BOLTS AND SCREWS, NICKEL ALLOY, CORROSION AND HEAT RESISTANT Upset Headed, Heat Treated, Roll Threaded 1975 F (1079.4 C) Heat Treatment
- Aerospace Material Specification
|Aerospace Material Specification||Bolts and Screws, Nickel Alloy, Corrosion and Heat Resistant, Upset Headed, Heat Treated, Roll Threaded, 1950°F Solution Heat Treatment (AMS 5708)|
|Aerospace Material Specification||Bolts and Screws Steel, Corrosion and Moderate Heat Resistant, Heat Treated, Roll Threaded (Ams 5616)|
|Aerospace Material Specification||BOLTS AND SCREWS, CORROSION AND HEAT RESISTANT STEEL Upset Headed, Heat Treated, Roll Threaded 1800°F (982°C) Solution and Precipitation Heat Treated|
Data Sets - Support Documents
|TABLE I||AMERICAN NATIONAL & UNIFIED THREADS|
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.