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EN 4156:2013

Current

Current

The latest, up-to-date edition.

Aerospace series - Rod ends, with self-aligning double row ball bearings and threaded shank in steel - Inner ring and balls in corrosion resisting steel - Dimensions and loads - Inch series

Published date

18-12-2013

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Foreword
1 Scope
2 Normative references
3 Symbols and definitions
4 Required characteristics
5 Qualification
6 Designation
7 Marking
8 Technical specification

This European Standard specifies the characteristics of adjustable rod ends with self-aligning double row ball bearing and threaded shank in steel, inner ring and balls in corrosion resisting steel.They consist of:a rod end comprising:either seals or shields;an optional longitudinal groove for locking purpose;an inner ring with balls.These rod ends are intended for use with flight control rods or rods for aerospace structures.They are intended to be used in the temperature range: – 54 °C to 150 °C.However, being lubricated with the following greases:very high pressure grease, ester type (code A), operational range – 73 °C to 121 °C according MIL PRF 23827 type IIvery high pressure grease, synthetic hydrocarbons, general purpose (code B), operational range  54 °C to 177 °C (see EN 2067), according MIL-PRF-81322.very hight pressure grease, lithium type (code C) operational range – 73 °C to 121 °C according MIL PRF-23827 type I.Their field of application when lubricated with code A grease is limited to 121 °C.

Committee
ASD-STAN
DevelopmentNote
Supersedes PREN 4156. (12/2013)
DocumentType
Standard
PublisherName
Comite Europeen de Normalisation
Status
Current
Supersedes

Standards Relationship
NF EN 4156 : 2014 Identical
NBN EN 4156 : 2014 Identical
NEN EN 4156 : 2014 Identical
NS EN 4156 : 2013 Identical
I.S. EN 4156:2013 Identical
PN EN 4156 : 2014 Identical
SN EN 4156:2014 Identical
UNI EN 4156 : 2014 Identical
UNE-EN 4156:2013 Identical
BS EN 4156:2013 Identical
DIN EN 4156:2014-03 Identical

EN 2133:2010 Aerospace series - Cadmium plating of steels with specified tensile strength ≤ 1 450 MPa, copper, copper alloys and nickel alloys
PREN 2135 : 200P1 AEROSPACE SERIES - STEEL FE-PL61 - CARBURIZED, HARDENED AND TEMPERED - BAR D[E] <= 40 MM
EN 2030:2013 Aerospace series - Steel X105CrMo17 (1.3544) - Hardened and tempered - Bars - De ≤ 150 mm
MIL-PRF-81322 Revision G:2005 GREASE, AIRCRAFT, GENERAL PURPOSE, WIDE TEMPERATURE RANGE, NATO CODE G-395
ISO 1132-1:2000 Rolling bearings — Tolerances — Part 1: Terms and definitions
ISO 8075:1985 Aerospace Surface treatment of hardenable stainless steel parts
EN 2424:2008 Aerospace series - Marking of aerospace products
ISO 3353-1:2002 Aerospace Lead and runout threads Part 1: Rolled external threads
ISO 3161:1999 Aerospace — UNJ threads — General requirements and limit dimensions

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