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SAE International - AMS4405

Aluminum Alloy, Alclad Sheet (6156-T4) 1.0Si - 0.90Cu - 0.60Mn - 0.90Mg Solution Heat Treated and Naturally Aged

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Organization: SAE International
Publication Date: 3 August 2006
Status: active
description:

This specification covers an aluminum alloy procured in the form of sheet Alclad on both sides.

Document History

AMS4405
August 3, 2006
Aluminum Alloy, Alclad Sheet (6156-T4) 1.0Si - 0.90Cu - 0.60Mn - 0.90Mg Solution Heat Treated and Naturally Aged
This specification covers an aluminum alloy procured in the form of sheet Alclad on both sides.

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:
ARP826 - ELECTRICAL COMPUTING RESOLVERS
Published by SAE International on July 6, 2010
This document covers resolvers which are used to perform coordinate transformations as well as sine and cosine computations, It includes both the categories of compensated and uncompensated resolvers...
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...
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