EN 6133:2019

SLOVENSKI STANDARD
01-julij-2019
Aeronavtika - Končnik z očesom in ležajem po EN 6096, s samomazalno oblogo iz
korozijsko odpornega jekla, z zelo velikim notranjim obročem in navojno ročico -
Mere in obremenitve - Palčne mere
Aerospace series - Rod-end, with bearing per EN 6096, with self-lubricating liner in
corrosion resisting steel, extra wide inner ring, external threaded shank - Dimensions
and loads - Inch series
Luft- und Raumfahrt - Ösenkopf mit Gelenklager nach EN 6096 mit selbstschmierender
Beschichtung aus korrosionsbeständigen Stahl, extra breiter Innenring, mit
Aussengewinde - Maße und Belastungen, Inch Reihe
Série aérospatiale - Embout à rotule lisse selon EN 6096 en acier inoxydable et garniture
autolubrifiante Bague interne extra large filetage extérieur - Dimensions et charges -
Série en inches
Ta slovenski standard je istoveten z: EN 6133:2019
ICS:
49.035 Sestavni deli za letalsko in Components for aerospace
vesoljsko gradnjo construction
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.

EN 6133
EUROPEAN STANDARD
NORME EUROPÉENNE
May 2019
EUROPÄISCHE NORM
ICS 49.035
English Version
Aerospace series - Rod-end, with bearing per EN 6096,
with self-lubricating liner in corrosion resisting steel, extra
wide inner ring, external threaded shank - Dimensions and
loads - Inch series
Série aérospatiale - Embout à rotule lisse suivant EN Luft- und Raumfahrt - Ösenkopf mit Gelenklager nach
6096, en acier résistant à la corrosion, à garniture EN 6096 mit selbstschmierender Beschichtung aus
autolubrifiante, bague intérieure extra large, avec korrosionsbeständigen Stahl, extra breiter Innenring,
filetage extérieur - Dimensions et charges - Série en mit Außengewinde - Maße und Belastungen, Inch
inches Reihe
This European Standard was approved by CEN on 5 November 2018.

CEN members are bound to comply with the CEN/CENELEC Internal Regulations which stipulate the conditions for giving this
European Standard the status of a national standard without any alteration. Up-to-date lists and bibliographical references
concerning such national standards may be obtained on application to the CEN-CENELEC Management Centre or to any CEN
member.
This European Standard exists in three official versions (English, French, German). A version in any other language made by
translation under the responsibility of a CEN member into its own language and notified to the CEN-CENELEC Management
Centre has the same status as the official versions.

CEN members are the national standards bodies of Austria, Belgium, Bulgaria, Croatia, Cyprus, Czech Republic, Denmark, Estonia,
Finland, Former Yugoslav Republic of Macedonia, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania,
Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Romania, Serbia, Slovakia, Slovenia, Spain, Sweden, Switzerland,
Turkey and United Kingdom.
EUROPEAN COMMITTEE FOR STANDARDIZATION
COMITÉ EUROPÉEN DE NORMALISATION

EUROPÄISCHES KOMITEE FÜR NORMUNG

CEN-CENELEC Management Centre: Rue de la Science 23, B-1040 Brussels
© 2019 CEN All rights of exploitation in any form and by any means reserved Ref. No. EN 6133:2019 E
worldwide for CEN national Members.

Contents
Page
European foreword . 3
Introduction . 4
1 Scope . 5
2 Normative references . 5
3 Terms, definitions and symbols . 6
4 Requirements . 6
4.1 Configuration, dimensions, tolerances and mass . 6
4.2 Surface roughness . 6
4.3 Right or left hand thread . 10
4.4 With or without longitudinal groove . 10
4.5 Materials . 10
4.6 Surface treatment . 10
4.7 Loads . 11
4.8 Starting torque values . 12
4.9 Temperature range . 12
5 Designation. 13
6 Marking . 13
7 Technical specification . 13
8 Quality management system . 13
Annex A (normative) Verification of fatigue loads . 14
A.1 Standard rod-end fatigue spectrum . 14
A.2 Method . 14
Annex B (informative) Standard evolution form . 15
Bibliography . 16

