Browse Standards AMS5708J
Historical Revised 2006-09-08

Nickel Alloy, Corrosion and Heat-Resistant, Bars, Forgings, and Rings 58Ni 19.5Cr 13.5Co 4.3Mo 3.0Ti 1.4Al Consumable Electrode or Vacuum Induction Melted 1975°F (1079°C) Solution Heat Treated AMS5708J

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, such as bolts and turbine blades, requiring high strength up to 1500 degrees F (816 degrees C) and oxidation resistance up to 1750 degrees F (954 degrees C), but usage is not limited to such applications.

AMS5708L
2015-01-15
Latest
Revised
AMS5708K
2008-03-27
Historical
Revised
AMS5708J
2006-09-08
Historical
Revised
AMS5708H
2002-11-21
Historical
Revised
AMS5708G
1995-12-01
Historical
Revised
AMS5708F
1990-04-01
Historical
Revised
AMS5708E
1981-10-01
Historical
Revised
AMS5708D
1981-01-15
Historical
Revised
AMS5708C
1973-12-01
Historical
Revised
AMS5708B
1970-11-01
Historical
Revised
AMS5708A
1970-05-01
Historical
Revised
AMS5708
1963-07-15
Historical
Issued

SAE MOBILUS

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

Access SAE MOBILUS »

Preview Document Add to Cart
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 off a customized subscription plan that lets you pay for just the documents that you neeed, when you need them.

Get Involved

Want to participate in updating this standard?

Join Committee Learn More
X