This specification covers an aircraft-quality, low-alloy steel in the form of bars and forgings 1.50 inches or less in diameter or least distance between parallel sides (thickness).
Rationale:
AMS6327M is the result of a Five-Year Review and update of the specification. The revision updates compostiion testing and reporting (see 3.1 and 3.1.2), addresses grain size requirements based on composition (see 3.1.1, 3.4.1, 4.2.1, 4.2.2, 4.4.1, and 8.4), addresses exceptions based on size (see 1.1, Table 2, 3.4.4.2, 3.7, 4.3.4, 5.2.1, and 8.7), updates the heat-treatment specification (see 3.2.2), addresses macrostructure requirements (see 3.4.2.1 and 8.8), updates decarburization test methods (see 3.4.3.3.1 and 3.4.3.3.2), updates based on changes in AMS2301 (see 4.2.1 and 4.4.4), adds note based on finish (see 8.5), and allows prior revision (see 8.6).
Related Topics:
Tensile strength
Heat treatment
Steel
Forging
Also known as: SAE AMS 6327
SAE MOBILUS
Subscribers can view annotate, and download all of SAE's content.
Learn More »