This standard was last reviewed and confirmed in 2015. Therefore this version remains current.
Specifies the characteristics of spherical plain bearings of the inch 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 structure and control mechanisms at temperatures of -55 °C to +163 °C.
Status: PublishedPublication date: 1995-07
Edition: 1Number of pages: 10
Technical Committee: ISO/TC 20 Aircraft and space vehicles
- ICS :
- 49.035 Components for aerospace construction
This standard contributes to the following Sustainable Development Goal:
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|std 1 61|
|std 2 61||Paper|
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Stage: 90.60 (Under review)
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