2011508

SAE AMS4344F

Aluminum Alloy, Extrusions 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr (7175-T73511) Solution Heat Treated, Stress Relieved by Stretching, Straightened, and Overaged

standard by SAE International , 04/10/2018

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Full Description

1.1 Form

This specification covers an aluminum alloy in the form of extruded bars, rods, and profiles 0.250 to 2.000 .inches (6.35 to 50.80 mm) in nominal thickness and up to 32 in2 (206 cm2), inclusive, in cross-sectional area (see 8.5).

1.2 Application

These extrusions have been used typically for structural applications requiring a combination of high tensile properties, moderate fatigue strength, stress-corrosion resistance, and good fracture toughness, but usage is not limited to such applications.

 

Product Details

Published:
04/10/2018
Number of Pages:
7
File Size:
1 file , 67 KB
Note:
This product is unavailable in Ukraine, Russia, Belarus
 

Document History

  1. SAE AMS4344G


    Aluminum Alloy, Extrusions 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr (7175-T73511) Solution Heat Treated, Stress Relieved by Stretching, Straightened, and Overaged

    • Most Recent

  2. SAE AMS4344F

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    viewing


    Aluminum Alloy, Extrusions 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr (7175-T73511) Solution Heat Treated, Stress Relieved by Stretching, Straightened, and Overaged

    • Historical Version

  3. SAE AMS4344E


    Aluminum Alloy, Extrusions 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr (7175-T73511) Solution Heat Treated, Stress Relieved by Stretching, Straightened, and Overaged

    • Historical Version

  4. SAE AMS4344D


    Aluminum Alloy, Extrusions 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr (7175-T73511) Solution Heat Treated, Stress Relieved by Stretching, Straightened, and Overaged

    • Historical Version

  5. SAE AMS4344C


    Aluminum Alloy, Extrusions, 5.6Zn 2.5Mg 1.6Cu 0.23Cr (7175-T73511) Solution Heat Treated, Stress Relieved by Stretching, Straightened, and Overaged

    • Historical Version