EN 4035:2006
(Main)Aerospace series - Rod ends, adjustable with self-aligning double row ball bearing in corrosion resisting steel, reduced internal radial clearance and threaded shank in titanium alloy - Dimensions and loads
Aerospace series - Rod ends, adjustable with self-aligning double row ball bearing in corrosion resisting steel, reduced internal radial clearance and threaded shank in titanium alloy - Dimensions and loads
This standard specifies the characteristics of adjustable rod ends with self-aligning double row ball bearing in corrosion resisting steel with reduced internal radial clearance and threaded shank in titanium alloy, designed to withstand only slow rotations and oscillations under load.
They consist of:
- a rod end comprising:
circumferential groove to identify location;
either seals or shields;
an optional longitudinal groove for locking purpose;
- an inner ring with balls.
These rod ends are intended for use with flight control rods or rods for aerospace structures.
They are intended to be used in the temperature range: - 54 °C to 150 °C.
However, being lubricated with the following greases:
- very high pressure grease, ester type (code A), operational range - 73 °C to 121 °C or
- very high pressure grease, synthetic hydrocarbons, general purpose (code B), operational range - 54 °C to 177 °C (see EN 2067),
their field of application when lubricated with code A grease is limited to 121 °C.
Luft- und Raumfahrt - Einstellbare Ösenköpfe mit zweireihigem Pendelkugellager aus korrosionsbeständigem Stahl, reduzierte radiale Lagerluft und Gewindeschaft aus Titanlegierung - Maße und Belastungen
Diese Norm legt die Eigenschaften von einstellbaren Ösenköpfen mit zweireihigem Pendelkugellager aus korrosionsbeständigem Stahl, mit reduzierter radialer Lagerluft und Gewindeschaft aus Titanlegierung fest, die so ausgelegt sind, dass sie unter Belastung nur langsamen Dreh- und Kippbewegungen standhalten.
Sie bestehen aus:
- einem Ösenkopf, der:
- mit einer Ringnut zur Kontrolle der Einschraubtiefe versehen ist;
- mit Dicht- oder Deckscheiben ausgerüstet ist;
- eine Längsnut zur Sicherung aufweisen kann;
- einem Innenring mit Kugeln.
Diese Ösenköpfe sind für Bediengestänge für Flugsteuerungen oder für Strukturstangen von Luftfahrzeugen bestimmt.
Sie sind für den Einsatz im Temperaturbereich von - 54 °C bis 150 °C bestimmt.
Da sie jedoch mit folgenden Fetten geschmiert werden:
- Hochdruckfett auf Esterbasis (Kennbuchstabe A); Betriebstemperaturbereich - 73 °C bis 121 °C oder
- Hochdruckfett auf der Basis von synthetischen Kohlenwasserstoffen zur allgemeinen Verwendung (Kennbuchstabe B), Betriebstemperaturbereich - 54 °C bis 177 °C (nach EN 2067),
ist ihr Anwendungsbereich bei Schmierung mit Fett mit dem Kennbuchstaben A auf 121 °C eingeschränkt.
Série aérospatiale - Embouts réglables à rotule sur deux rangées de billes en acier résistant à la corrosion, jeu radial réduit et à tige filetée en alliage de titane - Dimensions et charges
Aeronavtika - Nastavljivi drsni zgibi s samovarovalnim dvorednim nihalnim krogličnim ležajem iz korozijsko odpornega jekla, z zmanjšanim radialnim ohlapom ležaja in navojnim steblom iz titanove zlitine - Mere in nosilnosti
General Information
- Status
- Withdrawn
- Publication Date
- 02-May-2006
- Withdrawal Date
- 20-Jan-2026
- Technical Committee
- ASD-STAN - Aerospace
- Drafting Committee
- ASD-STAN/D 3 - Mechanical
- Current Stage
- 9960 - Withdrawal effective - Withdrawal
- Start Date
- 10-Mar-2021
- Completion Date
- 28-Jan-2026
Relations
- Effective Date
- 17-Mar-2021
- 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
- Effective Date
- 28-Jan-2026
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Frequently Asked Questions
EN 4035:2006 is a standard published by the European Committee for Standardization (CEN). Its full title is "Aerospace series - Rod ends, adjustable with self-aligning double row ball bearing in corrosion resisting steel, reduced internal radial clearance and threaded shank in titanium alloy - Dimensions and loads". This standard covers: This standard specifies the characteristics of adjustable rod ends with self-aligning double row ball bearing in corrosion resisting steel with reduced internal radial clearance and threaded shank in titanium alloy, designed to withstand only slow rotations and oscillations under load. They consist of: - a rod end comprising: circumferential groove to identify location; either seals or shields; an optional longitudinal groove for locking purpose; - an inner ring with balls. These rod ends are intended for use with flight control rods or rods for aerospace structures. They are intended to be used in the temperature range: - 54 °C to 150 °C. However, being lubricated with the following greases: - very high pressure grease, ester type (code A), operational range - 73 °C to 121 °C or - very high pressure grease, synthetic hydrocarbons, general purpose (code B), operational range - 54 °C to 177 °C (see EN 2067), their field of application when lubricated with code A grease is limited to 121 °C.
