This SAE Aerospace Standard (AS) establishes the geometric control requirements for bolts, screws, and studs where worded notes and symbolized notes are used for straightness, concentricity, squareness, and runout.
This specification covers a corrosion- and heat-resistant steel in the form of bars, wire, forgings, mechanical tubing up to 5.00 inches (127 mm), inclusive, in nominal diameter or least distance between parallel sides (thickness), and stock for forging or heading.
This SAE Aerospace Standard (AS) establishes the requirements for heat cured solid film lubricants. For other general or high temperature applications, refer to AS1701. This document requires qualified products.
This document aims to define the procurement requirements for helical coil threaded inserts manufactured from corrosion-resistant steel formed wire, with the chemical composition aligning with UNS S21800. It will enable insert manufacturers to adhere to specific standards to meet the criteria outlined in this procurement specification.