Aerospace series - Nuts, bihexagonal, self-locking, in heat resisting nickel base alloy NI-PH 2601 (Inconel 718), silver plated on thread - Classification: 1550 MPa (at ambient temperature)/600°C

This standard specifies the characteristics of self-locking bihexagonal nuts in NI-P100HT, silver plated on thread, for aerospace applications.
Classification: 1 550 MPa/600 °C

Luft- und Raumfahrt - Zwölfkantmuttern, selbstsichernd, - Aus hochwarmfester Nickelbasislegierung NI-P100HT (Inconel 718), Gewinde versilbert - - Klasse: 1 550 MPa (bei Raumtemperatur)/600 °C

Série aérospatiale - Ecrous bihexagonaux, a freinage interne, en alliage résistant a chaud a base de nickel NI-P100HT (Inconel 718), argentés sur filetages - Classification:1 550 MPa (a température ambiante)/600°C

Aerospace series - Nuts, bihexagonal, self-locking, in heat resisting nickel base alloy NI-PH 2601 (Inconel 718), silver plated on thread - Classification: 1550 MPa (at ambient temperature)/600°C

General Information

Status
Withdrawn
Publication Date
30-Apr-2004
Withdrawal Date
31-May-2005
Technical Committee
Current Stage
9900 - Withdrawal (Adopted Project)
Start Date
01-Jun-2005
Due Date
01-Jun-2005
Completion Date
01-Jun-2005

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Standards Content (Sample)

2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.Aerospace series - Nuts, bihexagonal, self-locking, in heat resisting nickel base alloy NI-PH 2601 (Inconel 718), silver plated on thread - Classification: 1550 MPa (at ambient temperature)/600°CLuft- und Raumfahrt - Zwölfkantmuttern, selbstsichernd, - Aus hochwarmfester Nickelbasislegierung NI-P100HT (Inconel 718), Gewinde versilbert - - Klasse: 1 550 MPa (bei Raumtemperatur)/600 °CSérie aérospatiale - Ecrous bihexagonaux, a freinage interne, en alliage résistant a chaud a base de nickel NI-P100HT (Inconel 718), argentés sur filetages - Classification:1 550 MPa (a température ambiante)/600°CAerospace series - Nuts, bihexagonal, self-locking, in heat resisting nickel base alloy NI-PH 2601 (Inconel 718), silver plated on thread - Classification: 1550 MPa (at ambient temperature)/600°C49.030.30MaticeNutsICS:Ta slovenski standard je istoveten z:EN 4117:2003SIST EN 4117:2004en01-maj-2004SIST EN 4117:2004SLOVENSKI
STANDARD



SIST EN 4117:2004



EUROPEAN STANDARDNORME EUROPÉENNEEUROPÄISCHE NORMEN 4117February 2003ICS 49.030.30English versionAerospace series - Nuts, bihexagonal, self-locking, in heatresisting nickel base alloy NI-PH 2601 (Inconel 718), silverplated on thread - Classification: 1550 MPa (at ambienttemperature)/600°CThis European Standard was approved by CEN on 19 August 2002.CEN members are bound to comply with the CEN/CENELEC Internal Regulations which stipulate the conditions for giving this EuropeanStandard the status of a national standard without any alteration. Up-to-date lists and bibliographical references concerning such nationalstandards may be obtained on application to the Management Centre or to any CEN member.This European Standard exists in three official versions (English, French, German). A version in any other language made by translationunder the responsibility of a CEN member into its own language and notified to the Management Centre has the same status as the officialversions.CEN members are the national standards bodies of Austria, Belgium, Czech Republic, Denmark, Finland, France, Germany, Greece,Hungary, Iceland, Ireland, Italy, Luxembourg, Malta, Netherlands, Norway, Portugal, Slovak Republic, Spain, Sweden, Switzerland andUnited Kingdom.EUROPEAN COMMITTEE FOR STANDARDIZATIONCOMITÉ EUROPÉEN DE NORMALISATIONEUROPÄISCHES KOMITEE FÜR NORMUNGManagement Centre: rue de Stassart, 36
B-1050 Brussels© 2003 CENAll rights of exploitation in any form and by any means reservedworldwide for CEN national Members.Ref. No. EN 4117:2003 ESIST EN 4117:2004



EN 4117:2003 (E)2ContentspageForeword.31Scope.32Normative references.33Required characteristics.43.1Configuration - Dimensions - Tolerances - Masses.43.2Material.43.3Surface treatment.44Designation.65Marking.66Technical specification.6SIST EN 4117:2004



EN 4117:2003 (E)3ForewordThis document EN 4117:2003 has been prepared by the European Association of Aerospace Manufacturers(AECMA).After enquiries and votes carried out in accordance with the rules
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