Aluminum Alloy, Plate 3.5Cu - 1.0Li - 0.40Mg - 0.35Mn - 0.45Ag - 0.12Zr (2050-T34) Solution Heat Treated and Stress Relieved
- Aerospace Material Specification
- AMS4372B
- Revised
Scope
Rationale
Recommended Content
Aerospace Material Specification | Steel Tubing (Seamless) Round 0.55ni 0.5cr 0.2mo (0.27 - 0.33c) Heat Treated (125,000 Tensile Strength) |
Aerospace Material Specification | Selective (Brush) Nickel Plating Low-Stressed, Hard Deposit |
Aerospace Material Specification | Titanium Alloy, Bars and Rods 3Al - 8V - 6Cr - 4Mo - 4Zr Consumable Electrode Melted Solution Heat Treated and Centerless Ground or Peeled and Polished |
Topic
Data Sets - Support Documents
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.
Reference
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