Browse Standards AMS4328B
Current REVISED 2019-11-25

Aluminum Alloy, Plate (2397-T87) 2.8Cu - 1.4Li - 0.30Mn - 0.12Zr - 0.10Zn Solution Heat Treated, Cold Worked, and Artificially Aged AMS4328B

This specification covers an aluminum alloy in the form of plate 3.000 to 6.000 inch (76.20 to 152.40 mm), inclusive, in nominal thickness (see 8.5).
AMS4328B
2019-11-25
Latest
Revised
AMS4328A
2013-04-19
Historical
Reaffirmed
AMS4328
2003-01-07
Historical
Issued

SAE MOBILUS

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

Access SAE MOBILUS »

Members save up to 10% 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 (2.7 Cu - 1.8 Li - 0.7 Zn) 2099-T86 Solution Heat Treated, Cold Worked and Artificially Aged

AMS4458A

View Details

STANDARD

Aluminum Alloy, Plate (2.7 Cu - 1.8 Li - 0.7 Zn) 2099-T86 Solution Heat Treated, Cold Worked and Artificially Aged

AMS4458A

View Details

STANDARD

Aluminum Alloy, Plate 6.2Zn - 1.8Cu - 2.4Mg - 0.13Zr (7010-T7451) Solution Heat Treated, Stress Relieved, and Precipitation Heat Treated

AMS4205D

View Details

Get Involved

Want to participate in updating this standard?

X