SAE AMS4216B-2003
Aluminum Alloy, Sheet 1.0Mg - 0.8Si - 0.8Cu - 0.50Mn (6013-T6) Solution Heat Treated and Artificially Aged UNS A96013

Standard No.
SAE AMS4216B-2003
Release Date
2003
Published By
Society of Automotive Engineers (SAE)
Status
Replace By
SAE AMS4216B-2013
Latest
SAE AMS4216C-2020
Scope
This specification covers an aluminum alloy in the form of sheet. This sheet has been used typically for structural parts requiring good strength, toughness, and fatigue properties and maximum corrosion resistance, but usage is not limited to such applications.

SAE AMS4216B-2003 Referenced Document

  • ASTM B660-02 Standard Practices for Packaging/Packing of Aluminum and Magnesium Products*2024-04-18 Update
  • ASTM B666/B666M-01 Standard Practice for Identification Marking of Aluminum and Magnesium Products*2024-04-18 Update
  • SAE AMS2355G-2002 Quality Assurance, Sampling and Testing Aluminum Alloys and Magnesium Alloys Wrought Products, Except Forging Stock, and Rolled, Forged, or Flash Welded Rings
  • SAE AMS2772-1997 Heat Treatment of Aluminum Alloy Raw Materials (01 1997)
  • SAE AS1990-1990 Aluminum Alloy Tempers

SAE AMS4216B-2003 history

  • 2020 SAE AMS4216C-2020 Aluminum Alloy, Sheet 1.0Mg - 0.8Si - 0.8Cu - 0.50Mn (6013-T6) Solution Heat Treated and Artificially Aged
  • 2013 SAE AMS4216B-2013 Aluminum Alloy, Sheet 1.0Mg - 0.8Si - 0.8Cu - 0.50Mn (6013-T6) Solution Heat Treated and Artificially Aged
  • 2003 SAE AMS4216B-2003 Aluminum Alloy, Sheet 1.0Mg - 0.8Si - 0.8Cu - 0.50Mn (6013-T6) Solution Heat Treated and Artificially Aged UNS A96013
  • 1998 SAE AMS4216A-1998 Aluminum Alloy@ Sheet 1.0Mg - 0.8Si - 0.8Cu - 0.50Mn (6013-T6) Solution Heat Treated and Artificially Aged (UNS A96013)
  • 1989 SAE AMS4216-1989 Aluminum Alloy Sheet 1.0Mg - 0.8Si - 0.8Cu - 0.50Mn (6013-T6) Solution Heat Treated and Artificially Aged
Aluminum Alloy, Sheet 1.0Mg - 0.8Si - 0.8Cu - 0.50Mn (6013-T6) Solution Heat Treated and Artificially Aged UNS A96013



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