AMS10133-1003 designates a specific material standard, likely pertaining to a metallic alloy or composite used in aerospace applications. Such specifications outline the precise chemical composition, mechanical properties (tensile strength, yield strength, elongation), heat treatment requirements, surface finish, and quality control measures that the material must adhere to. For instance, it might define the acceptable ranges for elements like chromium, nickel, or titanium within a particular steel alloy intended for aircraft components. Adherence to these requirements is demonstrated through rigorous testing and documentation.
Compliance with material specifications like this ensures consistency, reliability, and safety in critical aerospace structures and systems. Using materials that meet defined standards guarantees that parts manufactured from them will perform as expected under demanding conditions, such as extreme temperatures, high stresses, and corrosive environments. Historically, the development and implementation of these types of standards have been crucial in minimizing failures and improving the overall performance and lifespan of aircraft.
