SAE AMS4330B PDF

Name:
SAE AMS4330B PDF

Published Date:
04/03/2012

Status:
Active

Description:

Aluminum Alloy, Plate (2297-T87) 2.8Cu - 1.5Li - 0.30Mn - 0.12Zr Solution Heat Treated, Stretched, 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 alloy in the form of plate.

These products have been typically used in aerospace applications where low density is needed in combination with moderate strength, high fatigue resistance, good stress corrosion properties, and improved stiffness, but usage is not limited to such applications.

File Size :	1 file , 660 KB
Note :	This product is unavailable in Ukraine, Russia, Belarus
Published :	04/03/2012

History

SAE AMS4330E

Published Date: 12/07/2022

Aluminum Alloy, Plate (2297-T87) 2.8Cu - 1.5Li - 0.30Mn - 0.12Zr Solution Heat Treated, Stretched, and Artificially Aged

$23.7

SAE AMS4330D

Published Date: 11/30/2020

Aluminum Alloy, Plate (2297-T87) 2.8Cu - 1.5Li - 0.30Mn - 0.12Zr Solution Heat Treated, Stretched, and Artificially Aged

$21

SAE AMS4330C

Published Date: 01/12/2018

Aluminum Alloy, Plate (2297-T87) 2.8Cu - 1.5Li - 0.30Mn - 0.12Zr Solution Heat Treated, Stretched, and Artificially Aged (Stabilized: Jan 2018)

$22.2

SAE AMS4330B

Published Date: 04/03/2012

Aluminum Alloy, Plate (2297-T87) 2.8Cu - 1.5Li - 0.30Mn - 0.12Zr Solution Heat Treated, Stretched, and Artificially Aged

$21

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SAE AMS5950D

Published Date: 12/29/2020

Nickel Alloy, Corrosion and Heat-Resistant, Sheet and Strip 52.5Ni - 19Cr - 3.0Mo - 5.0Cb - 0.90Ti - 0.50Al - 18Fe Vacuum Induction and Consumable Electrode Melted Solution Heat Treated, Precipitation Hardenable

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SAE AMS4330B PDF

Aluminum Alloy, Plate (2297-T87) 2.8Cu - 1.5Li - 0.30Mn - 0.12Zr Solution Heat Treated, Stretched, and Artificially Aged

History

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