Aerospace series - Bolts, MJ threads, in titanium alloy TI-P64001 - Strength class: 1 100 MPa (at ambient temperature) - Technical specification

This standard specifies the characteristics, qualification and acceptance requirements for bolts with MJ threads in TI-P64001.
Strength class: 1 100 MPa
It is applicable whenever referenced.

Luft- und Raumfahrt - Schrauben, MJ-Gewinde, aus Titanlegierung TI-P64001 - Festigkeitsklasse: 1 100 MPa (bei Raumtemperatur) - Technische Lieferbedingungen

Série aérospatiale - Vis à filetage MJ, en alliage de titane TI-P64001 - Classe de résistance : 1 100 MPa (à température ambiante) - Spécification technique

Aerospace series - Bolts, MJ threads, in titanium alloy TI-P64001 - Strength class: 1 100 MPa (at ambient temperature) - Technical specification

General Information

Status
Withdrawn
Publication Date
09-Nov-2004
Withdrawal Date
07-May-2019
Technical Committee
Drafting Committee
Current Stage
9960 - Withdrawal effective - Withdrawal
Completion Date
08-May-2019

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SLOVENSKI STANDARD
SIST EN 3818:2005
01-junij-2005
1DGRPHãþD
SIST EN 3818:2004
Aerospace series - Bolts, MJ threads, in titanium alloy TI-P64001 - Strength class:
1 100 MPa (at ambient temperature) - Technical specification
Aerospace series - Bolts, MJ threads, in titanium alloy TI-P64001 - Strength class: 1 100
MPa (at ambient temperature) - Technical specification
Luft- und Raumfahrt - Schrauben, MJ-Gewinde, aus Titanlegierung TI-P64001 -
Festigkeitsklasse: 1 100 MPa (bei Raumtemperatur) - Technische Lieferbedingungen
Série aérospatiale - Vis a filetage MJ, en alliage de titane TI-P64001 - Classe de
résistance : 1 100 MPa (a température ambiante) - Spécification technique
Ta slovenski standard je istoveten z: EN 3818:2004
ICS:
49.030.20 Sorniki, vijaki, stebelni vijaki Bolts, screws, studs
SIST EN 3818:2005 en
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.

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SIST EN 3818:2005

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SIST EN 3818:2005



EUROPEAN STANDARD
EN 3818

NORME EUROPÉENNE

EUROPÄISCHE NORM
November 2004
ICS 49.030.20 Supersedes EN 3818:2003
English version
Aerospace series - Bolts, MJ threads, in titanium alloy TI-
P64001 - Strength class: 1 100 MPa (at ambient temperature) -
Technical specification
Série aérospatiale - Vis à filetage MJ, en alliage de titane Luft- und Raumfahrt - Schrauben, MJ-Gewinde, aus
TI-P64001 - Classe de résistance : 1 100 MPa (à Titanlegierung TI-P64001 - Festigkeitsklasse: 1 100 MPa
température ambiante) - Spécification technique (bei Raumtemperatur) - Technische Lieferbedingungen
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 3818:2004: E
worldwide for CEN national Members.

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SIST EN 3818:2005

EN 3818:2004 (E)
Contents Page
Foreword.3
1 Scope.4
2 Normative references.4
3 Terms and definitions .4
4 Quality assurance.6
4.1 Qualification.6
4.2 Acceptance.6
5 Requirements.6

2

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SIST EN 3818:2005
EN 3818:2004 (E)
Foreword
This document (EN 3818:2004) 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 n
...

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