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CEN
EN 3916:2008

EN 3916:2008

Current

Current

The latest, up-to-date edition.

Aerospace series - Insert, thin wall - Salvage procedure for components

Published date

06-08-2008

Publisher

Comite Europeen de Normalisation

Foreword
1 Scope
2 Normative references
3 Conditions of use
4 Re-machining of an existing insert hole
5 Insert and tapped hole particulars
6 Installation of oversize inserts
7 Minimum criteria for the installation and removal tools
   and their methods of application
8 Assembly drive tool and swage tool
9 Assembly procedure
   9.1 Insertion
   9.2 Swaging
   9.3 Gauging and inspection
10 Oversize insert removal, replacement and tools

1.1This specification covers the accepted methods for the reclamation of installation holes for standard thin wall inserts, within assemblies.1.2To enable rectification when defects or damage occur to the standard insert tapped installation hole, or to rectify any out of position of the hole within the specified parameters of use.1.3To control the machining of the existing insert hole and the installation requirements of the replacement oversize thin wall insert.

Committee
ASD-STAN
DevelopmentNote
Supersedes PREN 3916. (10/2008)
DocumentType
Standard
PublisherName
Comite Europeen de Normalisation
Status
Current
Supersedes

Standards Relationship
BS EN 3916:2008 Identical
I.S. EN 3916:2008 Identical
UNI EN 3916 : 2010 Identical
NBN EN 3916 : 2008 Identical
NEN EN 3916 : 2008 Identical
PN EN 3916 : 2008 Identical
NF EN 3916 : 2009 Identical
DIN EN 3916:2008-12 Identical
UNE-EN 3916:2008 Identical
NS EN 3916 : 1ED 2008 Identical
SN EN 3916 : 2008 Identical

DIN EN 3676:1998-02 AEROSPACE SERIES - INSERTS, THIN WALL, SELF-LOCKING - DESIGN STANDARD
BS EN 3676:1998 Inserts, thin wall, self-locking. Design standard
EN 3676:1998 Aerospace series - Inserts, thin wall, self-locking - Design standard

ISO 5855-2:1999 Aerospace MJ threads Part 2: Limit dimensions for bolts and nuts
EN 3913:2007 Aerospace series - Insert, thin wall, self-locking, short, in heat resisting nickel base alloy NI-PH2601 (Ni-P100HT, Inconel 718), silver plated on internal thread, for salvage of components
EN 3915 : 2008 Aerospace series - Insert, thin wall, self-locking, MJ threads, in heat resisting nickel base alloy NI-PH2601 (NI-P100HT, Inconel 718), for salvage of components - Classification: 1 275 MPa (at ambient temperature) / 550 °C - Technical specification
EN 3676:1998 Aerospace series - Inserts, thin wall, self-locking - Design standard
ISO 965-1:2013 ISO general purpose metric screw threads — Tolerances — Part 1: Principles and basic data
EN 3914:2008 Aerospace series - Insert, thin wall, self-locking, long, in heat resisting nickel base alloy NI-PH2601 (NI-P100HT, Inconel 718), silver plated on internal thread, for salvage of components

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