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

The load factor, which is a critical performance characteristic of the King Air 350, refers to the maximum aerodynamic load that the aircraft can safely handle during flight maneuvers while the flaps are retracted. In this instance, the correct load factor is +3.1g's and -1.24g's.

A load factor of +3.1g's indicates that the aircraft can withstand a positive load of over three times its weight, which is significant during maneuvers that involve climbing, turning, or rapid acceleration. The negative load factor of -1.24g's indicates that the aircraft is also capable of handling negative load, which is vital during specific flight conditions, such as hard descents or turbulence.

The figures demonstrate the aircraft's structural resilience, ensuring safety and performance under various operational scenarios. Various other choices present either higher or lower load limits, which do not align with the operational specifications of the King Air 350, making them unsuitable for accurate representation.