SIST EN 4123:2004

Aerospace series - Shank nuts, self-locking, in heat resisting nickel base alloy NI-PH2601 (Inconel 718), silver plated on thread - Classification: 1 550 MPa (at ambient temperature)/600 °C

This standard specifies the characteristics of self-locking shank nuts in NI-P100HT, silver plated on thread, for aerospace applications.
Classification: 1 550 MPa  ) / 600 °C

Série aérospatiale - Ecrous a sertir, a freinage interne, en alliage résistant a chaud a base de nickel NI-P100HT (Inconel 718), argentés sur filetage - Série aérospatiale -- Classification: 1 550 MPa (a température ambiante)/600°C

Aerospace series - Shank nuts, self-locking, in heat resisting nickel base alloy NI-PH2601 (Inconel 718), silver plated on thread - Classification: 1 550 MPa (at ambient temperature)/600 °C

General Information

• Status: Withdrawn
• Publication Date: 30-Apr-2004
• Withdrawal Date: 31-May-2005
• ICS: 49.030.30 - Nuts
• Technical Committee: I08 - Imaginarni 08
• Current Stage: 9900 - Withdrawal (Adopted Project)
• Start Date: 01-Jun-2005
• Due Date: 01-Jun-2005
• Completion Date: 01-Jun-2005
• Ref Project: EN 4123:2003 - Aerospace series - Shank nuts, self-locking, in heat resisting nickel base alloy NI-PH2601 (Inconel 718), silver plated on thread - Classification: 1 550 MPa (at ambient temperature)/600 °C

Relations

• Replaced By: SIST EN 4123:2005 - Aerospace series - Shank nuts, self-locking, in heat resisting nickel base alloy NI-PH2601 (Inconel 718), silver plated on thread - Classification: 1 550 MPa (at ambient temperature) / 600 °C
• Effective Date: 01-Jun-2005

Standards Content (Sample)

SLOVENSKI STANDARD
SIST EN 4123:2004
01-maj-2004
Aerospace series - Shank nuts, self-locking, in heat resisting nickel base alloy NI-
PH2601 (Inconel 718), silver plated on thread - Classification: 1 550 MPa (at
ambient temperature)/600 °C
Aerospace series - Shank nuts, self-locking, in heat resisting nickel base alloy NI-
PH2601 (Inconel 718), silver plated on thread - Classification: 1 550 MPa (at ambient
temperature)/600 °C
Série aérospatiale - Ecrous a sertir, a freinage interne, en alliage résistant a chaud a
base de nickel NI-P100HT (Inconel 718), argentés sur filetage - Série aérospatiale --
Classification: 1 550 MPa (a température ambiante)/600°C
Ta slovenski standard je istoveten z: EN 4123:2003
ICS:
49.030.30 Matice Nuts
SIST EN 4123:2004 en
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.

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SIST EN 4123:2004

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SIST EN 4123:2004
EUROPEAN STANDARD
EN 4123
NORME EUROPÉENNE
EUROPÄISCHE NORM
February 2003
ICS 49.030.30
English version
Aerospace series - Shank nuts, self-locking, in heat resisting
nickel base alloy NI-PH2601 (Inconel 718), silver plated on
thread - Classification: 1 550 MPa (at ambient
temperature)/600 °C
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 4123:2003 E
worldwide for CEN national Members.

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SIST EN 4123:2004
EN 4123:2003 (E)
Contents
Foreword.3
1 Scope .3
2 Normative references .3
3 Required characteristics.4
3.1 Configuration – Dimensions – Tolerances – Masses.4
3.2 Material.4
3.3 Surface treatment .4
4 Designation.6
5 Marking .6
6 Technical specification .6
2

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SIST EN 4123:2004
EN 4123:2003 (E)
Foreword
This document EN 4123:2003 has been prepared by the European Association of Aerospace Manufacturers
(AECMA).
After enquiries and votes carried out in a
...