Heat Treatment of Wrought Copper Beryllium Alloy Parts
- Aerospace Material Specification
- AMS2728A
- Revised
Scope
Recommended Content
Aerospace Material Specification | Forgings, Aluminum Alloys 2xxx and 7xxx, Heat-Treated, Finished-Part Properties: Short-Transverse Tensile Properties and Fracture Toughness |
Aerospace Material Specification | Steel, Investment Castings 0.95Cr - 0.20Mo (0.25 - 0.35C) (4130 Mod) Normalized or Normalized and Tempered |
Aerospace Material Specification | Steel, Investment Castings 0.95Cr - 0.20Mo (0.35 - 0.45C) (4140 Mod) Normalized or Normalized and Tempered |
Topic
Data Sets - Support Documents
Title | Description | Download |
---|---|---|
Unnamed Dataset 1 | ||
Unnamed Dataset 2 | ||
TABLE 1 | Soak Times for Solution Heat Treating | |
TABLE 2 | Precipitation Hardening Times and Conditions | |
TABLE 4 | Acceptance Sampling Plan | |
TABLE 3 | Hardness After Precipitation Hardening |
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.