Browse Standards AMS4470C
Current REVISED 2018-12-27

Aluminum Alloy, Plate (7085-T7451) 7.5Zn - 1.6Cu - 1.5Mg - 0.12Zr Solution Heat Treated, Stress-Relieved, and Overaged AMS4470C

This specification covers an aluminum alloy in the form of plate 3.000 to 7.000 inches (76.20 to 177.80 mm) in nominal thickness (see 8.5).
AMS4470C
2018-12-27
Latest
Revised
AMS4470B
2018-08-03
Historical
Revised
AMS4470A
2012-12-04
Historical
Revised
AMS4470
2009-10-23
Historical
Issued

SAE MOBILUS

Subscribers can view annotate, and download all of SAE's content. Learn More »

Access SAE MOBILUS »

Preview Document Add to Cart
Members save up to 11% off list price.
Login to see discount.
Special Offer: AeroPaks offers a customized subscription plan that is cost-effective and allows you to choose the number of downloads and Aerospace and Aerospace Material documents you need. Find more information here.
We also recommend:
STANDARD

Aluminum Alloy, Plate (7085-T7651) 7.5Zn - 1.6Cu - 1.5Mg - 0.12Zr Solution Heat Treated, Stress-Relieved, and Overaged

AMS4329B

View Details

STANDARD

Aluminum Alloy, Extruded Profiles (2196-T8511) 2.9Cu - 1.7Li - 0.4Mg - 0.4Ag - 0.10Zr Solution Heat Treated, Stress Relieved by Stretching and Artificially Aged

AMS4416B

View Details

STANDARD

Aluminum Alloy, Sheet 3.2Cu - 0.52Mg - 0.30Ag - 0.12Zr (2198-T8) Solution Heat Treated, Cold Worked, and Artificially Aged

AMS4412A

View Details

Get Involved

Want to participate in updating this standard?

Join Committee Learn More
X