Aluminum Alloy Die Forgings 4.0Cu - 2.0Ni - 0.68Mg (2018-T61) Solution and Precipitation Heat Treated

Aerospace Material Specification
AMS4140K
Stabilized

Published December 11, 2014 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
TABLE 2	Minimum Tensile Properties

Reference

Number	Title
AMS2355	TENSILE TESTING OF WROUGHT ALUMINUM AND MAGNESIUM PRODUCTS Except Forgings
AMS2772	HEAT TREATMENT OF ALUMINUM ALLOY RAW MATERIALS
AMS2808	IDENTIFICATION Forgings
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
ASTMB594	This document is not part of the subscrption.
ASTMB660	This document is not part of the subscrption.
ASTME1417	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

11 versions available

Revision History*

2014-12-11	\|	AMS4140K
2009-08-05	\|	AMS4140J
2006-04-24	\|	AMS4140H
1995-05-01	\|	AMS4140G
1985-07-01	\|	AMS4140F
1978-10-01	\|	AMS4140E
1952-06-01	\|	AMS4140D
1945-10-01	\|	AMS4140C
1944-11-01	\|	AMS4140B
1942-08-01	\|	AMS4140A
1942-01-01	\|	AMS4140

* 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, Plate 4.4Cu - 1.5Mg - 0.60Mn (2124-T8151) Solution Heat Treated, Stress Relieved, and Precipitation Heat Treated
Aerospace Material Specification	Forgings, Magnesium Alloy 5.5Zn - 0.45Zr (ZK60A-T5) Precipitation Heat Treated
Aerospace Material Specification	Aluminum Alloy, Die Forgings 6.2Zn - 2.3Cu - 2.2Mg - 0.12Zr (7050-T7452) Solution Heat Treated, Compression Stress-Relieved, and Overaged

Aluminum Alloy Die Forgings 4.0Cu - 2.0Ni - 0.68Mg (2018-T61) Solution and Precipitation Heat Treated

Scope

Rationale

Recommended Content

Topic

Data Sets - Support Documents

Issuing Committee

Reference

Revisions

Revision History*