SAE AMS4317B
Aluminum Alloy, Extruded Bar, Rod, and Shapes 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr 7075-T76(51X) Solution Heat Treated and Overaged
Historical
Standard by SAE International, 2019-07-02
Quick Links
Norma
Get answers for your technical
Standart Library
Find standards for your sector
Standart Chek
Verify updates for your standards
|
Name |
Available Formats |
Availability |
Language |
|---|---|---|---|
| AMS4317B.pdf |
Secure PDF |
Immediate Download | English |
| AMS4317B.pdf |
Online Access |
Request Quote | English |
Customers Who Bought This Also Bought
About This Item
This specification covers an aluminum alloy in the form of extruded bars, rods, and shapes up to 4.000 inches, incl (101.60 mm, incl) in nominal diameter or least thickness, and having a nominal cross-sectional area up to 20 in2 (129 cm2) (see 8.5).
AMS4317B revises Condition (3.2), Properties (3.3.1.2, 3.3.2.2), prohibits unauthorized exceptions (3.6), revises Reports (4.4) and Identification (5.1.1), and results from a Five-Year Review and update of this specification.
Please request information about the document. Contact Page
Standard Details
- Publication Date: 2019-07-02
- Standard Status: latest
- Publisher: SAE International
- Document Type: Aerospace Material Specification
- Subject: Aluminum alloys, Coatings, colorants, and finishes, Magnesium alloys, Tensile strength, Extrusion, Conductivity, Heat treatment, Forming, Wrought alloys
- Official SAE: Doi link
Document History
- New Version Available: AMS4317C (2025-04-14)
- This Version: AMS4317B (2019-07-02)
- Previous Version: AMS4317A (2012-01-06)
- Previous Version: AMS4317 (2005-07-25)
Please request information about the document. Contact Page
