Browse Standards AMS4330D
Historical REVISED 2020-11-30

Aluminum Alloy, Plate (2297-T87) 2.8Cu - 1.5Li - 0.30Mn - 0.12Zr Solution Heat Treated, Stretched, and Artificially Aged(STABILIZED Jan 2018) AMS4330D

This specification covers an aluminum alloy in the form of plate 1.500 to 6.000 inches (38.1 to 152.40 mm) thick (see 8.5).
AMS4330E
2022-12-07
Latest
Revised
AMS4330D
2020-11-30
Historical
Revised
AMS4330C
2018-01-12
Historical
Stabilized
AMS4330B
2012-04-03
Historical
Reaffirmed
AMS4330A
2003-07-14
Historical
Revised
AMS4330
2001-11-19
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 6.2Zn - 2.3Cu - 2.2Mg - 0.12Zr (7050-T7651) Solution Heat Treated, Stress Relieved, and Overaged

AMS4201G

View Details

STANDARD

Aluminum Alloy Die Forgings 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr (7075-T73) Solution and Precipitation Heat Treated

AMS4141H

View Details

STANDARD

Aluminum Alloy Plate 5.7Zn - 2.2Mg - 1.6Cu - 0.22Cr (7475-T7351) Solution Heat Treated, Stress Relieved by Stretching, and Precipitation Heat Treated

AMS4202E

View Details

Get Involved

Want to participate in updating this standard?

X