SAE Standards Works
E-25 General Standards for Aerospace and Propulsion Systems
AS7479C - Bolts and Screws, Steel, UNS S66286, 1650 °F Solution Heat Treated, Precipitation Heat Treated Before Roll Threaded
New Project Request
Not available for purchase at this time.
Bolts and Screws, Steel, UNS S66286, 1650 °F Solution Heat Treated, Precipitation Heat Treated Before Roll Threaded
This specification covers bolts and screws made from a corrosion and heat resistant, parcipitation hardenable iron base alloy of the type identified under the Unified Numbering System as UNS S66286, and of 130 000 psi tensile strength at room temperature, with maximum test temperature of parts at 1200 °F.<p>Primarily for aerospace propulsion system applications where a good combination of strength and resistance to relaxation at elevated temperatures is required.
Figure 5 and Figure 8 corrected, correct table number added and also note A added in Figure 8. Table 2A .3125-24 size UTS Reduced pitch Diameter load corrected.
. All rights reserved.
Intellectual Property Policy
Terms & Conditions