Aluminum Alloy, Clad One Side Sheet 0.6Mg - 0.35Si - 0.28Cu (No. 23 Brazing Sheet) As Fabricated
- Aerospace Material Specification
- AMS4465
- Issued
Scope
Rationale
Recommended Content
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| Aerospace Material Specification | Aluminum Alloy Plate (2027-T351) 4.4Cu - 1.2Mg - 0.8Mn - 0.10Zr Solution Heat Treated, Cold Worked and Naturally Aged |
| Aerospace Material Specification | Aluminum Alloy, Alclad Sheet and Plate 6.3Cu - 0.30Mn - 0.18Zr - 0.10V - 0.06Ti Alclad 2219-T31; Sheet, Solution Heat Treated and Cold Worked Alclad 2219-T351; Plate, Solution Heat Treated and Stress Relieved |
Topic
Data Sets - Support Documents
| Title | Description | Download |
|---|---|---|
| Unnamed Dataset 1 | ||
| Unnamed Dataset 2 | ||
| Unnamed Dataset 3 | ||
| TABLE 1 | COMPOSITION, CORE (6951) | |
| TABLE 2 | COMPOSITION, CLADDING (4045) | |
| TABLE 3A | MINIMUM TENSILE PROPERTIES, INCH/POUND UNITS (See ) | |
| TABLE 3B | MINIMUM TENSILE PROPERTIES, SI UNITS (See ) | |
| TABLE 4 | BENDING PARAMETERS | |
| TABLE 5 | AVERAGE CLADDING THICKNESS |
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.