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Aluminum Alloy, Hand Forgings and Rolled Rings 6.3Cu - 0.30Mn - 0.18Zr - 0.10V - 0.06Ti (2219-T852/T851) Solution Heat Treated, Mechanically Stress Relieved, and Precipitation Heat Treated

AMS D Nonferrous Alloys Committee
  • Aerospace Material Specification
  • AMS4144G
  • Current
Published 2020-02-18 by SAE International in United States
This specification covers an aluminum alloy in the form of hand forgings 17 inches (432 mm) and under in nominal thickness, and rolled rings up to 6 inches, incl (152 mm, incl) in nominal thickness at the time of heat treatment (see 8.5).
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Aluminum Alloy, Castings 5.0Si - 1.2Cu - 0.50Mg (C355.0-T6) Solution and Precipitation Heat Treated

AMS D Nonferrous Alloys Committee
  • Aerospace Material Specification
  • AMS4215J
  • Current
Published 2020-02-17 by SAE International in United States
This specification covers an aluminum alloy in the form of sand, permanent mold, composite mold, and investment castings.
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Aluminum Alloy, Extruded Rod, Bar and Profiles (7055-T74511) 8.0Zn - 2.3Cu - 2.0Mg - 0.16Zr Solution Heat Treated, Stress-Relieved, and Overaged

AMS D Nonferrous Alloys Committee
  • Aerospace Material Specification
  • AMS4324B
  • Current
Published 2020-02-10 by SAE International in United States
This specification covers an aluminum alloy in the form of extruded bars, rods, and profiles (shapes) produced with a cross sectional area of 24 square inches (155 square centimeters) maximum and a circumscribing circle (see 8.3) diameter (circle size) of 10.5 inches (267 mm) maximum, with a nominal thickness up to 3.000 inch (76.20 mm), inclusive (see 8.6).
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Minimization of High Temperature Oxidation, Aluminum Alloy Heat Treatment

AMS D Nonferrous Alloys Committee
  • Aerospace Standard
  • ARP7500
  • Current
Published 2020-02-05 by SAE International in United States
This recommended practice provides recommendations for minimizing high temperature oxidation (HTO) during the heat treatment of aluminum alloy products and parts. HTO leads to deterioration of properties.
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Aluminum Alloy, Plate (7065-T7451) 7.7Zn - 2.1Cu - 1.65Mg - 0.10Zr Solution Heat Treated, Stress-Relieved, and Overaged

AMS D Nonferrous Alloys Committee
  • Aerospace Material Specification
  • AMS4361A
  • Current
Published 2020-01-30 by SAE International in United States
This specification covers an aluminum alloy in the form of plate.
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Aluminum Alloy, Plate (7065-T7651) 7.7Zn - 2.1Cu - 1.65Mg - 0.10Zr Solution Heat Treated, Stress-Relieved, and Overaged

AMS D Nonferrous Alloys Committee
  • Aerospace Material Specification
  • AMS4351A
  • Current
Published 2020-01-30 by SAE International in United States
This specification covers an aluminum alloy in the form of plate.
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Aluminum Alloy, Alclad Sheet 6.2Zn - 2.3Cu - 2.2Mg - 0.12Zr (Alclad 7050-T76) Solution Heat Treated and Overaged

AMS D Nonferrous Alloys Committee
  • Aerospace Material Specification
  • AMS4243C
  • Current
Published 2020-01-13 by SAE International in United States
This specification covers an aluminum alloy in the form of alclad sheet 0.040 to 0.187 inch (1.02 to 4.75 mm) inclusive in nominal thickness (see 8.6).
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Aluminum Alloy, Plate 6.2Zn - 1.8Cu - 2.4Mg - 0.13Zr (7010-T7651) Solution Heat Treated, Stress Relieved, and Precipitation Heat Treated

AMS D Nonferrous Alloys Committee
  • Aerospace Material Specification
  • AMS4204D
  • Current
Published 2019-12-27 by SAE International in United States
This specification covers an aluminum alloy in the form of plate 0.250 to 5.500 inch (6.35 to 139.70 mm), inclusive in nominal thickness (see 8.5).
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Aluminum Alloy, Plate (7160-T7451) 7.0Zn – 2.2Cu – 1.5Mg - 0.10Zr Solution Heat Treated, Stress Relieved, and Overaged

AMS D Nonferrous Alloys Committee
  • Aerospace Material Specification
  • AMS4432
  • Current
Published 2019-12-19 by SAE International in United States
This specification covers an aluminum alloy in the form of plate 1.000 to 6.000 inch (25.40 to 152.40 mm), inclusive, in nominal thickness (see 8.4).
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Aluminum Alloy, Alclad Sheet 4.4Cu - 1.5Mg - 0.60Mn (Alclad 2024-O) Annealed, Fine Grain

AMS D Nonferrous Alloys Committee
  • Aerospace Material Specification
  • AMS4274B
  • Current
Published 2019-12-17 by SAE International in United States
This specification covers an aluminum alloy in the form of sheet 0.009 to 0.126 inch (0.23 to 3.20 mm) inclusive, in nominal thickness, alclad.
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