SIST EN 4135:2009

Aerospace series - Bolts, normal bi-hexagonal head, coarse tolerance normal shank, medium length thread, in titanium alloy, anodized, MoS2 lubricated - Classification: 1100 MPa (at ambient temperature)/315 °C

SIST EN 4135:2009

Name:SIST EN 4135:2009   Standard name:Aerospace series - Bolts, normal bi-hexagonal head, coarse tolerance normal shank, medium length thread, in titanium alloy, anodized, MoS2 lubricated - Classification: 1100 MPa (at ambient temperature)/315 °C
Standard number:SIST EN 4135:2009   language:English language
Release Date:20-Aug-2009   technical committee:I13 - Imaginarni 13
Drafting committee:   ICS number:49.030.20 - Bolts, screws, studs
SLOVENSKI STANDARD
SIST EN 4135:2009
01-oktober-2009
Aeronavtika - Sorniki, normalna dvanajstroba glava, široka toleranca, srednja
navojna dolžina, iz titanove zlitine, anodizirani, namazani z MoS2 - Klasifikacija:
1100 MPa (pri temperaturi okolice)/315 °C
Aerospace series - Bolts, normal bi-hexagonal head, coarse tolerance normal shank,
medium length thread, in titanium alloy, anodized, MoS2 lubricated - Classification: 1100
MPa (at ambient temperature)/315 °C
Luft- und Raumfahrt - Zwölfkantschrauben, mittlere Gewindelänge, aus Titanlegierung,
anodisiert, MoS2-geschmiert - Klasse: 1100 MPa (bei Raumtemperatur)/315 °C
Série aérospatiale - Vis à tête bihexagonale normale, tige normale à tolérance large,
filetage moyen, en alliage de titane, anodisées, lubrifiées MoS2 - Classification: 1100
MPa (à température ambiante)/315 °C
Ta slovenski standard je istoveten z: EN 4135:2009
ICS:
49.030.20 Sorniki, vijaki, stebelni vijaki Bolts, screws, studs
SIST EN 4135:2009 en,de
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.

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SIST EN 4135:2009

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SIST EN 4135:2009


EUROPEAN STANDARD
EN 4135

NORME EUROPÉENNE

EUROPÄISCHE NORM
July 2009
ICS 49.030.20
English Version
Aerospace series - Bolts, normal bi-hexagonal head, coarse
tolerance normal shank, medium length thread, in titanium alloy,
anodized, MoS2 lubricated - Classification: 1 100 MPa (at
ambient temperature) / 315 °C
Série aérospatiale - Vis à tête bihexagonale normale, tige Luft- und Raumfahrt - Zwölfkantschrauben, mittlere
normale à tolérance large, filetage moyen, en alliage de Gewindelänge, aus Titanlegierung, anodisiert, MoS2-
titane, anodisées, lubrifiées MoS2 - Classification : 1 100 geschmiert - Klasse: 1 100 MPa (bei Raumtemperatur) /
MPa (à température ambiante) / 315 °C 315 °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 lists 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 responsibility 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, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal,
Romania, Slovakia, Slovenia, Spain, Sweden, Switzerland and United Kingdom.






EUROPEAN COMMITTEE FOR STANDARDIZATION
COMITÉ EUROPÉEN DE NORMALISATION

EUROPÄISCHES KOMITEE FÜR NORMUNG

Management Centre: Avenue Marnix 17, B-1000 Brussels
© 2009 CEN All rights of exploitation in any form and by any means reserved Ref. No. EN 4135:2009: E
worldwide for CEN national Members.

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SIST EN 4135:2009
EN 4135:2009 (E)
Contents Page
Foreword .3
1 Scope .4
2 Normative references .4
3 Required characteristics .4
4 Designation .7
5 Marking .7
6 Technical specification .7

2

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SIST EN 4135:2009
EN 4135:2009 (E)
Foreword
This document (EN 4135:2009) 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 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 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, Ma
...

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