SIST EN 4119:2005

Aerospace series - Nuts, bihexagonal, self-locking, deep counterbore, in heat resisting steel FE-PA2601 (A286), silver plated on thread - Classification: 1 100 MPa (at ambient temperature) / 650 °C

This standard specifies the characteristics of self-locking bihexagonal nuts with deep counterbore in FE-PA92HT, silver plated on thread, for aerospace applications.
Classification: 1 100 MPa  ) I 650 °C  )

Luft- und Raumfahrt - Zwölfkantmuttern, selbstsichernd, mit zylindrischer Aussenkung, aus hochwarmfestem Stahl FE-PA2601 (A286), Gewinde versilbert - Klasse: 1 100 MPa (bei Raumtemperatur) / 650 °C

Diese Norm legt die Eigenschaften von selbstsichernden Zwölfkantmuttern mit zylindrischer Aussenkung aus FE PA2601, Gewinde versilbert, für Anwendungen in der Luft- und Raumfahrt fest.
Klasse: 1 100 MPa ) / 650 °C )

Série aérospatiale - Écrous bihexagonaux, a freinage interne, a chambrage profond, en acier résistant a chaud FE-PA2601 (A286), argentés sur filetage - Classification : 1 100 MPa (a température ambiante ) / 650 °C

Aerospace series - Nuts, bihexagonal, self-locking, deep counterbore, in heat resisting steel FE-PA2601 (A286), silver plated on thread - Classification: 1 100 MPa (at ambient temperature) / 650 °C

General Information

• Status: Published
• Publication Date: 31-May-2005
• ICS: 49.030.30 - Nuts
• Technical Committee: SS SPL - Technical Board for the general field
• Current Stage: 6060 - National Implementation/Publication (Adopted Project)
• Start Date: 01-Jun-2005
• Due Date: 01-Jun-2005
• Completion Date: 01-Jun-2005
• Ref Project: EN 4119:2004 - Aerospace series - Nuts, bihexagonal, self-locking, deep counterbore, in heat resisting steel FE-PA2601 (A286), silver plated on thread - Classification: 1 100 MPa (at ambient temperature) / 650 °C

Relations

• Replaces: SIST EN 4119:2004 - Aerospace series - Nuts, bihexagonal, self-locking, deep counterbored, in heat resisting steel FE-PA92HT (A286), silver plated on thread - Classification: 1 100 MPa (at ambient temperature) / 650°C
• Effective Date: 01-Jun-2005

Standards Content (Sample)

SLOVENSKI STANDARD
SIST EN 4119:2005
01-junij-2005
1DGRPHãþD
SIST EN 4119:2004
Aerospace series - Nuts, bihexagonal, self-locking, deep counterbore, in heat
resisting steel FE-PA2601 (A286), silver plated on thread - Classification: 1 100
MPa (at ambient temperature) / 650 °C
Aerospace series - Nuts, bihexagonal, self-locking, deep counterbore, in heat resisting
steel FE-PA2601 (A286), silver plated on thread - Classification: 1 100 MPa (at ambient
temperature) / 650 °C
Luft- und Raumfahrt - Zwölfkantmuttern, selbstsichernd, mit zylindrischer Aussenkung,
aus hochwarmfestem Stahl FE-PA2601 (A286), Gewinde versilbert - Klasse: 1 100 MPa
(bei Raumtemperatur) / 650 °C
Série aérospatiale - Écrous bihexagonaux, a freinage interne, a chambrage profond, en
acier résistant a chaud FE-PA2601 (A286), argentés sur filetage - Classification : 1 100
MPa (a température ambiante ) / 650 °C
Ta slovenski standard je istoveten z: EN 4119:2004
ICS:
49.030.30 Matice Nuts
SIST EN 4119:2005 en
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.

---------------------- Page: 1 ----------------------

SIST EN 4119:2005

---------------------- Page: 2 ----------------------

SIST EN 4119:2005



EUROPEAN STANDARD
EN 4119

NORME EUROPÉENNE

EUROPÄISCHE NORM
November 2004
ICS 49.030.30 Supersedes EN 4119:2003
English version
Aerospace series - Nuts, bihexagonal, self-locking, deep
counterbore, in heat resisting steel FE-PA2601 (A286), silver
plated on thread - Classification: 1 100 MPa (at ambient
temperature) / 650° C
Série aérospatiale - Écrous bihexagonaux, à freinage Luft- und Raumfahrt - Zwölfkantmuttern, selbstsichernd, mit
interne, à chambrage profond, en acier résistant à chaud zylindrischer Aussenkung, aus hochwarmfestem Stahl FE-
FE-PA2601 (A286), argentés sur filetage - Classification : 1 PA2601 (A286), Gewinde versilbert - Klasse: 1 100 MPa
100 MPa (à température ambiante ) / 650° C (bei Raumtemperatur) / 650° C
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 4119:2004: E
worldwide for CEN national Members.

---------------------- Page: 3 ----------------------

SIST EN 4119:2005

EN 4119:2004 (E)
Contents                                                                         Page

Foreword.3
1 Scope .4
2 Normative references .4
3 Required characteristics.4
4 Designation .6
5 Marking .6
6 Technical specification .6
2

---------------------- Page: 4 ----------------------

SIST EN 4119:2005
EN 4119:2004 (E)
Foreword
This document (EN 4119:2004) has been prepared by the European Association of Aerospace
Manufacturers - Standardization (AEC
...