PREN 3298 : 200P2
Withdrawn
View Superseded by
AEROSPACE SERIES - INSERTS, THIN WALL, SELF-LOCKING - INSTALLATION AND REMOVAL PROCEDURE
Hardcopy , PDF
English
12-14-2023
Foreword
1 Scope
2 Normative references
3 Hole serration profile (short inserts)
4 Installation of inserts
5 Minimum criteria for the installation and
removal tools and their methods of application
6 Assembly tools and gauges
6.1 General
6.2 Installation drive tool
6.3 Swage tools
7 Installation procedure
7.1 Insertion
7.2 Insert alignment prior to swaging
7.3 Swaging
7.4 After swage inspection
7.5 Inspection for minimum locking torque
8 Insert removal and replacement
Annex A (informative) Recommended tooling
Specifies the conditions of installation and removal (hole serration profile, tools, swaging procedure) of self-locking thin wall inserts defined by EN standards, for aerospace applications.
| Committee |
C8
|
| DocumentType |
Draft
|
| Pages |
16
|
| ProductNote |
Superseded by EN 3298:2008
|
| PublisherName |
Aerospace & Defence Industries Association of Europe
|
| Status |
Withdrawn
|
| SupersededBy |
| EN 3236:1998 | Aerospace series - Inserts, thin wall, self-locking, short, in heat resisting nickel base alloy NI-P100HT (Inconel 718), silver plated internal thread |
| EN 3237:1998 | Aerospace series - Inserts, thin wall, self-locking, long, in heat resisting nickel base alloy NI-P100HT (Inconel 718), silver plated internal thread |
| EN 3676:1998 | Aerospace series - Inserts, thin wall, self-locking - Design standard |
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