Heat Treatment of Low-Alloy Steel Parts Minimum Tensile Strength 220 ksi (1517 MPa) and Higher
- Aerospace Material Specification
- AMS2759/2K
- Revised
Scope
Rationale
Data Sets - Support Documents
Title | Description | Download |
---|---|---|
Unnamed Dataset 1 | ||
Table 1 | Atmospheres | |
Table 2A | Annealing, normalizing, and austenitizing temperatures and quenchants (inch/pound units) | |
Table 2B | Annealing, normalizing, and austenitizing temperatures and quenchants (SI units) | |
Table 3A | Tempering set temperatures (inch/pound units) | |
Table 3B | Tempering set temperatures (SI units) | |
Table 4 | Soak time for annealing, normalizing, and austenitizing | |
Table 5A | Maximum hardening size limits for steel parts (inches) | |
Table 5B | Maximum hardening size limits for steel parts (centimeters) |
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
Number | Title |
---|---|
AMS2418E | PLATING, COPPER |
AMS2424 | NICKEL PLATING Low Stressed Deposit |
AMS2759 | HEAT TREATMENT OF STEEL PARTS General Requirements |
ARP1820 | CHORD METHOD OF EVALUATING SURFACE MICROSTRUCTURAL CHARACTERISTICS |
ASTME384 | This document is not part of the subscrption. |