Steel, Corrosion and Heat Resistant, Welded Tubing 25Cr - 20Ni (SAE 30310) Solution Heat Treated
- Aerospace Material Specification
- AMS5577H
- Reaffirmed
Scope
Rationale
Recommended Content
| Aerospace Material Specification | Steel, Welded Tubing 0.95Cr - 0.20Mo (0.28 - 0.33C) (SAE 4130) |
| Aerospace Material Specification | Steel Tubing, Seamless 0.95Cr - 0.20Mo (0.28 - 0.33C) (SAE 4130) 125 ksi (862 MPa) Tensile Strength |
Topic
Data Sets - Support Documents
| Title | Description | Download |
|---|---|---|
| Unnamed Dataset 1 | ||
| Unnamed Dataset 2 | ||
| TABLE 1 | Composition | |
| TABLE 2A | Tensile Properties, Inch/Pound Units | |
| TABLE 2B | Tensile Properties, SI Units | |
| TABLE 3A | Minimum Flarability, Inch/Pound Units | |
| TABLE 3B | Minimum Flarability, 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.