AMS 5662 is the aerospace material specification for nickel alloy, corrosion and heat-resistant, bars, forgings, and rings.
What AMS 5662 covers
Nickel Alloy 718 is used for jet engines, rotor bolts and gas turbine operations.
Specifications that cross-reference AMS 5662 include AMS 2261, AMS 5663, AMS 5666, AMS 5708, AMS 5962, AMS Capable: AMS 5664, AMS 5909, ASME SB446, ASME SB637 and NACE API 6A718.
For AMS 5662 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.
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AMS 5662
DISCLAIMER: Alloy data sheets are for reference only, not for design purposes.
| 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% | |||||||||
| 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.
AMS 5662: questions and answers
What does AMS 5662 cover?
What does AMS 5662 cover?
AMS 5662 covers nickel alloy, corrosion and heat-resistant, bars, forgings, and rings.
Which specifications cross-reference AMS 5662?
Which specifications cross-reference AMS 5662?
AMS 2261, AMS 5663, AMS 5666, AMS 5708, AMS 5962, AMS Capable: AMS 5664, AMS 5909, ASME SB446, ASME SB637 and NACE API 6A718.
What is Nickel Alloy 718 used for?
What is Nickel Alloy 718 used for?
Jet engines, rotor bolts and gas turbine operations.