STEEL PLATE 2.0Cr - 10Ni - 8.0Co - 1.0Mo (0.10 - 0.14C) Premium Quality, Vacuum Melted, Solution Heat Treated
- Aerospace Material Specification
- AMS6544
- Issued
Scope
Topic
Data Sets - Support Documents
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TABLE I | ||
TABLE I | (SI) | |
TABLE II | ||
TABLE II | (SI) | |
TABLE III | Thickness Tolerances for Plate Up to 2.00 In., Incl. in Thickness | |
TABLE III (SI) | Thickness Tolerances for Plate Up to 50 mm, Incl, in Nominal Thickness | |
TABLE IV | Thickness Tolerances for Plate Over 2.00 In. in Nominal Thickness | |
TABLE IV (SI) | Thickness Tolerances for Plate Over 50 mm in Nominal Thickness | |
TABLE V | Width and Length Tolerances for Gas-Cut Rectangular Plates Over 2.0 In. in Nominal Thickness | |
TABLE V (SI) | Width and Length Tolerances for Gas-Cut Rectangular Plates Over 50 mm in Nominal Thickness | |
TABLE VI | Camber Tolerances | |
TABLE VI (SI) | Camber Tolerances | |
TABLE VII | Flatness Tolerances | |
TABLE VII (SI) | Flatness Tolerances |
Issuing Committee
AMS E Carbon and Low Alloy Steels Committee
The committee of Carbon and Low Alloy Steels, AMS Committee E, shall prepare, coordinate, and revise documents related to carbon and low alloy steels technology, such as steel cleanliness and steel quality assurance sampling, 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.
Reference
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