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I.S. EN 4015:2005

Current

Current

The latest, up-to-date edition.

AEROSPACE SERIES - INSERT, THICKWALL, SELF-LOCKING - INSTALLATION AND REMOVAL PROCEDURE

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

01-01-2005

Preview

For Harmonized Standards, check the EU site to confirm that the Standard is cited in the Official Journal.

Only cited Standards give presumption of conformance to New Approach Directives/Regulations.

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

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

DocumentType
Standard
Pages
16
PublisherName
National Standards Authority of Ireland
Status
Current
Supersedes

Standards Relationship
EN 4015:2004 Identical
NEN EN 4015 : 2006 Identical
NS EN 4015 : 2ED 2005 Identical
SN EN 4015 : 2005 Identical
UNI EN 4015 : 2005 Identical
NBN EN 4015 : 2005 Identical
BS EN 4015:2004 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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