BS EN 2588:2006
Aerospace series - Bearings, spherical plain in corrosion resisting steel with assembly slots - Dimensions and loads

Standard No.
BS EN 2588:2006
Release Date
2006
Published By
British Standards Institution (BSI)
Latest
BS EN 2588:2006
Replace
BS EN 2588:1992
Scope
This standard specifies the characteristics of spherical plain bearings in corrosion resisting steel, with assembly slots, metric series, with or without lubrication holes and groove, intended for use in fixed or moving parts of aircraft structure and control mechanisms. They may be used in the temperature range from – 54 °C to 150 °C. However, as they are lubricated with the following greases (see EN 2337): - ester type very high pressure grease (code letter A), operating range from – 73 °C to 121 °C or, - synthetic hydrocarbon type very high pressure grease general purpose (code letter B), operating range from – 54 °C to 177 °C. Their field of application when lubricated with grease code letter A is limited to 121 °C.

BS EN 2588:2006 Referenced Document

  • EN 2030 Aerospace series - Steel X105CrMo17 (1.3544) - Hardened and tempered - Bars - De = 150 mm*2024-04-18 Update
  • EN 2337 Aerospace series - Spherical plain bearings - Technical specification
  • EN 2424 Aerospace series - Marking of aerospace products*2008-05-01 Update
  • ISO 1132-1 Rolling bearings - Tolerances - Part 1: Terms and definitions
  • ISO 8075 Aerospace; Surface treatment of hardenable stainless steel parts

BS EN 2588:2006 history

  • 2006 BS EN 2588:2006 Aerospace series - Bearings, spherical plain in corrosion resisting steel with assembly slots - Dimensions and loads
  • 0000 BS EN 2588:1992
Aerospace series - Bearings, spherical plain in corrosion resisting steel with assembly slots - Dimensions and loads



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