SAE AMS4232B

$42.50

Format: PDF      In Stock

 

Sale!
-50%

SAE AMS4232B

$42.50

Aluminum Alloy Extrusion 2.7Cu 2.2Li 0.12Zr (2090-T86) Solution Heat Treated, Cold Worked, and Precipitation Heat Treated ( Reaffirmed: Apr 2006 )
standard by SAE International, 05/01/2001

Format: PDF      In Stock

 

Category:

NOTE: Our website provide PDF immediately download, sometimes when the payment is processed and you did not receive the file, please feel free to connect with us.

Description

This document has been declared “CANCELLED” by the Aerospace Materials Division, SAE as of December 2010. By this action, this document will remain listed in the Numerical Section of the Index of Aerospace Material Specifications indicating that it has been “CANCELLED”.

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.

Product Details

Published:
05/01/2001
File Size:
1 file , 1.6 MB