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
Technical Committee
Drafting Committee
Current Stage
9093 - Decision to confirm - Review Enquiry
Completion Date
30-Jun-2017

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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.

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.
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© 2004 CEN All rights of exploitation in any form and by any means reserved Ref. No. EN 4120:2004: E
worldwide for CEN national Members.

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
...

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