SIST EN 2898:2008

2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.Aerospace series - Corrosion and heat resisting steel rivets - Technical specificationHKQLþQDVSHFLILNDFLMDSérie aérospatiale - Rivets en acier résistant à chaud et à la corrosion - Spécification techniqueLuft- und Raumfahrt - Niete aus hochwarmfesten und korrosionsbeständigen Stählen - Technische LieferbedingungenTa slovenski standard je istoveten z:EN 2898:2008SIST EN 2898:2008en49.030.60ICS:SLOVENSKI
STANDARDSIST EN 2898:200801-junij-2008







EUROPEAN STANDARDNORME EUROPÉENNEEUROPÄISCHE NORMEN 2898March 2008ICS 49.030.60 English VersionAerospace series - Corrosion and heat resisting steel rivets -Technical specificationSérie aérospatiale - Rivets en acier résistant à chaud et àla corrosion - Spécification techniqueLuft- und Raumfahrt - Niete aus hochwarmfesten undkorrosionsbeständigen Stählen - TechnischeLieferbedingungenThis European Standard was approved by CEN on 12 December 2007.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 CEN 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 CEN Management Centre has the same status as theofficial versions.CEN members are the national standards bodies of Austria, Belgium, Bulgaria, 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© 2008 CENAll rights of exploitation in any form and by any means reservedworldwide for CEN national Members.Ref. No. EN 2898:2008: E



EN 2898:2008 (E) 2 Contents Page Foreword.3 1 Scope.4 2 Normative references.4 3 Terms and definitions.4 4 Required characteristics.5 5 Filing of documents.9 6 Certificate of conformity.9



EN 2898:2008 (E) 3 Foreword This document (EN 2898:2008) has been prepared by the Aerospace and Defence Industries Association of Europe - Standardization (ASD-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 ASD, 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 September 2008, and conflicting national standards shall be withdrawn at the latest by September 2008. 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 Regulations, the national standards organizations of the following countries are bound to implement this European Standard: Austria, Belgium, Bulgaria, 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 the United Kingdom.



EN 2898:2008 (E) 4 1 Scope This standard specifies the performance and test requirements for corrosion and heat resisting solid steel rivets intended for aerospace applications. It applies whenever it is specified in the document defining the rivet. Its use, after agreement between the customer and the supplier, for solid rivets made from other materials, requires determination, case by case, of the minimum tensile and double shear loads. 2 Normative references The following referenced documents are indispensable for the application of this document. For dated references, only the edition cited applies. For undated references, the latest edition of the referenced document (including any amendments) applies. ISO 2859-1, Sampling procedures for inspection by attributes — Part 1: Sampling schemes indexed by acceptance quality limit (AQL) for lot-by-lot inspection. EN 2002-001, Aerospace series — Metallic materials — Test methods — Part 001: Tensile testing at ambient temperature. EN 2002-7, Aerospace series — Metallic materials — Test methods — Part 7: Hardness test. 1) EN 2119, Aerospace series — Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15) — Solution treated and precipitation treated — Wires for rivets — 2 mm ≤ D ≤ 10 mm — Rm ≥ 960 MPa. 1) EN 2470, Steel FE-PA11 — Softened and cold drawn — Wires for rivets 1 mm ≤ D ≤ 10 mm — Aerospace series. 2) EN 3238, Aerospace series — Metallic materials — Test method — Shear test for wires and rivets. 3) 3 Terms and definitions For the purposes of this document, the following terms and definitions apply. 3.1 batch for all tests, inspections and supplies, a batch of rivets is defined as follows: finished rivets of the same form, diameter and length, manufactured by the same process, made from one material, batch from the same heat treatment furnace with the same surface treatment, and deriving from the same wire coil and the same place of manufacture The maximum mass of each batch is limited to 25 kg.
1) Published as ASD Prestandard at the date of publication of this standard. 2) Published as ASD Standard at the date of publication of this standard 3) In preparation at the date of publication of this standard.



EN 2898:2008 (E) 5 3.2 rivet wire samples for test, each rivet batch shall be accompanied by rivet wire samples taken from each end of the coil used to manufa
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