Newer Version Available

Aluminum Alloy, Sheet and Plate 4.4Mg - 0.70Mn - 0.15Cr (5083-0) Annealed

Aerospace Material Specification
AMS4056G
Reaffirmed

Published October 18, 2010 by SAE International in United States

Sector:

Aerospace

Issuing Committee:

AMS D Nonferrous Alloys Committee

Language: English

Data Sets - Support Documents

Title	Description	Download
Unnamed Dataset 1
Unnamed Dataset 2
TABLE 1	Composition
TABLE 2A	Tensile Properties, Inch/Pound Units
TABLE 2B	Tensile Properties, SI Units

Reference

Number	Title
AMS2355	TENSILE TESTING OF WROUGHT ALUMINUM AND MAGNESIUM PRODUCTS Except Forgings
ANSIH35.2	This document is not part of the subscrption.
ANSIH35.2M	This document is not part of the subscrption.
ASTMB660	This document is not part of the subscrption.
ASTMB666/B666M	This document is not part of the subscrption.
MAM2202	TOLERANCES, METRIC Aluminum Alloy and Magnesium Alloy Sheet and Plate
MAM2355	QUALITY ASSURANCE SAMPLING AND TESTING OF ALUMINUM ALLOYS AND MAGNESIUM ALLOYS Wrought Products (Except Forging Stock) and Flash Welded Rings Metric (SI) Units

Revisions

10 versions available

Revision History*

2023-09-21	\|	AMS4056J
2016-02-02	\|	AMS4056H
2010-10-18	\|	AMS4056G
1994-11-01	\|	AMS4056F
1989-07-01	\|	AMS4056E
1977-07-01	\|	AMS4056D
1968-05-01	\|	AMS4056C
1964-01-01	\|	AMS4056B
1961-07-01	\|	AMS4056A
1960-01-15	\|	AMS4056

* Redlines comparisons are available for those standards listed in the Revision History that contain a radio button. A redline comparison of the current version against a revision is accomplished by selecting the radio button next to the standard and then selecting 'compare'. At this time, Redline versions only exist for some AMS standards. SAE will continue to add redline versioning with ongoing updates to SAE MOBILUS.

Citation
	(MAC / WIN)
	(MAC / WIN)
	(MAC / WIN)
	(MAC / WIN)

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Item Number	Content Type
Title	Author(s)
Affiliation(s)	Publisher
Publish Date	Abstract/scope
Citation	DOI

Aerospace Material Specification	Aluminum Alloy, Plate (7055-T7751) 8.0Zn - 2.3Cu - 2.0Mg - 0.16Zr Solution Heat Treated, Stress Relieved, and Overaged
Aerospace Material Specification	Aluminum Alloy, Sheet and Plate 2.5Mg - 0.25Cr (5052-H32) Strain Hardened, Quarter-Hard, and Stabilized
Aerospace Material Specification	Aluminum Alloy, Drawn, Round Seamless Tubing 2.5Mg - 0.25Cr (5052-O) Annealed

Aluminum Alloy, Sheet and Plate 4.4Mg - 0.70Mn - 0.15Cr (5083-0) Annealed

Scope

Recommended Content

Topic

Data Sets - Support Documents

Issuing Committee

Reference

Revisions

Revision History*