Forgings, Aluminum Alloys 2xxx and 7xxx, Heat-Treated, Finished-Part Properties: Short-Transverse Tensile Properties and Fracture Toughness
- Aerospace Material Specification
- AMS4335A
- Stabilized
Scope
Rationale
Recommended Content
Aerospace Material Specification | Forgings, Titanium Alloys Heat-Treated, Finished-Part Properties: Short-Traverse Tensile, Fracture Toughness, and Longitudinal Time-Dependent-Tension |
Aerospace Material Specification | Titanium Alloy, Investment Castings 6Al - 4V Hot Isostatically Pressed |
Aerospace Material Specification | Casting, Structural Investment, Titanium Alloy 6Al - 4V Hot Isostatically Pressed |
Topic
Data Sets - Support Documents
Title | Description | Download |
---|---|---|
TABLE 1 | Classification of Forgings | |
Unnamed Dataset 2 | ||
Unnamed Dataset 3 | ||
TABLE 2 | Hardness Requirements for the -O1 Temper | |
TABLE 3 | Flash Extension Tolerances | |
TABLE 4 | Acceptance Sampling Plan for Hardness of -O1 Temper |
Issuing Committee
AMS D Nonferrous Alloys Committee
The committee of Nonferrous Alloys, AMS Committee D, shall prepare, coordinate, and revise documents related to nonferrous metals technology, such as aluminum, magnesium, and copper, 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.