AS7468: BOLTS AND SCREWS, COBALT-CHROMIUM-NICKEL ALLOY, CORROSION RESISTANT Forged Head, Roll Threaded After Aging, Fatigue Rated - 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 resistant, work-strengthened, cobalt-chromium-nickel alloy of the type identified under the Unified Numbering System as UNS R30035, and of 260 000 psi tensile strength at room temperature.

Meta Tags

Topics: Aircraft propulsion systems
Corrosion resistant alloys
Heat resistant materials

Details

DOI: https://doi.org/10.4271/AS7468

Pages: 25

Citation: SAE International Technical Standard, BOLTS AND SCREWS, COBALT-CHROMIUM-NICKEL ALLOY, CORROSION RESISTANT Forged Head, Roll Threaded After Aging, Fatigue Rated, SAE Standard AS7468, Issued January 1991, https://doi.org/10.4271/AS7468.

Additional Details

Publisher: SAE International

Published: Jan 17, 1991

Product Code: AS7468

Content Type: Technical Standard

Status: Issued

Language: English

Historical