EN 4120:2004

Aerospace series - Nuts, bihexagonal, self-locking, in heat resisting nickel base alloy NI-PH1302 (Waspaloy), silver plated on thread - Classification: 1 210 MPa (at ambient temperature) / 730 °C

This standard specifies the characteristics of self-locking bihexagonal nuts in NI-P1 01 HT, silver plated on thread, for aerospace applications.
Classification: 1 210 MPa / 730 °C

Luft- und Raumfahrt - Zwölfkantmuttern, selbstsichernd, aus hochwarmfester Nickelbasislegierung NI-PH1302 (Waspaloy), Gewinde versilbert - Klasse: 1 210 MPa (bei Raumtemperatur) / 730 °C

Diese Norm legt die Eigenschaften von selbstsichernden Zwölfkantmuttern aus NI-PH1302, Gewinde versilbert, für Anwendungen in der Luft- und Raumfahrt fest.
Klasse: 1 210 MPa ) / 730 °C )

Série aérospatiale - Écrous bihexagonaux, à freinage interne, en alliage résistant à chaud à base de nickel NI-PH1302 (Waspaloy), argentés sur filetage - Classification : 1 210 MPa (à température ambiante ) / 730 °C

Aerospace series - Nuts, bihexagonal, self-locking, in heat resisting nickel base alloy NI-PH1302 (Waspaloy), silver plated on thread - Classification: 1 210 MPa (at ambient temperature) / 730 °C

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 4120:2005 - Aerospace series - Nuts, bihexagonal, self-locking, in heat resisting nickel base alloy NI-PH1302 (Waspaloy), silver plated on thread - Classification: 1 210 MPa (at ambient temperature) / 730 °C

Relations

• Replaces: EN 4120:2003 - Aerospace series - Nuts, bihexagonal, self-locking, in heat resisting nickel base alloy NI-PH-1302 (Waspaloy), silver plated on thread - Classification: 1210 MPa (at ambient temperature) / 730°C
• Effective Date: 22-Dec-2008

Standards Content (Sample)

SLOVENSKI STANDARD
01-junij-2005
1DGRPHãþD
SIST EN 4120:2004
Aerospace series - Nuts, bihexagonal, self-locking, in heat resisting nickel base
alloy NI-PH1302 (Waspaloy), silver plated on thread - Classification: 1 210 MPa (at
ambient temperature) / 730 °C
Aerospace series - Nuts, bihexagonal, self-locking, in heat resisting nickel base alloy NI-
PH1302 (Waspaloy), silver plated on thread - Classification: 1 210 MPa (at ambient
temperature) / 730 °C
Luft- und Raumfahrt - Zwölfkantmuttern, selbstsichernd, aus hochwarmfester
Nickelbasislegierung NI-PH1302 (Waspaloy), Gewinde versilbert - Klasse: 1 210 MPa
(bei Raumtemperatur) / 730 °C
Série aérospatiale - Écrous bihexagonaux, a freinage interne, en alliage résistant a
chaud a base de nickel NI-PH1302 (Waspaloy), argentés sur filetage - Classification : 1
210 MPa (a température ambiante ) / 730 °C
Ta slovenski standard je istoveten z: EN 4120:2004
ICS:
49.030.30 Matice Nuts
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.

EUROPEAN STANDARD
EN 4120
NORME EUROPÉENNE
EUROPÄISCHE NORM
November 2004
ICS 49.030.30 Supersedes EN 4120:2003
English version
Aerospace series - Nuts, bihexagonal, self-locking, in heat
resisting nickel base alloy NI-PH1302 (Waspaloy), silver plated
on thread - Classification: 1 210 MPa (at ambient temperature) /
730° C
Série aérospatiale - Écrous bihexagonaux, à freinage Luft- und Raumfahrt - Zwölfkantmuttern, selbstsichernd,
interne, en alliage résistant à chaud à base de nickel NI- aus hochwarmfester Nickelbasislegierung NI-PH1302
PH1302 (Waspaloy), argentés sur filetage - Classification : (Waspaloy), Gewinde versilbert - Klasse: 1 210 MPa (bei
1 210 MPa (à température ambiante ) / 730° C Raumtemperatur) / 730° C
This European Standard was approved by CEN on 11 September 2003.

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Standard the status of a national standard without any alteration. Up-to-date lists and bibliographical references concerning such national
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© 2004 CEN All rights of exploitation in any form and by any means reserved Ref. No. EN 4120:2004: E
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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
Foreword
This document (EN 4120:2004) has been prepared by the European Association of Aerospace
Manufacturers - Standardization (AECMA-STAN).
After enquiries and votes carried out in acco
...