Newer Version Available

Steel, Sheet, Strip, and Plate 5.0Cr - 1.3Mo - 0.50V (0.38 - 0.43C) (H-11)

Aerospace Material Specification
AMS6437H
Revised

Published March 28, 2011 by SAE International in United States

Sector:

Issuing Committee:

AMS E Carbon and Low Alloy Steels Committee

Language: English

Data Sets - Support Documents

Title	Description	Download
Unnamed Dataset 1
Unnamed Dataset 2
TABLE 1	COMPOSITION
TABLE 2A	MAXIMUM DECARBURIZATION, INCH/POUND UNITS
TABLE 2B	MAXIMUM DECARBURIZATION, SI UNITS
TABLE 3	BEND REQUIREMENTS
TABLE 4	MINIMUM TENSILE PROPERTIES

Reference

Number	Title
AMS2252	TOLERANCES Alloy Steel Sheet and Strip
AMS2259	Chemical Check Analysis Limits, Wrought Low-Alloy and Carbon Steels
AMS2301	AIRCRAFT QUALITY STEEL CLEANLINESS Magnetic Particle Inspection Procedure
AMS2370	QUALITY ASSURANCE SAMPLING OF CARBON AND LOW ALLOY STEELS Wrought Products Except Forgings
AMS2807	IDENTIFICATION Carbon and Low-Alloy Steels, Corrosion and Heat Resistant Steels and Alloys Sheet, Strip, Plate, and Aircraft Tubing
ASTMA370	This document is not part of the subscrption.
ASTME112	This document is not part of the subscrption.
ASTME290	This document is not part of the subscrption.
ASTME350	This document is not part of the subscrption.
ASTME384	This document is not part of the subscrption.

Revisions

11 versions available

Revision History*

2020-05-19	\|	AMS6437K
2015-12-20	\|	AMS6437J
2011-03-28	\|	AMS6437H
2006-09-14	\|	AMS6437G
2001-09-01	\|	AMS6437F
1995-05-01	\|	AMS6437E
1991-10-01	\|	AMS6437D
1980-04-15	\|	AMS6437C
1971-11-15	\|	AMS6437B
1964-01-31	\|	AMS6437A
1959-11-01	\|	AMS6437

* 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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	(MAC / WIN)
	(MAC / WIN)
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Aerospace Material Specification	Steel Tubing, Seamless 0.95Cr - 0.20Mo (0.28 - 0.33C) (SAE 4130) 125 ksi (862 MPa) Tensile Strength
Aerospace Material Specification	Steel Tubing, Seamless 0.95Cr - 0.20Mo (0.28 - 0.33C) (SAE 4130) 150 ksi (1034 MPa) Tensile Strength

Steel, Sheet, Strip, and Plate 5.0Cr - 1.3Mo - 0.50V (0.38 - 0.43C) (H-11)

Scope

Rationale

Recommended Content

Topic

Data Sets - Support Documents

Issuing Committee

Reference

Revisions

Revision History*