SAE AMSS6758A
- Steel, Chrome-Molybdenum (4130) Bars and Reforging Stock (Aircraft Quality)
- standard by SAE International, 04/03/2013
- Category: SAE
$81.00
$41.00
This specification has been declared NONCURRENT by the Aerospace Materials Division, SAE, as of September, 2003. It is recommended, therefore, that this specification not be specified for new designs. NONCURRENT refers to those specifications that have been widely used and may be required on some existing designs in the future. The Aerospace Materials Division, however, does not recommend these specifications for future use in new designs. Similar but not necessarily identical products are covered by the following specifications: SAE AMS 6346 Steel, Bars, 0.95Cr - 0.20Mo (0.28 - 0.33C) (SAE 4130) Hardened and Tempered, 125 ksi (862 MPa) Tensile StrengthSAE AMS 6348 Steel, Bars, 0.95Cr - 0.20Mo (0.28 - 0.33C) (SAE 4130) NormalizedSAE AMS 6370 Steel, Bars, Forgings, and Rings, 0.95Cr - 0.20Mo (0.28 - 0.33C)SAE AMS 6528 Steel, Bars, 0.95Cr - 0.20Mo (0.28 - 0.33C) Special Aircraft-Quality, NormalizedThis specification covers chrome-molybdenum (4130) steel bars and forging stock of aircraft quality.
PDF
All of our standards document are available in PDF (Portable Document Format), an electronic, downloadable format.You will be able to download the file in your account downloads.
Multi-User Access
After purchasing, you have the ability to assign each license to a specific user.
Printable
At any time, you are permitted to make printed copies for your and your members' reference use.
