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.
Status: PublishedPublication date: 1995-07
Edition: 1Number of pages: 5
Technical Committee: ISO/TC 20 Aircraft and space vehicles
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|std 1 38|
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