SAE AMS5622F - Online Standart

SAE AMS5622F

Steel, Corrosion-Resistant, Bars, Wire, Forgings, Tubing, and Rings 16Cr - 4.0Ni - 0.30Cb - 4.0Cu Solution Heat Treated, Precipitation Hardenable Consumable Electrode Remelted

Historical
Standard by SAE International, 2013-08-12

SKU: 32b4770e6185 Category:

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About This Item

This specification covers a premium aircraft-quality corrosion-resistant steel in the form of bars, wire, forgings, mechanical tubing, flash welded rings in the solution heat treated condition (See 8.4), and stock for forging, flash welded rings, or heading. AMS5622F identifies a new procedure for ordering in the precipitation heat treated condition (1.1.1), includes a restriction on bar being cut from plate (3.3.1.4), revises macrostructure requirements (3.5.1.1), clarifies thickness of bars (3.5.2.2), revises Heat Treatment (3.4) clarifies tensile orientation for transverse tests (3.5.2.2.1.3), and revises Reports (4.4).

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Standard Details

  • Publication Date: 2013-08-12

  • Standard Status: historical

  • Publisher: SAE International

  • Document Type: Aerospace Material Specification

  • Subject: Heat treatment, Tensile strength, Cobalt alloys, Titanium alloys, Welding, Identification, Steel, Heat resistant materials, Corrosion

  • Official SAE: Doi link

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