SAE AMSQQA250/15C
Aluminum Alloy Alclad 7178, Plate and Sheet
Latest
Standard by SAE International, 2014-02-14
Quick Links
Norma
Get answers for your technical
Standart Library
Find standards for your sector
Standart Chek
Verify updates for your standards
Name 7200_0f2e2a-b0> |
Available Formats 7200_9f48b8-b6> |
Availability 7200_1cf621-be> |
Language 7200_17533e-f8> |
---|---|---|---|
AMSQQA250_15C.pdf 7200_7bf73d-e0> |
Secure PDF 7200_a93470-04> |
Immediate Download 7200_f1e434-c8> | English 7200_75b6b2-1e> |
AMSQQA250_15C.pdf 7200_bf7ad0-2a> |
Online Access 7200_c4fff2-3b> |
Request Quote 7200_726d65-8c> | English 7200_98db50-6c> |
Customers Who Bought This Also Bought
About This Item
This specification covers the specific requirements for 7178 aluminum alloy alclad plate and sheet; the general requirements are covered in AMS-QQ-A-250. The plate and sheet covered by this specification shall be an integral composite product consisting of a heat-treatable aluminum alloy (7178) core with thin layers of an aluminum alloy (7072) anodic to the core and of approximately equal thickness bonded to both surfaces.
AMS-QQ-A-250/15C has been designated stabilized because alloy 7178 is not recommended for new designs.
Please request information about the document. Contact Page
Standard Details
- Publication Date: 2014-02-14
- Standard Status: latest
- Publisher: SAE International
- Document Type: Aerospace Material Specification
- Subject: Heat treatment, Aluminum alloys, Tensile strength, Munitions, Chromium, Magnesium, Manganese, Titanium,
- Official SAE: Doi link
Document History
- This Version: AMSQQA250/15C (2014-02-14)
- Previous Version: AMSQQA250/15B (2012-09-28)
- Previous Version: AMSQQA250/15A (1998-09-01)
- Previous Version: AMSQQA250/15 (1997-08-01)
Please request information about the document. Contact Page