Alloy Bars, Forgings, and Rings, Corrosion and Heat Resistant Nickel Base - 15.5Cr - 16Mo - 3.8W - 5.5Fe Solution Heat Treated
- Aerospace Material Specification
- AMS5750D
- Stabilized
Scope
Rationale
Recommended Content
Aerospace Material Specification | Titanium Alloy Bars, Forgings and Forging Stock 8Al - 1Mo - 1V Duplex Annealed |
Aerospace Material Specification | Nickel Alloy, Corrosion and Heat Resistant, Seamless Tubing 47.5Ni - 22Cr - 1.5Co - 9.0Mo - 0.60W - 18.5Fe Solution Heat Treated |
Aerospace Material Specification | Aluminum Alloy, Hand Forgings 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr (7075-T7452) Solution Heat Treated, Stress Relieved, and Precipitation Heat Treated |
Data Sets - Support Documents
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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.