Aerospace series - Bolts, double hexagon head, relieved shank, long thread, in titanium alloy TI-P64001, MoS2 coated - Strength Class: 1 100 MPa (at ambient temperature)

This standard specifies the characteristics of double hexagon headed bolts with relieved shank and long thread in TI-P64001, MoS2 coated, for aerospace applications.
Strength class: 1 100 MPa

Luft- und Raumfahrt - Zwölfkantschrauben, Dünnschaft, langes Gewinde, aus Titanlegierung TI-P64001, MoS2-beschichtet - Festigkeitsklasse: 1 100 MPa (bei Raumtemperatur)

Série aérospatiale - Vis à tête bihexagonale, fût dégagé, filetage long, en alliage de titane TI-P64001, revêtues MoS2 - Classe de résistance : 1 100 MPa (à température ambiante)

Aerospace series - Bolts, double hexagon head, relieved shank, long thread, in titanium alloy TI-P64001, MoS2 coated - Strength Class: 1 100 MPa (at ambient temperature)

General Information

Status
Published
Publication Date
09-Nov-2004
Withdrawal Date
30-May-2005
Technical Committee
Drafting Committee
Current Stage
9093 - Decision to confirm - Review Enquiry
Completion Date
30-Jun-2017

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SLOVENSKI STANDARD
SIST EN 3724:2005
01-junij-2005
1DGRPHãþD
SIST EN 3724:2004
Aerospace series - Bolts, double hexagon head, relieved shank, long thread, in
titanium alloy TI-P64001, MoS2 coated - Strength Class: 1 100 MPa (at ambient
temperature)
Aerospace series - Bolts, double hexagon head, relieved shank, long thread, in titanium
alloy TI-P64001, MoS2 coated - Strength Class: 1 100 MPa (at ambient temperature)
Luft- und Raumfahrt - Zwölfkantschrauben, Dünnschaft, langes Gewinde, aus
Titanlegierung TI-P64001, MoS2-beschichtet - Festigkeitsklasse: 1 100 MPa (bei
Raumtemperatur)
Série aérospatiale - Vis a tete bihexagonale, fut dégagé, filetage long, en alliage de
titane TI-P64001, revetues MoS2 - Classe de résistance : 1 100 MPa (a température
ambiante)
Ta slovenski standard je istoveten z: EN 3724:2004
ICS:
49.030.20 Sorniki, vijaki, stebelni vijaki Bolts, screws, studs
SIST EN 3724:2005 en
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.

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SIST EN 3724:2005

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SIST EN 3724:2005



EUROPEAN STANDARD
EN 3724

NORME EUROPÉENNE

EUROPÄISCHE NORM
November 2004
ICS 49.030.20 Supersedes EN 3724:2003
English version
Aerospace series - Bolts, double hexagon head, relieved shank,
long thread, in titanium alloy TI-P64001, MoS2 coated - Strength
Class: 1 100 MPa (at ambient temperature)
Série aérospatiale - Vis à tête bihexagonale, fût dégagé, Luft- und Raumfahrt - Zwölfkantschrauben, Dünnschaft,
filetage long, en alliage de titane TI-P64001, revêtues langes Gewinde, aus Titanlegierung TI-P64001, MoS2-
MoS2 - Classe de résistance : 1 100 MPa (à température beschichtet - Festigkeitsklasse: 1 100 MPa (bei
ambiante) Raumtemperatur)
This European Standard was approved by CEN on 11 September 2003.

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 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 translation
under the responsibility of a CEN member into its own language and notified to the Central Secretariat has the same status as the official
versions.

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 STANDARDIZATION
COMITÉ EUROPÉEN DE NORMALISATION

EUROPÄISCHES KOMITEE FÜR NORMUNG

Management Centre: rue de Stassart, 36  B-1050 Brussels
© 2004 CEN All rights of exploitation in any form and by any means reserved Ref. No. EN 3724:2004: E
worldwide for CEN national Members.

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SIST EN 3724:2005

EN 3724:2004 (E)
Contents                                                                       Page

Foreword.3
1 Scope .4
2 Normative references .4
3 Required characteristics.4
4 Designation .8
5 Marking .8
6 Technical specification .8
2

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SIST EN 3724:2005
EN 3724:2004 (E)
Foreword
This document (EN 3724:2004) has been prepared by the European Association of Aerospace
Manufacturers - Standardization (AECMA-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 Se
...

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