Browse Standards AMS4232A
Historical Reaffirmed 2006-04-24

Aluminum Alloy Extrusions, 2.7Cu - 2.2Li - 0.12Zr (2090-T86), Solution Heat Treated, Cold Worked, and Precipitation Heat Treated AMS4232A

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

These extrusions have been used typically for parts in structural applications requiring strength similar to 7050-T6 with good exfoliation resistance and with a lower density of approximately 7.8%, but usage is not limited to such applications.

AMS4232C
2012-10-25
Latest
Revised
AMS4232B
2010-12-02
Historical
Revised
AMS4232A
2006-04-24
Historical
Reaffirmed
AMS4232
1994-04-01
Historical
Reaffirmed

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