EN 4123:2018

Aerospace series - Shank nuts, self-locking, in heat resisting nickel base alloy NI-PH2601 (Inconel 718), silver plated on thread - Classification: 1 550 MPa (at ambient temperature) / 600 °C

This document specifies the characteristics of self-locking shank nuts in NI PH2601, silver plated on thread, for aerospace applications.
Classification: 1 550 MPa / 600 °C.

Luft- und Raumfahrt - Einnietmuttern, selbstsichernd, aus hochwarmfester Nickelbasislegierung NI-PH2601 (Inconel 718), Gewinde versilbert - Klasse: 1 550 MPa (bei Raumtemperatur) / 600 °C

Diese Europäische Norm legt die Eigenschaften von selbstsichernden Einnietmuttern aus NI PH2601, Gewinde versilbert, für Anwendungen in der Luft  und Raumfahrt fest.
Klasse: 1 550 MPa/600 °C

Série aérospatiale - Écrous à sertir, à freinage interne, en alliage résistant à chaud à base de nickel NI-PH2601 (Inconel 718), argentés sur filetage - Classification : 1 550 MPa (à température ambiante ) / 600 °C

Cette présente Norme européenne spécifie les caractéristiques des écrous à sertir, à freinage interne, en NI PH2601, argentés sur filetage, pour applications aérospatiales.
Classification : 1 550 MPa / 600 °C.

Aeronavtika - Zakovičene matice, samovarovalne, iz toplotno odporne zlitine na nikljevi osnovi NI-PH2601 (Inconel 718), posrebreni navoji - Klasifikacija: 1550 MPa (pri temperaturi okolice)/600 °C

Ta dokument določa lastnosti samoblokirnih sidrnih matic s posrebreni navoji iz NI-PH2601 za uporabo v aeronavtiki.
Klasifikacija: 1 550 MPa1/600 °C2.

General Information

• Status: Published
• Publication Date: 15-May-2018
• Withdrawal Date: 29-Nov-2018
• ICS: 49.030.30 - Nuts
• Technical Committee: ASD-STAN - Aerospace
• Drafting Committee: ASD-STAN/D 3/S 2 - Fasteners
• Current Stage: 6060 - Definitive text made available (DAV) - Publishing
• Start Date: 16-May-2018
• Completion Date: 16-May-2018
• Ref Project: SIST EN 4123:2018 - Aerospace series - Shank nuts, self-locking, in heat resisting nickel base alloy NI-PH2601 (Inconel 718), silver plated on thread - Classification: 1 550 MPa (at ambient temperature) / 600 °C

Relations

• Replaces: EN 4123:2004 - Aerospace series - Shank nuts, self-locking, in heat resisting nickel base alloy NI-PH2601 (Inconel 718), silver plated on thread - Classification: 1 550 MPa (at ambient temperature) / 600 °C
• Effective Date: 08-Jun-2022

Standards Content (Sample)

2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.Luft- und Raumfahrt - Einnietmuttern, selbstsichernd, aus hochwarmfester Nickelbasislegierung NI-PH2601 (Inconel 718), Gewinde versilbert - Klasse: 1 550 MPa (bei Raumtemperatur) / 600 °CSérie aérospatiale - Écrous à sertir, à freinage interne, en alliage résistant à chaud à base de nickel NI-PH2601 (Inconel 718), argentés sur filetage - Classification : 1 550 MPa (à température ambiante ) / 600 °CAerospace series - Shank nuts, self-locking, in heat resisting nickel base alloy NI-PH2601 (Inconel 718), silver plated on thread - Classification: 1 550 MPa (at ambient temperature) / 600 °C49.030.30MaticeNutsICS:Ta slovenski standard je istoveten z:EN 4123:2018SIST EN 4123:2018en,fr,de01-julij-2018SIST EN 4123:2018SLOVENSKI
STANDARDSIST EN 4123:20051DGRPHãþD



SIST EN 4123:2018



EUROPEAN STANDARD NORME EUROPÉENNE EUROPÄISCHE NORM
EN 4123
May
t r s z ICS
v {ä r u rä u r Supersedes EN
v s t uã t r r vEnglish Version
Aerospace series æ Shank nutsá selfælockingá in heat resisting nickel base alloy NIplated on thread æ ClassificaSérie aérospatiale æ Écrous à sertirá à freinage interneá en alliage résistant à chaud à base de nickel NIæPH t x r s
Luftæ und Raumfahrt æ Einnietmutterná selbstsicherndá aus hochwarmfester Nickelbasislegierung NIæPH t x r s This European Standard was approved by CEN on
t t January
t r s zä
egulations which stipulate the conditions for giving this European Standard the status of a national standard without any alterationä Upætoædate lists and bibliographical references concerning such national standards may be obtained on application to the CENæCENELEC Management Centre or to any CEN memberä
translation under the responsibility of a CEN member into its own language and notified to the CENæCENELEC Management Centre has the same status as the official versionsä
CEN members are the national standards bodies of Austriaá Belgiumá Bulgariaá Croatiaá Cyprusá Czech Republicá Denmarká Estoniaá Finlandá Former Yugoslav Republic of Macedoniaá Franceá Germanyá Greeceá Hungaryá Icelandá Irelandá Italyá Latviaá Lithuaniaá Luxembourgá Maltaá Netherlandsá Norwayá Polandá Portugalá Romaniaá Serbiaá Slovakiaá Sloveniaá Spainá Swedená Switzerlandá Turkey and United Kingdomä
EUROPEAN COMMITTEE FOR STANDARDIZATION COMITÉ EUROPÉEN DE NORMALISATION EUROPÄISCHES KOMITEE FÜR NORMUNG
CEN-CENELEC Management Centre:
Rue de la Science 23,
B-1040 Brussels
9
t r s z CEN All rights of exploitation in any form and by any means reserved worldwide for CEN national Membersä Refä Noä EN
v s t uã t r s z ESIST EN 4123:2018



EN 4123:2018 (E) 2 Contents
Page European foreword . 3 1 Scope . 4 2 Normative references . 4 3 Required characteristics . 4 3.1 Configuration — Dimensions — Tolerances — Masses . 4 3.2 Material . 4 3.3 Surface treatment . 4 4 Designation. 6 5 Marking . 6 6 Technical specification . 6
SIST EN 4123:2018



EN 4123:2018 (E) 3 European foreword This document (EN 4123:2018) has been prepared by the Aerospace and Defence Industries Association of Europe — Standardization (ASD-STAN). After enquiries and votes carried out in accordance with the rules of this Association, this Standard has received the approval of the National Associations and the Official Services of the member countries of ASD, prior to its presentation to CEN. This European Standard shall be given the status of a national standard, either by publication of an identical text or by endorsement, at the latest by November 2018, and conflicting national standards shall be withdrawn at the latest by
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