ALLOY BARS, FORGINGS, AND RINGS, CORROSION AND HEAT RESISTANT Nickel Base - 19.5Cr - 13.5Co - 4.3Mo - 3.0Ti - 1.4Al Solution, Stabilization, and Precipitation Heat Treated 1825 - 1900 F (996.1 - 1037.8 C) Treatment Consumable Electrode or Vacuum Induction Melted
- Aerospace Material Specification
- AMS5707
- Issued
Recommended Content
Aerospace Material Specification | Rings, Flash Welded Corrosion and Heat-Resistant Austenitic Steels, Austenitic-Type Iron, Nickel or Cobalt Alloys, or Precipitation-Hardenable Alloys |
Aerospace Material Specification | Alloy, Corrosion and Heat-Resistant, Bars, Forgings, and Rings, 21Cr - 20Ni - 20Co - 3.0Mo - 2.5W - 1.0(Cb+Ta) - 0.15N - 32Fe Solution Heat Treated |
Aerospace Material Specification | Steel, Corrosion- and Heat-Resistant, Welding Wire 13Cr - 8.0Ni - 2.3Mo - 1.1Al Vacuum Melted |
Topic
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.
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