EN 4122:2004

Aerospace series - Shank nuts, self-locking, 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 shank nuts in FE-PA92HT, silver plated on thread, for aerospace applications.
Classification : 1 100 MPa / 650 °C

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

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

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

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

General Information

• Status: Withdrawn
• Publication Date: 09-Nov-2004
• Withdrawal Date: 15-May-2018
• ICS: 49.030.30 - Nuts
• Technical Committee: ASD-STAN - Aerospace
• Drafting Committee: ASD-STAN/D 3 - Mechanical
• Current Stage: 9960 - Withdrawal effective - Withdrawal
• Completion Date: 16-May-2018
• Ref Project: SIST EN 4122:2005 - Aerospace series - Shank nuts, self-locking, in heat resisting steel FE-PA2601 (A286), silver plated on thread - Classification: 1 100 MPa (at ambient temperature) / 650 °C

Relations

• Replaces: EN 4122:2003 - Aerospace series - Shank nuts, self-locking, in heat resisting steel FE-PA92HT (A286), silver plated on thread - Classification: 1 100MPa (at ambient temperature) / 650°C
• Effective Date: 22-Dec-2008
• Replaced By: EN 4122:2018 - Aerospace series - Shank nuts, self-locking, in heat resisting steel FE-PA2601 (A286), silver plated on thread - Classification: 1 100 MPa (at ambient temperature) / 650 °C
• Effective Date: 08-Jun-2022

Standards Content (Sample)

SLOVENSKI STANDARD
01-junij-2005
1DGRPHãþD
SIST EN 4122:2004
Aerospace series - Shank nuts, self-locking, in heat resisting steel FE-PA2601
(A286), silver plated on thread - Classification: 1 100 MPa (at ambient
temperature) / 650 °C
Aerospace series - Shank nuts, self-locking, in heat resisting steel FE-PA2601 (A286),
silver plated on thread - Classification: 1 100 MPa (at ambient temperature) / 650 °C
Luft- und Raumfahrt - Einnietmuttern, selbstsichernd, aus hochwarmfestem Stahl FE-
PA2601 (A286), Gewinde versilbert - Klasse: 1 100 MPa (bei Raumtemperatur) / 650 °C
Série aérospatiale - Écrous a sertir, a freinage interne, 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 4122:2004
ICS:
49.030.30 Matice Nuts
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.

EUROPEAN STANDARD
EN 4122
NORME EUROPÉENNE
EUROPÄISCHE NORM
November 2004
ICS 49.030.30 Supersedes EN 4122:2003
English version
Aerospace series - Shank nuts, self-locking, in heat resisting
steel FE-PA2601 (A286), silver plated on thread - Classification:
1 100 MPa (at ambient temperature) / 650° C
Série aérospatiale - Écrous à sertir, à freinage interne, en Luft- und Raumfahrt - Einnietmuttern, selbstsichernd, aus
acier résistant à chaud FE-PA2601 (A286), argentés sur hochwarmfestem Stahl FE-PA2601 (A286), Gewinde
filetage - Classification : 1 100 MPa (à température versilbert - Klasse: 1 100 MPa (bei Raumtemperatur) / 650°
ambiante ) / 650° C 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 4122:2004: 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 4122:2004) has been prepared by the European Association of Aerospace
Manu
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