EN 3907:2004
(Main)Aerospace series - Bolts, double hexagon head, normal shank, long thread, in titanium alloy TI-P64001, MoS2 coated - Classification: 1 100 MPa (at ambient temperature) / 350 °C
Aerospace series - Bolts, double hexagon head, normal shank, long thread, in titanium alloy TI-P64001, MoS2 coated - Classification: 1 100 MPa (at ambient temperature) / 350 °C
This standard specifies the characteristics of double hexagon headed bolts with normal shank and long thread in titanium alloy TI-P63, MoS2 coated for aerospace applications.
Classification: 1 100 MPa ) / 350 °C
Luft- und Raumfahrt - Zwölfkantschrauben, langes Gewinde, aus Titanlegierung TI-P64001, MoS2 beschichtet - Klasse: 1 100 MPa (bei Raumtemperatur) / 350 °C
Diese Norm legt die Eigenschaften von Zwölfkantschrauben mit langem Gewinde, aus Titanlegierung TI P64001, MoS2-beschichtet, für Anwendungen in der Luft- und Raumfahrt fest.
Klasse: 1 100 MPa )/350 °C ).
Série aérospatiale - Vis à tête bihexagonale, fût normal, filetage long, en alliage de titane TI-P64001, revêtues MoS2 - Classification : 1 100 MPa (à température ambiante) / 350 °C
Aerospace series - Bolts, double hexagon head, normal shank, long thread, in titanium alloy TI-P64001, MoS2 coated - Classification: 1 100 MPa (at ambient temperature) / 350 °C
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Standards Content (Sample)
SLOVENSKI STANDARD
SIST EN 3907:2005
01-junij-2005
1DGRPHãþD
SIST EN 3907:2004
Aerospace series - Bolts, double hexagon head, normal shank, long thread, in
titanium alloy TI-P64001, MoS2 coated - Classification: 1 100 MPa (at ambient
temperature) / 350 °C
Aerospace series - Bolts, double hexagon head, normal shank, long thread, in titanium
alloy TI-P64001, MoS2 coated - Classification: 1 100 MPa (at ambient temperature) / 350
°C
Luft- und Raumfahrt - Zwölfkantschrauben, langes Gewinde, aus Titanlegierung TI-
P64001, MoS2 beschichtet - Klasse: 1 100 MPa (bei Raumtemperatur) / 350 °C
Série aérospatiale - Vis a tete bihexagonale, fut normal, filetage long, en alliage de titane
TI-P64001, revetues MoS2 - Classification : 1 100 MPa (a température ambiante) / 350 °
C
Ta slovenski standard je istoveten z: EN 3907:2004
ICS:
49.030.20 Sorniki, vijaki, stebelni vijaki Bolts, screws, studs
SIST EN 3907:2005 en
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.
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SIST EN 3907:2005
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SIST EN 3907:2005
EUROPEAN STANDARD
EN 3907
NORME EUROPÉENNE
EUROPÄISCHE NORM
November 2004
ICS 49.030.20 Supersedes EN 3907:2003
English version
Aerospace series - Bolts, double hexagon head, normal shank,
long thread, in titanium alloy TI-P64001, MoS2 coated -
Classification: 1 100 MPa (at ambient temperature) / 350° C
Série aérospatiale - Vis à tête bihexagonale, fût normal, Luft- und Raumfahrt - Zwölfkantschrauben, langes
filetage long, en alliage de titane TI-P64001, revêtues Gewinde, aus Titanlegierung TI-P64001, MoS2-beschichtet
MoS2 - Classification : 1 100 MPa (à température - Klasse: 1 100 MPa (bei Raumtemperatur) / 350° C
ambiante) / 350° C
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,
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© 2004 CEN All rights of exploitation in any form and by any means reserved Ref. No. EN 3907:2004: E
worldwide for CEN national Members.
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SIST EN 3907:2005
EN 3907:2004 (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 3907:2005
EN 3907:2004 (E)
Foreword
This document (EN 3907:2004) 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
...
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