Load factors must be considered in structural design from "summary" of Aircraft Structures & Systems EASA Module 13 B2 by
Load factors are critical considerations in the structural design of aircraft. These factors are used to account for the maximum loads that an aircraft may experience during its operation. They are applied to various components of the aircraft, such as the wings, fuselage, and landing gear, to ensure that they can withstand these loads without failing. Load factors are typically expressed as a ratio of the maximum load that an aircraft can experience to the weight of the aircraft itself. For example, a load factor of 2 would mean that the aircraft can withstand twice its own weight in loads. This ensures that the aircraft is structurally sound and can safely operate in a variety of conditions. When designing aircraft structures, engineers must carefully...
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