Aerospace series - Rod-ends, adjustable self-aligning plain bearing with self-lubricating liner and threaded shank in corrosion resisting steel - Dimensions and loads

This standard specifies the characteristics of adjustable rod-ends consisting of:
   a self-aligning ball bearing with self-lubricating liner, EN 2501,
                a rod-end with threaded shank consisting of:
   a circumferential groove to identity location,
   an optional longitudinal groove for locking purposes.
These rod-ends are intended for use with flying control rods or rods for aerospace structures. They shall be used within the temperature range from: - 55 °C to 163 °C.

Luft- und Raumfahrt - Ösenkopf, einstellbar mit Gelenklager mit selbstschmierender Beschichtung und Gewindeschaft aus korrosionsbeständigem Stahl - Maße und Belastungen

Diese Norm legt die Eigenschaften von einstellbaren Ösenköpfen mit:
   einem Gelenklager mit selbstschmierender Beschichtung nach EN 2501;
   einem Ösenkopf mit Gewindeschaft, der:
   mit einer Ringnut zur Kontrolle der Einschraubtiefe versehen ist;
   eine Längsnut zur Sicherung aufweisen kann;
fest.
Diese Ösenköpfe sind für Bediengestänge für Flugsteuerungen oder für Strukturstangen von Luftfahrzeugen vorgesehen. Sie sind für den Ersatz im Temperaturbereich von -55 °C bis 163 °C vorgesehen.

Série aérospatiale - Embouts réglables à rotule, à garniture autolubrifiante, à tige filetée, en acier résistant à la corrosion - Dimensions et charges

Aeronavtika - Drsni zgibi, nastavljivi drsni ležaji s samomazalno oblogo in navojnim steblom, iz korozijsko odpornega jekla - Mere in nosilnosti

General Information

Status
Published
Publication Date
13-Jun-2006
Withdrawal Date
30-Dec-2006
Technical Committee
ASD-STAN - Aerospace
Drafting Committee
ASD-STAN/D 3 - Mechanical
Current Stage
9093 - Decision to confirm - Review Enquiry
Start Date
31-May-2017
Completion Date
28-Jan-2026

Relations

Effective Date
28-Jan-2026
Effective Date
28-Jan-2026
Effective Date
28-Jan-2026
Effective Date
28-Jan-2026
Effective Date
28-Jan-2026
Effective Date
28-Jan-2026
Effective Date
28-Jan-2026
Effective Date
28-Jan-2026

Overview

EN 4198:2006 - Aerospace series - Rod-ends, adjustable self-aligning plain bearing with self-lubricating liner and threaded shank in corrosion resisting steel - Dimensions and loads - defines the dimensional, material and load characteristics for adjustable rod-ends used in aerospace flying control rods and structural rod applications. The standard applies to rod-ends that combine a self-aligning ball bearing with a self-lubricating liner (per EN 2501) and a threaded shank in corrosion resisting steel, and covers design features such as identification grooves and optional locking grooves. Use temperature range is −55 °C to 163 °C.

Key topics and requirements

  • Scope and configuration
    • Specifies rod-end assemblies: self-aligning plain bearing (EN 2501) + threaded rod-end body.
    • Identifying features: circumferential groove (identification) and optional longitudinal groove (for locking).
    • Groove(s) are to be painted red for identification.
  • Dimensions and tolerances
    • Detailed dimensional tables and tolerances (Figure 1, Tables 1 & 2) define diameters, thread lengths, and form limits.
    • Surface roughness values given before surface treatment.
  • Materials and hardness
    • Rod-end bodies in corrosion resisting steel per referenced aerospace steels (e.g., EN 2539 / EN 3161 family).
    • Specified hardness range for rod-end body (example: HRC 35–42).
    • Plain bearing liner per EN 2501 (self-lubricating).
  • Loads and performance
    • Permissible dynamic radial loads, axial push-out loads, starting torques and ultimate static loads are specified (numeric values provided in the standard’s load table).
    • Users must apply appropriate safety factors for permissible static loads.
  • Surface treatment & marking
    • Surface treatment options referenced to ISO 8075; marking per EN 2424 (category A).
  • Designation
    • Standard includes a clear designation/part-numbering scheme (example: EN4198L06KT) and codes for thread direction and groove options.

Applications and who uses it

  • Typical applications: flying control rods, actuator links, aerospace structural rods and mechanisms requiring self-aligning articulation.
  • Primary users:
    • Aerospace design and mechanical engineers (component selection, interface design).
    • Procurement and specification writers (calling out EN 4198 rod-ends in procurement documents).
    • QA/inspection and maintenance teams (verification of dimensions, loads, markings and corrosion-resistant treatments).
    • Manufacturers of rod-ends and bearing assemblies (product design and certification).

