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CEN
EN 3541:1992

EN 3541:1992

Current

Current

The latest, up-to-date edition.

Aerospace series - Rod ends, adjustable, self-aligning ball bearing with threaded shank - Dimensions, torques, clearances and loads

Published date

01-04-1992

Publisher

Comite Europeen de Normalisation

Foreword
1 Scope
2 Field of application
3 Normative references
4 Symbols
5 Required characteristics
6 Designation
7 Marking
8 Technical specification

This standard specifies the characteristics of adjustable rod ends with self-aligning ball bearing and threaded shank. They consist of: 1) a rod end comprising circumferential groove to identify location, either seals or shields, an optional longitudinal groove for locking purpose; 2) an inner ring with balls

Committee
ASD-STAN
DocumentType
Standard
PublisherName
Comite Europeen de Normalisation
Status
Current

Standards Relationship
UNE-EN 3541:1992 Identical
NBN EN 3541 : 1992 Identical
DIN EN 3541:1992-06 Identical
SNV DIN EN 3541 : 1992 Identical
BS EN 3541:1992 Identical
NS EN 3541 : 1ED 1992 Identical
NF EN 3541 : 1992 Identical
NEN EN 3541 : 1992 Identical
UNI EN 3541 : 1992 Identical
I.S. EN 3541:1993 Identical
PN EN 3541 : 1999 Identical

DIN EN 2644:1998-06 AEROSPACE SERIES - ROD ASSEMBLIES FOR FLIGHT CONTROLS - TECHNICAL SPECIFICATION
BS EN 2644:1998 Rod assemblies for flight controls. Technical specification
EN 2644 : 1998 AEROSPACE SERIES - ROD ASSEMBLIES FOR FLIGHT CONTROLS - TECHNICAL SPECIFICATION

ISO 1132:1980 Rolling bearings — Tolerances — Definitions
PREN 2031 : 1 AEROSPACE SERIES - STEEL FE-PL31 - HARDENED AND TEMPERED - BARS
ISO 5855-2:1999 Aerospace MJ threads Part 2: Limit dimensions for bolts and nuts
PREN 2067 : 1989 ROD-ENDS, WITH SELF-ALIGNING BALL BEARING - TECHNICAL SPECIFICATION
PREN 2135 : 200P1 AEROSPACE SERIES - STEEL FE-PL61 - CARBURIZED, HARDENED AND TEMPERED - BAR D[E] <= 40 MM
ISO 3353:1992 Aerospace — Rolled threads for bolts — Lead and runout requirements
PREN 2133 : 200P1 AEROSPACE SERIES - CADMIUM PLATING OF STEELS WITH SPECIFIED TENSILE STRENGTH <= 1450 MPA, COPPER, COPPER ALLOYS AND NICKEL ALLOYS

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