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Aluminum Alloy Extrusions 4.4Cu - 1.5Mg - 0.60Mn (2024-T3) Solution Heat Treated

Aerospace Material Specification
AMS4152L
Reaffirmed

Published August 01, 2000 by SAE International in United States

Sector:

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	Minimum Tensile Properties, Inch/Pound Units
TABLE 2B	Minimum Tensile Properties, SI Units
TABLE 3A	Minimum Tensile Properties, Inch/Pound Units
TABLE 3B	Minimum Tensile Properties, SI Units

Reference

Number	Title
AMS2205	TOLERANCES Aluminum and Aluminum Alloy Bars, Rods and Shapes Extruded
AMS2355	TENSILE TESTING OF WROUGHT ALUMINUM AND MAGNESIUM PRODUCTS Except Forgings
AMS2811	IDENTIFICATION Aluminum and Magnesium Alloy Wrought Products
ARP823	Minimizing Stress-Corrosion Cracking in Wrought Heat-Treatable Aluminum Alloy Products
ASTMB594	This document is not part of the subscrption.
ASTMB660	This document is not part of the subscrption.
MAM2205	Tolerances, Metric, Aluminum Alloy and Magnesium Alloy Extrusions (Cance
MAM2355	QUALITY ASSURANCE SAMPLING AND TESTING OF ALUMINUM ALLOYS AND MAGNESIUM ALLOYS Wrought Products (Except Forging Stock) and Flash Welded Rings Metric (SI) Units
MIL-H-6088	This document is not part of the subscrption.

Revisions

14 versions available

Revision History*

2019-06-17	\|	AMS4152N
2018-05-03	\|	AMS4152M
2011-08-10	\|	AMS4152K
2000-08-01	\|	AMS4152L
1978-04-01	\|	AMS4152J
1967-11-01	\|	AMS4152H
1964-01-01	\|	AMS4152G
1956-02-01	\|	AMS4152F
1952-06-01	\|	AMS4152E
1946-11-01	\|	AMS4152D
1946-06-01	\|	AMS4152C
1943-10-01	\|	AMS4152B
1942-12-01	\|	AMS4152A
1941-11-01	\|	AMS4152

* 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
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Aerospace Material Specification	Aluminum Alloy, Extrusions 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr (7075-T73511) Solution Heat Treated, Stress Relieved by Stretching, and Overaged
Aerospace Material Specification	Magnesium Alloy, Extrusions 5.5Zn - 0.45Zr (ZK60A-T5) Precipitation Heat Treated
Aerospace Material Specification	Aluminum Alloy Extrusions 7.8Zn - 2.6Mg - 2.0Cu - 0.10Zr - (7068-T6511) Solution Heat Treated, Stress Relieved, and Precipitation Heat Treated

Aluminum Alloy Extrusions 4.4Cu - 1.5Mg - 0.60Mn (2024-T3) Solution Heat Treated

Scope

Recommended Content

Topic

Data Sets - Support Documents

Issuing Committee

Reference

Revisions

Revision History*