• EN 4156:2013

    Current The latest, up-to-date edition.

    Aerospace series - Rod ends, with self-aligning double row ball bearings and threaded shank in steel - Inner ring and balls in corrosion resisting steel - Dimensions and loads - Inch series

    Available format(s): 

    Language(s): 

    Published date:  18-12-2013

    Publisher:  Comite Europeen de Normalisation

    Pure ENs are not available for sale, please purchase a suitable national adoption

    Sorry this product is not available in your region.

    Add To Cart

    Table of Contents - (Show below) - (Hide below)

    Foreword
    1 Scope
    2 Normative references
    3 Symbols and definitions
    4 Required characteristics
    5 Qualification
    6 Designation
    7 Marking
    8 Technical specification

    Abstract - (Show below) - (Hide below)

    This European Standard specifies the characteristics of adjustable rod ends with self-aligning double row ball bearing and threaded shank in steel, inner ring and balls in corrosion resisting steel.They consist of:a rod end comprising: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 according MIL PRF 23827 type IIvery high pressure grease, synthetic hydrocarbons, general purpose (code B), operational range  54 °C to 177 °C (see EN 2067), according MIL-PRF-81322.very hight pressure grease, lithium type (code C) operational range – 73 °C to 121 °C according MIL PRF-23827 type I.Their field of application when lubricated with code A grease is limited to 121 °C.

    General Product Information - (Show below) - (Hide below)

    Committee ASD-STAN
    Development Note Supersedes PREN 4156. (12/2013)
    Document Type Standard
    Publisher Comite Europeen de Normalisation
    Status Current
    Supersedes

    Standards Referencing This Book - (Show below) - (Hide below)

    EN 2133:2010 Aerospace series - Cadmium plating of steels with specified tensile strength ≤ 1 450 MPa, copper, copper alloys and nickel alloys
    PREN 2135 : 200P1 AEROSPACE SERIES - STEEL FE-PL61 - CARBURIZED, HARDENED AND TEMPERED - BAR D[E] <= 40 MM
    EN 2030:2013 Aerospace series - Steel X105CrMo17 (1.3544) - Hardened and tempered - Bars - De ≤ 150 mm
    MIL-PRF-81322 Revision G:2005 GREASE, AIRCRAFT, GENERAL PURPOSE, WIDE TEMPERATURE RANGE, NATO CODE G-395
    ISO 1132-1:2000 Rolling bearings — Tolerances — Part 1: Terms and definitions
    ISO 8075:1985 Aerospace Surface treatment of hardenable stainless steel parts
    EN 2424:2008 Aerospace series - Marking of aerospace products
    EN 2067:1996/AC:1996 AEROSPACE SERIES - ROD ENDS WITH SELF-ALIGNING BALL BEARINGS - TECHNICAL SPECIFICATION
    ISO 3353-1:2002 Aerospace Lead and runout threads Part 1: Rolled external threads
    ISO 3161:1999 Aerospace — UNJ threads — General requirements and limit dimensions
    • Access your standards online with a subscription

      Features

      • Simple online access to standards, technical information and regulations
      • Critical updates of standards and customisable alerts and notifications
      • Multi - user online standards collection: secure, flexibile and cost effective