Related standards

  • EN 2501 - Bearings, spherical plain with self‑lubricating liner (used for the bearing element)
  • EN 2068 - Rod ends technical specification
  • EN 2424 - Marking of aerospace products
  • ISO 3353-1, ISO 5855-2, ISO 8075 - thread, tolerance and surface-treatment references

EN 4198 is essential when specifying aerospace-grade rod-ends: it ensures consistent dimensions, reliable load ratings, and compatibility with aerospace materials and marking practices.

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Frequently Asked Questions

EN 4198:2006 is a standard published by the European Committee for Standardization (CEN). Its full title is "Aerospace series - Rod-ends, adjustable self-aligning plain bearing with self-lubricating liner and threaded shank in corrosion resisting steel - Dimensions and loads". This standard covers: This standard specifies the characteristics of adjustable rod-ends consisting of: a self-aligning ball bearing with self-lubricating liner, EN 2501, a rod-end with threaded shank consisting of: a circumferential groove to identity location, an optional longitudinal groove for locking purposes. These rod-ends are intended for use with flying control rods or rods for aerospace structures. They shall be used within the temperature range from: - 55 °C to 163 °C.

This standard specifies the characteristics of adjustable rod-ends consisting of: a self-aligning ball bearing with self-lubricating liner, EN 2501, a rod-end with threaded shank consisting of: a circumferential groove to identity location, an optional longitudinal groove for locking purposes. These rod-ends are intended for use with flying control rods or rods for aerospace structures. They shall be used within the temperature range from: - 55 °C to 163 °C.

EN 4198:2006 is classified under the following ICS (International Classification for Standards) categories: 49.035 - Components for aerospace construction. The ICS classification helps identify the subject area and facilitates finding related standards.

EN 4198:2006 has the following relationships with other standards: It is inter standard links to EN 2424:2008, EN 2068:1996, EN 3161:2007, EN 13848-1:2003+A1:2008, EN 2501:1988, EN 13522:2001, EN 2755:2021, CEN/TS 13130-12:2005. Understanding these relationships helps ensure you are using the most current and applicable version of the standard.

EN 4198:2006 is available in PDF format for immediate download after purchase. The document can be added to your cart and obtained through the secure checkout process. Digital delivery ensures instant access to the complete standard document.

Standards Content (Sample)


2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.Aeronavtika - Drsni zgibi, nastavljivi drsni ležaji s samomazalno oblogo in navojnim steblom, iz korozijsko odpornega jekla - Mere in nosilnostiLuft- und Raumfahrt - Ösenkopf, einstellbar mit Gelenklager mit selbstschmierender Beschichtung und Gewindeschaft aus korrosionsbeständigem Stahl - Maße und BelastungenSérie aérospatiale - Embouts réglables à rotule, à garniture autolubrifiante, à tige filetée, en acier résistant à la corrosion - Dimensions et chargesAerospace series - Rod-ends, adjustable self-aligning plain bearing with self-lubricating liner and threaded shank in corrosion resisting steel - Dimensions and loads49.035Sestavni deli za letalsko in vesoljsko gradnjoComponents for aerospace constructionICS:Ta slovenski standard je istoveten z:EN 4198:2006SIST EN 4198:2009en,de01-september-2009SIST EN 4198:2009SLOVENSKI
STANDARD
EUROPEAN STANDARDNORME EUROPÉENNEEUROPÄISCHE NORMEN 4198June 2006ICS 49.035 English VersionAerospace series - Rod-ends, adjustable self-aligning plainbearing with self-lubricating liner and threaded shank incorrosion resisting steel - Dimensions and loadsSérie aérospatiale - Embouts réglables à rotule, à garnitureautolubrifiante, à tige filetée, en acier résistant à lacorrosion - Dimensions et chargesLuft- und Raumfahrt - Ösenkopf, einstellbar mitGelenklager mit selbstschmierender Beschichtung undGewindeschaft aus korrosionsbeständigem Stahl - Maßeund BelastungenThis European Standard was approved by CEN on 20 April 2006.CEN members are bound to comply with the CEN/CENELEC Internal Regulations which stipulate the conditions for giving this EuropeanStandard the status of a national standard without any alteration. Up-to-date lists and bibliographical references concerning such nationalstandards 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 translationunder the responsibility of a CEN member into its own language and notified to the Central Secretariat has the same status as the officialversions.CEN members are the national standards bodies of Austria, Belgium, Cyprus, Czech Republic, Denmark, Estonia, Finland, France,Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Romania,Slovakia, Slovenia, Spain, Sweden, Switzerland and United Kingdom.EUROPEAN COMMITTEE FOR STANDARDIZATIONCOMITÉ EUROPÉEN DE NORMALISATIONEUROPÄISCHES KOMITEE FÜR NORMUNGManagement Centre: rue de Stassart, 36
B-1050 Brussels© 2006 CENAll rights of exploitation in any form and by any means reservedworldwide for CEN national Members.Ref. No. EN 4198:2006: ESIST EN 4198:2009
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