SIST EN 2881:2009

Aerospace series - Nuts, anchor, self-locking, fuel resistant, sealing, floating, two lug, with counterbore, in corrosion resisting steel, passivated, MoS2 lubricated, metric series - Classification: 900 MPa (at ambient temperature)/120 °C

SIST EN 2881:2009

Name:SIST EN 2881:2009   Standard name:Aerospace series - Nuts, anchor, self-locking, fuel resistant, sealing, floating, two lug, with counterbore, in corrosion resisting steel, passivated, MoS2 lubricated, metric series - Classification: 900 MPa (at ambient temperature)/120 °C
Standard number:SIST EN 2881:2009   language:English language
Release Date:09-Sep-2009   technical committee:I13 - Imaginarni 13
Drafting committee:   ICS number:49.030.30 - Nuts
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.Luft- und Raumfahrt - Annietmuttern, selbstsichernd, kraftstoffbeständing, druckdicht, beweglich, beiderseitiger Flansch, mit zylindrischer Aussenkung, aus korrosionsbeständigem Stahl, passiviert, MoS2-geschmiert, metrische Reihe - Klasse: 900 MPa (bei Raumtemperatur)/120 °CSérie aérospatiale - Écrous à river, à freinage interne, étanches au carburant, flottants, double patte, avec chambrage, en acier résistant à la corrosion, passivés, lubrifiés MoS2, série métrique - Classification: 900 MPa (à température ambiante)/120 °CAerospace series - Nuts, anchor, self-locking, fuel resistant, sealing, floating, two lug, with counterbore, in corrosion resisting steel, passivated, MoS2 lubricated, metric series - Classification: 900 MPa (at ambient temperature)/120 °C49.030.30MaticeNutsICS:Ta slovenski standard je istoveten z:EN 2881:2006SIST EN 2881:2009en,de01-oktober-2009SIST EN 2881:2009SLOVENSKI
STANDARD



SIST EN 2881:2009



EUROPEAN STANDARDNORME EUROPÉENNEEUROPÄISCHE NORMEN 2881May 2006ICS 49.030.30 English VersionAerospace series - Nuts, anchor, self-locking, fuel resistant,sealing, floating, two lug, with counterbore, in corrosion resistingsteel, passivated, MoS2 lubricated - Classification: 900 MPa (atambient temperature) / 120
CSérie aérospatiale - Écrous à river, à freinage interne,étanches au carburant, flottants, double patte, avecchambrage, en acier résistant à la corrosion, passivés,lubrifiés MoS2, série métrique - Classification : 900 MPa (àtempérature ambiante) / 120
CLuft- und Raumfahrt - Annietmuttern, selbstsichernd,druckdicht, kraftstoffbeständing, beweglich, beiderseitigerFlansch, mit zylindrischer Aussenkung, auskorrosionsbeständigem Stahl, passiviert, MoS2-geschmiert- Klasse: 900 MPa (bei Raumtemperatur) / 120
CThis European Standard was approved by CEN on 6 February 2006.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 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 translationunder the responsibility of a CEN member into its own language and notified to the Central Secretariat has the same status as the officialversions.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 STANDARDIZATIONCOMITÉ EUROPÉEN DE NORMALISATIONEUROPÄISCHES KOMITEE FÜR NORMUNGManagement Centre: rue de Stassart, 36
B-1050 Brussels© 2006 CENAll rights of exploitation in any form and by any means reservedworldwide for CEN national Members.Ref. No. EN 2881:2006: ESIST EN 2881:2009



EN 2881:2006 (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 2881:2009



EN 2881:2006 (E) 3 Foreword This European Standard (EN 2881:2006) 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 received the approval of the National Associations and the Official Services of the member countries of AECMA, 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 November 2006, and conflicting national standards shall be withdrawn at the latest by November 2006. 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 patent rights. According to the CEN/CENELEC Internal Regulatio
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