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Aluminum Alloy 2024, Bar, Rod, Shapes, Tube, and Wire, Extruded

AMS D Nonferrous Alloys Committee
  • Aerospace Material Specification
  • AMSQQA200/3A
  • Current
Published 2019-11-19 by SAE International in United States

This specification covers the specific requirements for aluminum alloy 2024 bar, rod, shapes, tube, and wire produced by extrusion.

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Aluminum Alloy, Bar, Rod, Shapes, Structural Shapes, Tube, and Wire, Extruded: General Specification for

AMS D Nonferrous Alloys Committee
  • Aerospace Material Specification
  • AMSQQA200C
  • Current
Published 2019-11-19 by SAE International in United States

This specification covers the general requirements for aluminum alloy bar, rod, shapes, structural shapes, tube, and wire extruded. Specific requirements for these products in a particular alloy are covered by the applicable detailed specification (See 6.3).

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Aluminum Alloy, Extrusion 3.7Cu - 1.15Li - 0.5Zn - 0.45Ag - 0.4Mg - 0.3Mn - 0.1Zr (2055-T84) Solution Heat Treated, Stress Relieved by Stretching 2% to 5% and Aged

AMS D Nonferrous Alloys Committee
  • Aerospace Material Specification
  • AMS4257
  • Current
Published 2019-11-12 by SAE International in United States
This specification covers an aluminum alloy in the form of extruded bars, rods, and profiles.
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Aluminum Alloy Extrusions, 7.9Zn - 1.6Cu - 2.2Mg - 0.16Cr (7249-T76511), Solution Heat Treated, Stress-Relieved, Straightened, and Overaged

AMS D Nonferrous Alloys Committee
  • Aerospace Material Specification
  • AMS4293A
  • Current
Published 2019-10-24 by SAE International in United States

This specification covers an aluminum alloy procured in the form of extruded bars, rods, wire, profiles (shapes) and tubing up to 1.499 inches (38.07 mm), inclusive in nominal diameter or least thickness (bars, rods, wire, profiles) or nominal wall thickness (tubing) (see 8.6).

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Aluminum Alloy, Extrusions 1.0Mg - 0.60Si - 0.30Cu - 0.20Cr (6061-T6511) Solution Heat Treated, Stress Relieved by Stretching, Straightened, and Precipitation Heat Treated

AMS D Nonferrous Alloys Committee
  • Aerospace Material Specification
  • AMS4173G
  • Current
Published 2019-10-17 by SAE International in United States

This specification covers an aluminum alloy in the form of extruded bars, rods, wire, profiles, and tubing. These extrusions have been used typically for parts requiring moderate strength and where distortion during machining must be minimized, but usage is not limited to such applications.

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Aluminum Alloy, Alclad Sheet and Plate 6.3Cu - 0.30Mn - 0.18Zr - 0.10V - 0.06Ti Alclad 2219-T31; Sheet, Solution Heat Treated and Cold Worked Alclad 2219-T351; Plate, Solution Heat Treated and Stress Relieved

AMS D Nonferrous Alloys Committee
  • Aerospace Material Specification
  • AMS4095E
  • Current
Published 2019-10-01 by SAE International in United States
This specification covers an aluminum alloy in the form of sheet and plate 0.020 to 0.499 inch (0.51 to 12.67 mm) inclusive, in nominal thickness (see 8.4) alclad two sides.
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Aluminum Alloy, Hand Forgings 7.5Zn - 1.6Cu - 1.5Mg - 0.12Zr (7085-T7452) Solution Heat Treated, Compression Stress-Relieved, and Overaged

AMS D Nonferrous Alloys Committee
  • Aerospace Material Specification
  • AMS4414
  • Current
Published 2019-09-19 by SAE International in United States
This specification covers an aluminum alloy in the form of hand forgings 12 inches (305 mm) and under in nominal thickness and of forging stock.
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Castings, Sand, Magnesium Alloy 5.1Y - 3.0Re - 0.70Zr (WE54A - T6) Solution and Precipitation Heat Treated

AMS D Nonferrous Alloys Committee
  • Aerospace Material Specification
  • AMS4426B
  • Current
Published 2019-09-19 by SAE International in United States
This specification covers a magnesium alloy in the form of sand castings.
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Aluminum Alloy, Alclad Sheet and Plate 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr (7075; -T76 Sheet, -T7651 Plate) Solution and Precipitation Heat Treated

AMS D Nonferrous Alloys Committee
  • Aerospace Material Specification
  • AMS4316B
  • Current
Published 2019-09-10 by SAE International in United States
This specification covers an aluminum alloy in the form of Alclad sheet and plate 0.040 to 1.000 inch, incl (1.02 to 25.40 mm, incl) in nominal thickness (see 8.4).
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Aluminum Alloy, Sheet and Plate, Alclad 4.4Cu - 1.5Mg - 0.60Mn (2024, -T3 Sheet/-T351 Plate with 1-1/2% Alclad) Solution Heat Treated, Cold Worked and Naturally Aged

AMS D Nonferrous Alloys Committee
  • Aerospace Material Specification
  • AMS4041T
  • Current
Published 2019-09-03 by SAE International in United States
This specification covers an aluminum alloy in the form of sheet and plate alclad two sides, over 0.187 to 1.000 inch (over 4.750 to 25.40 mm) in nominal thickness, supplied in the -T3/-T351 temper.
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