Aluminum Alloy, Sheet and Plate, Alclad 4.4Cu - 1.5Mg - 0.60Mn (Alclad 2024-O, Sheet and Plate) Annealed; or when specified, “As Fabricated” (2024-F)
- Aerospace Material Specification
- AMS4461
- Issued
Scope
Rationale
Recommended Content
Aerospace Material Specification | Aluminum Alloy Sheet and Plate, Alclad 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr (Alclad 7075-O) Annealed or when specified, “As Fabricated” (Alclad 7075-F) |
Aerospace Material Specification | Heat Treatment of Wrought Aluminum Alloy Parts |
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 | TENSILE PROPERTIES IN ANNEALED CONDITION, INCH/POUND UNITS | |
TABLE 3B | TENSILE PROPERTIES IN ANNEALED CONDITION, SI UNITS | |
TABLE 4 | BENDING PARAMETERS IN ANNEALED CONDITION | |
TABLE 5A | TENSILE PROPERTIES IN T42, T62, AND T72 TEMPER, INCH/POUND UNITS | |
TABLE 5B | TENSILE PROPERTIES IN T42, T62, AND T72 TEMPER, SI UNITS | |
TABLE 6 | 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.