Aluminum Alloy Plate 5.7Zn - 2.2Mg - 1.6Cu - 0.22Cr (7475-T7351) Solution Heat Treated, Stress Relieved by Stretching, and Precipitation Heat Treated

Aerospace Material Specification
AMS4202E
Revised

Published February 04, 2019 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
Unnamed Dataset 4
Table 1	Composition
Table 2A	Minimum tensile properties, inch-pound units
Table 2B	Minimum tensile properties, SI units
Table 3	Minimum plane-strain fracture toughness, KIC
Table 4	Ultrasonic class

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.
AS1990	Aluminum Alloy Tempers
ASTMB594	This document is not part of the subscrption.
ASTMB645	This document is not part of the subscrption.
ASTMB646	This document is not part of the subscrption.
ASTMB660	This document is not part of the subscrption.
ASTMB666	This document is not part of the subscrption.
ASTME1304	This document is not part of the subscrption.
ASTME399	This document is not part of the subscrption.
ASTME602	This document is not part of the subscrption.
ASTME645	This document is not part of the subscrption.
MAM2202	Tolerances, Metric, Aluminum Alloy and Magnesium Alloy Sheet and Plate (Cance
MAM2355	Quality Assurance, Sampling and Testing, Aluminum Alloys and Magnesium Alloys, Wrought Products, Except Forging Stock, and Rolled, Forged, or Flash Welded Rings
MIL-H-6088	This document is not part of the subscrption.

Revisions

6 versions available

Revision History*

2019-02-04	\|	AMS4202E
2012-03-29	\|	AMS4202D
1994-04-01	\|	AMS4202C
1987-04-01	\|	AMS4202B
1981-07-01	\|	AMS4202A
1978-07-15	\|	AMS4202

* 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-T851) Solution Heat Treated, Stretched, and Precipitation Heat Treated
Aerospace Material Specification	Aluminum Alloy, Plate 6.4Zn - 2.4Mg - 2.2Cu - 0.12Zr (7150-T7751) Solution Heat Treated, Stress Relieved, and Overaged
Aerospace Material Specification	Aluminum Alloy, Alclad, Sheet 5.7Zn - 2.2Mg - 1.6Cu - 0.22Cr (Alclad 7475-T761) Solution and Precipitation Heat Treated

Aluminum Alloy Plate 5.7Zn - 2.2Mg - 1.6Cu - 0.22Cr (7475-T7351) Solution Heat Treated, Stress Relieved by Stretching, and Precipitation Heat Treated

Scope

Rationale

Recommended Content

Topic

Data Sets - Support Documents

Issuing Committee

Reference

Revisions

Revision History*