Steel, Bars 0.90 - 1.03C
- Aerospace Material Specification
- AMS5132L
- Revised
Scope
Rationale
Recommended Content
Aerospace Material Specification | Titanium Alloy, Forgings 5Al - 2.5Sn Annealed, 110 ksi (758 MPa) Yield Strength |
Aerospace Material Specification | Qualification Sampling and Testing of Steels for Transverse Tensile Properties |
Topic
Data Sets - Support Documents
Title | Description | Download |
---|---|---|
Unnamed Dataset 1 | ||
Unnamed Dataset 2 | ||
Table 1 | Composition | |
Table 2 | Hardness | |
Table 3A | Diameter tolerances, inch/pound units | |
Table 3B | Diameter tolerances, SI units |
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.