EN 3818:2003

Aerospace series - Bolts with MJ threads, in titanium alloy TI-P64001 - Classification: 1100 MPa (at ambient temperature) - Technical specification

This standard specifies the characteristics, qualification and acceptance requirements for bolts with MJ threads in TI-P63.
Classification : 1 100 MPa
It is applicable whenever referenced.

Série aérospatiale - Vis à filetage MJ, en alliage de titane TI-P63 - Classification:1 100 MPa (à température ambiante) - Spécification technique

Aerospace series - Bolts with MJ threads, in titanium alloy TI-P64001 - Classification: 1100 MPa (at ambient temperature) - Technical specification

General Information

• Status: Withdrawn
• Publication Date: 25-Feb-2003
• Withdrawal Date: 09-Nov-2004
• ICS: 49.030.20 - Bolts, screws, studs
• Technical Committee: ASD/MECH - Mechanical
• Drafting Committee: ASD/MECH - Mechanical
• Current Stage: 9960 - Withdrawal effective - Withdrawal
• Start Date: 10-Nov-2004
• Completion Date: 10-Nov-2004
• Ref Project: SIST EN 3818:2004 - Aerospace series - Bolts with MJ threads, in titanium alloy TI-P64001 - Classification: 1100 MPa (at ambient temperature) - Technical specification

Relations

• Replaced By: EN 3818:2004 - Aerospace series - Bolts, MJ threads, in titanium alloy TI-P64001 - Strength class: 1 100 MPa (at ambient temperature) - Technical specification
• Effective Date: 22-Dec-2008

Standards Content (Sample)

SLOVENSKI STANDARD
SIST EN 3818:2004
01-maj-2004
Aerospace series - Bolts with MJ threads, in titanium alloy TI-P64001 -
Classification: 1100 MPa (at ambient temperature) - Technical specification
Aerospace series - Bolts with MJ threads, in titanium alloy TI-P64001 - Classification:
1100 MPa (at ambient temperature) - Technical specification
Série aérospatiale - Vis a filetage MJ, en alliage de titane TI-P63 - Classification:1 100
MPa (a température ambiante) - Spécification technique
Ta slovenski standard je istoveten z: EN 3818:2003
ICS:
49.030.20 Sorniki, vijaki, stebelni vijaki Bolts, screws, studs
SIST EN 3818:2004 en
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.

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SIST EN 3818:2004

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SIST EN 3818:2004
EUROPEAN STANDARD
EN 3818
NORME EUROPÉENNE
EUROPÄISCHE NORM
February 2003
ICS 49.030.20
English version
Aerospace series - Bolts with MJ threads, in titanium alloy TI-
P64001 - Classification: 1100 MPa (at ambient temperature) -
Technical specification
This European Standard was approved by CEN on 19 August 2002.
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 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 Management Centre has the same status as the official
versions.
CEN members are the national standards bodies of Austria, Belgium, Czech Republic, Denmark, Finland, France, Germany, Greece,
Hungary, Iceland, Ireland, Italy, Luxembourg, Malta, Netherlands, Norway, Portugal, Slovak Republic, 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
© 2003 CEN All rights of exploitation in any form and by any means reserved Ref. No. EN 3818:2003 E
worldwide for CEN national Members.

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SIST EN 3818:2004
EN 3818:2003 (E)
Contents
page
Foreword.3
1 Scope .4
2 Normative references .4
3 Terms and definitions.5
4 Quality assurance .7
5 Requirements .7
Annex A (informative) Tensile and tension fatigue - areas and loads formulae.25
A.1 Cross sectional area values.25
A.2 Formulae.25
A.2.1 Cross sectional area.25
A.2.2 Tensile test load.26
A.2.3 Tension fatigue test load.26
2

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SIST EN 3818:2004
EN 3818:2003 (E)
Foreword
This document EN 3818:2003 has been prepared by the European Association of Aerospace Manufacturers
(AECMA).
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
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