Steel Bars and Forgings 0.50cr 0.55ni 0.25mo (0.38 0.43c) (SAE 8740) Heat Treated, 125 Ksi (862 Mpa) Tensile Strength

Standard:
Revised:
  • 2003-01-22
 
  • HISTORICAL Access the latest revision: AMS6327L
Publisher:
  • SAE International
Pages:
8
Scope:

This specification covers an aircraft-quality, low-alloy steel in the form of bars and forgings.

These products have been used typically for parts, such as nuts, bolts, and screws, 1.50 inch (38.1 mm) and under in section thickness, requiring a minimum tensile strength of 125,000 (862 MPa) but usage is not limited to such applications.

History:
Standard Published Revision Status
AMS6327L 2017-09-22 Latest Revised
2012-10-03 Historical Revised
2007-10-16 Historical Revised
2003-01-22 Historical Revised
2000-10-01 Historical Reaffirmed
1981-01-15 Historical Revised
1972-11-15 Historical Revised
1966-09-30 Historical Revised
1951-06-01 Historical Revised
1945-07-01 Historical Revised
1943-04-01 Historical Revised
1942-09-01 Historical Issued
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