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Aluminum Alloy, Plate 1.6Cu - 2.2Mg - 0.22Cr - 5.7Zn (7475-T7651) Solution Heat Treated, Stress Relieved by Stretching, and Precipitation Heat Treated

  • Aerospace Material Specification
  • AMS4089F
  • Current
Published 2020-06-18 by SAE International in United States
This content contains downloadable datasets
Annotation ability available
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Aluminum Alloy, Extruded Wide Panel Profiles (7150-T77511) 6.4Zn - 2.4Mg - 2.2Cu - 0.12Zr Solution Heat Treated, Stress-Relieved, Straightened and Overaged

  • Aerospace Material Specification
  • AMS4325A
  • Current
Published 2020-05-05 by SAE International in United States
This content contains downloadable datasets
Annotation ability available
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Clamp Assembly, Saddle Type, Cushioned, General Specification For

  • Aerospace Standard
  • AS85449B
  • Current
Published 2020-04-21 by SAE International in United States
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Bolts, Cobalt-Chromium-Nickel Alloy UNS R30035, Tensile Strength 260 ksi, Procurement Specification

  • Aerospace Standard
  • AS7468C
  • Current
Published 2020-04-11 by SAE International in United States
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Aluminum Alloy, Extrusion 2.7Cu - 1.8Li - 0.7Zn - 0.3Mn - 0.3Mg - 0.08Zr (2099-T83) Solution Heat Treated, Stress Relieved by Stretching 1 to 4% and Aged

  • Aerospace Material Specification
  • AMS4287B
  • Current
Published 2020-04-10 by SAE International in United States
This content contains downloadable datasets
Annotation ability available
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Inspection, Ultrasonic, Wrought Metals, Process for

  • Aerospace Material Specification
  • AMSSTD2154D
  • Current
Published 2020-04-03 by SAE International in United States
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Annotation ability available
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Titanium Bars, Wire, Forgings, and Rings Commercially Pure 70 ksi (483 MPa) Yield Strength

  • Aerospace Material Specification
  • AMS4921P
  • Current
Published 2020-04-02 by SAE International in United States
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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

  • Aerospace Material Specification
  • AMS4144G
  • Current
Published 2020-02-18 by SAE International in United States
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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

  • Aerospace Material Specification
  • AMS4324B
  • Current
Published 2020-02-10 by SAE International in United States
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Minimization of High Temperature Oxidation, Aluminum Alloy Heat Treatment

  • Aerospace Standard
  • ARP7500
  • Current
Published 2020-02-05 by SAE International in United States
Annotation ability available