SIST EN 4014:2004
(Main)Aerospace series - Inserts, thickwall, self-locking - Design standard
Aerospace series - Inserts, thickwall, self-locking - Design standard
This standard specifies the use and installation hole dimensions for EN standard, self-locking, thickwall inserts and provisions for component salvage, for aerospace applications.
Aerospace series - Inserts, thickwall, self-locking - Design standard
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2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.Aerospace series - Inserts, thickwall, self-locking - Design standardAerospace series - Inserts, thickwall, self-locking - Design standard49.030.30MaticeNutsICS:Ta slovenski standard je istoveten z:EN 4014:2003SIST EN 4014:2004en01-maj-2004SIST EN 4014:2004SLOVENSKI
STANDARD
SIST EN 4014:2004
EUROPEAN STANDARDNORME EUROPÉENNEEUROPÄISCHE NORMEN 4014January 2003ICS 49.030.30English versionAerospace series - Inserts, thickwall, self-locking - DesignstandardThis European Standard was approved by CEN on 2 June 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, Slovakia, Spain, Sweden, Switzerland and UnitedKingdom.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 4014:2003 ESIST EN 4014:2004
EN 4014:2003 (E)2ContentspageForeword.31Scope.32Normative references.33Design.34Use.54.1General.54.2Performance.64.3Installation restrictions.65Required characteristics.75.1Installation hole.75.2Serration.86Installation.87Provisions for component salvage.98Designation.99Indication on drawings.99.1Drawing definition.99.2Assembly drawing.10SIST EN 4014:2004
EN 4014:2003 (E)3ForewordThis document (EN 4014:2003) has been prepared by the European Association of Aerospace Manufacturers –Standardization (AECMA-STAN).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 July 2003, and conflicting national standards shall be withdrawn at the latest byJuly 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,Slovakia, Spain, Sweden, Switzerland and the United Kingdom.1 ScopeThis standard specifies the use and installation hole dimensions for EN standard, self-locking, thickwall inserts andprovisions for component salvage, for aerospace applications.2 Normative referencesISO 5855-1Aerospace - MJ threads - Part 1: General requirementsISO 5855-2Aerospace - MJ threads - Part 2 : Limit dimensions for bolts and nutsEN 3831Aerospace series - Inserts, thickwall, self-locking, in heat resisting steel FE-PM3801 (17-4PH), MoS2coated 1)EN 4015Aerospace series - Inserts, thickwall, self-locking - Installation and removal procedure 1)3 DesignTypical examples of installed inserts are shown in figures 1 an
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