SIST EN 4420:2004
(Main)Aerospace series - Clips, spring tension, in alloy steel FE-PA3903
Aerospace series - Clips, spring tension, in alloy steel FE-PA3903
This standard specifies the characteristics of spring tension clips for the support of electrical harnesses, in FE-PA3903 for aerospace applications.
Maximum operating temperature: 250 °C
Luft- und Raumfahrt - Federklammern aus legiertem Stahl FE-PA3903
Diese Norm legt die Eigenschaften von Federklammern aus FE PA3903 zur Halterung von elektrischen Leitungsbündeln für Anwendungen in der Luft- und Raumfahrt fest.
Maximale Betriebstemperatur: 250 °C
Série aérospatiale - Colliers lyre, en acier allié FE-PA3903
La présente norme spécifie les caractéristiques des colliers lyre, en acier allié FE-PA3903, utilisés comme support des harnais électriques, pour applications aéronautiques.
Température maximale de fonctionnement : 250 °C.
Aerospace series - Clips, spring tension, in alloy steel FE-PA3903
General Information
Standards Content (Sample)
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.Aerospace series - Clips, spring tension, in alloy steel FE-PA3903Luft- und Raumfahrt - Federklammern aus legiertem Stahl FE-PA3903Série aérospatiale - Colliers lyre, en acier allié FE-PA3903Aerospace series - Clips, spring tension, in alloy steel FE-PA390349.030.50Podložke in drugi blokirni elementiWashers and other locking elementsICS:Ta slovenski standard je istoveten z:EN 4420:2003SIST EN 4420:2004en01-maj-2004SIST EN 4420:2004SLOVENSKI
STANDARD
SIST EN 4420:2004
EUROPEAN STANDARDNORME EUROPÉENNEEUROPÄISCHE NORMEN 4420February 2003ICS 49.030.50English versionAerospace series - Clips, spring tension, in alloy steel FE-PA3903This 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 4420:2003 ESIST EN 4420:2004
EN 4420:2003 (E)2ContentsForeword.31Scope.32Normative references.33Required characteristics.43.1Configuration – Dimensions – Tolerances – Masses.43.2Material.44Designation.75Marking.76Technical specification.77Application.7SIST EN 4420:2004
EN 4420:2003 (E)3ForewordThis document EN 4420:2003 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
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