Aerospace series - Nuts, hexagon, self-locking, in heat resisting steel, MoS2 lubricated - Classification: 1 100 MPa (at ambient temperature)/315 °C

This standard specifies characteristics of self-locking hexagonal nuts, with flange, in heat resisting steel, MoS2 lubricated.
Classification: 1 100 MPa ) / 315 °C ).

Luft- und Raumfahrt - Sechskantmuttern, selbstsichernd, aus hochwarmfestem Stahl, MoS2-geschmiert - Klasse: 1 100 MPa (bei Raumtemperatur)/315 °C

Diese Norm legt die Eigenschaften von selbstsichernden Sechskantmuttern mit Flansch aus hochwarmfestem Stahl, MoS2-geschmiert, fest.
Klasse: 1 100 MPa ) / 315 °C ).

Série aérospatiale - Ecrous hexagonaux, à freinage interne, en acier résistant à chaud, lubrifiés MoS2 - Classification: 1 100 MPa (à température ambiante)/315 °C

Aeronavtika - Matice, šestrobe, samozapiralne, iz toplotnoodpornega jekla, namazane z MoS2 - Klasifikacija: 1100 MPa (pri temperaturi okolice)/315 °C

General Information

Status
Published
Publication Date
01-Apr-2009
Technical Committee
Current Stage
6060 - National Implementation/Publication (Adopted Project)
Start Date
23-Mar-2009
Due Date
28-May-2009
Completion Date
02-Apr-2009

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2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.Aeronavtika - Matice, šestrobe, samozapiralne, iz toplotnoodpornega jekla, namazane z MoS2 - Klasifikacija: 1100 MPa (pri temperaturi okolice)/315 °CLuft- und Raumfahrt - Sechskantmuttern, selbstsichernd, aus hochwarmfestem Stahl, MoS2-geschmiert - Klasse: 1 100 MPa (bei Raumtemperatur)/315 °CSérie aérospatiale - Ecrous hexagonaux, à freinage interne, en acier résistant à chaud, lubrifiés MoS2 - Classification: 1 100 MPa (à température ambiante)/315 °CAerospace series - Nuts, hexagon, self-locking, in heat resisting steel, MoS2 lubricated - Classification: 1 100 MPa (at ambient temperature)/315 °C49.030.30MaticeNutsICS:Ta slovenski standard je istoveten z:EN 3536:2006SIST EN 3536:2009en,de01-maj-2009SIST EN 3536:2009SLOVENSKI
STANDARD



SIST EN 3536:2009



EUROPEAN STANDARD NORME EUROPÉENNE EUROPÄISCHE NORM
EN 3536
July 2006 ICS 49.030.30 English Version
Aerospace series - Nuts, hexagon, self-locking, in heat resisting steel, MoS2 lubricated - Classification: 1 100 MPa (at ambient temperature)/315 °C
Série aérospatiale - Ecrous hexagonaux, à freinage interne, en acier résistant à chaud, lubrifiés MoS2 - Classification: 1 100 MPa (à température ambiante)/315 °C
Luft- und Raumfahrt - Sechskantmuttern, selbstsichernd, aus hochwarmfestem Stahl, MoS2-geschmiert - Klasse: 1 100 MPa (bei Raumtemperatur)/315 °C This European Standard was approved by CEN on 9 March 2006.
CEN members are bound to comply with the CEN/CENELEC Internal Regulations which stipulate the conditions for giving this European Standard the status of a national standard without any alteration. Up-to-date lists and bibliographical references concerning such national standards may be obtained on application to the Central Secretariat or to any CEN member.
This European Standard exists in three official versions (English, French, German). A version in any other language made by translation under the responsibility of a CEN member into its own language and notified to the Central Secretariat has the same status as the official versions.
CEN members are the national standards bodies of Austria, Belgium, Cyprus, Czech Republic, Denmark, Estonia, Finland, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Romania, Slovakia, Slovenia, Spain, Sweden, Switzerland and United Kingdom.
EUROPEAN COMMITTEE FOR STANDARDIZATION
COMITÉ EUROPÉEN DE NORMALISATION EUROPÄISCHES KOMITEE FÜR NORMUNG
Management Centre: rue de Stassart, 36
B-1050 Brussels © 2006 CEN All rights of exploitation in any form and by any means reserved worldwide for CEN national Members. Ref. No. EN 3536:2006: ESIST EN 3536:2009



EN 3536:2006 (E) 2 Contents Page Foreword.3 1 Scope.4 2 Normative references.4 3 Required characteristics.5 4 Designation.7 5 Marking.7 6 Technical specification.7
SIST EN 3536:2009



EN 3536:2006 (E) 3 Foreword This European Standard (EN 3536:2006) has been prepared by the AeroSpace and Defense Industries Asso-ciation of Europe - Standardization (ASD-STAN). After enquiries and votes carried out in accordance with the rules of this Association, this Standard has re-ceived 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 January 2007, and conflicting national standards shall be withdrawn at the latest by January 2007. Attention is drawn to the possibility that some of the elements of this document may be the subject of patent rights. CEN [and/or CENELEC] shall not be held responsible for identifying any or all such p
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