Browse Standards AMS4154R
Historical REVISED 2015-01-05

Aluminum Alloy, Extrusions 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr (7075-T6, 7075-T6510, 7075-T6511) Solution Heat Treated, Stress Relieved by Stretching when Required and Precipitation Heat Treated AMS4154R

This specification covers an aluminum alloy in the form of extruded bars, rods, wire, profiles, and tubing.
AMS4154S
2023-11-10
Latest
Revised
AMS4154R
2015-01-05
Historical
Revised
AMS4154P
2011-05-23
Historical
Revised
AMS4154N
2008-05-01
Historical
Reaffirmed
AMS4154M
1998-03-01
Historical
Revised
AMS4154L
1990-07-01
Historical
Revised
AMS4154K
1978-10-01
Historical
Revised
AMS4154J
1968-05-01
Historical
Revised
AMS4154H
1967-11-01
Historical
Revised
AMS4154G
1967-04-01
Historical
Revised
AMS4154F
1962-06-01
Historical
Revised
AMS4154E
1962-01-01
Historical
Revised
AMS4154D
1952-06-01
Historical
Revised
AMS4154C
1948-11-01
Historical
Revised
AMS4154B
1947-07-01
Historical
Revised
AMS4154A
1946-11-01
Historical
Revised
AMS4154
1945-10-01
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 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr (7075-T6511) Solution Heat Treated, Stress Relieved by Stretching, Straightened and Precipitation Heat Treated

AMS4169L

View Details

STANDARD

Aluminum Alloy, Extrusions 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr (7075-T73, 7075-T73511, 7075-T73510) Solution Heat Treated, Stress Relieved by Stretching when required, and Overaged

AMS4617A

View Details

STANDARD

Aluminum Alloy, Extrusions 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr (7075-O) Annealed

AMS4476A

View Details

Get Involved

Want to participate in updating this standard?

X