SAE AMS6327J
Steel Bars and Forgings 0.50Cr - 0.55Ni - 0.25Mo (0.38 - 0.43C) (SAE 8740) Heat Treated, 125 ksi (862 MPa) Tensile Strength
Historical
Standard by SAE International, 2007-10-16
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| AMS6327J.pdf |
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| AMS6327J.pdf |
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About This Item
This specification covers an aircraft-quality, low-alloy steel in the form of bars and forgings.
AMS 6327J results from a Five Year Review and update of this specification.
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Standard Details
- Publication Date: 2007-10-16
- Standard Status: historical
- Publisher: SAE International
- Document Type: Aerospace Material Specification
- Subject: Heat treatment, Steel, Tensile strength, Identification numbers, Quality assurance, Chemicals, Alloys, Nickel, Corrosion
- Official SAE: Doi link
Document History
- New Version Available: AMS6327M (2024-06-13)
- Previous Version: AMS6327L (2017-09-22)
- Previous Version: AMS6327K (2012-10-03)
- This Version: AMS6327J (2007-10-16)
- Previous Version: AMS6327H (2003-01-22)
- Previous Version: AMS6327G (2000-10-01)
- Previous Version: AMS6327F (1981-01-15)
- Previous Version: AMS6327E (1972-11-15)
- Previous Version: AMS6327D (1966-09-30)
- Previous Version: AMS6327C (1951-06-01)
- Previous Version: AMS6327B (1945-07-01)
- Previous Version: AMS6327A (1943-04-01)
- Previous Version: AMS6327 (1942-09-01)
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