BS EN 4136-2009 Aerospace series - Bolts normal bi-hexagonal head coarse tolerance normal shank long thread in alloy steel cadmium plated - Classification 1100 MPa (at ambient temp.pdf
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1、BS EN 4136:2009ICS 49.030.20NO COPYING WITHOUT BSI PERMISSION EXCEPT AS PERMITTED BY COPYRIGHT LAWBRITISH STANDARDAerospace series Bolts, normal bi-hexagonal head, coarse tolerance normal shank, long thread, in alloy steel, cadmium plated Classification: 1 100 MPa (at ambient temperature) / 235 null
2、CIncorporatingcorrigendumSeptember 2010 National forewordThis British Standard is the UK implementation of EN 4136:2009, incorporating corrigendum September 2010.The UK participation in its preparation was entrusted to Technical Committee ACE/12, Aerospace fasteners and fastening systems.A list of o
3、rganizations represented on this committee can be obtained on request to its secretary.This publication does not purport to include all the necessary provisions of a contract. Users are responsible for its correct application.Compliance with a British Standard cannot confer immunity from legal oblig
4、ations.BS EN 4136:2009This British Standardwas published under theauthority of the StandardsPolicy and StrategyCommittee on 31 July 2009 BSI 2010Amendments/corrigenda issued since publicationDate Comments 30 November 2010 Implementation of CEN corrigendum September 2010. Correction to row 1, column
5、4 of Table 1ISBN 978 0 580 73074 0EUROPEAN STANDARD NORME EUROPENNE EUROPISCHE NORM EN 4136 July 2009 ICS 49.030.30 English Version Aerospace series - Bolts, normal bi-hexagonal head, coarse tolerance normal shank, long thread, in alloy steel, cadmium plated - Classification: 1 100 MPa (at ambient t
6、emperature) / 235 C Srie arospatiale - Vis tte bihexagonale normale, tige normale tolrance large, filetage long, en acier alli, cadmies - Classification: 1 100 MPa ( temprature ambiante) / 235 C Luft- und Raumfahrt - Zwlfkantschrauben, langes Gewinde, aus legiertem Stahl, verkadmet - Klasse: 1 100 M
7、Pa (bei Raumtemperatur) / 235 C This European Standard was approved by CEN on 6 June 2009. CEN members are bound to comply with the CEN/CENELEC Internal Regulations which stipulate the conditions for giving this European Standard the status of a national standard without any alteration. Up-to-date l
8、ists and bibliographical references concerning such national standards 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 translation under the r
9、esponsibility of a CEN member into its own language and notified to the CEN Management Centre has the same status as the official versions. CEN members are the national standards bodies of Austria, Belgium, Bulgaria, Cyprus, Czech Republic, Denmark, Estonia, Finland, France, Germany, Greece, Hungary
10、, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Romania, Slovakia, Slovenia, Spain, Sweden, Switzerland and United Kingdom. EUROPEAN COMMITTEE FOR STANDARDIZATION COMIT EUROPEN DE NORMALISATION EUROPISCHES KOMITEE FR NORMUNG Management Centre:
11、Avenue Marnix 17, B-1000 Brussels 2009 CEN All rights of exploitation in any form and by any means reserved worldwide for CEN national Members. Ref. No. EN 4136:2009: EIncorporating corrigendum September 2010EN 4136:2009 (E) 2 Contents Page Foreword 3 1 Scope 4 2 Normative references 4 3 Required ch
12、aracteristics .5 4 Designation 7 5 Marking .7 6 Technical specification .7 BS EN 4136:2009EN 4136:2009 (E) 3 Foreword This document (EN 4136:2009) has been prepared by the Aerospace and Defence Industries Association of Europe - Standardization (ASD-STAN). After enquiries and votes carried out in ac
13、cordance 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
14、 of an identical text or by endorsement, at the latest by January 2010, and conflicting national standards shall be withdrawn at the latest by January 2010. 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
15、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, Estoni
16、a, 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. BS EN 4136:2009EN 4136:2009 (E) 4 1 Scope This standard specifies the ch
17、aracteristics of bolts, normal bi-hexagonal head, coarse tolerance normal shank, long thread, in alloy steel, cadmium plated. Classification: 1 100 MPa 1) / 235 C 2)2 Normative references The following referenced documents are indispensable for the application of this document. For dated references,
18、 only the edition cited applies. For undated references, the latest edition of the referenced document (including any amendments) applies. EN 2133, Aerospace series Cadmium plating of steels with specified tensile strength 1 450 MPa, copper, copper alloys and nickel alloys. EN 2137, Steel FE-PL75 1
19、100 MPa Rm 1 250 MPa Bars De 100 mm Aerospace series.3)EN 2424, Aerospace series Marking of aerospace products. EN 2442 4), Steel FE-PL711 1 100 MPa Rm 1 300 MPa Bars and wires De 25 mm Aerospace series. 3)EN 3514, Aerospace series Steel FE-PL711 Hardened and tempered 1 100 Rm 1 300 MPa Bar and wire
20、 for bolts De 25 mm. 5)EN 9100, Aerospace series Quality management systems Requirements (based on ISO 9001:2000) and Quality systems Model for quality assurance in design, development, production, installation and servicing (based on ISO 9001:1994). EN 9133, Aerospace series Quality management syst
21、ems Qualification procedure for aerospace standard parts. ISO 3203, Aerospace Bolts, normal bihexagonal head, normal or pitch diameter shank, long length MJ threads, metallic material, coated or uncoated, strength classes less than or equal to 1 100 MPa Dimensions. ISO 3353-1, Aerospace Lead and run
22、out threads Part 1: Rolled external threads. ISO 4095, Aerospace Bihexagonal drives Wrenching configuration Metric series. ISO 5855-2, Aerospace MJ threads Part 2: Limit dimensions for bolts and nuts. ISO 7689, Aerospace Bolts, with MJ threads, made of alloy steel, strength class 1 100 MPa Procureme
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