UNLIMITED FREE
ACCESS TO THE WORLD'S BEST IDEAS

SUBMIT
Already a GlobalSpec user? Log in.

This is embarrasing...

An error occurred while processing the form. Please try again in a few minutes.

Customize Your GlobalSpec Experience

Select Your Free Newsletters

Industry Newsletters

Select Your Free Product Alerts

Finish!
Privacy Policy

This is embarrasing...

An error occurred while processing the form. Please try again in a few minutes.

SAE International - AMS4410A

Aluminum Alloy Plate (7081-T7451) 7.2Zn - 1.5Cu - 2.0Mg - 0.10Zr Solution Heat Treated, Stress Relieved and Overaged

active
Buy Now
Organization: SAE International
Publication Date: 7 May 2019
Status: active
description:

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

Document History

AMS4410A
May 7, 2019
Aluminum Alloy Plate (7081-T7451) 7.2Zn - 1.5Cu - 2.0Mg - 0.10Zr Solution Heat Treated, Stress Relieved and Overaged
This specification covers an aluminum alloy in the form of plate.

References

This document references:
AMS2355 - TENSILE TESTING OF WROUGHT ALUMINUM AND MAGNESIUM PRODUCTS Except Forgings
Published by SAE International on September 1, 1965
A description is not available for this item.
This document references:
AMS2772 - HEAT TREATMENT OF ALUMINUM ALLOY RAW MATERIALS
Published by SAE International on January 1, 1997
This specification covers requirements and recommendations for the heat treatment of wrought aluminum alloy raw materials (See 8.1.1 and 8.1.8 ). It is intended to replace MIL-H-6088.
This document references:
AS1990 - ALUMINUM ALLOY TEMPERS
Published by SAE International on January 1, 1990
A description is not available for this item.
This document references:
AS1990A - ALUMINUM ALLOY TEMPERS
Published by SAE International on May 1, 1998
The purpose of this SAE Aerospace Standard (AS) is to provide a description of the temper nomenclature system for aluminum alloys used in the aerospace industry by combining information from...
View Less
View All
Advertisement