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Aluminum Alloy, Alclad Sheet and Plate 4.4Cu - 1.5Mg - 0.60Mn (Alclad 2024 and 1-1/2% Alclad 2024-0) Annealed

Aerospace Material Specification
AMS4040M
Reaffirmed

Published June 11, 2009 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
Unnamed Dataset 3
TABLE 1	Composition, Core (2024)
TABLE 2	Composition, Cladding (1230)
TABLE 3A	Tensile Properties, Inch/Pound Units
TABLE 3B	Tensile Properties, SI Units
TABLE 4	Bending Parameters
TABLE 5A	Minimum Tensile Properties, Inch/Pound Units
TABLE 5B	Minimum Tensile Properties, SI Units
TABLE 6	Bending Parameters
TABLE 7	Cladding Thickness

Reference

Number	Title
AMS2355	TENSILE TESTING OF WROUGHT ALUMINUM AND MAGNESIUM PRODUCTS Except Forgings
AMS2772	HEAT TREATMENT OF ALUMINUM ALLOY RAW MATERIALS
ANSIH35.2	This document is not part of the subscrption.
ANSIH35.2M	This document is not part of the subscrption.
ARP823	Minimizing Stress-Corrosion Cracking in Wrought Heat-Treatable Aluminum Alloy Products
ASTMB660	This document is not part of the subscrption.
ASTMB666/B666M	This document is not part of the subscrption.
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

15 versions available

Revision History*

2018-02-15	\|	AMS4040P
2012-07-25	\|	AMS4040N
2009-06-11	\|	AMS4040M
1995-03-01	\|	AMS4040L
1989-04-01	\|	AMS4040K
1983-07-01	\|	AMS4040J
1974-12-01	\|	AMS4040H
1967-11-01	\|	AMS4040G
1964-06-01	\|	AMS4040F
1958-04-01	\|	AMS4040E
1955-03-01	\|	AMS4040D
1952-06-01	\|	AMS4040C
1946-04-01	\|	AMS4040B
1942-08-01	\|	AMS4040A
1941-11-01	\|	AMS4040

* 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.

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Aerospace Material Specification	Aluminum Alloy, Sheet and Plate 1.0Mg - 0.60Si - 0.28Cu - 0.20Cr (6061-O) Annealed
Aerospace Material Specification	Aluminum Alloy, Sheet and Plate 6.3Cu - 0.30Mn - 0.18Zr - 0.10V - 0.06Ti (2219-O) Annealed or when specified, “As Fabricated” (2219-F)

Aluminum Alloy, Alclad Sheet and Plate 4.4Cu - 1.5Mg - 0.60Mn (Alclad 2024 and 1-1/2% Alclad 2024-0) Annealed

Scope

Recommended Content

Topic

Data Sets - Support Documents

Issuing Committee

Reference

Revisions

Revision History*