Browse Standards AMS4341E
Historical REAFFIRMED 2011-11-03

Aluminum Alloy, Extrusions 6.2Zn - 2.3Cu - 2.2Mg - 0.12Zr (7050-T73511) Solution Heat Treated, Stress Relieved by Stretching, Straightened, and Overaged AMS4341E

This specification covers an aluminum alloy in the form of extruded bars, rods, wire, profiles, and tubing.
AMS4341H
2024-01-16
Latest
Revised
AMS4341G
2018-04-10
Historical
Revised
AMS4341F
2018-03-04
Historical
Revised
AMS4341E
2011-11-03
Historical
Reaffirmed
AMS4341D
1998-03-01
Historical
Revised
AMS4341C
1991-10-01
Historical
Revised
AMS4341B
1986-04-01
Historical
Revised
AMS4341A
1986-01-01
Historical
Revised
AMS4341
1978-04-15
Historical
Issued

SAE MOBILUS

Subscribers can view annotate, and download all of SAE's content. Learn More »

Access SAE MOBILUS »

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 7.7Zn - 2.4Mg - 1.6Cu - 0.16Cr (7049-T73511) Solution Heat Treated, Stress Relieved, and Overaged

AMS4157E

View Details

STANDARD

Aluminum Alloy, Extrusions 7.7Zn - 2.4Mg - 1.6Cu - 0.16Cr (7049-T76511) Solution Heat Treated, Stress Relieved, Straightened, and Overaged

AMS4159F

View Details

STANDARD

Aluminum Alloy, Extrusions 6.2Zn - 2.3Cu - 2.2Mg - 0.12Zr (7050-T76511) Solution Heat Treated, Stress Relieved, Straightened, and Overaged

AMS4340G

View Details

Get Involved

Want to participate in updating this standard?

X