Browse Standards AMS5670C
Historical REVISED 1993-04-01

Nickel Alloy, Corrosion and Heat Resistant, Bars, Forgings, and Rings, 72Ni 15.5Cr 0.95Cb 2.5Ti 0.70Al 7.0Fe, 1800°F (982°C) Solution Heat Treated, Precipitation Hardenable AMS5670C

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.

These products have been used typically for parts requiring high strength in the range 800 to 1100 degrees F (427 to 593 degrees C), particularly those parts which are formed or welded and then precipitation heat treated to develop required properties, but usage is not limited to such applications.

AMS5670G
2018-08-17
Latest
Revised
AMS5670F
2012-02-09
Historical
Reaffirmed
AMS5670B
2011-08-15
Historical
Reaffirmed
AMS5670E
1999-01-01
Historical
Revised
AMS5670D
1996-04-01
Historical
Revised
AMS5670C
1993-04-01
Historical
Revised
AMS5670A
1981-07-01
Historical
Revised
AMS5670
1969-05-01
Historical
Issued

SAE MOBILUS

Subscribers can view annotate, and download all of SAE's content. Learn More »

Access SAE MOBILUS »

Members save up to 18% off list price.
Login to see discount.
Special Offer: Purchase more aerospace standards and aerospace material specifications and save! AeroPaks offer a customized subscription plan that lets you pay for just the documents that you need, when you need them.

Get Involved

Want to participate in updating this standard?

X