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Fastener standards for materials address the very metals that fasteners are composed of. With different applications requiring varying levels of corrosion resistance, resistance to deformity and high strength at different high temperatures, different manufacturing processes, dimensions, as well as considerations of matching metals to prevent galvanic corrosion. This list addresses those made from alloys other than nickel and steel.
This SAE Aerospace Standard (AS) provides material identification codes for aluminum alloys, copper alloys, carbon steels, alloy steels, titanium alloys, corrosion resistant materials, and heat resistant materials that are used to make AN, MS, and AS engine and propeller standard utility parts. This document also provides similar material codes for company parts (such as nuts, bolts, etc.) having design configuration similar to other company parts or the engine and propeller standard utility parts (AN, MS, and AS) that are not of the same material.
This specification covers one type of brass in the form of wire (see 8.5 ).
The specification covers a titanium alloy in the form of wire.
This specification covers a titanium alloy in the form of compacts produced by pressing and sintering a blend of elemental titanium powder and aluminum-vanadium alloy powder (see 8.6 ).
This specification covers a corrosion and heat-resistant nickel alloy in the form of bars, forgings, and stock for forging or heading.
This specification covers a corrosion- and heat-resistant iron-chromium-nickel-cobalt alloy in the form of bars, wire, forgings, flash welded rings, and stock for forging, flash welded rings, or heading.
This specification covers a corrosion and heat-resistant alloy in the form of bars, forgings, flash welded rings, and stock for forging, flash welded rings, or heading.
This specification covers a corrosion- and heat-resistant alloy in the form of bars, forgings, flash-welded rings, and stock for forging, flash-welded rings, or heading.
This specification covers a corrosion and heat-resistant, work strengthened cobalt-nickel-chromium alloy in the form of bars 2 inches (50.8 mm) and under in nominal diameter (see 8.2).
This specification covers a corrosion- and heat-resistant, work-strengthened, and aged cobalt-nickel-chromium alloy in the form of bars 2 inches (50 mm) and under in nominal diameter.