Titanium Alloy Bars, Wire, and Forgings 7Al - 4Mo Solution and Precipitation Heat Treated

Aerospace Material Specification
AMS4970L
Revised

Published June 29, 2020 by SAE International in United States

Sector:

Issuing Committee:

AMS G Titanium and Refractory Metals Committee

Language: English

Data Sets - Support Documents

Title	Description	Download
Unnamed Dataset 1
Unnamed Dataset 2
Table 1	Composition
Table 2A	Minimum tensile properties, inch/pound units
Table 2B	Minimum tensile properties, SI units

Reference

Number	Title
AMS2241	TOLERANCES Stainless Steel Bars
AMS2249	CHEMICAL CHECK ANALYSIS LIMITS Titanium and Titanium Alloys
AMS2368	Sampling and Testing of Wrought Titanium Raw Material Except Forgings and Forging Stock
AMS2750	PYROMETRY
AMS2808	Identification Forgings
AMS2809	Identification Titanium and Titanium Alloy Wrought Products
ARP982	Minimizing Stress-Corrosion Cracking in Wrought Titanium Alloy Products
ASTME139	This document is not part of the subscrption.
ASTME1409	This document is not part of the subscrption.
ASTME1447	This document is not part of the subscrption.
ASTME1941	This document is not part of the subscrption.
ASTME2371	This document is not part of the subscrption.
ASTME292	This document is not part of the subscrption.
ASTME8	This document is not part of the subscrption.
ASTME8/E8M	This document is not part of the subscrption.

Revisions

12 versions available

Revision History*

2020-06-29	\|	AMS4970L
2016-09-20	\|	AMS4970K
2012-09-25	\|	AMS4970J
2008-02-15	\|	AMS4970H
2003-03-14	\|	AMS4970G
1994-04-01	\|	AMS4970F
1994-04-01	\|	AMS4970E
1978-07-15	\|	AMS4970D
1970-05-01	\|	AMS4970C
1969-11-01	\|	AMS4970B
1966-03-15	\|	AMS4970A
1965-09-01	\|	AMS4970

* 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)
	(MAC / WIN)

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Aerospace Material Specification	Titanium Alloy Sheet, Strip, and Plate 8Al - 1V - 1Mo Single Annealed
Aerospace Material Specification	Titanium Alloy Sheet, Strip, and Plate 13.5V - 11Cr - 3.0Al Solution Heat Treated
Aerospace Material Specification	Titanium Alloy Sheet, Strip, and Plate 6Al - 6V - 2Sn Solution Heat Treated

Titanium Alloy Bars, Wire, and Forgings 7Al - 4Mo Solution and Precipitation Heat Treated

Scope

Rationale

Recommended Content

Topic

Data Sets - Support Documents

Issuing Committee

Reference

Revisions

Revision History*