This standard specifies the characteristics of adjustable rod ends with self-aligning double row ball bearing in corrosion resisting steel with reduced internal radial clearance and threaded shank in titanium alloy, designed to withstand only slow rotations and oscillations under load. They consist of: - a rod end comprising: circumferential groove to identify location; either seals or shields; an optional longitudinal groove for locking purpose; - an inner ring with balls. These rod ends are intended for use with flight control rods or rods for aerospace structures. They are intended to be used in the temperature range: - 54 °C to 150 °C. However, being lubricated with the following greases: - very high pressure grease, ester type (code A), operational range - 73 °C to 121 °C or - very high pressure grease, synthetic hydrocarbons, general purpose (code B), operational range - 54 °C to 177 °C (see EN 2067), their field of application when lubricated with code A grease is limited to 121 °C.
EN 4035:2006 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 4035:2006 has the following relationships with other standards: It is inter standard links to EN 4035:2021, EN 2424:2008, EN 3813:2013, EN 3289:1994, EN 2067:1996, EN 840-6:2004+A1:2008, CEN/TS 13130-12:2005, EN 2808:1997, EN 13522:2001, EN ISO 15195:2003. Understanding these relationships helps ensure you are using the most current and applicable version of the standard.
EN 4035:2006 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.QLKDOQLPWLLuft- und Raumfahrt - Einstellbare Ösenköpfe mit zweireihigem Pendelkugellager aus korrosionsbeständigem Stahl, reduzierte radiale Lagerluft und Gewindeschaft aus Titanlegierung - Maße und BelastungenSérie aérospatiale - Embouts réglables à rotule sur deux rangées de billes en acier résistant à la corrosion, jeu radial réduit et à tige filetée en alliage de titane - Dimensions et chargesAerospace series - Rod ends, adjustable with self-aligning double row ball bearing in corrosion resisting steel, reduced internal radial clearance and threaded shank in titanium alloy - Dimensions and loads49.035Sestavni deli za letalsko in vesoljsko gradnjoComponents for aerospace constructionICS:Ta slovenski standard je istoveten z:EN 4035:2006SIST EN 4035:2009en,de01-september-2009SIST EN 4035:2009SLOVENSKI
STANDARD
EUROPEAN STANDARDNORME EUROPÉENNEEUROPÄISCHE NORMEN 4035May 2006ICS 49.035 English VersionAerospace series - Rod ends, adjustable with self-aligningdouble row ball bearing in corrosion resisting steel, reducedinternal radial clearance and threaded shank in titanium alloy -Dimensions and loadsSérie aérospatiale - Embouts réglables à rotule sur deuxrangées de billes en acier résistant à la corrosion, jeu radialréduit et à tige filetée en alliage de titane - Dimensions etchargesLuft- und Raumfahrt - Einstellbare Ösenköpfe mitzweireihigem Pendelkugellager aus korrosionsbeständigemStahl, reduzierte radiale Lagerluft und Gewindeschaft ausTitanlegierung - Maße und BelastungenThis European Standard was approved by CEN on 16 March 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 4035:2006: ESIST EN 4035:2009
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