EN 2880:2018

Aerospace series - Nuts, anchor, self-locking, fuel resistant, sealing, floating, two lug, with counterbore, in alloy steel, cadmium plated, MoS₂ lubricated - Classification: 900 MPa (at ambient temperature) / 120 °C

This document specifies the characteristics of self-locking, fuel resistant, sealing, floating, two lug anchor nuts, with counterbore, in alloy steel, cadmium plated, MoS2 lubricated.
Classification: 900 MPa/120 °C.

Luft- und Raumfahrt - Annietmuttern, selbstsichernd, druckdicht, kraftstoffbeständig, beweglich, beiderseitiger Flansch, mit zylindrischer Aussenkung, aus legiertem Stahl, verkadmet, MoS₂-geschmiert - Klasse: 900 MPa (bei Raumtemperatur) / 120 °C

Diese Europäische Norm legt die Eigenschaften von selbstsichernden, kraftstoffbeständigen, abdichtenden, beweglichen Annietmuttern mit beiderseitigem Flansch, mit zylindrischer Aussenkung, in Stahllegierung, mit Kadmierung und MoS2-Schmierung fest.
Klasse: 900 MPa1/120 °C2.

Série aérospatiale - Écrous à river, à freinage interne, étanches au carburant, flottants, double patte, avec chambrage, en acier allié, cadmiés, lubrifiés MoS₂ - Classification: 900 MPa (à température ambiante) / 120 °C

Aeronavtika - Zakovne matice, samozaporne, odporne proti gorivu, tesnjene, premične, dvostranske, z izvrtino za valjaste vijake, iz legiranega jekla, kadmirane, mazane z MoS2 - Klasifikacija: 900 MPa (pri okoljski temperaturi)/120 °C

Ta dokument določa lastnosti samozapornih, proti gorivu odpornih, tesnjenih, premičnih, dvostranskih zakovnih matic, z izvrtino za valjaste vijake, iz legiranega jekla, kadmiranih, mazanih z MoS2.
Klasifikacija: 900 MPa/120 °C.

General Information

• Status: Withdrawn
• Publication Date: 04-Sep-2018
• Withdrawal Date: 09-Apr-2019
• ICS: 49.030.30 - Nuts
• Technical Committee: ASD-STAN - Aerospace
• Drafting Committee: ASD-STAN/D 3/S 2 - Fasteners
• Current Stage: 9960 - Withdrawal effective - Withdrawal
• Completion Date: 10-Apr-2019
• Ref Project: SIST EN 2880:2018 - Aerospace series - Nuts, anchor, self-locking, fuel resistant, sealing, floating, two lug, with counterbore, in alloy steel, cadmium plated, MoS₂ lubricated - Classification: 900 MPa (at ambient temperature) / 120 °C

Relations

• Merged Into: EN 2880:2018+AC:2019 - Aerospace series - Nuts, anchor, self-locking, fuel resistant, sealing, floating, two lug, with counterbore, in alloy steel, cadmium plated, MoS₂ lubricated - Classification: 900 MPa (at ambient temperature) / 120 °C
• Effective Date: 16-Jan-2023

Standards Content (Sample)

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01-november-2018
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Ta slovenski standard je istoveten z: EN 2880:2018
ICS:
49.030.30 Matice Nuts
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.

EN 2880
EUROPEAN STANDARD
NORME EUROPÉENNE
September 2018
EUROPÄISCHE NORM
ICS 49.030.30 Supersedes
English Version
Aerospace series - Nuts, anchor, self-locking, fuel resistant,
sealing, floating, two lug, with counterbore, in alloy steel,
cadmium plated, MoS2 lubricated - Classification: 900 MPa
(at ambient temperature) / 120 °C
Série aérospatiale - Écrous à river, à freinage interne, Luft- und Raumfahrt - Annietmuttern, selbstsichernd,
étanches au carburant, flottants, double patte, avec druckdicht, kraftstoffbeständig, beweglich,
chambrage, en acier allié, cadmiés, lubrifiés MoS2 - beiderseitiger Flansch, mit zylindrischer Aussenkung,
Classification: 900 MPa (à température ambiante) / aus legiertem Stahl, verkadmet, MoS2-geschmiert -
120 °C Klasse: 900 MPa (bei Raumtemperatur) / 120 °C
This European Standard was approved by CEN on 11 June 2018.

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 CEN-CENELEC Management Centre or to any CEN
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This European Standard exists in three official versions (English, French, German). A version in any other language made by
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© 2018 CEN All rights of exploitation in any form and by any means reserved Ref. No. EN 2880:2018 E
worldwide for CEN national Members.

Contents
Page
European foreword . 3
1 Scope . 4
2 Normative references . 4
3 Required characteristics . 5
4 Designation. 8
5 Marking . 8
6 Technical specification . 8

European foreword
This document (EN 2880:2018) 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 Standard has
received the approval of the National Associations and the Official Services of the member countries of
ASD, 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 March 2019, and conflicting national standards shall
be withdrawn at the latest by March 2019.
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.
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