EN 3542:2018

Aerospace series - Inserts, screw thread, helical coil, self-locking, in heat resisting nickel base alloy NI-PH2801 (Inconel X750)

This document specifies the characteristics of inserts, self locking, helical coil, tanged insertion drive, with MJ screw thread in NI PH2801 material, for aerospace applications.
Maximum test temperature: 550 °C.

Luft- und Raumfahrt - Draht-Gewindeeinsätze, selbstsichernd, aus hochwarmfester Nickelbasislegierung NI-PH2801 (Inconel X750)

Dieses Dokument legt die Eigenschaften von selbstsichernden Draht Gewindeeinsätzen, Einbau mit Mitnehmerzapfen, mit MJ-Gewinde aus NI PH2801 zur Verwendung in der Luft  und Raumfahrt fest.
Maximale Prüftemperatur: 550 °C

Série aérospatiale - Filets rapportés, à freinage interne, en alliage résistant à chaud à base de nickel NI-PH2801 (Inconel X750)

La présente norme spécifie les caractéristiques des filets rapportés, à freinage interne, avec vis à filetage MJ en NI-PH2801, pour les applications aérospatiales.
Température maximale d'essai : 550 °C

Aeronavtika - Vložki s spiralnim navojem, samozapiralni, iz toplotnoodporne zlitine na nikljevi osnovi Ni-PH2801 (Inconel X750)

Ta evropski standard določa značilnosti vložkov, varnostnih mehanizmov, vijačnih tuljav, pogona s stičnim vložkom in navoje vijakov iz NI-PH2801 za uporabo v aeronavtiki.
Najvišja preskusna temperatura: 550 °C.

General Information

• Status: Published
• Publication Date: 17-Apr-2018
• Withdrawal Date: 30-Oct-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: 18-Apr-2018
• Completion Date: 18-Apr-2018
• Ref Project: SIST EN 3542:2018 - Aerospace series - Inserts, screw thread, helical coil, self-locking, in heat resisting nickel base alloy Ni-PH2801 (Inconel X750)

Relations

• Replaces: EN 3542:1998 - Aerospace series - Inserts, screw thread, helical coil, self-locking, in heat resisting nickel base alloy NI-PH2801 (Inconel X750)
• Effective Date: 25-Apr-2018
• Revised: prEN 3542 - Aerospace series - Inserts, screw threads, helical coil, self-locking, tanged insertion drive, in heat resisting nickel base alloy NI-PH2801 (Inconel X750)
• Effective Date: 29-Jul-2020

Standards Content (Sample)

2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.Aeronavtika - Vložki s spiralnim navojem, samozapiralni, iz toplotnoodporne zlitine na nikljevi osnovi Ni-PH2801 (Inconel X750)Luft- und Raumfahrt - Draht-Gewindeeinsätze, selbstsichernd aus hochwarmfester Nickelbasislegierung NI-PH2801 (Inconel X750)Série aérospatiale - Filets rapportés, à freinage interne, en alliage résistant à chaud à base de nickel NI-PH2801 (Inconel X750)Aerospace series - Inserts, screw thread, helical coil, self-locking, in heat resisting nickel base alloy Ni-PH2801 (Inconel X750)49.030.30MaticeNutsICS:Ta slovenski standard je istoveten z:EN 3542:2018SIST EN 3542:2018en,fr,de01-julij-2018SIST EN 3542:2018SLOVENSKI
STANDARDSIST EN 3542:20011DGRPHãþD



SIST EN 3542:2018



EUROPEAN STANDARD NORME EUROPÉENNE EUROPÄISCHE NORM
EN 3542
April
t r s z ICS
v {ä r u rä u r Supersedes EN
u w v tã s { { zEnglish Version
Aerospace series æ Insertsá screw threadá helical coilá selfælockingá in heat resisting nickel base alloy NIæPH t z r s Série aérospatiale æ Filets rapportésá à freinage interneá en alliage résistant à chaud à base de nickel NIæPH t z r s
Luftæ und Raumfahrt æ DrahtæGewindeeinsätzeá selbstsicherndá aus hochwarmfester 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
u w v tã t r s z ESIST EN 3542:2018



EN 3542:2018 (E) 2 Contents
Page European foreword . 3 Introduction . 4 1 Scope . 5 2 Normative references . 5 3 Required characteristics . 5 3.1 Configuration — Dimensions — Tolerances — Masses . 5 3.2 Material . 5 3.3 Material identification . 5 4 Designation. 9 5 Marking . 9 6 Technical specification . 9
SIST EN 3542:2018



EN 3542:2018 (E) 3 European foreword This document (EN 3542:2018) 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 October
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