EN 4014:2004

Aerospace series - Inserts, thickwall, self-locking - Design standard

This standard specifies the use and installation hole dimensions for EN standard, self-locking, thickwall inserts and provisions for component salvage, for aerospace applications.

Luft- und Raumfahrt - Gewindeeinsätze, dickwandig, Selbstsichernd - Konstruktionsnorm

Diese Norm legt die Verwendung und Maße von Einbaulöchern für selbstsichernde, dickwandige Gewindeeinsätze nach EN-Normen sowie Vorkehrungen zur Reparatur von Bauteilen für Anwendungen in der Luft  und Raumfahrt fest.

Série aérospatiale - Douilles filetées, à paroi renforcée, à freinage interne - Norme de conception

Aerospace series - Inserts, thickwall, self-locking - Design standard

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 4014:2005 - Aerospace series - Inserts, thickwall, self-locking - Design standard

Relations

• Replaces: EN 4014:2003 - Aerospace series - Inserts, thickwall, self-locking - Design standard
• Effective Date: 22-Dec-2008

Standards Content (Sample)

SLOVENSKI STANDARD
01-junij-2005
1DGRPHãþD
SIST EN 4014:2004
Aerospace series - Inserts, thickwall, self-locking - Design standard
Aerospace series - Inserts, thickwall, self-locking - Design standard
Luft- und Raumfahrt - Gewindeeinsätze, dickwandig, Selbstsichernd - Konstruktionsnorm
Série aérospatiale - Douilles filetées, a paroi renforcée, a freinage interne - Norme de
conception
Ta slovenski standard je istoveten z: EN 4014:2004
ICS:
49.030.30 Matice Nuts
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.

EUROPEAN STANDARD
EN 4014
NORME EUROPÉENNE
EUROPÄISCHE NORM
November 2004
ICS 49.030.30 Supersedes EN 4014:2003
English version
Aerospace series - Inserts, thickwall, self-locking - Design
standard
Série aérospatiale - Douilles filetées, à paroi renforcée, à Luft- und Raumfahrt - Gewindeeinsätze, dickwandig,
freinage interne - Norme de conception Selbstsichernd - Konstruktionsnorm
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 4014:2004: E
worldwide for CEN national Members.

Contents Page
Foreword.3
1 Scope.4
2 Normative references.4
3 Design.4
4 Use.5
4.1 General.5
4.2 Performance.6
4.3 Installation restrictions.6
5 Required characteristics.7
5.1 Installation hole.7
5.2 Serration.8
6 Installation.9
7 Provisions for component salvage.9
8 Designation.9
9 Indication on drawings.9
9.1 Drawing definition.9
9.2 Assembly drawing.10

Foreword
This document (EN 4014:2004) 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 identical
text or by endorsement, at the latest by May 2005, and conflicting national standards shall be withdrawn at
the latest by May 2005.
This document supersedes EN 4014:2003.
According to the CEN/CENELEC Internal Regulations, the national standards organizations of the following
countries are bound to implement this European Standard: 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.
1 Scope
This standard specifies the use and installation hole dimensions for EN standard, self-locking, thickwall
inserts and provisions for component salvage, for aerospace applications.
2 Normative references
The following referenced documents are indispensable for the application of this document. For dated
references, only the edition cited applies. For undated references, the latest edition of the referenced
document (including any amendments) applies.
ISO 5855-1, Aerospace – MJ threads – Part 1: General requirements
ISO 5855-2, Aerospace – MJ threads – Part 2: Limit dimensions for bolts and nuts
EN 3831, Aerospace series – Inserts, thickwall, self-locking, MJ threads, in heat resisting steel FE-PM3801
(17-4PH), MoS coated
...