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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.

 
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Copper-Beryllium Alloy, Bars, Rods, Shapes, and Forgings, 98Cu - 1.9Be, Solution Heat Treated TB00 (A)

AMS D Nonferrous Alloys Committee
  • Aerospace Material Specification
  • AMS4650N
  • Current
Published 2019-04-11 by SAE International in United States

This specification covers a copper-beryllium alloy in the form of bars, rods, shapes, and forgings.

 
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Filler Metal, Aluminum Brazing, 12Si

AMS D Nonferrous Alloys Committee
  • Aerospace Material Specification
  • AMS4185F
  • Current
Published 2019-04-11 by SAE International in United States

This specification covers an aluminum alloy in the form of wire, sheet, foil, pig, grains, shot, and chips.

 
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Copper-Beryllium Alloy, Bars and Rods, 98Cu - 1.9Be, Solution and Precipitation Heat Treated (TF00, formerly AT)

AMS D Nonferrous Alloys Committee
  • Aerospace Material Specification
  • AMS4533E
  • Current
Published 2019-04-11 by SAE International in United States

This specification covers a copper beryllium alloy in the form of bars and rods.

 
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Heat Treatment of Wrought Aluminum Alloy Parts

AMS D Nonferrous Alloys Committee
  • Aerospace Material Specification
  • AMS2770P
  • Current
Published 2019-04-08 by SAE International in United States

This specification specifies the engineering requirements for heat treatment, by part fabricators (users) or their vendors or subcontractors, of parts (see 8.6.1). It also covers heat treatment by warehouses or distributors converting raw material from one temper to another temper (see 1.3 and 8.5). It covers the following aluminum alloys:

 
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Aluminum Alloy, Extrusions, 1.0Mg - 0.60Si - 0.28Cu - 0.20Cr (6061-T4511 or T4510), Solution Heat Treated and Stress Relieved by Stretching

AMS D Nonferrous Alloys Committee
  • Aerospace Material Specification
  • AMS4172G
  • Current
Published 2019-03-26 by SAE International in United States

This specification covers an aluminum alloy in the form of extruded bars, rods, wire, profiles, and tubing.

 
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Aluminum Alloy, Extrusions, 4.4Cu – 1.5Mg – 0.60Mn (2024-T81) Solution Heat Treated, Cold Worked, and Precipitation Heat Treated

AMS D Nonferrous Alloys Committee
  • Aerospace Material Specification
  • AMS4491
  • Current
Published 2019-03-08 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.

 

Aluminum Alloy, Extrusions, 4.4Cu - 1.5Mg - 0.60Mn (2024-T8510), Solution Heat Treated, Cold Worked, Stress-Relieved by Stretching, and Precipitation Heat Treated, Unstraightened

AMS D Nonferrous Alloys Committee
  • Aerospace Material Specification
  • AMS4481
  • Current
Published 2019-03-01 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.

 

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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