Browse Standards AMS4413B
Historical REVISED 2019-05-10

Aluminum Alloy, Plate 3.5Cu - 1.0Li - 0.40Mg - 0.35Mn - 0.45Ag - 0.12Zr (2050-T84) Solution Heat Treated, Stress Relieved, and Artificially Aged AMS4413B

This specification covers an aluminum-lithium alloy in the form of plate 0.500 to 6.500 inch (12.70 to 165.10 mm) inclusive, in thickness (see 8.5).
AMS4413C
2023-12-20
Latest
Revised
AMS4413B
2019-05-10
Historical
Revised
AMS4413A
2012-12-20
Historical
Revised
AMS4413
2007-10-31
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 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, 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, Plate (7055-T7751) 8.0Zn - 2.3Cu - 2.0Mg - 0.16Zr Solution Heat Treated, Stress Relieved, and Overaged

AMS4206C

View Details

STANDARD

Aluminum Alloy, Sheet and Plate 4.0Cu - 1.0Li - 0.40Mg - 0.35Ag - 0.13Zr (2195-T8) Solution Heat Treated, Cold Worked, and Artificially Aged

AMS4474B

View Details

Get Involved

Want to participate in updating this standard?

Join Committee Learn More
X