Steel Sheet and Plate Low Alloy, Heat Treated 90,000 psi (621 MPa) and 100,000 psi (690 MPa) Yield Strength
- Aerospace Material Specification
- AMS6386D
- Stabilized
Scope
Rationale
Topic
Data Sets - Support Documents
| Title | Description | Download |
|---|---|---|
| Unnamed Dataset 1 | ||
| Unnamed Dataset 2 | ||
| TABLE II | ||
| TABLE II | (SI) | |
| Unnamed Dataset 5 | ||
| Unnamed Dataset 6 | ||
| TABLE III | ||
| TABLE III | (SI) | |
| Unnamed Dataset 9 | For Thicknesses Up to 1.250 In. (31.75 mm), Incl: | |
| Unnamed Dataset 10 | For Thicknesses Over 1.250 to 2.000 In. (31.75 to 50.80 mm), Incl: | |
| Unnamed Dataset 11 | For Thicknesses Over 2.000 to 4.000 In. (50.80 to 101.60 mm), Inch |
Issuing Committee
AMS E Carbon and Low Alloy Steels Committee
The committee of Carbon and Low Alloy Steels, AMS Committee E, shall prepare, coordinate, and revise documents related to carbon and low alloy steels technology, such as steel cleanliness and steel quality assurance sampling, 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.