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About This Item

 

Full Description

This specification covers an aircraft-quality, low-alloy steel in the form of bars. These bars have been used typically for parts, 0.50 inch (12.7 mm) and under in section thickness at time of heat treatment, requiring a through-hardening steel capable of developing hardness as high as 35 HRC when properly hardened and tempered and also parts of greater thickness but requiring proportionately lower hardness, but usage is not limited to such applications.
 

Document History

  1. SAE AMS6348F


    Steel, Bars Aircraft Quality 0.95Cr - 0.20Mo (0.28 to 0.33C) (4130) Normalized

    • Most Recent
  2. SAE AMS6348E


    Steel, Bars 0.95Cr - 0.20Mo (0.28 to 0.33C) (SAE 4130) Normalized

    • Historical Version
  3. SAE AMS6348D

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    Steel, Bars 0.95Cr - 0.20Mo (0.28 to 0.33C) (SAE 4130) Normalized

    • Historical Version
  4. SAE AMS6348C


    Steel, Bars, 0.95Cr - 0.20Mo (0.28 to 0.33C) (SAE 4130), Normalized

    • Historical Version