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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

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.


Dates of withdrawal of national standards are available from NSAI.

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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