Aluminum Alloy Sheet and Plate, Alclad One Side 4.4Cu - 1.5Mg - 0.60Mn (Clad One Side 2024-O) Annealed
- Aerospace Material Specification
- AMS4077J
- Revised
Scope
Rationale
Recommended Content
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Aerospace Material Specification | Aluminum Alloy, Sheet and Plate, Alclad 4.4Cu - 1.5Mg - 0.60Mn (2024-O with 1 ½% Alclad); Annealed |
Aerospace Material Specification | Aluminum Alloy, Sheet 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr (7075-O) Annealed, Fine Grained |
Topic
Data Sets - Support Documents
Title | Description | Download |
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Unnamed Dataset 1 | ||
Unnamed Dataset 2 | ||
Unnamed Dataset 3 | ||
Table 1 | Composition, core (2024) | |
Table 2 | Composition, cladding (1230) | |
Table 3A | O temper tensile properties, inch/pound units | |
Table 3B | O temper tensile properties, SI units | |
Table 4 | Bending parameters | |
Table 5A | T42 temper minimum tensile properties, inch/pound units | |
Table 5B | T42 temper minimum tensile properties, SI units | |
Table 6 | Bending parameters | |
Table 7 | Cladding thickness, percent of total 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.