Heat Treatment of Carbon and Low-Alloy Steel Parts Minimum Tensile Strength Below 220 ksi (1517 MPa)
- Aerospace Material Specification
- AMS2759/1G
- Revised
Scope
Rationale
Data Sets - Support Documents
Title | Description | Download |
---|---|---|
Unnamed Dataset 1 | ||
Table 1 | Atmospheres | |
Table 2A | Annealing, normalizing, and austenitizing set temperatures and quenchants (inch/pound units) | |
Table 2B | Annealing, normalizing, and austenitizing set temperatures and quenchants (SI units) | |
Table 3A | Suggested tempering temperatures (°F) | |
Table 3B | Suggested tempering temperatures (°C) | |
Table 4A | Suggested approximate tempering temperatures based on as-quenched hardness (°F) | |
Table 4B | Suggested approximate tempering temperatures based on as-quenched hardness (°C) | |
Table 5 | Soak time for annealing, normalizing, and austenitizing | |
Table 6A | Maximum hardening size limits for steel parts (inches) | |
Table 6B | Maximum hardening size limits for steel parts (cm) |
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. |