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Aluminum Alloy, Seamless Drawn Tubing 1.0Mg - 0.60Si - 0.28Cu - 0.20Cr (6061-T4) Solution Heat Treated and Naturally Aged
- Aerospace Material Specification
- AMS4480A
- Revised
Downloadable datasets available
Annotation ability available
Sector:
Issuing Committee:
Language:
English
Scope
This specification covers an aluminum alloy in the form of seamless, drawn tubing from 0.025 to 0.500 inches (0.64 to 12.70 mm) in wall thickness (see 8.6).
Rationale
AMS4480A prohibits unauthorized exceptions Form (1.1), Exceptions (3.6), revises Properties (3.2, 3.3.2.1), Reports (4.4.1), and Identification (5.1.1). It also identifies the difference between extruded and drawn tubing (1.1.1 and 8.9) and is the result of 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 | |
| Table 2A | Minimum tensile properties, inch/pound units (see ) | |
| Table 2B | Minimum tensile properties, SI units (see ) |
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.
Reference
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