What is the maximum load factor for the Arrow aircraft?

The maximum load factor for the Arrow aircraft is specified as 3.8 G. This value represents the maximum stress that the aircraft can handle without structural failure during positive maneuvers. Load factors are crucial in understanding the capabilities and limitations of an aircraft, especially during turns, turbulence, or aerobatics, where forces can exceed standard operational limits. The 3.8 G limit indicates that the structure is designed to maintain integrity under violent activity, thus ensuring safety for maneuvers that may impose high aerodynamic loads.

Understanding the significance of the load factor helps pilots make informed decisions regarding maneuvering and operational limits, ensuring that they remain within safe parameters to prevent structural damage or loss of control.