Aluminum Alloy, Plate (7085-T7451), 7.5Zn - 1.6Cu - 1.5Mg - 0.12Zr, Solution Heat Treated, Stress-Relieved, and Overaged

Standard:
Revised:
  • 2012-12-04
 
  • CURRENT
Publisher:
  • SAE International
Pages:
6
Scope:

This specification covers an aluminum alloy in the form of plate. This product may be used in aerospace applications requiring a high level of mechanical properties and fracture toughness, good resistance to stress-corrosion cracking and resistance to exfoliation corrosion, but usage is not limited to such applications.

Rationale:

AMS4470A adds 3.000-4.000 thickness 7085-T7451 aluminum plate to this document, modifies tensile (Table 2) and fracture toughness properties (Table 3) for expanded gage ranges, and revises fracture toughness specimen criteria (3.3.5).

History:
Standard Published Revision Status
AMS4470A 2012-12-04 Latest Revised
2009-10-23 Historical Issued
Access
Now
SAE MOBILUS Subscriber? You may already have access.
Buy
Select
Price
List
Download
$76.00
Add
Mail
$76.00
Members save up to 18% off list price.
Grade
If you are currently using this technical report:
Share
HTML for Linking to Page
Page URL

Related Items

Training / Education
2013-04-09
Technical Paper / Journal Article
2011-10-04
Technical Paper / Journal Article
2004-11-02
Technical Paper / Journal Article
2013-10-07
Training / Education
2017-10-23
Training / Education
2017-10-19