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Nickel 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 nickel alloys.


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.


SAE AMS 5667P-2020

Nickel Alloy, Corrosion and Heat-Resistant, Bars, Forgings, and Rings 72Ni - 15.5Cr - 0.95Cb - 2.5Ti - 0.70Al - 7.0Fe Equalized, Precipitation Hardenable

This specification covers a corrosion and heat-resistant nickel alloy in the form of bars, forgings, flash welded rings, and stock for forging, flash welded rings, or heading.


SAE AMS 5668K-2019

Nickel Alloy, Corrosion and Heat-Resistant, Bars, Forgings, and Rings, 72Ni - 15.5Cr - 7.0Fe - 2.5Ti - 1.0Cb (Nb) - 0.70Al, 2100 °F (1149 °C) Solution and Precipitation Heat Treated

This specification covers a corrosion and heat-resistant nickel alloy in the form of bars, forgings, flash welded rings 10.0 inches (254 mm) and under in nominal diameter or distance between parallel sides, and stock of any size for forging, flash welded rings, or heading (see 8.6).





SAE AMS 5711F-2020

Nickel Alloy, Corrosion and Heat-Resistant, Bars, Forgings, and Rings 65Ni - 15.8Cr - 15.2Mo - 0.30Al - 0.05La Solution Heat Treated

This specification covers a corrosion and heat-resistant nickel alloy in the form of bars, forgings, flash welded rings, and stock for forging, flash welded rings, or heading.




SAE AMS 5754N-2019

Nickel Alloy, Corrosion and Heat-Resistant, Bars, Forgings, and Rings, 47.5Ni - 22Cr - 1.5Co - 9.0Mo - 0.60W - 18.5Fe, Solution Heat Treated

This specification covers a corrosion and heat-resistant nickel alloy in the form of bars, forgings, flash welded rings, and stock for forging, flash welded rings, or heading.


SAE AMS 5891C-2019

Nickel Alloy, Corrosion and Heat-Resistant, Bars, Forgings, and Rings, 60Ni - 22Cr - 2.0Mo - 14W - 0.35Al - 0.03La, Solution Heat Treated

This specification covers a corrosion and heat-resistant nickel alloy in the form of bars, forgings, flash welded rings, and stock for forging, flash welded rings, or heading.


SAE AMS 5962A-2003 (SAE AMS5962A-2003)

Nickel Alloy, Corrosion and Heat-Resistant, Round Bars and Wire 52.5Ni 19Cr 3.0Mo 5.1Cb 0.90Ti 0.50Al 19Fe Consumable Electrode or Vacuum Induction Melted 1775\mDF (968\mDFC) Solution Treated and Cold Worked Precipitation Hardenable ( Reaffirmed: Aug 2007 )

This specification covers a corrosion and heat resistant work strengthened nickel alloy in the form of bars and wire, 1 1/2 inches (38 mm) and under in nomial diameter. These products have been used typically for parts, such as fasteners, requiring a room temperature minimum tensile strength of 220 ksi (1517 MPa) after precipitation heat treatement for use up to 900 \mDF (482 \mDC) and having oxidation resistance up to 1800 \mDF (982 \mDC), but usage is not limited to such applications.


SAE MAM 5706C-2003 (SAE MAM5706C-2003)

Nickel Alloy, Corrosion and Heat Resistant, Bars, Forgings, and Rings 57Ni 19.5Cr 13.5Co 4.3Mo 3.0Ti 1.4Al 0.006B 0.05Zr, Consumable Electrode or Vacuum Induction Melted, 995 to 1040┬░C Solution Heat Treated

This specification covers a corrosion and heat resistant nickel alloy in the form of bars, forgings, flash welded rings, and stock for forging, flash welded rings, or heading procured in SI (metric) units. AMS 5706 is the inch/pound version of this MAM. These products have been used typically for parts, such as fasteners, flanges, and rings, requiring high strength up to 815 degrees C and oxidation resistance up to 955 degrees C, particularly those parts which are formed or welded and then heat treated to develop required properties, but usage is not limited to such applications.


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