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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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Heat Treatment of Parts in a Vacuum

AMS F Corrosion Heat Resistant Alloys Committee
  • Aerospace Material Specification
  • AMS2769C
  • Current
Published 2019-07-12 by SAE International in United States
This specification establishes the requirements and procedures for heat treating parts in vacuum/partial pressure and shall be used as a supplementary document to primary heat treating specifications as applicable.
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Nonferrous Metals Bundle

  • Professional Development
  • PD281944
Published 2019-05-14

Nonferrous materials are malleable, are non-magnetic, and have no iron content which gives them higher resistance to rust and corrosion. The following five on-demand courses are included in the Nonferrous  Metals bundle.  Each course is approximately one-hour in duration. See Topics/Outline for additional details.

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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.
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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.
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Tube, Aluminum Alloy, Drawn, Seamless, 7075

AMS D Nonferrous Alloys Committee
  • Aerospace Material Specification
  • AMSWWT700/7B
  • Current
Published 2018-12-27 by SAE International in United States
This specification covers the specific requirements for seamless tube drawn from aluminum alloy 7075.
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Aluminum Alloy, 2017, Bar, Rod, and Wire, Rolled, Drawn, or Cold Finished

AMS D Nonferrous Alloys Committee
  • Aerospace Material Specification
  • AMSQQA225/5A
  • Current
Published 2018-11-06 by SAE International in United States
This specification covers the specific requirements for 2017 aluminum alloy bar, rod and wire produced by rolling, drawing or cold finishing.
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Nickel Alloy, Brazing Filler Metal 82Ni - 4.5Si - 7.0Cr - 3.1B - 3.0Fe 1780 °F (971 °C) Solidus to 1830 °F (999 °C) Liquidus Range

AMS F Corrosion Heat Resistant Alloys Committee
  • Aerospace Material Specification
  • AMS4777J
  • Current
Published 2018-08-28 by SAE International in United States
This specification covers a nickel alloy in the form of wire, rod, strip, foil, and powder and a viscous mixture (paste) of the powder in a suitable binder.
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Technical Report on Low Cycle Fatigue Properties Ferrous and Non-Ferrous Materials

Materials, Processes and Parts Council
  • Ground Vehicle Standard
  • J1099_201808
  • Current
Published 2018-08-24 by SAE International in United States
Information that provides design guidance in avoiding fatigue failures is outlined in this SAE Information Report. Of necessity, this report is brief, but it does provide a basis for approaching complex fatigue problems. Information presented here can be used in preliminary design estimates of fatigue life, the selection of materials and the analysis of service load and/or strain data. The data presented are for the “low cycle” or strain-controlled methods for predicting fatigue behavior. Note that these methods may not be appropriate for materials with internal defects, such as cast irons, which exhibit different tension and compression stress-strain behavior.
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