(U.S. Patent No. 5,087,415)

(UNS K92580)

Nominal analysis
0.23 C, 3.10 Cr, 11.10 Ni, 1.20 Mo, 13.40 Co, Bal. Fe

An alloy providing high hardness and strength combined with exceptional ductility and toughness. This alloy should be considered for aircraft and aerospace structural components requiring high strength, high fracture toughness and exceptional stress corrosion cracking resistance. AerMet 100 may be considered for use up to about 800°F (427°C). This alloy is not subject to the same restrictions as AF1410, thus may be considered a substitute.

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