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Aluminum Alloy, Sheet and Plate, Alclad 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr (Alclad 7075; -T6 Sheet - T651 Plate) Solution and Precipitation Heat Treated
- Aerospace Material Specification
- AMS4049M
- Revised
Downloadable datasets available
Annotation ability available
Sector:
Issuing Committee:
Language:
English
Scope
This specification covers an aluminum alloy in the form of sheet and plate with thickness from 0.008 to 4.000 inch, incl (0.20 to 101.6 mm, incl), clad on two sides (see 8.4).
Rationale
AMS4049M revises Condition (3.2.1, 3.2.2), Properties (3.3.5), deleted the weight limit previously applicable to ultrasonic inspection (3.4), revised Reports (4.4.1), and is a Five Year Review and update of this specification.
Topic
Data Sets - Support Documents
| Title | Description | Download |
|---|---|---|
| [Unnamed Dataset 1] | ||
| [Unnamed Dataset 2] | ||
| [Unnamed Dataset 3] | ||
| Table 1 | Composition, core (7075) | |
| Table 2 | Composition, cladding (7072) | |
| Table 3A | Minimum tensile properties, inch/pound units | |
| Table 3B | Minimum tensile properties, SI units | |
| Table 4 | Bending parameters | |
| Table 5 | Minimum average cladding thickness | |
| Table 6 | Ultrasonic class |
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.