SAE AMS4232B PDF

SAE AMS4232B PDF

Name:
SAE AMS4232B PDF

Published Date:
05/01/2001

Status:
Active

Description:

Aluminum Alloy Extrusion 2.7Cu 2.2Li 0.12Zr (2090-T86) Solution Heat Treated, Cold Worked, and Precipitation Heat Treated ( Reaffirmed: Apr 2006 )

Publisher:
SAE International

Document status:
Active

Format:
Electronic (PDF)

Delivery time:
10 minutes

Delivery time (for Russian version):
200 business days

SKU:

Choose Document Language:
$21
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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.
File Size : 1 file , 1.6 MB
Note : This product is unavailable in Ukraine, Russia, Belarus
Published : 05/01/2001

History

SAE AMS4232E
Published Date: 09/09/2024
Aluminum Alloy Extrusions 2.7Cu - 2.2Li - 0.12Zr (2090-T86) Solution Heat Treated, Cold Worked, and Precipitation Heat Treated (Stabilized: Sep 2024)
$22.2
SAE AMS4232D
Published Date: 08/14/2018
Aluminum Alloy Extrusions 2.7Cu - 2.2Li - 0.12Zr (2090-T86) Solution Heat Treated, Cold Worked, and Precipitation Heat Treated
$20.7
SAE AMS4232C
Published Date: 10/25/2012
Aluminum Alloy Extrusions 2.7Cu - 2.2Li - 0.12Zr (2090-T86) Solution Heat Treated, Cold Worked, and Precipitation Heat Treated
$16.8
SAE AMS4232B
Published Date: 05/01/2001
Aluminum Alloy Extrusion 2.7Cu 2.2Li 0.12Zr (2090-T86) Solution Heat Treated, Cold Worked, and Precipitation Heat Treated ( Reaffirmed: Apr 2006 )
$21

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