Your Selections

AMS D Nonferrous Alloys Committee
Show Only

Collections

File Formats

Content Types

Dates

Sectors

Topics

Publishers

Committees

 
new

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).

 
new

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).

 
new

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.

 
new

Magnesium Alloy, Direct Chill Strand Cast, 2.8Nd - 1.4Gd - 0.4Zn - 0.6Zr (EV31A - T6), Solution and Precipitation Heat Treated

AMS D Nonferrous Alloys Committee
  • Aerospace Material Specification
  • AMS4431
  • Current
Published 2019-05-14 by SAE International in United States

This specification covers a magnesium alloy in the form of direct chill strand cast round material up to 9.0 inch diameter and rectangular material up to 10 inch by 27.5 inch cross-section (see 8.4) for the purpose of machine from solid applications (see 8.2.1).

 
new

Aluminum Alloy, Plate, 3.5Cu - 1.0Li - 0.40Mg - 0.35Mn - 0.45Ag - 0.12Zr (2050-T84), Solution Heat Treated, Stress Relieved, and Artificially Aged

AMS D Nonferrous Alloys Committee
  • Aerospace Material Specification
  • AMS4413B
  • Current
Published 2019-05-10 by SAE International in United States

This specification covers an aluminum-lithium alloy in the form of plate 0.500 to 6.500 inch (12.70 to 165.10 mm) inclusive, in thickness (see 8.5).

 
new

Aluminum Alloy Plate (7081-T7451), 7.2Zn - 1.5Cu - 2.0Mg - 0.10Zr, Solution Heat Treated, Stress Relieved and Overaged

AMS D Nonferrous Alloys Committee
  • Aerospace Material Specification
  • AMS4410A
  • Current
Published 2019-05-07 by SAE International in United States

This specification covers an aluminum alloy in the form of plate.

 
new

Aluminum Alloy Plate (7081-T7651), 7.2Zn - 1.5Cu - 2.0Mg - 0.10Zr, Solution Heat Treated, Stress Relieved and Overaged

AMS D Nonferrous Alloys Committee
  • Aerospace Material Specification
  • AMS4411A
  • Current
Published 2019-05-07 by SAE International in United States

This specification covers an aluminum alloy in the form of plate.

 

Copper-Nickel-Tin Alloy, Bars and Rods 77Cu - 15Ni - 8Sn Solution Annealed, Cold Finished and Spinodal Hardened (TX TS)

AMS D Nonferrous Alloys Committee
  • Aerospace Material Specification
  • AMS4597A
  • Current
Published 2019-04-30 by SAE International in United States
This specification covers a copper-nickel-tin alloy in the form of bars and rods.
Datasets icon
Annotation icon
 

Heat Treatment of Wrought Copper Beryllium Alloy Parts

AMS D Nonferrous Alloys Committee
  • Aerospace Material Specification
  • AMS2728C
  • Current
Published 2019-04-30 by SAE International in United States
This specification establishes the requirements for heat treatment of wrought copper beryllium parts (See 1.2.2 and 8.2.1) by users or by their vendors or subcontractors.
Datasets icon
Annotation icon
 

Minimizing Stress-Corrosion Cracking in Wrought High-Strength Aluminum Alloy Products

AMS D Nonferrous Alloys Committee
  • Aerospace Standard
  • ARP823F
  • Current
Published 2019-04-17 by SAE International in United States
The purpose of this recommended practice is to provide the aerospace industry with recommendations concerning minimizing stress-corrosion cracking (SCC) in wrought high-strength aluminum alloy products.
Datasets icon
Annotation icon