General Information

Abstract

This European Standard specifies the characteristics of screws, pan head, six lobe recess, coarse tolerance normal shank, medium length thread, in titanium alloy, anodized, MoS2 lubricated.
Classification : 1 100 MPa / 315 °C.

Status
Withdrawn
Publication Date
17-Nov-2009
Withdrawal Date
22-Sep-2026
Technical Committee
ASD-STAN - Aerospace
Drafting Committee
ASD-STAN/D 3 - Mechanical
Current Stage
9093 - Decision to confirm - Review Enquiry
Start Date
30-Jun-2017
Completion Date
23-Sep-2026

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Effective Date
06-Feb-2013
Effective Date
25-Aug-2026
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25-Aug-2026
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Effective Date
28-Jan-2026
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28-Jan-2026
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28-Jan-2026
Effective Date
28-Jan-2026
Effective Date
28-Jan-2026
Effective Date
28-Jan-2026

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Frequently Asked Questions

EN 4178:2009 is a standard published by the European Committee for Standardization (CEN). Its full title is "Aerospace series - Screws, pan head, six lobe recess, coarse tolerance normal shank, medium length thread, in titanium alloy, anodized, MoS2 lubricated - 1 100 MPa (at ambient temperature) / 315 °C". This standard covers: This European Standard specifies the characteristics of screws, pan head, six lobe recess, coarse tolerance normal shank, medium length thread, in titanium alloy, anodized, MoS2 lubricated. Classification : 1 100 MPa / 315 °C.

This European Standard specifies the characteristics of screws, pan head, six lobe recess, coarse tolerance normal shank, medium length thread, in titanium alloy, anodized, MoS2 lubricated. Classification : 1 100 MPa / 315 °C.

EN 4178:2009 is classified under the following ICS (International Classification for Standards) categories: 49.030.10 - Screw threads. The ICS classification helps identify the subject area and facilitates finding related standards.

EN 4178:2009 has the following relationships with other standards: It is inter standard links to EN 4178:2017, ISO 5855-2:1999, ISO 9152:1998, ISO 7913:1994, ISO 3353-1:2002, EN 2424:2008, EN 9133:2018, EN 2491:2011, EN 3911:2010, EN 9100:2018, EN 840-6:2004+A1:2008, EN 14460:2006. Understanding these relationships helps ensure you are using the most current and applicable version of the standard.

EN 4178:2009 is available in PDF format for immediate download after purchase. The document can be added to your cart and obtained through the secure checkout process. Digital delivery ensures instant access to the complete standard document.

Standards Content (Sample)


SLOVENSKI STANDARD
01-januar-2010
Aeronavtika - Vijaki, valjasta glava, šestzoba vdolbina, široka toleranca, srednja
navojna dolžina, iz titanove zlitine, anodizirani, mazani z MoS2 - 1100 MPa (pri
temperaturi okolice)/315 °C
Aerospace series - Screws, pan head, six lobe recess, coarse tolerance normal shank,
medium length thread, in titanium alloy, anodized, MoS2 lubricated - 1100 MPa (at
ambient temperature)/315 °C
Luft- und Raumfahrt - Flachkopfschrauben mit Sechs-Bogenzahn; mit mittlerer
Gewindelänge, aus Titanlegierung, anodisiert, MoS2-geschmiert - 1100 MPa (bei
Raumtemperatur)/315 °C
Série aérospatiale - Vis à tête cylindrique, à empreinte six lobes, tige normale à
tolérance large, filetage moyen, en alliage de titane, anodisées, lubrifiées MoS2 - 1100
MPa (à température ambiante)/315 °C
Ta slovenski standard je istoveten z: EN 4178:2009
ICS:
49.030.10 Navoji Screw threads
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.

EUROPEAN STANDARD
EN 4178
NORME EUROPÉENNE
EUROPÄISCHE NORM
November 2009
ICS 49.030.10
English Version
Aerospace series - Screws, pan head, six lobe recess, coarse
tolerance normal shank, medium length thread, in titanium alloy,
anodized, MoS2 lubricated - 1 100 MPa (at ambient
temperature) / 315 °C
Série aérospatiale - Vis à tête cylindrique, à empreinte six Luft- und Raumfahrt - Flachkopfschrauben mit Sechs-
lobes, tige normale à tolérance large, filetage moyen, en
Bogenzahn; mit mittlerer Gewindelänge, aus
alliage de titane, anodisées, lubrifiées MoS2 - 1 100 MPa (à Titanlegierung, anodisiert, MoS2-geschmiert - 1 100 MPa
température ambiante) / 315 °C (bei Raumtemperatur) / 315 °C
This European Standard was approved by CEN on 17 September 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 4178:2009: E
worldwide for CEN national Members.

Contents Page
Foreword .3
1 Scope .4
2 Normative references .4
3 Required characteristics .5
3.1 Configuration – Dimensions – Masses .5
3.2 Tolerances of form and position .5
3.3 Materials .5
3.4 Surface treatment .5
4 Designation .8
5 Marking .8
6 Technical specification .8

Foreword
This document (EN 4178:2009) 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 May 2010, and conflicting national standards shall be withdrawn at the
latest by May 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 follow
...