Steel, Corrosion and Heat Resistant, Wire 18Cr - 11.5Ni - 0.70Cb (SAE 30347) Solution Heat Treated
- Aerospace Material Specification
- AMS5674E
- Reaffirmed
Scope
Rationale
Recommended Content
| Aerospace Material Specification | Steel, Corrosion Resistant, Bars and Wire 18Cr - 9.0Ni (302) Solution Heat Treated, Cold Drawn and Stress Relieved 125 ksi (862 MPa) Tensile Strength |
| Aerospace Material Specification | Iron-Nickel Alloy, Strip 49Fe - 5.3Cr - 42Ni - 2.5Ti - 0.55Al Solution Heat Treated, Cold Rolled, 50% Reduction |
| Aerospace Material Specification | Steel, Corrosion and Heat-Resistant, Sheet, Strip, and Plate 12.5Cr (410) Annealed |
Topic
Data Sets - Support Documents
| Title | Description | Download |
|---|---|---|
| Unnamed Dataset 1 | ||
| Unnamed Dataset 2 | ||
| TABLE 1 | Composition | |
| TABLE 2A | Maximum Tensile Properties, Inch/Pound Units | |
| TABLE 2B | Maximum Tensile Properties, SI Units |
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.