SAE AMS6352H-2004 PDF

Scope: This specification covers an aircraft-quality, low-alloy steel in the form of sheet, strip, and plate. These products have been used typically for heat treated parts and structures that may require welding during fabrication, but usage is not limited to such applications. It may be through-hardened to a minimum tensile strength of 180 ksi (1241 MPa) in sections 0.125 inch (3.18 mm) and under in nominal thickness and proportionately lower strength in heavier section thicknesses.

SAE AMS6352H-2004 history

2023 SAE AMS6352M-2023 Steel Sheet, Strip, and Plate 0.95Cr - 0.20Mo (0.33 - 0.38C) (SAE 4135)
2018 SAE AMS6352L-2018 Steel Sheet@ Strip@ and Plate 0.95Cr - 0.20Mo (0.33 - 0.38C) (SAE 4135) (UNS G41350)
2013 SAE AMS6352K-2013 Steel Sheet, Strip, and Plate, 0.95Cr - 0.20Mo (0.33 - 0.38C) (SAE 4135)
2009 SAE AMS6352J-2009 Steel Sheet, Strip, And Plate, 0.95Cr 0.20Mo (0.33-0.38C) (SAE 4135)
2004 SAE AMS6352H-2004 Steel Sheet, Strip, And Plate, 0.95Cr 0.20Mo (0.33-0.38C) (SAE 4135)
1999 SAE AMS6352G-1999 Steel Sheet, Strip, and Plate 0.95Cr - 0.20Mo (0.33 - 0.38C) (SAE 4135) UNS G41350
1994 SAE AMS6352F-1994 STEEL SHEET, STRIP, AND PLATE 0.95Cr - 0.20Mo (0.33 - 0.38C) (SAE 4135)
1990 SAE AMS6352F-1990 Steel Sheet@ Strip@ and Plate 0.95Cr - 0.20Mo (0.33 - 0.38C) (SAE 4135)
1984 SAE AMS6352E-1984 STEEL SHEET@ STRIP AND PLATE 0.95Cr - 0.20Mo (0.33 - 0.38C) (SAE 4135) (UNS G41350)
1979 SAE AMS6352D-1979 STEEL SHEET@ STRIP AND PLATE 0.95Cr - 0.20Mo (0.33 - 0.38C) (SAE 4135)
1971 SAE AMS6352C-1971 STEEL SHEET@ STRIP AND PLATE 0.95Cr - 0.20Mo (0.32 - 0.38C) (SAE 4135)
1950 SAE AMS6352B-1950 STEEL SHEET AND STRIP 0.95Cr - 0.2Mo (0.32 - 0.39C) (SAE 4135H)
1942 SAE AMS6352A-1942 STEEL PLATE@ SHEET AND STRIP Chromium Molybdenum (.32 - .39 Carbon)
1939 SAE AMS6352-1939 STEEL SHEET OR STRIP Chromium Molybdenum