EN 3831:2004

Aerospace series - Inserts, thickwall, self-locking, MJ threads, in heat resisting steel FE-PM3801 (17-4PH), MoS2 coated

This standard specifies the characteristics of self-locking, thickwall inserts, in FE-PM3801, MoS2 coated, for aerospace applications.
Maximum test temperature: 350 °C

Luft- und Raumfahrt - Gewindeeinsätze, dickwandig, selbstsichernd, MJ-Gewinde, aus hochwarmfestem Stahl FE-PM3801 (17-4PH), MoS2-beschichtet

Série aérospatiale - Douilles filetées, à paroi renforcée, à freinage interne, à filetage MJ, en acier résistant à chaud FE-PM3801 (17-4PH), revêtues MoS2

La présente norme spécifie les caractéristiques des douilles filetées, à paroi renforcée, à freinage interne, à filetage MJ, en FE PM3801, revêtues MoS2, pour applications aérospatiales.
Température maximale d'essai : 350 °C.
Pour les procédures de conception et d'installation, voir EN 4014 et EN 4015.

Aerospace series - Inserts, thickwall, self-locking, MJ threads, in heat resisting steel FE-PM3801 (17-4PH), MoS2 coated

General Information

• Status: Published
• Publication Date: 09-Nov-2004
• Withdrawal Date: 30-May-2005
• ICS: 49.030.30 - Nuts
• 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 3831:2005 - Aerospace series - Inserts, thickwall, self-locking, MJ threads, in heat resisting steel FE-PM3801 (17-4PH), MoS2 coated

Relations

• Replaces: EN 3831:2003 - Aerospace series - Inserts, thickwall, self-locking, in heat resisting steel FE-PM3801 (17-4PH), MoS2 coated
• Effective Date: 22-Dec-2008

Standards Content (Sample)

SLOVENSKI STANDARD
01-junij-2005
1DGRPHãþD
SIST EN 3831:2004
Aerospace series - Inserts, thickwall, self-locking, MJ threads, in heat resisting
steel FE-PM3801 (17-4PH), MoS2 coated
Aerospace series - Inserts, thickwall, self-locking, MJ threads, in heat resisting steel FE-
PM3801 (17-4PH), MoS2 coated
Luft- und Raumfahrt - Gewindeeinsätze, dickwandig, selbstsichernd, MJ-Gewinde, aus
hochwarmfestem Stahl FE-PM3801 (17-4PH), MoS2-beschichtet
Série aérospatiale - Douilles filetées, a paroi renforcée, a freinage interne, a filetage MJ,
en acier résistant a chaud FE-PM3801 (17-4PH), revetues MoS2
Ta slovenski standard je istoveten z: EN 3831:2004
ICS:
49.030.30 Matice Nuts
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.

EUROPEAN STANDARD
EN 3831
NORME EUROPÉENNE
EUROPÄISCHE NORM
November 2004
ICS 49.030.30 Supersedes EN 3831:2003
English version
Aerospace series - Inserts, thickwall, self-locking, MJ threads, in
heat resisting steel FE-PM3801 (17-4PH), MoS2 coated
Série aérospatiale - Douilles filetées, à paroi renforcée, à Luft- und Raumfahrt - Gewindeeinsätze, dickwandig,
freinage interne, à filetage MJ, en acier résistant à chaud selbstsichernd, MJ-Gewinde, aus hochwarmfestem Stahl
FE-PM3801 (17-4PH), revêtues MoS2 FE-PM3801 (17-4PH), MoS2-beschichtet
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 3831:2004: E
worldwide for CEN national Members.

Contents                                                                         Page

Foreword.3
1 Scope .4
2 Normative references .4
3 Required characteristics.4
4 Insert definition.5
5 Designation .6
6 Marking .6
7 Technical specification .6
Foreword
This document (EN 3831:2004) 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 Standa
...