STEEL, CORROSION RESISTANT, WIRE 17Cr - 7.1Ni - 1.1Al Cold Drawn, Precipitation-Hardenable
- Aerospace Material Specification
- AMS5678D
- Revised
Scope
Recommended Content
| Aerospace Material Specification | Steel, Corrosion Resistant, Safety Wire, 18Cr - 11.5Ni (SAE 30305), Solution Heat Treated, Cold Finished |
| Aerospace Material Specification | Steel, Corrosion-Resistant, Wire 19Cr - 9.5Ni (304) Solution Heat Treated |
Topic
Data Sets - Support Documents
| Title | Description | Download |
|---|---|---|
| Unnamed Dataset 1 | ||
| Unnamed Dataset 2 | ||
| TABLE 1 | Composition | |
| TABLE 2A | Tensile Strength, Condition C, Inch/Pound Units | |
| TABLE 2B | Tensile Strength, Condition C, SI Units | |
| TABLE 3A | Coiling Parameters, Inch/Pound Units | |
| TABLE 3B | Coiling Parameters, SI Units | |
| TABLE 4A | Tensile Strength, Condition CH900 Inch/Pound Units | |
| TABLE 4B | Tensile Strength, Condition CH900, 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.