SIST EN 4710-001:2015

2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.Luft- und Raumfahrt - Druckverschlüsse nicht-strukturelle Anwendungen - Teil 001: Technische LieferbedingungenSérie aérospatiale - Fixations rapides filetées pour applications non-structurales - Partie 001 : Spécification techniqueAerospace series - Quick release fastening systems for non-structural applications - Part 001: Technical specification49.030.01Vezni elementi na splošnoFasteners in generalICS:Ta slovenski standard je istoveten z:EN 4710-01:2015SIST EN 4710-001:2015en,fr,de01-december-2015SIST EN 4710-001:2015SLOVENSKI
STANDARD



SIST EN 4710-001:2015



EUROPEAN STANDARD NORME EUROPÉENNE EUROPÄISCHE NORM
EN 4710-01
October
t r s w ICS
v {ä r u w English Version
Aerospace series æ Quick release fastening systems for nonæstructural applications æ Part
r sã Technical specification Série aérospatiale æ Fixations rapides filetées pour applications nonæstructurales æ Partie
r s ã Spécification technique
Luftæ und Raumfahrt æ Schnellverschlüsse für nichtæstrukturelle Anwendungen æ Teil
r sã Technische Lieferbedingungen This European Standard was approved by CEN on
w March
t r s wä
egulations which stipulate the conditions for giving this European Standard the status of a national standard without any alterationä Upætoædate lists and bibliographical references concerning such national standards may be obtained on application to the CENæCENELEC Management Centre or to any CEN memberä
translation under the responsibility of a CEN member into its own language and notified to the CENæCENELEC Management Centre has the same status as the official versionsä
CEN members are the national standards bodies of Austriaá Belgiumá Bulgariaá Croatiaá Cyprusá Czech Republicá Denmarká Estoniaá Finlandá Former Yugoslav Republic of Macedoniaá Franceá Germanyá Greeceá Hungaryá Icelandá Irelandá Italyá Latviaá Lithuaniaá Luxembourgá Maltaá Netherlandsá Norwayá Polandá Portugalá Romaniaá Slovakiaá Sloveniaá Spainá Swedená Switzerlandá Turkey and United Kingdomä
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CEN-CENELEC Management Centre:
Avenue Marnix 17,
B-1000 Brussels
9
t r s w CEN All rights of exploitation in any form and by any means reserved worldwide for CEN national Membersä Refä Noä EN
v y s ræ r sã t r s w ESIST EN 4710-001:2015



EN 4710-01:2015 (E) 2 Contents
Page European foreword . 3 1 Scope . 4 2 Normative references . 4 3 Terms and definitions . 4 4 Requirements . 5 5 Inspections and tests . 5 6 Test equipment and parameters . 9 7 Quality assurance . 10 8 Sampling . 10
SIST EN 4710-001:2015



EN 4710-01:2015 (E) 3 European foreword This document (EN 4710-01:2015) 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 European 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 April 2016, and conflicting national standards shall be withdrawn at the latest by April 2016. 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, Croatia, Cyprus, Czech Republic, Denmark, Estonia, Finland, Former Yugoslav Republic of Macedonia, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Romania, Slovakia, Slovenia, Spain, Sweden, Switzerland, Turkey and the United Kingdom. SIST EN 4710-001:2015



EN 4710-01:2015 (E) 4 1 Scope This European Standard specifies the required characteristics, inspections, tests, quality assurance requirements, conditions for qualification acceptance and delivery of quick release fastening systems.
This European Standard applies to all fastening systems for use in fuselage interior equipment and non-structural or secondary structural area. It may be applied when referred to in the product standard or in a design specification. 2 Normative references The following documents, in whole or in part, are normatively referenced in this document and are indispensable for its application. For dated references, only the edition cited applies. For undated references, the latest edition of the referenced document (including any amendments) applies. EN 2424, Aerospace series — Marking of aerospace products EN 2826, Aerospace series — Burning behaviour of non metallic materials under the influence of radiating heat and flames — Determination of gas components in the smoke EN 3844-2, Aerospace series — Flammability of non metallic materials — Part 2: Small burner test, horizontal — Determination of the horizontal flame propagation EN 9100, Quality Management Systems — Requirements for Aviation, Space and Defense Organizations
EN 9102:2006, Aerospace series — Quality systems — First article inspection EN 9133, Aerospace series — Quality management systems — Qualification procedure for aerospace standard parts EN 10204, Metallic products — Types of inspection documents EN ISO 8785, Geometrical product specification (GPS) — Surface imperfections — Terms, definitions and parameters (ISO 8785) EN ISO 9001, Quality management systems — Requirements (ISO 9001) EN ISO 9227, Corrosion tests in artificial atmospheres — Salt spray tests (ISO 9227) FAR/JAR/CS 25.853, Compartment Interiors 1) 3 Terms and definitions For the purposes of this document, the following terms and definitions apply. 3.1 fasteners quick release fastening systems are parts, capable of being easily and quickly operated, with or without usage of special tools for closing and opening, for fastening and release of parts such as covers, linings, equipment, etc.
1) Published by: European Aviation Safety Agency, Postfach 101253, D-50452 Koeln, Germany. SIST EN 4710-001:2015



EN 4710-01:2015 (E) 5 3.2 lot finished parts of the same dimensions, made from the same material, produced in the same production run, heat treated and surface protected in the same manner and submitted for testing at the same time 3.3 qualification test a test or series of tests to demonstrate that the products comply with the requirements stipulated in this specification and/or in a product standard and are accomplished according to documented parameters and under reproducible conditions 3.4 acceptance test a test or series of tests to demonstrate that the characteristics of manufactured products comply with the requirements 3.5 first article inspection FAI complete, independent, and documented physical and functional inspection process to verify that prescribed production methods have produced an acceptable item as specified by engineering drawings, planning, purchase order, engineering specifications, and/or other applicable design documents [SOURCE: EN 9102:2006, 3.5] 3.6 tolerance compensation ability of the spring clamp to cover assembly and installation tolerances 4 Requirements See Table 1, if not specified in the relevant product standard. 5 Inspections and tests 5.1 Qualification test All product qualification activities shall be carried out in accordance with a Qualification Test Program prepared by the manufacturer and approved by the
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