Nickel Alloy, Corrosion and Heat-Resistant, Wire 72Ni - 15.5Cr - 0.95Cb - 2.5Ti - 0.70Al - 7.0Fe No. 1 Temper, Precipitation Hardenable
- Aerospace Material Specification
- AMS5698G
- Reaffirmed
Scope
Rationale
Recommended Content
Topic
Data Sets - Support Documents
Title | Description | Download |
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Unnamed Dataset 1 | ||
Unnamed Dataset 2 | ||
TABLE 1 | Composition | |
TABLE 2A | Tensile Strength, Inch/Pound Units | |
TABLE 2B | Tensile Strength, SI Units | |
TABLE 3 | Wrapping Parameters | |
TABLE 4A | Minimum Tensile Strength, Inch/Pound Units | |
TABLE 4B | Minimum Tensile Strength, SI Units | |
TABLE 5A | Round and Square Wire Tolerance, Inch/Pound Units | |
TABLE 5B | Round and Square Wire Tolerance, SI Units | |
TABLE 6A | Flat Wire Tolerances, Inch/Pound Units | |
TABLE 6B | Flat Wire Tolerances, 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.