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Other Alloys

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.

SAE AS 269J-2018

Identification of Material for AN, MS, and AS Engine and Propeller Standard Utility Parts and Also for Company Parts

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.

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SAE AMS 4713G-2019

Brass, Wire, 65Cu - 35Zn, Eighth-Hard (H00)

This specification covers one type of brass in the form of wire.

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SAE AMS 4982G-2020

Titanium Alloy Wire 44.5 Cb

The specification covers a titanium alloy in the form of wire.

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SAE AMS 4993F-2017

Titanium Alloy, Blended Powder Compacts, Sintered 6Al - 4V

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SAE AMS 5746F-2005 (SAE AMS5746F-2005)

Alloy Bars and Forgings, Corrosion and Heat Resistant, 15Cr 45Ni 4.1Mo 4.1W 3.0Ti 1.0Al 31Fe, Consumable Electrode Vacuum Melted, Solution and Precipitation Heat Treated

This specification covers a corrosion and heat resistant nickel alloy in the form of bars, forgings, and stock for forging or heading. Primarily for parts such as turbine rotors, shafts, blades, bolts, dowels, and fittings requiring high strength up to 1600 degrees F (871 degrees C) and oxidation resistance up to 1800 degrees F (982 degrees C).

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SAE AMS 5750D-2017

Alloy Bars, Forgings, and Rings, Corrosion and Heat Resistant Nickel Base - 15.5Cr - 16Mo - 3.8W - 5.5Fe Solution Heat Treated

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SAE AMS 5768L-2018

Alloy, Corrosion and Heat-Resistant, Bars, Forgings, and Rings, 21Cr - 20Ni - 20Co - 3.0Mo - 2.5W - 1.0Cb - 0.15N - 31Fe, Solution and Precipitation Heat Treated

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.

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SAE AMS 5769G-2020

Alloy, Corrosion and Heat-Resistant, Bars, Forgings, and Rings, 21Cr - 20Ni - 20Co - 3.0Mo - 2.5W - 1.0(Cb+Ta) - 0.15N - 32Fe, Solution Heat Treated

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.

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SAE AMS 5877B-2002 (SAE AMS5877B-2002)

Iron Alloy, Corrosion and Heat Resistant, Bars, Forgings, and Rings 29Fe 22Cr 21Ni 18.5Co 3.2Mo 2.8W 0.78Ta 0.30Al 0.052Zr 0.05La 0.20N, Solution Heat Treated ( Reaffirmed: Oct 2006 )

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. These products have been used typically for parts, such as turbine rotors, shafts, blades, and bolts, requiring high strength and oxidation resistance up to 2000 degrees F (1093 degree C), but usage is not limited to such applications.

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SAE AMS 5919B-2018

Cobalt-Nickel Alloy, Corrosion and Heat-Resistant, Round Bars 19Cr - 36Co - 25Ni - 7.0Mo - 0.50Cb (Nb) - 2.9Ti - 0.20Al - 9.0Fe Vacuum Induction Plus Vacuum Consumable Electrode Melted Solution Heat Treated and Work Strengthened, Modified Strength

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).

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SAE AMS 5920B-2018

Cobalt-Nickel Alloy, Corrosion and Heat-Resistant, Round Bars 19Cr - 36Co - 25Ni - 7.0Mo - 0.50Cb (Nb) - 2.9Ti - 0.20Al - 9.0Fe Vacuum Induction Plus Vacuum Consumable Electrode Melted Solution Heat Treated, Work-Strengthened and Aged, Modified Strength

This specification covers a corrosion and heat-resistant, work-strengthened and aged cobalt-nickel-chromium alloy in the form of bars 2 inches (50.8 mm) and under in nominal diameter (see 8.2).

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