Nickel Alloy, Corrosion and Heat-Resistant, Bars, Forgings, and Rings 57Ni 19.5Cr 13.5Co 4.3Mo 3.0Ti 1.4Al 0.006B 0.05Zr Consumable Electrode or Vacuum Induction Melted 1825 to 1900°F Solution Heat Treated
- Aerospace Material Specification
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 procured in inch/pound units.
MAM 5706 is the metric version of this AMS.
These products have been used typically for parts, such as fasteners, flanges, and rings, requiring high strength up to 1500 degrees F and oxidation resistance up to 1750 degrees F, particularly those parts which are formed or welded and then heat treated to develop required properties, but usage is not limited to such applications.
Data Sets - Support Documents
The committee of Corrosion and Heat Resistant Steels and Alloys and Specialty Steels and Alloys, AMS Committee F, will prepare, coordinate, and revise documents related to corrosion and heat resistant steels and alloys and specialty steels and alloys technology, such as stainless steels and nickel and base alloys, through the participation of metals suppliers, users, and interested government agencies. Committee activities shall provide a forum for the cooperative interchange of ideas and experience of the participants, resulting in the publication of specifications that embody sound, established aerospace industry practices and requirements to serve the suppliers and customers of aerospace materials.