Browse Standards AMS4169B
Historical Revised 1963-01-01

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 AMS4169B

This specification covers an aluminum alloy in the form of extruded bars, rods, wire, profiles, and tubing.

These extrusions have been used typically for parts subject to excessive warpage during machining and for parts requiring high strength and whose fabrication does not involve welding or forming, but usage is not limited to such applications.

Certain design and processing procedures may cause these products to become susceptible to stress-corrosion cracking; SAE ARP 823 recommends practices to minimize such conditions.

AMS4169L
2012-01-09
Latest
Canceled
AMS4169G
2011-08-10
Historical
Reaffirmed
AMS4169K
2008-05-02
Historical
Reaffirmed
AMS4169J
1998-03-01
Historical
Revised
AMS4169H
1992-04-01
Historical
Revised
AMS4169F
1979-10-01
Historical
Revised
AMS4169E
1978-07-01
Historical
Revised
AMS4169D
1968-11-01
Historical
Revised
AMS4169C
1967-11-01
Historical
Revised
AMS4169B
1963-01-01
Historical
Revised
AMS4169A
1960-11-01
Historical
Revised
AMS4169
1960-06-01
Historical
Issued

SAE MOBILUS

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

Access SAE MOBILUS »

Members save up to 18% off list price.
Login to see discount.
Special Offer: Purchase more aerospace standards and aerospace material specifications and save! AeroPaks off a customized subscription plan that lets you pay for just the documents that you neeed, when you need them.

Get Involved

Want to participate in updating this standard?

X