Browse Standards AMS4326A
Current REVISED 2018-02-15

Aluminum Alloy, 2013, Extruded Bar, Rod, and Profiles 1.0Mg - 0.80Si - 1.8Cu - 0.20Cr (2013 -T6511) Solution Heat Treated, Stress-Relieved by Stretching, and Aged AMS4326A

This specification covers an aluminum alloy in the form of extruded bars, rods, and integrated profiles up to 0.200 inch (5.08.mm), inclusive, in nominal thickness (see 8.5).
AMS4326A
2018-02-15
Latest
Revised
AMS4326
2017-11-14
Historical
Reaffirmed

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, Plate (7055-T7751) 8.0Zn - 2.3Cu - 2.0Mg - 0.16Zr Solution Heat Treated, Stress Relieved, and Overaged

AMS4206C

View Details

STANDARD

Aluminum Alloy, Plate 5.7Zn - 2.2Mg - 1.6Cu - 0.22Cr (7475-T651) Solution Heat Treated, Stress Relieved, and Precipitation Heat Treated

AMS4090F

View Details

STANDARD

Disilicide Diffusion Coating of Molybdenum and Molybdenum Alloys Pack Cementation Method

AMS2465D

View Details

Get Involved

Want to participate in updating this standard?

Join Committee Learn More
X