Nickel Alloy, Corrosion and Heat Resistant, Sheet, Strip, and Plate 62ni 21.5cr 9.0mo 3.7(Cb+Ta) Annealed
- Aerospace Material Specification
- MAM5599C
- Cancelled
Scope
This specification covers a corrosion and heat resistant nickel alloy in the form of sheet, strip, and plate procured in SI (metric) units.
AMS 5599, specified in inch/pound version of this MAM.
These products have been used typically for parts requiring corrosion and oxidation resistance up to 1095 degrees C, particularly where such parts may require welding during fabrication, but usage is not limited to such applications.
Recommended Content
Aerospace Material Specification | Nickel Alloy, Corrosion and Heat Resistant, Sheet, Strip, and Plate 47.5ni 22cr 1.5co 9.0mo 0.60w 18.5fe, Solution Heat Treated |
Aerospace Material Specification | Nickel Alloy, Corrosion and Heat-Resistant, Sheet, Strip, and Plate 72Ni - 15.5Cr - 0.95Cb(Nb) - 2.5Ti - 0.70Al - 7.0Fe Annealed |
Aerospace Material Specification | Cobalt Alloy, Corrosion- and Heat-Resistant, Sheet, Strip, and Plate 40Co - 22Cr - 22Ni - 14.5W - 0.07La Solution Heat Treated |
Data Sets - Support Documents
Issuing Committee
AMS F Corrosion and Heat Resistant Alloys Committee
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.