I.S. EN 4015:2005
Current
The latest, up-to-date edition.
AEROSPACE SERIES - INSERT, THICKWALL, SELF-LOCKING - INSTALLATION AND REMOVAL PROCEDURE
Hardcopy , PDF
English
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 |
| 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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