SAE AMS6472H-2024
Steel, Bars and Forgings and Forging Stock, Nitriding, 1.6Cr - 0.35Mo - 1.1Al (0.38 - 0.43C) (135 Mod), Aircraft Quality, Hardened and Tempered, 112 ksi (772 Mpa) Tensile Strength

Standard No.
SAE AMS6472H-2024
Release Date
2024
Published By
Society of Automotive Engineers (SAE)
Latest
SAE AMS6472H-2024
 

Scope
This specification covers an aircraft-quality, low-alloy steel in the form of heat-treated bars and forgings, and of forging stock. This material has been used typically for nitrided parts requiring high surface hardness, resistance to heat, and less distortion than parts fabricated from steel requiring quenching to case harden, but usage is not limited to such applications. This steel may be case hardened in dissociated ammonia gas to provide a minimum case hardness of 900 HV.

SAE AMS6472H-2024 Referenced Document

  • AS 1182 Infant and child clothing sizing coding scheme for underwear and outerwear*2025-05-09 Update
  • ASTM A370 Standard Test Methods and Definitions for Mechanical Testing of Steel Products
  • ASTM A751 Standard Test Methods, Practices, and Terminology for Chemical Analysis of Steel Products
  • ASTM E1077 Standard Test Methods for Estimating the Depth of Decarburization of Steel Specimens
  • ASTM E140 Standard Hardness Conversion Tables for Metals Relationship Among Brinell Hardness, Vickers Hardness, Rockwell Hardness, Superficial Hardness, Knoop Hardness, and Scleroscope Hardness
  • ASTM E381 Standard Method of Macroetch Testing Steel Bars, Billets, Blooms, and Forgings

SAE AMS6472H-2024 history

  • 2024 SAE AMS6472H-2024 Steel, Bars and Forgings and Forging Stock, Nitriding, 1.6Cr - 0.35Mo - 1.1Al (0.38 - 0.43C) (135 Mod), Aircraft Quality, Hardened and Tempered, 112 ksi (772 Mpa) Tensile Strength
  • 2018 SAE AMS6472G-2018 Steel@ Bars and Forgings@ Nitriding 1.6Cr - 0.35Mo - 1.1Al (0.38 - 0.43C) (135 Mod) Hardened and Tempered@ 112 ksi (772 MPa) Tensile Strength (UNS K24065)
  • 2014 SAE AMS6472F-2014 Steel, Bars and Forgings, Nitriding 1.6Cr - 0.35Mo - 1.1Al (0.38 - 0.43C) (135 Mod) Hardened and Tempered, 112 ksi (772 MPa) Tensile Strength
  • 2010 SAE AMS6472E-2010 Steel Bars and Forgings, Nitriding 1.6Cr 0.35Mo 1.1Al (0.38-0.43C)(135 Mod) Hardened and Tempered, 112 ksi (772 MPa) Tensile Strength
  • 2006 SAE AMS6472D-2006 Steel, Bars and Forgings, Nitriding 1.6Cr - 0.35Mo - 1.1Al (0.38 - 0.43C) Hardened and Tempered, 112 ksi (772 MPa) Tensile Strength
  • 2001 SAE AMS6472D-2001 Steel Bars and Forgings, Nitriding 1.6Cr 0.35Mo 1.1Al (0.38-0.43C) Hardened and Tempered, 112 ksi (772 MPa) Tensile Strength
  • 1995 SAE AMS6472C-1995 STEEL BARS AND FORGINGS, NITRIDING 1.6Cr - 0.35Mo - 1.1Al (0.38 - 0.43C) Hardened and Tempered, 112 ksi (772 MPa) Tensile Strength
  • 1991 SAE AMS6472C-1991 Steel Bars and Forgings@ Nitriding 1.6Cr - 0.35Mo - 1.1Al (0.38 - 0.43C) Hardened and Tempered@ 112 ksi (772 MPa) Tensile Strength
  • 1984 SAE AMS6472B-1984 STEEL BARS AND FORGINGS@ NITRIDING 1.6Cr – 0.35Mo – 1.1Al (0.38 – 0.43C) Heat and Treated@ 112@000 psi (772 MPa) Tensile Strength (UNS K24065)
  • 1971 SAE AMS6472A-1971 STEEL BARS AND FORGINGS@ NITRIDING 1.6Cr – 0.35Mo – 1.13Al (0.38 – 0.43C) Heat Treated@ 112@000 psi (772 MN/M2) Tensile
  • 1965 SAE AMS6472-1965 STEEL BARS AND FORGINGS@ NITRIDING 1.6Cr – 0.35Mo – 1.13Al (0.38 – 0.43C) Heat Treated (112@000 psi Tensile)
Steel, Bars and Forgings and Forging Stock, Nitriding, 1.6Cr - 0.35Mo - 1.1Al (0.38 - 0.43C) (135 Mod), Aircraft Quality, Hardened and Tempered, 112 ksi (772 Mpa) Tensile Strength

Standard and Specification




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