EN 6057:2020

Aerospace series - Rod-end with bearing EN 4265 in corrosion resisting steel, internal threaded shank - Dimensions and loads, Inch series

This European standard specifies the characteristics of adjustable rod-ends consisting of:
- a spherical plain bearing, metal to metal, in corrosion resisting steel, wide series (EN 4265)
- a rod end with internal threaded shank
They are intended for use in fixed or moving parts of the aircraft structure and their control mechanisms

Luft- und Raumfahrt - Ösenkopf mit Gelenklager nach EN 4265 aus korrosionsbeständigem Stahl, mit Innengewinde - Maße und Belastungen, Inch-Reihe

Diese Europäische Norm legt die Eigenschaften verstellbarer Ösenköpfe fest. Diese bestehen aus
- einem Gelenklager, Metall auf Metall, korrosionsbeständigem Stahl, breite Reihe (EN 4265) und
- einem Gelenkstangenende  mit Innengewindeschaft.
Diese sind für den Einsatz in starren oder beweglichen Teilen des Flugzeugs sowie dessen Kontroll-mechanismen bestimmt.

Série aérospatiale - Embout à rotule lisse suivant EN 4265, en acier résistant à la corrosion, avec filetage intérieur - Dimensions et charges - Série en inches

Le présent document spécifie les caractéristiques des embouts ajustables qui se composent :
- d’une rotule lisse, métal à métal, en acier résistant à la corrosion, série large (EN 4265) ;
- d’un embout avec tige à filetage intérieur.
Elles sont destinées à être utilisées pour les parties fixes ou mobiles de la structure des aéronefs et leurs mécanismes de contrôle.

Aeronavtika - Končnik z očesom in ležajem po EN 4265 iz korozijsko odpornega jekla, z zunanjo navojno ročico - Mere in obremenitve - Palčne mere

General Information

• Status: Published
• Publication Date: 27-Oct-2020
• Withdrawal Date: 29-Apr-2021
• ICS: 49.035 - Components for aerospace construction
• Technical Committee: ASD-STAN - Aerospace
• Drafting Committee: ASD-STAN/D 3/S 1 - Parts of Mechanical Systems
• Current Stage: 6060 - Definitive text made available (DAV) - Publishing
• Start Date: 28-Oct-2020
• Completion Date: 28-Oct-2020
• Ref Project: SIST EN 6057:2021 - Aerospace series - Rod-end with bearing EN 4265 in corrosion resisting steel, internal threaded shank - Dimensions and loads, Inch series

Standards Content (Sample)

SLOVENSKI STANDARD
01-januar-2021
Aeronavtika - Končnik z očesom in ležajem po EN 4265 iz korozijsko odpornega
jekla, z zunanjo navojno ročico - Mere in obremenitve - Palčne mere
Aerospace series - Rod-end with bearing EN 4265 in corrosion resisting steel, internal
threaded shank - Dimensions and loads, Inch series
Luft- und Raumfahrt - Ösenkopf mit Gelenklager nach EN 4265 aus
korrosionsbeständigem Stahl, mit Innengewinde - Maße und Belastungen, Inch Reihe
Série aérospatiale - Embout avec rotule lisse en acier par EN 4265 résistant à la
corrosion, avec le filetage intérieur - Dimensions et charges série en inches
Ta slovenski standard je istoveten z: EN 6057:2020
ICS:
49.025.10 Jekla Steels
49.035 Sestavni deli za letalsko in Components for aerospace
vesoljsko gradnjo construction
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.

EN 6057
EUROPEAN STANDARD
NORME EUROPÉENNE
October 2020
EUROPÄISCHE NORM
ICS 49.035
English Version
Aerospace series - Rod-end with bearing EN 4265 in
corrosion resisting steel, internal threaded shank -
Dimensions and loads, Inch series
Série aérospatiale - Embout à rotule lisse suivant EN Luft- und Raumfahrt - Ösenkopf mit Gelenklager nach
4265, en acier résistant à la corrosion, avec filetage EN 4265 aus korrosionsbeständigem Stahl, mit
intérieur - Dimensions et charges - Série en inches Innengewinde - Maße und Belastungen, Inch Reihe
This European Standard was approved by CEN on 6 January 2020.

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
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 CEN-CENELEC Management
Centre has the same status as the official versions.

