AS7475: BOLTS AND SCREWS, WORK-STRENGTHENED ALLOY, CORROSION AND HEAT RESISTANT Forged Head, Roll Threaded After Aging - Technical Standard

Features

Issuing Committee: E-25 General Standards for Aerospace and Propulsion Systems

Scope

Content: This procurement specification covers aircraft quality bolts and screws made from a corrosion and heat resistant, work-strengthened, cobalt-chromium-nickel alloy of the type identified under the Unified Numbering System as UNS R30159, and of 260 000 psi tensile strength at room temperature, with maximum test temperature of parts at 1200°F.

Meta Tags

Topics: Corrosion resistant alloys
Heat resistant materials

Details

DOI: https://doi.org/10.4271/AS7475

Pages: 26

Citation: SAE International Technical Standard, BOLTS AND SCREWS, WORK-STRENGTHENED ALLOY, CORROSION AND HEAT RESISTANT Forged Head, Roll Threaded After Aging, SAE Standard AS7475, Issued January 1991, https://doi.org/10.4271/AS7475.

Additional Details

Publisher: SAE International

Published: Jan 17, 1991

Product Code: AS7475

Content Type: Technical Standard

Status: Issued

Language: English

Historical