SAE AMS4405A-2012
Aluminum Alloy, Alclad Sheet (6156-T4) 1.0Si 0.90Cu 0.60Mn 0.90Mg Solution Heat Treated and Naturally Aged

Standard No.
SAE AMS4405A-2012
Release Date
2012
Published By
Society of Automotive Engineers (SAE)
Status
 2018-04
Replace By
SAE AMS4405B-2018
Latest
SAE AMS4405C-2018
Scope
This specification covers an aluminum alloy procured in the form of sheet Alclad on both sides. These products have been used typically for formed structural parts requiring good formability in T4 temper and ability to develop improved resistance to fatigue crack growth and high toughness with moderate strength when aged to T62 temper, but usage is not limited to such applications.

SAE AMS4405A-2012 Referenced Document

  • ASTM B660-08 Standard Practices for Packaging/Packing of Aluminum and Magnesium Products*2024-04-19 Update
  • ASTM B666/B666M-08 Standard Practice for Identification Marking of Aluminum and Magnesium Products*2024-04-19 Update
  • ASTM E647-11 Standard Test Method for Measurement of Fatigue Crack Growth Rates*2024-04-19 Update
  • SAE AMS2355 TENSILE TESTING OF WROUGHT ALUMINUM AND MAGNESIUM PRODUCTS Except Forgings
  • SAE AMS2772-1997 Heat Treatment of Aluminum Alloy Raw Materials (01 1997)
  • SAE AS1990-1990 Aluminum Alloy Tempers

SAE AMS4405A-2012 history

  • 2018 SAE AMS4405C-2018 Aluminum Alloy@ Alclad Sheet (6156-T4) 1.0Si - 0.90Cu - 0.60Mn - 0.90Mg Solution Heat Treated and Naturally Aged (UNS AA6156)
  • 2018 SAE AMS4405B-2018 Aluminum Alloy@ Alclad Sheet (6156-T4) 1.0Si - 0.90Cu - 0.60Mn - 0.90Mg Solution Heat Treated and Naturally Aged (UNS AA6156)
  • 2012 SAE AMS4405A-2012 Aluminum Alloy, Alclad Sheet (6156-T4) 1.0Si 0.90Cu 0.60Mn 0.90Mg Solution Heat Treated and Naturally Aged
  • 2006 SAE AMS4405-2006 Aluminum Alloy, Alclad Sheet (6156-T4) 1.0Si - 0.90Cu - 0.60Mn - 0.90Mg Solution Heat Treated and Naturally Aged



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