Aluminum Alloy, Castings, 4.7cu 0.60ag 0.35mn 0.25mg 0.25ti (B201.0-T7) Solution Heat Treated and Overaged Aircraft

Standard:
Revised:
  • 1997-09-01
 
  • HISTORICAL Access the latest revision: AMS4242C
Publisher:
  • SAE International
Pages:
11
Scope:

This specification covers an aluminum alloy in the form of castings.

These castings have been used typically for aircraft components requiring high strength and reliability, but usage is not limited to such applications.

Alloy B201.0, the alloy designated in this specification, has restricted composition within the limits of alloy A201.0.

History:
Standard Published Revision Status
AMS4242C 2015-09-01 Latest Revised
2012-09-27 Historical Reaffirmed
1997-09-01 Historical Revised
1986-07-01 Historical Issued
AKA:
  • SAE AMS 4242
Sector:
Access
Now
SAE MOBILUS Subscriber? You may already have access.
Buy
Select
Price
List
Download
$78.00
Add
Mail
$78.00
Members save up to 18% off list price.
Grade
If you are currently using this technical report:
Share
HTML for Linking to Page
Page URL

Related Items

Technical Paper / Journal Article
2013-09-17
Book
2012-11-01
Training / Education
2017-10-19