Skip to main content

AMS 5664 | Alloy Bars, Forgings, and Rings, Corrosion and Heat Resistant Nickel Base | Consumable Electrode or Vacuum Induction Melted 1950 °F (1066 °C) Solution Heat Treated, Precipitation Hardenable

What AMS 5664 covers

AMS 5664 is the aerospace material specification for alloy bars, forgings, and rings, corrosion and heat resistant nickel base.

AMS 5664 applies to nickel alloy 718, as alloy bars, forgings, and rings, corrosion and heat resistant nickel base, in the consumable electrode or vacuum induction melted 1950 °f (1066 °c) solution heat treated, precipitation hardenable condition.

Titanium Industries stocks Nickel Alloy 718 Round Bar to AMS 5664.

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

Specifications that cross-reference AMS 5664 include AMS 2261, AMS 5662, AMS 5663, AMS 5708, AMS 5962, AMS Capable: AMS 5663, AMS 5664, AMS 5909, ASME SB446 and ASME SB637.

For AMS 5664 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 5664

AMS 5664

Nickel Alloy: 718

Product Forms: Alloy Bars, Forgings, and Rings, Corrosion and Heat Resistant Nickel Base

Condition: Consumable Electrode or Vacuum Induction Melted 1950 °F (1066 °C) Solution Heat Treated, Precipitation Hardenable

Scope: This specification covers a corrosion and heat resistant nickel alloy in the form of bars, forgings, flash welded rings 10 inches (254 mm) and under in least nominal cross-sectional dimension, and stock of any size for forging or flash welded rings.

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 5664 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 5664 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 5664: questions and answers

What does AMS 5664 cover?

AMS 5664 covers a corrosion and heat resistant nickel alloy in the form of bars, forgings, flash welded rings 10 inches (254 mm) and under in least nominal cross-sectional dimension, and stock of any size for forging or flash welded rings.

Which products does Titanium Industries stock to AMS 5664?

Nickel Alloy 718 Round Bar.

Which specifications cross-reference AMS 5664?

AMS 2261, AMS 5662, AMS 5663, AMS 5708, AMS 5962, AMS Capable: AMS 5663, AMS 5664, AMS 5909, ASME SB446 and ASME SB637.

What is Nickel Alloy 718 used for?

Jet engines, rotor bolts and gas turbine operations.

English · language options require JavaScript