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Aluminum Alloy, Extrusions, 4.4Cu – 1.5Mg – 0.60Mn (2024-T3511), Solution Heat Treated, Cold Worked, Stress-Relieved by Stretching, and Straightened

AMS D Nonferrous Alloys Committee
  • Aerospace Material Specification
  • AMS4165J
  • Current
Published 2019-02-18 by SAE International in United States

This specification covers an aluminum alloy in the form of extruded bars, rods, wire, profiles, and tubing produced with cross sectional area of 32 in2 (206 cm2) maximum.

 
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Aluminum Alloy, Clad Two Sides Sheet, 1.25Mn - 0.12Cu (No. 12-0 Brazing Sheet), Annealed

AMS D Nonferrous Alloys Committee
  • Aerospace Material Specification
  • AMS4064G
  • Current
Published 2019-02-13 by SAE International in United States

This specification covers an aluminum alloy in the form of clad sheet 0.006 to 0.249 inch (0.015 to 6.32 mm) inclusive, in thickness (see 8.5).

 
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Aluminum Alloy, Forgings and Rolled or Forged Rings, (6061-T6), Solution and Precipitation Heat Treated

AMS D Nonferrous Alloys Committee
  • Aerospace Material Specification
  • AMS4127K
  • Current
Published 2019-02-06 by SAE International in United States

This specification covers an aluminum alloy in the form of die forgings not over 4 inches (102 mm) in nominal thickness at time of heat treatment , hand forgings with as-forged thickness not exceeding 8 inches (203 mm) and the cross-sectional area not greater than 256 in2, forged or rolled rings 3.5 inches (89 mm) and under in nominal thickness at time of heat treatment and having an OD-to-wall thickness ratio of 10:1 or greater, and stock of any size for forgings and rings (see 8.6).

 
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Aluminum Alloy, Rolled or Cold Finished Bars, Rods, and Wire, 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr (7075-T73, T7351), Solution Heat Treated, Stress Relieved by Stretching, and Overaged

AMS D Nonferrous Alloys Committee
  • Aerospace Material Specification
  • AMS4124F
  • Current
Published 2019-02-06 by SAE International in United States

This specification covers an aluminum alloy in the form of rolled or cold finished bars, rods, and wire up to 6.000 inches (152.40 mm) in nominal diameter or least nominal dimension (see 8.6).

 
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Aluminum Alloy Plate, 5.7Zn - 2.2Mg - 1.6Cu - 0.22Cr (7475-T7351), Solution Heat Treated, Stress Relieved by Stretching, and Precipitation Heat Treated

AMS D Nonferrous Alloys Committee
  • Aerospace Material Specification
  • AMS4202E
  • Current
Published 2019-02-04 by SAE International in United States

This specification covers an aluminum alloy in the form of plate 0.250 to 4.000 inch (6.35 to 101.60 mm) inclusive, in thickness (see 8.6).

 

Magnesium Alloy, Sand Castings 3.2 Rare Earths - 2.5Zn - 0.70Zr (EZ33A-T5) Precipitation Heat Treated

AMS D Nonferrous Alloys Committee
  • Aerospace Material Specification
  • AMS4442H
  • Current
Published 2019-01-04 by SAE International in United States
This specification covers a magnesium alloy in the form of sand castings.
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Magnesium Alloy, Investment Castings 8.7Al - 0.70Zn - 0.22Mn (AZ91C-T6) Solution and Precipitation Heat Treated

AMS D Nonferrous Alloys Committee
  • Aerospace Material Specification
  • AMS4452F
  • Current
Published 2019-01-04 by SAE International in United States
This specification covers a magnesium alloy in the form of investment castings.
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Aluminum Alloy, Rolled or Forged Rings 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr (7075-T7351, 7075-T7352) Solution Heat Treated, Mechanically Stress Relieved, and Precipitation Heat Treated

AMS D Nonferrous Alloys Committee
  • Aerospace Material Specification
  • AMS4311F
  • Current
Published 2019-01-04 by SAE International in United States
This specification covers an aluminum alloy in the form of rolled or forged rings up to 6 inches (152 mm) inclusive, in nominal thickness at the time of heat treatment, and having an OD to wall thickness ratio of 10 or greater (see 8.6).
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Aluminum Alloy Tubing, Seamless, Drawn 1.8Cu - 1.0Mg - 0.8Si - 0.20Cr Solution Heat Treated, Stress-Relieved by Stretching, and Aged (2013-T4511)

AMS D Nonferrous Alloys Committee
  • Aerospace Material Specification
  • AMS4469A
  • Current
Published 2019-01-04 by SAE International in United States
This specification covers an aluminum alloy in the form of seamless, drawn tubing having a nominal wall thickness of 0.120 to 0.400 inch (3.00 to 10.00 mm) inclusive (see 8.4).
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Magnesium Alloy, Investment Castings 10Al (AM100A-T6) Solution and Precipitation Heat Treated

AMS D Nonferrous Alloys Committee
  • Aerospace Material Specification
  • AMS4455H
  • Current
Published 2019-01-04 by SAE International in United States
This specification covers a magnesium alloy in the form of investment castings.
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