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
Buy this standard
|std 1 61|
|std 2 61||Paper|