SIST EN 4710-006:2015

Aerospace series - Quick release fastening systems for non-structural applications - Part 006: Stud - quick-release and locking

This European Standard specifies the dimensions, mass, tolerances and static values of stud - quickrelease
and locking for use in fuselage interior equipment and non-structural or secondary structural
area.
This European Standard is to be used in conjunction with EN 4710-03, EN 4710-04, EN 4710-05 and
EN 4710-07 as described in EN 4710-02.
The applicable temperature range is -55 °C to 85 °C.

Luft- und Raumfahrt - Druckverschlüsse nicht-strukturelle Anwendungen - Teil 006: Bolzen - Schnell Auslösend und Schließend

Diese Europäische Norm legt die Maße, Massen, Toleranzen und statischen Werte von Bolzen, schnell auslösend und schließend fest, die bei der Inneneinrichtung von Luftfahrzeugen und in nicht strukturellen oder Sekun¬därstrukturbereichen verwendet werden.
Diese Europäische Norm ist in Verbindung mit EN 4710 03, EN 4710 04, EN 4710 05 und EN 4710 07 wie in EN 4710 02 beschrieben anzuwenden.
Der gültige Temperaturbereich ist zwischen −55 °C und 85 °C.

Série aérospatiale - Fixations rapides filetées pour applications non-structurales - Partie 006 : Pion à démontage et à verrouillage rapide

La présente Norme européenne spécifie les dimensions, la masse, les tolérances et les valeurs statiques des pions à démontage et à verrouillage rapide pour utilisation dans les équipements intérieurs et dans les zones non structurales ou structurales secondaires du fuselage.
La présente Norme européenne doit être utilisée conjointement avec les EN 4710-03, EN 4710-04, EN 4710-05 et EN 4710-07 comme décrit dans l’EN 4710 02.
La gamme de température applicable est comprise entre - 55 °C et 85 °C.

Aeronavtika - Spončni sistemi za hitro sprostitev za nestrukturne aplikacije - 006. del: Stojni vijak - hitro sproščanje in zapiranje

Ta evropski standard določa dimenzije, maso, tolerance in statične vrednosti stojnega vijaka za hitro sproščanje in zapiranje za uporabo v notranji opremi v trupu letala ter nestrukturnem ali sekundarnem strukturnem območju.
Ta evropski standard je treba uporabljati v povezavi s standardi EN 4710-03, EN 4710-04, EN 4710-05 in
EN 4710-07, kot je opisano v standardu EN 4710-02. Delovna temperatura je med –55 °C in 85 °C.

General Information

• Status: Published
• Publication Date: 08-Nov-2015
• ICS: 49.030.20 - Bolts, screws, studs
• Technical Committee: I13 - Imaginarni 13
• Current Stage: 6060 - National Implementation/Publication (Adopted Project)
• Start Date: 29-Oct-2015
• Due Date: 03-Jan-2016
• Completion Date: 09-Nov-2015
• Ref Project: EN 4710-06:2015 - Aerospace series - Quick release fastening systems for non-structural applications - Part 06: Stud - quick-release and locking

Standards Content (Sample)

2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.Luft- und Raumfahrt - Druckverschlüsse nicht-strukturelle Anwendungen - Teil 006: Bolzen - Schnell Auslösend und SchließendSérie aérospatiale - Fixations rapides filetées pour applications non-structurales - Partie 006 : Pion à démontage et à verrouillage rapideAerospace series - Quick release fastening systems for non-structural applications - Part 006: Stud - quick-release and locking49.030.20Sorniki, vijaki, stebelni vijakiBolts, screws, studsICS:Ta slovenski standard je istoveten z:EN 4710-06:2015SIST EN 4710-006:2015en,fr,de01-december-2015SIST EN 4710-006:2015SLOVENSKI
STANDARD



SIST EN 4710-006:2015



EUROPEAN STANDARD NORME EUROPÉENNE EUROPÄISCHE NORM
EN 4710-06
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 xã Stud æ quickærelease and locking Sßrie aßrospatiale æ Fixations rapides filetßes pour applications nonæstructurales æ Partie
r x ã Pion à dßmontage et à verrouillage rapide
Luftæ und Raumfahrt æ Schnellverschlüsse für nichtæstrukturelle Anwendungen æ Teil
r xã Bolzen æ Schnell auslösend und schließend 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
EUROPEAN COMMITTEE FOR STANDARDIZATION COMITÉ EUROPÉEN DE NORMALISATION EUROPÄISCHES KOMITEE FÜR NORMUNG
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 xã t r s w ESIST EN 4710-006:2015



EN 4710-06:2015 (E) 2 Contents
Page European foreword . 3 1 Scope . 4 2 Normative references . 4 3 Requirements . 5 4 Designation. 8 5 Marking . 9 6 Technical specification . 9
SIST EN 4710-006:2015



EN 4710-06:2015 (E) 3 European foreword This document (EN 4710-06:2015) 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 4710-006:2015



EN 4710-06:2015 (E) 4 1 Scope This European Standard specifies the dimensions, mass, tolerances and static values of stud - quick-release and locking for use in fuselage interior equipment and non-structural or secondary structural area.
This European Standard is to be used in conjunction with EN 4710-03, EN 4710-04, EN 4710-05 and EN 4710-07 as described in EN 4710-02. The applicable temperature range is -55 °C to 85 °C. 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
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