Steel, Corrosion Resistant, Bars and Wire, 18Cr - 9.0Ni (SAE 30302), Solution Heat Treated and Cold Drawn, 125 ksi (862 MPa) Tensile Strength
- Aerospace Material Specification
This specification covers a corrosion-resistant steel in the form of bars and wire 0.75 inch (19 mm) and under in nominal diameter or distance between parallel sides.
These products have been used typically for small parts, such as bolts, screws, and clevis pins, requiring corrosion resistance up to 700 degrees F (371 degrees C) and which may be fabricated by heading or by machining from bars or wire and roll threading, but usage is not limited to such applications.
|Aerospace Material Specification||Steel, Corrosion-Resistant, Sheet, Strip, and Plate 19Cr – 9.2Ni (SAE 30304) Solution Heat Treated|
|Aerospace Material Specification||Steel, Corrosion-Resistant, Sheet, Strip, and Plate 18Cr - 9.0Ni (302) Solution Heat Treated|
|Aerospace Material Specification||Steel, Corrosion-Resistant, Bars, Wire, Forgings, Tubing, and Rings 16Cr - 4.0Ni - 0.30Cb - 4.0Cu Solution Heat Treated, Precipitation Hardenable Consumable Electrode Remelted|
Data Sets - Support Documents
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.