Hello. Sign In
Standards Store




SAE AMS6478

Revision B, September 2005

Complete Document

Steel, Bars and Forgings 3.1Cr - 11.5Ni - 13.5Co - 1.2Mo (0.21 - 0.25C) Vacuum Melted, Annealed Heat Treatable to 290 ksi (1999 MPa) Tensile Strength

Includes all amendments and changes through Cancellation Notice , September 2005


View Abstract
Product Details
Document History

Detail Summary

Superseded By: SAE AMS6532

EN
Additional Comments:
CNCL S/S BY SAE AMS6532
Format
Details
Price (USD)
PDF
Single User
$98.00
Print
In Stock
$102.00
Add to Cart

Product Details:

  • Revision: Revision B, September 2005
  • Published Date: September 2005
  • Status: Superseded By:
  • Superseded By: SAE AMS6532
  • Document Language: English
  • Published By: SAE International (SAE)
  • Page Count: 9
  • ANSI Approved: No
  • DoD Adopted: No

Description / Abstract:

Form: This specification covers a premium aircraft-quality alloy steel in the form of bars, forgings, and forging stock.

Application: These products have been used typically for parts requiring a combination of high strength, high toughness, and weldability, but usage is not limited to such applications. Product after heat treatment should attain a minimum tensile strength of 290 ksi (1999 MPa) and yield strength of 245 ksi (1689 MPa).
AIA/NAS Aerospace Standards