Browse Standards AMS4338A
Historical REAFFIRMED 2012-09-27

Aluminum Alloy, Extrusions 4.0Cu - 1.3Mg - 0.60Mn (2026-T3511) Solution Heat Treated and Stress Relieved by Stretching AMS4338A

This specification covers an aluminum alloy in the form of extruded bars, rods, and profiles (shapes).
AMS4338B
2018-04-03
Latest
Revised
AMS4338A
2012-09-27
Historical
Reaffirmed
AMS4338
2001-09-01
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, Extrusions 4.0Cu - 1.3Mg - 0.60Mn (2026-T3511) Solution Heat Treated and Stress Relieved by Stretching

AMS4338B

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, Extrusions and Rings 1.0Mg - 0.60Si - 0.28Cu - 0.20Cr - (6061-T6) Solution and Precipitation Heat Treated

AMS4150N

View Details

Get Involved

Want to participate in updating this standard?

Join Committee Learn More
X