EN 3914:2008
Current
The latest, up-to-date edition.
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
28-05-2008
Foreword
Introduction
1 Scope
2 Normative references
3 Required characteristics
3.1 Configuration - Dimensions - Tolerances - Masses
3.2 Material
3.3 Surface treatment
4 Designation
5 Marking and identification
6 Technical specification
This standard specifies the characteristics of long self locking, thin wall salvage inserts, in NI-PH2601 (NI P100HT), with silver plated internal thread, for aerospace applications.Maximum test temperature 550 °C.
Committee |
ASD-STAN
|
DevelopmentNote |
Supersedes PREN 3914. (02/2009)
|
DocumentType |
Standard
|
PublisherName |
Comite Europeen de Normalisation
|
Status |
Current
|
Supersedes |
Standards | Relationship |
NBN EN 3914 : 2008 | Identical |
BS EN 3914:2008 | Identical |
SN EN 3914 : 2008 | Identical |
I.S. EN 3914:2008 | Identical |
UNE-EN 3914:2008 | Identical |
UNI EN 3914 : 2008 | Identical |
DIN EN 3914:2008-12 | Identical |
NS EN 3914 : 1ED 2008 | Identical |
PN EN 3914 : 2008 | Identical |
NEN EN 3914 : 2008 | Identical |
NF EN 3914 : 2008 | Identical |
NF EN 3916 : 2009 | AEROSPACE SERIES - INSERT, THIN WALL - SALVAGE PROCEDURE FOR COMPONENTS |
I.S. EN 3916:2008 | AEROSPACE SERIES - INSERT, THIN WALL - SALVAGE PROCEDURE FOR COMPONENTS |
EN 3916:2008 | Aerospace series - Insert, thin wall - Salvage procedure for components |
BS EN 3916:2008 | Aerospace series. Insert, thin wall. Salvage procedure for components |
ISO 5855-2:1999 | Aerospace MJ threads Part 2: Limit dimensions for bolts and nuts |
PREN 4376 : 200P1 | AEROSPACE SERIES - HEAT RESISTING ALLOY NI-PH2601 (NICR19FE19NB5MO3) - SOLUTION TREATED AND PRECIPITATION TREATED - BAR AND SECTION - D[E] <= 200 MM |
EN 2786:2008 | Aerospace series - Electrolytic silver plating of fasteners |
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 3298:2008 | Aerospace series - Inserts, thin wall, self-locking - Installation and removal procedure |
PREN 4377 : 200P1 | AEROSPACE SERIES - HEAT RESISTING ALLOY NI-PH2601 (NICR19FE19NB5MO3) - NON HEAT TREATED - FORGING STOCK - A OR D <= 300 MM |
PREN 2404 : 2 | AEROSPACE SERIES - HEAT RESISTING NICKEL BASE ALLOY NI-P100-HT - SOLUTION TREATED AND PRECIPITATION TREATED - BARS |
PREN 3916 : 200P1 | AEROSPACE SERIES - INSERT, THIN WALL - SALVAGE PROCEDURE FOR COMPONENTS |
EN 2424:2008 | Aerospace series - Marking of aerospace products |
ISO 965-1:2013 | ISO general purpose metric screw threads — Tolerances — Part 1: Principles and basic data |
TR 3198 : 2013 | AEROSPACE SERIES - MANUFACTURERS' IDENTIFICATION MONOGRAMS AND MARKS FOR EN AEROSPACE PRODUCTS |
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