This specification covers a premium aircraft-quality corrosion-resistant steel in the form of bars, wire, forgings, mechanical tubing, flash welded rings up to 8.0 inches (203 mm) in diameter or least distance between parallel sides in the solution heat treated condition (see 8.4), and stock of any size for forging, flash welded rings, or heading (see 8.8).
Rationale:
AMS5622G results from a Five-Year Review and update of this specification with changes to Title, Composition to update applicable analysis standards (3.1), Melting Practice (3.2), Condition (3.3), Precipitation heat treatments (Table 3), added tensile test strain rates (3.5.2.2.1.1), added product outside of size range (3.5.2.3), prohibits unauthorized exceptions (3.8 and 4.4.6), Reports (4.4), and Identification (5.2.1.1).
Related Topics:
Materials properties
Heat treatment
Steel
Corrosion resistant alloys
Tensile strength
Cobalt alloys
Titanium alloys
Metal finishing
Wrought alloys
Metals
Also known as: SAE AMS 5622
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