Steel, Corrosion-Resistant, Bars, Wire, Tubing, and Forgings 15.5Cr – 1.5Si – 0.3Mo – 0.1N (0.45 – 0.60C) for Bearing Applications
- Aerospace Material Specification
- AMS5926
- Reaffirmed
Scope
Rationale
Recommended Content
Aerospace Material Specification | Steel, Bars, Forgings, and Tubing 2.7Si - 0.85Cr - 1.8Ni - 0.4Mo - 0.2V - (0.37 - 0.44C) Double Vacuum Melted |
Aerospace Material Specification | Steel, Corrosion-Resistant, Bars, Wire, and Forgings 17Cr 0.52Mo (0.95 1.20C) (SAE 51440C) for Bearing Applications |
Aerospace Material Specification | Steel, Corrosion and Heat Resistant, Welded Tubing 25Cr - 20Ni (310) Solution Heat Treated |
Topic
Data Sets - Support Documents
Title | Description | Download |
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Unnamed Dataset 1 | ||
Unnamed Dataset 2 | ||
TABLE 1 | COMPOSITION | |
TABLE 3 | MICRO-INCLUSION RATING LIMITS | |
TABLE 4A | MAXIMUM DECARBURIZATION, INCH/POUND UNITS | |
TABLE 4B | MAXIMUM DECARBURIZATION, SI UNITS |
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.