What is the maximum load factor when the flaps are down on the King Air 350?

The maximum load factor when the flaps are down on the King Air 350 is +2.0g's and -0.0g's. This specification is crucial for pilots to understand, as it outlines the aircraft's structural limits when operating with the flaps extended. The positive load factor indicates the maximum amount of load the aircraft can safely carry while climbing or during maneuvers with the flaps deployed, while the negative load factor of -0.0g's suggests that the aircraft should not encounter any significant negative g-loads with the flaps extended. This limitation is particularly important to ensure the safe operation of the aircraft during various flight scenarios, especially when considering the effects of stalling, control surface effectiveness, and overall aircraft stability. Understanding these limitations helps pilots maintain safety and performance standards during flight operations.