lead to loss of control or structural damage, especially with the additional aerodynamic drag created by deployed gear or flaps.

By staying at 0 Gs, pilots can ensure adequate performance and safety margins while managing the asymmetrical forces that can arise from the deployment of these components.