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new

Aluminum Alloy, Clad One Side, Sheet, 1.25Mn - 0.12Cu (No. 11-0 Brazing Sheet), Annealed

AMS D Nonferrous Alloys Committee
  • Aerospace Material Specification
  • AMS4063F
  • Current
Published 2019-07-18 by SAE International in United States

This specification covers an aluminum alloy in the form of clad sheet from 0.006 to 0.249 inches (0.15 to 6.32 mm), inclusive, in thickness (see 8.6).

 
new

Aluminum Alloy, Rolled or Cold Finished, Bars and Rods, 12.2Si - 1.0Mg - 0.90Cu - 0.90Ni (4032-T651), Solution Heat Treated, Stress Relieved, Artificially Aged

AMS D Nonferrous Alloys Committee
  • Aerospace Material Specification
  • AMS4319C
  • Current
Published 2019-07-12 by SAE International in United States

This specification covers an aluminum alloy in the form of bars and rods 0.750 to 3.500 inches (19.05 to 88.90 mm), inclusive, in nominal diameter or least distance between parallel sides (see 8.5).

 
new

Castings, Aluminum Alloy Sand, 5.0Si - 1.2Cu - 0.50Mg (355.0-T71), Solution Heat Treated and Overaged

AMS D Nonferrous Alloys Committee
  • Aerospace Material Specification
  • AMS4214K
  • Current
Published 2019-07-12 by SAE International in United States

This specification covers an aluminum alloy in the form of sand castings.

 
new

Aluminum Alloy, Extruded Profiles (2043-T85), 2.8Cu - 1.65Li - 0.35Mg - 0.1Zr, Solution Heat Treated, Stress Relieved by Stretching, and Aged

AMS D Nonferrous Alloys Committee
  • Aerospace Material Specification
  • AMS4450
  • Current
Published 2019-07-03 by SAE International in United States

This specification covers an aluminum alloy in the form of extruded rods, bars, and profiles (shapes) produced with thickness between 0.040 and 2.500 inches (1.02 to 38.10 mm) in thickness, and having a maximum cross sectional area of 23 in2 (15000 mm2) and a maximum circumscribing circle diameter (circle size) of 16 inches (406 mm) (see 8.4.1).

 
new

Aluminum Alloy, Extruded Bar, Rod, and Shapes, 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr, 7075-T76(51X) Solution Heat Treated and Overaged

AMS D Nonferrous Alloys Committee
  • Aerospace Material Specification
  • AMS4317B
  • Current
Published 2019-07-02 by SAE International in United States

This specification covers an aluminum alloy in the form of extruded bars, rods, and shapes up to 4.000 inches, incl (101.60 mm, incl) in nominal diameter or least thickness, and having a nominal cross-sectional area up to 20 in2 (129 cm2) (see 8.5).

 
new

Copper Alloy, Brazing Filler Metal, 52.5Cu - 38Mn - 9.5Ni, 1615 to 1700 °F (879 to 927 °C) Solidus-Liquidus Range

AMS D Nonferrous Alloys Committee
  • Aerospace Material Specification
  • AMS4764G
  • Current
Published 2019-06-17 by SAE International in United States

This specification covers a copper alloy in the form of wire, rod, sheet, strip, foil, and powder and a viscous mixture (paste) of powder in a suitable binder.

 
new

Aluminum Alloy Extrusions, 4.4Cu - 1.5Mg - 0.60Mn (2024-T3), Solution Heat Treated and Cold Worked

AMS D Nonferrous Alloys Committee
  • Aerospace Material Specification
  • AMS4152N
  • Current
Published 2019-06-17 by SAE International in United States

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

 

Aluminum Alloy, Plate, 3.5Cu - 1.0Li - 0.40Mg - 0.35Mn - 0.45Ag - 0.12Zr (2050-T34), Solution Heat Treated and Stress Relieved

AMS D Nonferrous Alloys Committee
  • Aerospace Material Specification
  • AMS4372A
  • Current
Published 2019-05-23 by SAE International in United States

This specification covers an aluminum-lithium alloy in the form of plate 0.500 to 6.500 inches (12.70 to 165.00 mm) in nominal thickness (see 8.5).

 

Copper-Beryllium Alloy, Bars and Rods, 98Cu - 1.9Be, Solution Heat Treated, Cold Worked, and Precipitation Heat Treated (TH04, formerly HT)

AMS D Nonferrous Alloys Committee
  • Aerospace Material Specification
  • AMS4534D
  • Current
Published 2019-05-14 by SAE International in United States

This specification covers a copper beryllium alloy in the form of bars and rods up to 3.000 inches (76.20 mm), inclusive, in nominal diameter or least distance between parallel sides (see 8.7).

 

Aluminum Alloy, Extrusions and Rings, 1.0Mg - 0.60Si - 0.28Cu - 0.20Cr - (6061-T6), Solution and Precipitation Heat Treated

AMS D Nonferrous Alloys Committee
  • Aerospace Material Specification
  • AMS4150N
  • Current
Published 2019-05-14 by SAE International in United States

This specification covers an aluminum alloy in the form of extruded bars, rods, wire, profiles, and tubing, flash welded rings fabricated from extruded stock, and stock for flash welded rings.