PREN 4015 : 200P1
Withdrawn
View Superseded by
AEROSPACE SERIES - INSERTS, THICKWALL, SELF-LOCKING - INSTALLATION AND REMOVAL PROCEDURE
Hardcopy , PDF
English
12-16-2023
1 Scope
2 Normative references
3 Insert information
4 Hole serration profile
5 Inspection requirements before installation
6 Installation tools
7 Checks of insert position and crimping
8 Inspection of minimum self-locking torque
9 Insert removal
10 Repair
Defines the conditions of installation and removal procedure (hole serration profile, tools, swaging) of self-locking thickwall inserts specified by EN standards, for aerospace applications.
| Committee |
C8
|
| DocumentType |
Draft
|
| Pages |
13
|
| ProductNote |
Superseded by EN 4015:2004
|
| PublisherName |
Aerospace & Defence Industries Association of Europe
|
| Status |
Withdrawn
|
| SupersededBy |
| Standards | Relationship |
| DIN EN 4015:2006-10 | Identical |
| PREN 4014 : 200P1 | AEROSPACE SERIES - INSERTS, THICKWALL, SELF-LOCKING - DESIGN STANDARD |
| PREN 3831 : 200P2 | AEROSPACE SERIES - INSERTS, THICKWALL, SELF-LOCKING, IN HEAT RESISTING STEEL FE-PM3801 (17-4PH), MOS[2] COATED |
| PREN 3899 : 200P1 | AEROSPACE SERIES - INSERTS, THICKWALL, SELF-LOCKING, MJ THREADS, IN HEAT RESISTING STEEL FE-PM3801 (17-4PH) - TECHNICAL SPECIFICATION |
| PREN 4014 : 200P1 | AEROSPACE SERIES - INSERTS, THICKWALL, SELF-LOCKING - DESIGN STANDARD |
| PREN 3831 : 200P2 | AEROSPACE SERIES - INSERTS, THICKWALL, SELF-LOCKING, IN HEAT RESISTING STEEL FE-PM3801 (17-4PH), MOS[2] COATED |
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