This specification covers a corrosion- and heat-resistant nickel alloy in the form of sheet, strip, and plate 0.010 to 2.000 inches (0.25 to 50.80 mm), inclusive, in nominal thickness.
Rationale
AMS5870G is the result of a Five-Year Review and update of the specification. The revision updates the Title with the common name, updates composition testing and reporting (see 3.1 and 3.1.1), revises finish requirements (see 3.2.1), updates strain rate (see 3.3.1.1), clarifies bend testing (see 3.3.2) and prohibits unauthorized exceptions (see 3.3.1.2, 4.4.1, and 8.4).
The committee of Corrosion and Heat Resistant Steels and Alloys and Specialty Steels and Alloys, AMS Committee F, will prepare, coordinate, and revise documents related to corrosion and heat resistant steels and alloys and specialty steels and alloys technology, such as stainless steels and nickel and base alloys, through the participation of metals suppliers, users, and interested government agencies. Committee activities shall provide a forum for the cooperative interchange of ideas and experience of the participants, resulting in the publication of specifications that embody sound, established aerospace industry practices and requirements to serve the suppliers and customers of aerospace materials.
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