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

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

31-12-2013

Publisher

British Standards Institution

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

Defines 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.

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 high 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 codes A and C grease is limited to 121 °C.

Committee	ACE/12
DevelopmentNote	Supersedes 09/30204325 DC. (01/2014)
DocumentType	Standard
Pages	16
PublisherName	British Standards Institution
Status	Current
Supersedes	09/30204325 DC : 0

Standards	Relationship
EN 4156:2013	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
EN 2067:1996/AC:1996	AEROSPACE SERIES - ROD ENDS WITH SELF-ALIGNING BALL BEARINGS - TECHNICAL SPECIFICATION
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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BS EN 4156:2013

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

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