Aerospace series. Inserts, thickwall, self-locking. Installation and removal procedure

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

16-12-2004

Publisher

British Standards Institution

Foreword
1 Scope
2 Normative references
3 Insert information
4 Broaching
5 Hole serration profile
6 Inspection requirements before installation
7 Installation tools
8 Checks of insert position and crimping
9 Inspection of minimum self-locking torque
10 Insert removal
11 Repair

Gives the conditions of installation and removal procedure (hole serration profile, tools, swaging) of self-locking thickwall inserts defined by EN standards, for aerospace applications.

This standard specifies the conditions of installation and removal procedure (hole serration profile, tools, swaging) of self-locking thickwall inserts defined by EN standards, for aerospace applications.

Committee	ACE/12
DocumentType	Standard
Pages	18
PublisherName	British Standards Institution
Status	Current
Supersedes	BS EN 4015:2003

Standards	Relationship
EN 4015:2004	Identical
NEN EN 4015 : 2006	Identical
NS EN 4015 : 2ED 2005	Identical
SN EN 4015 : 2005	Identical
I.S. EN 4015:2005	Identical
UNI EN 4015 : 2005	Identical
NBN EN 4015 : 2005	Identical
NF EN 4015 : 2005	Identical
DIN EN 4015:2006-10	Identical

EN 3831 : 2004	Aerospace series - Inserts, thickwall, self-locking, MJ threads, in heat resisting steel FE-PM3801 (17-4PH), MoS2 coated
EN 4014:2004	Aerospace series - Inserts, thickwall, self-locking - Design standard

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BS EN 4015:2004

Aerospace series. Inserts, thickwall, self-locking. Installation and removal procedure

Table of Contents

Abstract

Scope

General Product Information

International Equivalents

Standards Referencing This Book

Category

Subcategory