I want to emphasize that ASTM F3114-15 has been replaced by ASTM F3114-19.
1.ASTM F3114-15,whose title is Standard Specification for Structures.
2.ASTM F3114-15 addresses the structural requirements that apply to all portions of the airframe regardless of component, system, or structure.
3. Terminology
3. 1 See Terminology F3060 for more definitions and abbreviations.
4. Strength
4.1 Loads-Strength requirements are specified in terms of limit loads (the maximum loads to be expected in service) and ultimate loads (limit loads multiplied by prescribed factors of (safety)
4.2 Factor of Safery-Unless otherwise provided, a factor of safety of 1.5 must be used.
Keywords of this standard:Airframes – Force, Pressure – Load Distribution – Small Airplanes – Strength
If you want to know more about this standard, you can download it and read it in detail.

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