Abstract

Specifies the characteristics of spherical plain bearings of the metric series (without rolling elements) in corrosion-resisting steel with self-lubricating liner for elevated loads at ambient temperature, for use in fixed and moving parts of the aircraft structur and control mechanisms at temperatures of -55 °C to +163 °C.


General information 

  • Status
     :  Withdrawn
    Publication date
     : 1995-07
  • Edition
     : 1
    Number of pages
     : 5
  • Technical Committee
     : ISO/TC 20 Aircraft and space vehicles
  • ICS
     :
    49.035 Components for aerospace construction

Sustainable Development Goals

This standard contributes to the following Sustainable Development Goal:

9
Industry, Innovation and Infrastructure

Life cycle


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