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AMS 5962| Nickel Alloy, Corrosion and Heat Resistant, Bar and Wire | Consumable Electrode or Vacuum Induction Melted 1775 °F (968 °C) Solution Treated and Cold Worked Precipitation Hardenable

What AMS 5962 covers

AMS 5962 is the aerospace material specification for nickel alloy, corrosion and heat resistant, bar and wire.

AMS 5962 applies to nickel alloy 718, as nickel alloy, corrosion and heat resistant, bar and wire, in the consumable electrode or vacuum induction melted 1775 °f (968 °c) solution treated and cold worked precipitation hardenable condition.

Titanium Industries stocks Nickel Alloy 718 Round Bar to AMS 5962.

Nickel Alloy 718 is used for jet engines, rotor bolts and gas turbine operations.

Specifications that cross-reference AMS 5962 include AMS 2261, AMS 5662, AMS 5664, AMS 5708, AMS 5909, ASME SB446, ASME SB637, NACE API 6A718, NACE Per MR 0175 and ASTM B446.

For AMS 5962 material, request a quote online or contact your nearest Titanium Industries location. The information on this page is for reference only and does not replace the specification itself.

Round bar, one of the product forms Titanium Industries stocks to AMS 5962

AMS 5962

Nickel Alloy: 718

Product Forms: Nickel Alloy, Corrosion and Heat Resistant, Bar and Wire

Condition: Consumable Electrode or Vacuum Induction Melted 1775 °F (968 °C) Solution Treated and Cold Worked Precipitation Hardenable

Scope: This specification covers a corrosion and heat resistant work strengthened nickel alloy in the form of bars and wire.

Product availability:

DISCLAIMER: The use of this information should be considered strictly voluntary. Information contained in this page or across the domain, may contain typographical errors and are for reference only. Information presented are purely generalizations and are not a substitution for AMS specifications.

DISCLAIMER: Alloy data sheets are for reference only, not for design purposes.

AMS 5962 Specification — Table 1
Chemical Composition
Ni 52.5%  Cr 19.0%  Mo 3.05%  C <=0.45%  Nb 5.035%
 Mn <=0.35%  Si <=0.35%  P <=0.010%:  S <=0.010%  Cu <=0.230%
 Co <=1.00%
AMS 5962 Specification — Table 2
Mechanical Properties
Tensile Strength: 14 - 220 ksi Yield Strength: 80 - 150 ksi Elongation: 18 - 27.0%

Tensile properties and associated requirements vary due to orientation, section thickness, and engineering requirements.

Nickel Alloy 718 Applications:

  • Jet engines
  • Rotor Bolts
  • Gas turbine operations

Cross Reference Specifications

Discounted Products

AMS 5962: questions and answers

What does AMS 5962 cover?

AMS 5962 covers a corrosion and heat resistant work strengthened nickel alloy in the form of bars and wire.

Which products does Titanium Industries stock to AMS 5962?

Nickel Alloy 718 Round Bar.

Which specifications cross-reference AMS 5962?

AMS 2261, AMS 5662, AMS 5664, AMS 5708, AMS 5909, ASME SB446, ASME SB637, NACE API 6A718, NACE Per MR 0175 and ASTM B446.

What is Nickel Alloy 718 used for?

Jet engines, rotor bolts and gas turbine operations.

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