Heat Treatment Austenitic Corrosion-Resistant Steel Parts
- Aerospace Material Specification
- AMS2759/4D
- Revised
Scope
Rationale
Recommended Content
Aerospace Material Specification | Heat Treatment Martensitic Corrosion-Resistant Steel Parts |
Aerospace Material Specification | Heat Treatment of Carbon and Low-Alloy Steel Parts Minimum Tensile Strength Below 220 ksi (1517 MPa) |
Aerospace Material Specification | Heat Treatment of Low-Alloy Steel Parts Minimum Tensile Strength 220 ksi (1517 MPa) and Higher |
Topic
Data Sets - Support Documents
Title | Description | Download |
---|---|---|
Unnamed Dataset 1 | ||
Unnamed Dataset 2 | ||
Table 1 | Annealing treatments for austenitic corrosion resistant steel parts | |
Table 2 | Soaking time for austenitic corrosion resistant steel parts |
Issuing Committee
AMS F Corrosion and Heat Resistant Alloys Committee
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.