EN 2882:2023
(Main)Aerospace series - Nut, hexagonal, self-locking, with counterbore and captive washer, in steel, cadmium plated, MoS2 lubricated - Classification: 1 100 MPa (at ambient temperature) / 235 °C
Aerospace series - Nut, hexagonal, self-locking, with counterbore and captive washer, in steel, cadmium plated, MoS2 lubricated - Classification: 1 100 MPa (at ambient temperature) / 235 °C
This document specifies the characteristics for hexagon nuts, with counterbore and captive washer, with a self-locking feature achieved by forming the upper portion out-of-round, in steel, cadmium plated, MoS2 lubricated, classification 1 100 MPa /235 °C .
Luft- und Raumfahrt - Sechskantmutter, selbstsichernd, mit Aussenkung und Bördelscheibe, aus Stahl, verkadmet, MoS2‑geschmiert - Klasse: 1 100 MPa (bei Raumtemperatur)/235 °C
Dieses Dokument legt die Eigenschaften von Sechskantmuttern mit Aussenkung, Bördelscheibe und einer durch Verformung des oberen Teils erzeugten Selbstsicherung, aus Stahl, verkadmet, MoS2 geschmiert, Klasse: 1 100 MPa /235 °C , fest.
Série aérospatiale - Écrou hexagonal, à freinage interne, avec chambrage et rondelle captive, en acier, cadmié, lubrifié au MoS2 - Classification : 1 100 MPa (à température ambiante)/235 °C
Le présent document spécifie les caractéristiques des écrous hexagonaux, avec chambrage et rondelle captive, avec déformation de la partie supérieure du faux-rond pour assurer le freinage, en acier, cadmiés, lubrifiés au MoS2, classification 1 100 MPa/235 °C.
Aeronavtika - Matice, šestrobe, samozapiralne, z ugreznjeno in robljeno podložko, iz jekla, kadmirane, mazane z MoS2 - Klasifikacija: 1100 MPa (pri temperaturi okolice)/235 °C
Ta dokument določa značilnosti šestrobih matic z ugreznjeno in robljeno podložko, s samozapiralno funkcijo. ki jo zagotavlja ovalna oblika zgornjega dela, iz jekla, kadmiranih, mazanih z MoS2, s klasifikacijo 1100 MPa/235 °C.
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Standards Content (Sample)
SLOVENSKI STANDARD
01-februar-2024
Aeronavtika - Matice, šestrobe, samozapiralne, z ugreznjeno in robljeno podložko,
iz jekla, kadmirane, mazane z MoS2 - Klasifikacija: 1100 MPa (pri temperaturi
okolice)/235 °C
Aerospace series - Nut, hexagonal, self-locking, with counterbore and captive washer, in
steel, cadmium plated, MoS2 lubricated - Classification: 1 100 MPa (at ambient
temperature) / 235 °C
Luft- und Raumfahrt - Sechskantmuttern, selbstsichernd, mit Aussenkung und
Bördelscheibe, aus Stahl, verkadmet, MoS2 geschmiert - Klasse: 1 100 MPa (bei
Raumtemperatur) / 235 °C
Série aérospatiale - Écrous hexagonaux, à freinage interne, avec chambrage et rondelle
captive, en acier, cadmiés, lubrifiés MoS2 - Classification: 1 100 MPa (à température
ambiante)/235 °C
Ta slovenski standard je istoveten z: EN 2882:2023
ICS:
49.030.30 Matice Nuts
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.
EN 2882
EUROPEAN STANDARD
NORME EUROPÉENNE
November 2023
EUROPÄISCHE NORM
ICS 49.030.30 Supersedes EN 2882:2006
English Version
Aerospace series - Nut, hexagonal, self-locking, with
counterbore and captive washer, in steel, cadmium plated,
MoS2 lubricated - Classification: 1 100 MPa (at ambient
temperature) / 235 °C
Série aérospatiale - Écrou hexagonal, à freinage Luft- und Raumfahrt - Sechskantmutter,
interne, avec chambrage et rondelle captive, en acier, selbstsichernd, mit Aussenkung und Bördelscheibe, aus
cadmié, lubrifié au MoS2 - Classification : 1 100 MPa (à Stahl, verkadmet, MoS2 geschmiert - Klasse: 1 100 MPa
température ambiante)/235 °C (bei Raumtemperatur) / 235 °C
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© 2023 CEN All rights of exploitation in any form and by any means reserved Ref. No. EN 2882:2023 E
worldwide for CEN national Members.
Contents Page
European foreword . 3
1 Scope . 4
2 Normative references . 4
3 Terms and definitions . 5
4 Required characteristics . 5
4.1 Configuration – Dimensions – Masses . 5
4.2 Materials . 5
4.3 Surface treatment . 5
5 Designation . 8
6 Marking . 8
7 Technical specification . 8
8 Quality management systems . 8
European foreword
This document (EN 2882:2023) has been prepared by the Aerospace and Defence Industries
Association of Europe – Standardization (ASD-STAN).
After enquiries and votes carried out in accordance with the rules of this Association, this document has
received the approval of the National Associations and the Official Services of the member countries of
ASD-STAN, prior to its presentation to CEN.
This European Standard shall be given the status of a national standard, either by publication of an
identical text or by endorsement, at the latest by May 2023, and conflicting national standards shall be
withdrawn at the latest by May 2023.
Attention is drawn to the possibility that some of the elements of this document may be the subject of
patent rights. CEN shall not be held responsible for identifying any or all such patent rights.
This document supersedes EN 2882:2006.
— normative references updated;
— Clause 3 added;
— Subclause 4.2 „Materials“ revised;
— Clause 7 “Quality management system” added;
— document editorially revised.
Any feedback and questions on this document should be directed to the users’ national standards body.
A complete listing of these bodies can be found on the CEN website.
According to the CEN-CENELEC Internal Regulations, the national standards organizations of the
following countries are bound to implement this European Standard:
...
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