Aluminum Alloy, Sheet and Plate, Alclad 4.4Cu - 1.5Mg - 0.60Mn (2024-O with 1 ½% Alclad); Annealed
- Aerospace Material Specification
- AMS4040N
- Revised
Scope
Rationale
Recommended Content
Topic
Data Sets - Support Documents
| Title | Description | Download |
|---|---|---|
| Unnamed Dataset 1 | ||
| Unnamed Dataset 2 | ||
| Unnamed Dataset 3 | ||
| TABLE 1A | COMPOSITION, CORE (2024) | |
| TABLE 1B | COMPOSITION, CLADDING (1230) | |
| TABLE 2A | TENSILE PROPERTIES IN ANNEALED CONDITION, INCH/POUND UNITS | |
| TABLE 2B | TENSILE PROPERTIES IN ANNEALED CONDITION, SI UNITS | |
| TABLE 4A | TENSILE PROPERTIES IN T42 TEMPER, INCH/POUND UNITS | |
| TABLE 4B | TENSILE PROPERTIES IN T42 TEMPER, SI UNITS | |
| TABLE 5 | BENDING PARAMETERS |
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.