SAE AMS4050H
Aluminum Alloy, Plate 6.2Zn - 2.3Cu - 2.2Mg - 0.12Zr (7050-T7451) Solution Heat Treated, Stress Relieved, and Overaged
Historical
Standard by SAE International, 2011-11-03
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 |
|---|---|---|---|
| AMS4050H.pdf |
Secure PDF |
Immediate Download | English |
| AMS4050H.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 plate.
This document has been reaffirmed to comply with the SAE five-year review policy.
Please request information about the document. Contact Page
Standard Details
- Publication Date: 2011-11-03
- Standard Status: historical
- Publisher: SAE International
- Document Type: Aerospace Material Specification
- Subject: Heat treatment, Aluminum alloys, Magnesium alloys, Tensile strength, Conductivity, Quality assurance, Finishing, Identification,
- Official SAE: Doi link
Document History
- New Version Available: AMS4050K (2021-04-22)
- Previous Version: AMS4050J (2014-12-22)
- This Version: AMS4050H (2011-11-03)
- Previous Version: AMS4050G (2000-06-01)
- Previous Version: AMS4050F (1998-11-01)
- Previous Version: AMS4050E (1992-07-01)
- Previous Version: AMS4050D (1991-10-01)
- Previous Version: AMS4050C (1984-10-01)
- Previous Version: AMS4050B (1984-04-01)
- Previous Version: AMS4050A (1977-07-15)
- Previous Version: AMS4050 (1974-12-15)
Please request information about the document. Contact Page
