SIST EN 4176:2006

2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.DOXPLQLMHPLuft- und Raumfahrt - Paßniete, mit 100° normalem Senkkopf oder Universalkopf, Zug-/Schertyp, aus Titanlegierung TI-P64001, anodisiert oder mit aluminiumpigmentierter Beschichtung - Ringe aus Titan TI-P99002 oder Aluminiumlegierung 2024 - Metrische Reihe - Technische LieferbedingungSérie aérospatiale - Rivets a bague sertie, a tete fraisée 100° normale ou a tete cylindrique, a traction ou a cisaillement, a tolérance serrée, en alliage de titane TI-P64001, anodisés ou avec revetement alumino-organique - Bagues en titane TI-P99002 ou en alliage d'aluminium 2024 - Série métrique - Spécification techniqueAerospace series - Lockbolts, 100° countersunk normal head or protruding head, tension- / sheartype, close tolerance, in titanium alloy TI-P64001, anodized or with aluminium pigmented coating - Collars in titanium TI-P99002 or aluminium alloy 2024 - Metric series - Technical specification49.030.20Sorniki, vijaki, stebelni vijakiBolts, screws, studs49.025.30TitanTitanium49.025.20AluminijAluminiumICS:Ta slovenski standard je istoveten z:EN 4176:2005SIST EN 4176:2006en01-september-2006SIST EN 4176:2006SLOVENSKI
STANDARD
EUROPEAN STANDARDNORME EUROPÉENNEEUROPÄISCHE NORMEN 4176December 2005ICS 49.030.20 English VersionAerospace series - Lockbolts, 100
countersunk normal head orprotruding head, tension- / sheartype, close tolerance, intitanium alloy TI-P64001, anodized or with aluminium pigmentedcoating - Collars in titanium TI-P99002 or aluminium alloy 2024 -Metric series - Technical specificationSérie aérospatiale - Rivets à bague sertie, à tête fraisée100
normale ou à tête cylindrique, à traction ou àcisaillement, à tolérance serrée, en alliage de titane TI-P64001, anodisés ou avec revêtement alumino-organique -Bagues en titane TI-P99002 ou en alliage d'aluminium2024 - Série métrique - Spécification techniqueLuft- und Raumfahrt - Paßniete, mit 100
normalemSenkkopf oder Universalkopf, Zug- Schertyp, ausTitanlegierung TI-P64001, anodisiert oder mit Aluminiumpigmentierter Beschichtung - Ringe aus Titan TI-P99002oder Aluminiumlegierung 2024 - Metrische Reihe -Technische LieferbedingungThis European Standard was approved by CEN on 26 October 2005.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, 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© 2005 CENAll rights of exploitation in any form and by any means reservedworldwide for CEN national Members.Ref. No. EN 4176:2005: ESIST EN 4176:2006

1) Published as AECMA Prestandard at the date of publication of this standard. 2) Published by: American Society of Mechanical Engineers (ASME), 3, Park Avenue, New York, NY 10017, USA. 3) Published by: Department of Defense (DOD), the Pentagon, Washington, DC 20301, USA. 4) Published by: Aerospace Industries Association of America, Inc. (AIA), 1250 Eye Street, NW; Suite 1100, Washington, DC 20005, USA. SIST EN 4176:2006

Design and construction Conventional measuring methods Table 5 of MIL-STD-19165.1.1.1
Head protrusion (100° countersunk head) In accordance with the standard part drawings referenced within this specification NAS 527
NAS 527 5.1.2
Material Titanium alloy TI-P64001 (6Al-4V) – shear strength ≥ 675 MPa – Composition requirements apply to finished lockbolts. As described by lockbolt manufacturer to assure production parts conform to applicable specifications 5.1.2.1
Lubricant In accordance with standard part drawings reference this specification. See applicable specification Visual examination
Table 6 5.1.3
Dimensions Q 5.1.3.1
General dimensions Conventional measuring methods MIL-STD-19165.1.3.2
Surface texture The dimensions and any deviations in form and position, measured at ambient temperature, shall be within the limits specified in the definition document. B46.1 Visual examination A Table 4 5.1.4
Protective treatment 5.1.4.1
Finish In accordance with standard part drawings reference this specification. See applicable specification Visual examination
Table 6 qualification 5.1.5
Manufacturing 5.1.5.1
Heat treatment Shall develop mechanical properties as defined herein, without adverse effect on metallurgical properties as defined herein. Test of shear and metallurgical properties verifies heat treatment.
As applicable in accordance with test requirementsQ 5.1.6
Mechanical properties 5.1.6.1
Tensile strength Table 3 values are applicable to lockbolts having
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