SAE AMS4413 PDF

SAE AMS4413 PDF

Name:
SAE AMS4413 PDF

Published Date:
10/31/2007

Status:
Active

Description:

Aluminum Alloy, Plate 3.5 Cu 1.0Li .40Mg .35Mn .45Ag 0.12Zr (2050-T84) Solution Heat Treated, Stress Relieved, and Artificially Aged

Publisher:
SAE International

Document status:

Active

Format:

Electronic (PDF)

Delivery time:

10 minutes

Delivery time (for Russian version):

200 business days

SKU:

This specification covers an aluminum-lithium alloy in the form of plate.

This plate has been used typically for parts where low density is needed in combination with a high level of mechanical properties and very good resistance to stress-corrosion cracking, but usage is not limited to such applications.

File Size :	1 file , 460 KB
Note :	This product is unavailable in Ukraine, Russia, Belarus
Published :	10/31/2007

History

Published Date: 12/20/2023

Aluminum Alloy, Plate 3.5Cu - 1.0Li - 0.40Mg - 0.35Mn - 0.45Ag - 0.12Zr (2050-T84) Solution Heat Treated, Stress Relieved, and Artificially Aged

$22.2

Published Date: 05/10/2019

Aluminum Alloy, Plate 3.5Cu - 1.0Li - 0.40Mg - 0.35Mn - 0.45Ag - 0.12Zr (2050-T84) Solution Heat Treated, Stress Relieved, and Artificially Aged

$20.7

Published Date: 12/20/2012

Aluminum Alloy, Plate 3.5Cu - 1.0Li - 0.40Mg - 0.35Mn - 0.45Ag - 0.12Zr (2050-T84) Solution Heat Treated, Stress Relieved, and Artificially Aged

$18.3

Published Date: 10/31/2007

Aluminum Alloy, Plate 3.5 Cu 1.0Li .40Mg .35Mn .45Ag 0.12Zr (2050-T84) Solution Heat Treated, Stress Relieved, and Artificially Aged

$16.8

Related products

Published Date: 08/03/2020

FITTING, NIPPLE, REDUCER, FLARELESS TUBE TO PIPE, EXTERNAL THREAD

$20.7

Published Date: 09/01/1946

A Method of Ground Resonance Testing for Helicopters

$24.9

Published Date: 06/02/2023

FITTING END, INTERNAL FLARE, DESIGN STANDARD

$22.2

Best-Selling Products