SAE AS3506B PDF

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Insert – Screw Thread, Thin Wall, Self-Locking, UNS N07718, Silver Plated, Class: 185 ksi/1025 °F, Procurement Specification

Category: AS Tags: Assembling, Heat resistant alloys, Heat resistant materials, Heat treatment, Identification numbers, Manufacturing processes, Materials identification, Nickel alloys, Production

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Description

This SAE Aerospace Standard (AS) establishes the requirements for AS3504 and AS3505 thin wall self-locking inserts made from a corrosion and heat resistant, age hardenable nickel base alloy of the type identified under the Unified Numbering System as UNS N07718.

History

AS3506B	2019-04-09	Latest	Reaffirmed
AS3506A	2004-03-24	Historical	Revised
AS3506	2001-10-01	Historical	Reaffirmed

ISSUING COMMITTEE	E-25 General Standards for Aerospace and Propulsion Systems
DATE	2019-04-09
DOI	https://doi.org/10.4271/AS3506B
ISCURRENT	Current
PAGE	14
PUBLISHER	SAE International
REVISED	REAFFIRMED