What is the maximum yaw axis deflection during stall?

The correct response indicates that the maximum yaw axis deflection during a stall for the King Air 350 is 30 degrees. Understanding this limitation is critical because excessive yaw during a stall can lead to a loss of control, particularly in multi-engine aircraft where asymmetric thrust can exacerbate yaw tendencies.

A 30-degree deflection represents a manageable level for pilots when recovering from a stall. Staying within this limitation is essential for maintaining stability and ensuring that the aircraft can be effectively controlled during recovery maneuvers. Knowing this specific yaw axis deflection helps in developing proper stall recognition skills and recovery techniques, which are vital for flight safety.

Understanding the significance of yaw axis limits is crucial in real-world scenarios, as it equips pilots with the knowledge of how much yaw deviation may occur before experiencing adverse flight characteristics, thereby informing safety and operational procedures.