Ams: 2759/2

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Modified with vanadium for improved toughness in airframe structural fittings. ams 2759/2

Achieving uniform 220+ ksi tensile strength requires highly disciplined, multi-stage furnace operations designed to manage phase changes and prevent internal structural defects. | If you need

Parts shall be heated to the austenitizing temperature appropriate for the specific steel grade. Holding times shall be sufficient to ensure through-heating of the heaviest cross-section. Achieving uniform 220+ ksi tensile strength requires highly

is the definitive aerospace material specification governing the thermal processing of low-alloy steel components engineered to achieve an ultimate tensile strength of 220 ksi (1517 MPa) and higher . Maintained by SAE International , this sub-tier specification must always be executed in tandem with the overarching parent standard, AMS 2759 , which outlines foundational requirements for steel heat treatment.

Heat Treatment of Low-Alloy Steels: Understanding AMS 2759/2 Requirements for High-Strength Parts Source: Typically found in Heat Treating Progress (ASM International) or SAE Technical Papers.

It provides specific parameters for thermal processing, including: Hardening and tempering temperatures. Quenching media and procedures.