Aerospace series. Insert, thin wall. Salvage procedure for components

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

09-30-2008

Publisher

British Standards Institution

Foreword
1 Scope
2 Normative references
3 Conditions of use
4 Re-machining of an existing insert hole
5 Insert and tapped hole particulars
6 Installation of oversize inserts
7 Minimum criteria for the installation and removal
   tools and their methods of application
8 Assembly drive tool and swage tool
9 Assembly procedure
   9.1 Insertion
   9.2 Swaging
   9.3 Gauging and inspection
10 Oversize insert removal, replacement and tools

Provides the accepted methods for the reclamation of installation holes for standard thin wall inserts, within assemblies.

1.1 This specification covers the accepted methods for the reclamation of installation holes for standard thin wall inserts, within assemblies. 1.2 To enable rectification when defects or damage occur to the standard insert tapped installation hole, or to rectify any out of position of the hole within the specified parameters of use. 1.3 To control the machining of the existing insert hole and the installation requirements of the replacement oversize thin wall insert.

Committee	ACE/12
DocumentType	Standard
Pages	18
PublisherName	British Standards Institution
Status	Current

Standards	Relationship
EN 3916:2008	Identical

ISO 5855-2:1999	Aerospace MJ threads Part 2: Limit dimensions for bolts and nuts
EN 3913:2007	Aerospace series - Insert, thin wall, self-locking, short, in heat resisting nickel base alloy NI-PH2601 (Ni-P100HT, Inconel 718), silver plated on internal thread, for salvage of components
EN 3915 : 2008	Aerospace series - Insert, thin wall, self-locking, MJ threads, in heat resisting nickel base alloy NI-PH2601 (NI-P100HT, Inconel 718), for salvage of components - Classification: 1 275 MPa (at ambient temperature) / 550 °C - Technical specification
EN 3676:1998	Aerospace series - Inserts, thin wall, self-locking - Design standard
ISO 965-1:2013	ISO general purpose metric screw threads — Tolerances — Part 1: Principles and basic data
EN 3914:2008	Aerospace series - Insert, thin wall, self-locking, long, in heat resisting nickel base alloy NI-PH2601 (NI-P100HT, Inconel 718), silver plated on internal thread, for salvage of components

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BS EN 3916:2008

Aerospace series. Insert, thin wall. Salvage procedure for components

Table of Contents

Abstract

Scope

General Product Information

International Equivalents

Standards Referencing This Book

Category

Subcategory