CEN members are the national standards bodies of Austria, Belgium, Bulgaria, Croatia, Cyprus, Czech Republic, Denmark, Estonia,
Finland, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway,
Poland, Portugal, Republic of North Macedonia, Romania, Serbia, Slovakia, Slovenia, Spain, Sweden, Switzerland, Turkey and
United Kingdom.
EUROPEAN COMMITTEE FOR STANDARDIZATION
COMITÉ EUROPÉEN DE NORMALISATION

EUROPÄISCHES KOMITEE FÜR NORMUNG

CEN-CENELEC Management Centre: Rue de la Science 23, B-1040 Brussels
© 2020 CEN All rights of exploitation in any form and by any means reserved Ref. No. EN 6057:2020 E
worldwide for CEN national Members.

Contents
Page
European foreword . 3
Introduction . 4
1 Scope . 5
2 Normative references . 5
3 Terms, definitions and symbols . 6
4 Requirements . 6
4.1 Configuration, dimensions, tolerances and mass . 6
4.2 Surface roughness . 9
4.3 Material . 9
4.4 Surface treatment . 9
4.5 Loads and clearance . 10
4.6 Right or left hand thread . 10
4.7 Loads . 10
4.8 Clearance . 11
4.9 Temperature range and lubricant . 11
5 Designation. 12
6 Marking . 12
7 Technical specification . 12
8 Quality management systems . 12
Annex A (normative) Verification of fatigue loads . 13
A.1 Standard rod-end fatigue spectrum . 13
A.2 Method . 13
Bibliography . 15

European foreword
This document (EN 6057:2020) 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-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 April 2021, and conflicting national standards shall be
withdrawn at the latest by April 2021.
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.
According to the CEN-CENELEC Internal Regulations, the national standards organizations of the
following countries are bound to implement this European Standard: Austria, Belgium, Bulgaria,
Croatia, Cyprus, Czech Republic, Denmark, Estonia, Finland, Former Yugoslav Republic of Macedonia,
France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta,
Netherlands, Norway, Poland, Portugal, Romania, Serbia, Slovakia, Slovenia, Spain, Sweden, Switzerland,
Turkey and the United Kingdom.
Introduction
This document is published at edition P2. Former P1 and drafts may exist of Airbus development only
but without any ASD-STAN official publication. In consequence configuration management
discrepancies with these unofficial documents are under Airbus responsibility.
1 Scope
This European standard specifies the characteristics of adjustable rod-ends consisting of:
— a spherical plain bearing, metal to metal, in corrosion resisting steel, wide series (EN 4265)
— a rod-end with internal threaded shank
They are intended for use in fixed or moving parts of the aircraft structure and their control
mechanisms.
2 Normative references
The following documents are referred to in the text in such a way that some or all of their content
constitutes requirements of this document. For dated references, only the edition cited applies. For
undated references, the latest edition of the referenced document (including any amendments) applies.
EN 2133, Aerospace series — Cadmium plating of steels with specified tensile strength ≤ 1450 MPa,
copper, copper alloys and nickel alloys
EN 2424, Aerospace series — Marking of aerospace products
EN 4265, Aerospace series — Bearing sperical plain, metal-to-metal in corrosion resisting steel — Wide
series — Dimensions and loads — Inch series
EN 6099, Aerospace series — Rod-end with plain bearing — Technical specification
ISO 1132-1, Rolling bearings — Tolerances — Definitions
ISO 3161, Aerospace — UNJ threads — General requirements and limit dimensions
ISO 8074, Aerospace — Surface treatment of austenitic stainless steel parts
MIL-PRF-23827, Grease, aircraft and instrument, gear and actuator screw, NATO Code Nummer G-354,
metric
MIL-PRF-46010, Lubricant, solid film, heat cured, corrosion-inhibiting
MIL-PRF-81322, Grease, aircraft, general purpose, wide temperature range
SAE AMS 5643, Steel, corrosion resistant, bars, wire, forgings, tubing, and rings 16Cr-4.0Ni-0.30(Cb+Ta)-
4.0Cu solution heat treated, precipitation hardenable
TR 4475, Aerospace series — Bearings and mechanical transmissions for airframe applications —
Vocabulary
1 Published as ASD-STAN Prestandard at the date of publication of this standard by AeroSpace and Defence
Industries Association o
...