What is the load factor limit during normal operations for the King Air 350 when flaps are up?

The load factor limit during normal operations for the King Air 350 when the flaps are up is +3.1g's and -1.24g's. This limit reflects the aircraft's structural design and performance capabilities, ensuring safety and operational reliability under various flight conditions.

The positive load factor indicates how much load the aircraft can withstand in terms of vertical forces; in this case, +3.1g's means the aircraft can handle forces up to 3.1 times the weight of the aircraft in a positive maneuver, such as pulling up from a dive. The negative load limit of -1.24g's indicates the structural integrity under downward-facing forces, such as in a push over maneuver.

This specific limit is crucial for pilots to adhere to, as exceeding these values can lead to structural failure or reduced control of the aircraft. Understanding these limitations is an essential part of flight safety and ensuring that flight operations remain within safe parameters.