SAE AMS4344-1984 PDF

Scope: Form: This specification covers an aluminium alloy in the form of extruded bars@ rods@ wire@ shapes@ and tubing. Application: Primarily for structuralapplications requiring a combination of high tensile properties@ moderate fatigue strength@ stress-corrosion resistance@ and good fracture toughness.

SAE AMS4344-1984 history

2024 SAE AMS4344G-2024 Aluminum Alloy, Extrusions 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr (7175-T73511) Solution Heat Treated, Stress Relieved by Stretching, Straightened, and Overaged
2018 SAE AMS4344F-2018 Aluminum Alloy@ Extrusions 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr (7175-T73511) Solution Heat Treated@ Stress Relieved by Stretching@ Straightened@ and Overaged (UNS A97175)
2018 SAE AMS4344E-2018 Aluminum Alloy@ Extrusions 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr (7175-T73511) Solution Heat Treated@ Stress Relieved by Stretching@ Straightened@ and Overaged (UNS A97175)
2011 SAE AMS4344D-2011 Aluminum Alloy, Extrusions, 5.6Zn 2.5Mg 1.6Cu 0.23Cr (7175-T73511) Solution Heat Treated, Stress Relieved by Stretching, Straightened, and Overaged
2006 SAE AMS4344C-2006 Aluminum Alloy, Extrusions 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr (7175-T73511) Solution Heat Treated, Stress Relieved by Stretching, Staightened,, and Overaged UNS A97175
1998 SAE AMS4344B-1998 Aluminum Alloy, Extrusions, 5.6Zn 2.5Mg 1.6Cu 0.23Cr Solution Heat Treated, Stress Relieved by Stretching, Straightened, and Overaged
1990 SAE AMS4344A-1990 Aluminum Alloy Extrusions 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr (7175-T73511) Solution Heat Treated@ Stress Relieved@ and Overaged
1984 SAE AMS4344-1984 ALUMINUM ALLOY@ EXTRUSIONS 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr (7175-T73511) Solution Heat Treated@ Stress Relieved@ and Pricipitation Heat Treated (UNS A97175)