Brazing, Nickel Alloy Filler Metal
- Aerospace Material Specification
- AMS2675G
- Reaffirmed
Scope
Rationale
Recommended Content
Aerospace Material Specification | Nickel Alloy, Brazing Filler Metal 73Ni - 0.75C - 4.5Si - 14Cr - 3.1B - 4.5Fe 1790 °F (977 °C) Solidus to 1970 °F (1077 °C) Liquidus |
Aerospace Material Specification | Titanium Alloy Direct Deposited Products 6Al - 4V Annealed |
Aerospace Standard | Couplings, Clamp, Grooved, V-Band |
Topic
Data Sets - Support Documents
Title | Description | Download |
---|---|---|
Unnamed Dataset 1 | ||
TABLE 1 | Nickel Plating Thickness Requirements for Furnace Atmosphere | |
TABLE 2 | Sampling for Acceptance Tests |
Issuing Committee
AMS B Finishes Processes and Fluids Committee
The committee of Finishes, Processes, and Fluids, AMS Committee B, shall prepare, coordinate, and revise documents related to processing technology, such as plating, brazing, coatings and compounds, through the participation of process 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 processes.
Reference
Number | Title |
---|---|
AMS2403 | NICKEL PLATING |
AMS2424 | NICKEL PLATING Low Stressed Deposit |
AMS2750 | PYROMETRY |
AMS4775 | Nickel Alloy, Brazing Filler Metal 73Ni 0.75C 4.5Si 14Cr 3.1B 4.5Fe, 1790 to 1970°F (977 to 1077°C) Solidus-Liquidus Range |
ANSIB46.1 | This document is not part of the subscrption. |
MIL-STD-2073-1 | This document is not part of the subscrption. |