Newer Version Available

ALUMINUM ALLOY, HEAT RESISTANT, CASTINGS 5.OCu - 1.5Ni - 0.25Mn - 0.25Sb - 0.25Co - 0.20Ti - 0.20Zr (203.0-T7) Solution Heat Treated and Stabilized

Aerospace Material Specification
AMS4225C
Issued

Published July 01, 1996 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
TABLE 3	Minimum Tensile Properties
TABLE 4	Minimum Tensile Properties
TABLE 5	Minimum Tensile Properties
TABLE 6	Minimum Tensile Properties
TABLE 7	Minimum Tensile Properties

Reference

Number	Title
AMS2360	ROOM TEMPERATURE TENSILE PROPERTIES OF CASTINGS
AMS2361	ELEVATED TEMPERATURE TENSILE PROPERTIES OF CASTINGS
AMS2694	REPAIR WELDING OF AEROSPACE CASTINGS
AMS2771	HEAT TREATMENT OF ALUMINUM ALLOY CASTINGS
AMS2804	IDENTIFICATION Castings
ASTMB557	This document is not part of the subscrption.
ASTMB557M	This document is not part of the subscrption.
ASTMB660	This document is not part of the subscrption.
ASTME101	This document is not part of the subscrption.
ASTME139	This document is not part of the subscrption.
ASTME21	This document is not part of the subscrption.
ASTME227	This document is not part of the subscrption.
ASTME29	This document is not part of the subscrption.
ASTME34	This document is not part of the subscrption.
ASTME607	This document is not part of the subscrption.
ASTME716	This document is not part of the subscrption.
MAM2771	Heat Treatment of Aluminum Alloy Castings

Revisions

6 versions available

Revision History*

2018-03-04	\|	AMS4225E
2017-11-14	\|	AMS4225D
1996-07-01	\|	AMS4225C
1995-05-01	\|	AMS4225B
1984-04-01	\|	AMS4225A
1968-11-01	\|	AMS4225

* 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, Castings 5.0Si - 1.2Cu - 0.50Mg (355.0-T51) Precipitation Heat Treated
Aerospace Material Specification	Aluminum Alloy, Heat-Resistant, Castings 5.0Cu - 1.5Ni - 0.25Mn - 0.25Sb - 0.25Co - 0.20Ti - 0.20Zr (203.0-T6) Solution Heat Treated and Precipitation Heat Treated
Aerospace Material Specification	Aluminum Alloy, Castings 4.5Cu - 0.70Ag - 0.30Mn - 0.25Mg - 0.25Ti (A201.0-T4) Solution Heat Treated and Naturally Aged

ALUMINUM ALLOY, HEAT RESISTANT, CASTINGS 5.OCu - 1.5Ni - 0.25Mn - 0.25Sb - 0.25Co - 0.20Ti - 0.20Zr (203.0-T7) Solution Heat Treated and Stabilized

Scope

Recommended Content

Topic

Data Sets - Support Documents

Issuing Committee

Reference

Revisions

Revision History*