SIST EN 4323:2004

Aerospace series - Screws, 100° countersunk head, six lobe recess, threaded to head, in titanium alloy TI-P64001, anodized, MoS2 coated - Classification: 900 MPa (at ambient temperature)/350 °C

This standard specifies the characteristics of screws with 100° countersunk head with six lobe recess, threaded to head, in TI-P63, anodized, MoS2 coated, for aerospace applications.
Classification: 900 MPa  )  / 350 °C

Série aérospatiale - Vis a tete fraisée 100°, a empreinte six lobes, filetées sous tete en alliage de titane TI-P63, anodisées, revetues MoS2 - Classification: 900 MPa (a température ambiante)/350°C

Aerospace series - Screws, 100° countersunk head, six lobe recess, threaded to head, in titanium alloy TI-P64001, anodized, MoS2 coated - Classification: 900 MPa (at ambient temperature)/350 °C

General Information

• Status: Withdrawn
• Publication Date: 30-Apr-2004
• Withdrawal Date: 31-May-2005
• ICS: 49.030.20 - Bolts, screws, studs
• Technical Committee: I08 - Imaginarni 08
• Current Stage: 9900 - Withdrawal (Adopted Project)
• Start Date: 01-Jun-2005
• Due Date: 01-Jun-2005
• Completion Date: 01-Jun-2005
• Ref Project: EN 4323:2003 - Aerospace series - Screws, 100° countersunk head, six lobe recess, threaded to head, in titanium alloy TI-P64001, anodized, MoS2 coated - Classification: 900 MPa (at ambient temperature)/350 °C

Relations

• Replaced By: SIST EN 4323:2005 - Aerospace series - Screws, 100° countersunk head, six lobe recess, threaded to head, in titanium alloy TI-P64001, anodized, MoS2 coated - Classification: 900 MPa (at ambient temperature) / 350 °C
• Effective Date: 01-Jun-2005

Standards Content (Sample)

2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.Aerospace series - Screws, 100° countersunk head, six lobe recess, threaded to head, in titanium alloy TI-P64001, anodized, MoS2 coated - Classification: 900 MPa (at ambient temperature)/350 °CSérie aérospatiale - Vis a tete fraisée 100°, a empreinte six lobes, filetées sous tete en alliage de titane TI-P63, anodisées, revetues MoS2 - Classification: 900 MPa (a température ambiante)/350°CAerospace series - Screws, 100° countersunk head, six lobe recess, threaded to head, in titanium alloy TI-P64001, anodized, MoS2 coated - Classification: 900 MPa (at ambient temperature)/350 °C49.030.20Sorniki, vijaki, stebelni vijakiBolts, screws, studsICS:Ta slovenski standard je istoveten z:EN 4323:2003SIST EN 4323:2004en01-maj-2004SIST EN 4323:2004SLOVENSKI
STANDARD



SIST EN 4323:2004



EUROPEAN STANDARDNORME EUROPÉENNEEUROPÄISCHE NORMEN 4323February 2003ICS 49.030.20English versionAerospace series - Screws, 100° countersunk head, six loberecess, threaded to head, in titanium alloy TI-P64001, anodized,MoS2 coated - Classification: 900 MPa (at ambienttemperature)/350 °CThis European Standard was approved by CEN on 14 September 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 4323:2003 ESIST EN 4323:2004



EN 4323:2003 (E)2ContentsForeword.31Scope.32Normative references.33Required characteristics.43.1Configuration – Dimensions – Tolerances – Masses.43.2Materials.43.3Surface treatment.44Designation.85Marking.86Technical specification.8SIST EN 4323:2004



EN 4323:2003 (E)3ForewordThis document EN 4323:2003 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 Int
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