EN 4323:2004

Aerospace series - Screws, 100° countersunk head, six lobe recess, threaded to head, in titanium alloy TI-P64001, anodized, MoS2 coated - Classification: 900 MPa (at ambient temperature) / 350 °C

This standard specifies the characteristics of screws with 100° countersunk head with six lobe recess, threaded to head, in TI-P64001, anodized, MoS2 coated, for aerospace applications.
Classification: 900 MPa  ) / 350 °C  )

Luft- und Raumfahrt - 100° -Senkschrauben, Sechs-Bogenzahn, Gewinde bis Kopf, aus Titanlegierung TI-P64001, anodisiert, MoS2-beschichtet - Klasse: 900 MPa (bei Raumtemperatur)/350 °C

Diese Norm legt die Eigenschaften von Schrauben mit 100° Senkkopf, Sechs Bogenzahn-Innenantrieb und Gewinde bis Kopf, aus TI P64001, anodisiert, MoS2-beschichtet, für Anwendungen in der Luft- und Raumfahrt fest.
Klasse: 900 MPa )/350 °C )

Série aérospatiale - Vis à tête fraisée 100°, à empreinte six lobes, filetées sous tête, en alliage de titane TI-P64001, anodisées, revêtues MoS2 - Classification : 900 MPa (à température ambiante) / 350 °C

Aerospace series - Screws, 100° countersunk head, six lobe recess, threaded to head, in titanium alloy TI-P64001, anodized, MoS2 coated - Classification: 900 MPa (at ambient temperature) / 350 °C

General Information

• Status: Published
• Publication Date: 09-Nov-2004
• Withdrawal Date: 30-May-2005
• ICS: 49.030.20 - Bolts, screws, studs
• Technical Committee: ASD-STAN - Aerospace
• Drafting Committee: ASD-STAN/D 3 - Mechanical
• Current Stage: 9093 - Decision to confirm - Review Enquiry
• Completion Date: 30-Jun-2017
• Ref Project: SIST EN 4323:2005 - Aerospace series - Screws, 100° countersunk head, six lobe recess, threaded to head, in titanium alloy TI-P64001, anodized, MoS2 coated - Classification: 900 MPa (at ambient temperature) / 350 °C

Relations

• Replaces: EN 4323:2003 - Aerospace series - Screws, 100° countersunk head, six lobe recess, threaded to head, in titanium alloy TI-P64001, anodized, MoS2 coated - Classification: 900 MPa (at ambient temperature)/350 °C
• Effective Date: 22-Dec-2008

Standards Content (Sample)

SLOVENSKI STANDARD
01-junij-2005
1DGRPHãþD
SIST EN 4323:2004
Aerospace series - Screws, 100° countersunk head, six lobe recess, threaded to
head, in titanium alloy TI-P64001, anodized, MoS2 coated - Classification: 900 MPa
(at ambient temperature) / 350 °C
Aerospace series - Screws, 100° countersunk head, six lobe recess, threaded to head, in
titanium alloy TI-P64001, anodized, MoS2 coated - Classification: 900 MPa (at ambient
temperature) / 350 °C
Luft- und Raumfahrt - 100° -Senkschrauben, Sechs-Bogenzahn, Gewinde bis Kopf, aus
Titanlegierung TI-P64001, anodisiert, MoS2-beschichtet - Klasse: 900 MPa (bei
Raumtemperatur)/350 °C
Série aérospatiale - Vis a tete fraisée 100°, a empreinte six lobes, filetées sous tete, en
alliage de titane TI-P64001, anodisées, revetues MoS2 - Classification : 900 MPa (a
température ambiante) / 350 °C
Ta slovenski standard je istoveten z: EN 4323:2004
ICS:
49.030.20 Sorniki, vijaki, stebelni vijaki Bolts, screws, studs
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.

EUROPEAN STANDARD
EN 4323
NORME EUROPÉENNE
EUROPÄISCHE NORM
November 2004
ICS 49.030.20 Supersedes EN 4323:2003
English version
Aerospace series - Screws, 100° countersunk head, six lobe
recess, threaded to head, in titanium alloy TI-P64001, anodized,
MoS2 coated - Classification: 900 MPa (at ambient temperature)
/ 350° C
Série aérospatiale - Vis à tête fraisée 100° , à empreinte Luft- und Raumfahrt – 100° Senkschrauben, Sechs-
six lobes, filetées sous tête, en alliage de titane TI-P64001, Bogenzahn, Gewinde bis Kopf, aus Titanlegierung TI-
anodisées, revêtues MoS2 - Classification : 900 MPa (à P64001, anodisiert, MoS2 beschichtet - Klasse: 900 MPa
température ambiante) / 350° C (bei Raumtemperatur) / 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
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© 2004 CEN All rights of exploitation in any form and by any means reserved Ref. No. EN 4323:2004: E
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Contents                                                                   Page

Foreword.3
1 Scope .4
2 Normative references .4
3 Required characteristics.4
3.1 Configuration – Dimensions – Tolerances – Masses .4
3.2 Materials .4
3.3 Surface treatment .4
4 Designation .7
5 Marking .7
6 Technical specifications .7
Foreword
This document (EN 4323:2004) 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 Services of the member countries of
AECMA, prior to its presentation to CEN.
This European Standard shall be given the status of a national standard, either by publication of an
...