SIST EN 3724:2004
(Main)Aerospace series - Bolts, double hexagon head, relieved shank, long thread, in titanium alloy TI-P64001, MoS2 coated - Classification: 1 100 MPa (at ambient temperature)
Aerospace series - Bolts, double hexagon head, relieved shank, long thread, in titanium alloy TI-P64001, MoS2 coated - Classification: 1 100 MPa (at ambient temperature)
This standard specifies the characteristics of double hexagon headed bolts with relieved shank and long thread, in titanium alloy TI-P63, MoS2 coated, for aerospace applications. Classification: 1 100 MPa.
Série aérospatiale - Vis a tete bihexagonale, a tige réduite, filetage long, en alliage de titane TI-P63, revetues MoS2 - Classification:1 100 MPa (a température ambiante)
Aerospace series - Bolts, double hexagon head, relieved shank, long thread, in titanium alloy TI-P64001, MoS2 coated - Classification: 1 100 MPa (at ambient temperature)
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2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.Aerospace series - Bolts, double hexagon head, relieved shank, long thread, in titanium alloy TI-P64001, MoS2 coated - Classification: 1 100 MPa (at ambient temperature)Série aérospatiale - Vis a tete bihexagonale, a tige réduite, filetage long, en alliage de titane TI-P63, revetues MoS2 - Classification:1 100 MPa (a température ambiante)Aerospace series - Bolts, double hexagon head, relieved shank, long thread, in titanium alloy TI-P64001, MoS2 coated - Classification: 1 100 MPa (at ambient temperature)49.030.20Sorniki, vijaki, stebelni vijakiBolts, screws, studsICS:Ta slovenski standard je istoveten z:EN 3724:2003SIST EN 3724:2004en01-maj-2004SIST EN 3724:2004SLOVENSKI
STANDARD
SIST EN 3724:2004
EUROPEAN STANDARDNORME EUROPÉENNEEUROPÄISCHE NORMEN 3724February 2003ICS 49.030.20English versionAerospace series - Bolts, double hexagon head, relieved shank,long thread, in titanium alloy TI-P64001, MoS2 coated -Classification: 1 100 MPa (at ambient temperature)This European Standard was approved by CEN on 19 August 2003.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 3724:2003 ESIST EN 3724:2004
EN 3724:2003 (E)2ContentspageForeword.31Scope and field of application.42Normative references.43Required characteristics.53.1Configuration - Dimensions - Tolerances – Masses.53.2Material.53.3Surface coating.54Designation.95Marking.96Technical specification.9SIST EN 3724:2004
EN 3724:2003 (E)3ForewordThis document EN 3724:2003 has been prepared by the European Association of Aerospace Manufacturers(AECMA).After enquiries and votes carried out in accordance with the rules of this Association, this Standard has receivedthe approval of the National Associations and the Official Services of the member countries of AECMA, prior to itspresentation to CEN.This European Standard shall be given the status of a national standard, either by publication of an identical text orby endorsement, at the latest by August 2003, and conflicting national standards shall be withdrawn at the latest byAugust 2003.According to the CEN/CENELEC Internal Regulations, the national standards organizations of the followingcountries are bound to implement this European Standard : Austria, Belgium, Czech Republic, Denmark, Finland,France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Luxembourg, Malta, Netherlands, Norway, Portugal,Slovak Republic, Spain, Sweden, Switzerland and United Kingdom.SIST EN 3724:2004
EN 3724:2003 (E)41 Scope and field of applicationThis standard specifies the characteristics of double hexagon headed bolts with relieved shank and long thread, intitanium alloy TI-P64001, MoS2 coated, for aerospace applications.Classification: 1 100 MPa 1).2 Normative referencesThis European Standard incorporates by dated or undated reference, provisions from other publications. Thesenormative references are cited at the appropriate places in the text, and the publications are listed hereafter. Fordated references, subsequent amendments to or revisions of any of these publications apply to this EuropeanStandard only when incorporated in it by amendment or revision. For undated references the latest edition of thepublication referred to applies (including amendments).ISO 3353, Aerospace - Rolled threads for bolts - Lead and runout requirements.ISO 4095, Aerospace - Bihexagonal drives - Wrenching configuration - Metric series.ISO 5855-2, Aerospace - MJ threads - Part 2: Limit dimensions for bolts and nuts.EN 2424, Aerospace series - Marking o
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