Browse Standards AMS4364A
Current REVISED 2021-09-15

Aluminum Alloy, Plate, 7.9Zn - 1.8Cu - 2.0Mg - 0.10Zr (7099-T7651) Solution Heat Treated, Stress Relieved, and Overaged AMS4364A

This specification covers an aluminum alloy in the form of plate from 1.000 to 6.000 inches (25.40 to 152.40 mm) in thickness (see 8.6).
AMS4364A
2021-09-15
Latest
Revised
AMS4364
2016-01-12
Historical
Issued

SAE MOBILUS

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

Access SAE MOBILUS »

Members save up to 9% 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, Forgings, 4.3zn 3.3mg 0.6cu 0.2mn 0.2cr, Solution and Precipitation Heat Treated, Low Residual Stresses

AMS4136A

View Details

STANDARD

Aluminum Alloy, Sheet and Plate 4.4Cu - 1.5Mg - 0.60Mn; (2024-T861), Solution Heat Treated and Cold Worked, and Artificially Aged

AMS4271A

View Details

STANDARD

Test Method and Limits for Bow Height of Aluminum Sheet Samples After Chemical Milling

AS6507

View Details

Get Involved

Want to participate in updating this standard?

X