European foreword
This document (EN 6133:2019) has been prepared by the Aerospace and Defence Industries
Association of Europe - Standardization (ASD-STAN).
After enquiries and votes carried out in accordance with the rules of this Association, this Standard has
received the approval of the National Associations and the Official Services of the member countries of
ASD, prior to its presentation to CEN.
This European Standard shall be given the status of a national standard, either by publication of an
identical text or by endorsement, at the latest by November 2019 and conflicting national standards
shall be withdrawn at the latest by November 2019.
Attention is drawn to the possibility that some of the elements of this document may be the subject of
patent rights. CEN shall not be held responsible for identifying any or all such patent rights.
According to the CEN-CENELEC Internal Regulations, the national standards organizations of the
following countries are bound to implement this European Standard: Austria, Belgium, Bulgaria,
Croatia, Cyprus, Czech Republic, Denmark, Estonia, Finland, Former Yugoslav Republic of Macedonia,
France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta,
Netherlands, Norway, Poland, Portugal, Romania, Serbia, Slovakia, Slovenia, Spain, Sweden, Switzerland,
Turkey and the United Kingdom.
Introduction
This document is published at edition P2. Former P1 and drafts may exist of Airbus development only
but without any ASD-STAN official publication. In consequence configuration management
discrepancies with these unofficial documents are under Airbus responsibility.
1 Scope
This European standard specifies the characteristics of adjustable rod-ends consisting of:
— a self-aligning spherical plain bearing with self-lubricating liner per EN 6096;
— a rod-end with threaded shank with an optional longitudinal groove for locking purposes.
They are intended for use in fixed or moving parts of the aircraft structure and their control
mechanisms.
2 Normative references
The following documents are referred to in the text in such a way that some or all of their content
constitutes requirements of this document. For dated references, only the edition cited applies. For
undated references, the latest edition of the referenced document (including any amendments) applies.
EN 2068, Aerospace series — Rod ends with self-lubricating self-aligning bearings — Technical
specification
EN 2133, Aerospace series — Cadmium plating of steels with specified tensile strength ≤ 1 450 MPa,
copper, copper alloys and nickel alloys
EN 2424, Aerospace series — Marking of aerospace products
EN 6096, Aerospace series — Bearing, spherical plain with self-lubricating liner, extra wide inner ring in
corrosion resisting steel — Dimensions and loads — Inch series
ISO 1132-1, Rolling bearings — Tolerances — Part 1: Terms and definitions
ISO 3161, Aerospace — UNJ threads — General requirements and limit dimensions
ISO 8074, Aerospace — Surface treatment of austenitic stainless steel parts
NAS 559, Lock-rod end (key type)
TR 4475, Bearings and mechanical transmissions for airframe applications — Vocabulary
SAE AMS 5643, Steel, corrosion resistant, bars wire, forgings, tubing and rings
16Cr-4.0Ni-0.30(Cb+Ta)-4.0Cu solution heat treated, precipitation hardenable

1 Published by: Aerospace Industries Association of America, Inc. (AIA), 1250 Eye Street, N.W., Washington, D.C.
20005-3924, USA.
2 Published as ASD-STAN Technical Report at the date of publication of this European standard by AeroSpace
and Defence industries Association of Europe – Standardization (ASD-STAN) (www.asd-stan.org).
3 Terms, definitions and symbols
For the purposes of this document, the terms and definitions given in TR 4475 apply.
ISO and IEC maintain terminological databases for use in standardization at the following addresses:
— ISO Online browsing platform: available at http://www.iso.org/obp
— IEC Electropedia: available at http://www.electropedia.org/
Symbols of limit deviations are in accordance with definitions of ISO 1132-1.
α maximum angle of tilt of the outer ring with respect to the inner ring, with the spherical surface
of the outer ring being completely in contact with the inner ring
C permissible static radial load
s
C push out loads
p
single plane mean bore diameter deviation
∆
dmp
∆ deviation of a single bore diameter
ds
C fatigue loads
f
4 Requirements
4.1 Configuration, dimensions, tolerances and mass
See Figure 1 and Table 1.
Table 1: Dimensions and tolerances are expressed in millimeters (inches).
Figure 1: Dimensions and tolerances for Ra max. are expressed in μm (μin).
Dimensions and tolerances are measured after surface treatment.
4.2 Surface roughness
In accordance with Figure 1.
Surface roughness is measured before surface treatment.
Key
a
1 Marking
According to ISO 3353
b
2 Type code D Thread, pitch diameter
c
3 Type code E Groove as per NAS 559
d
Usable length for groove
e
TFE – liner
Figure 1 — Configuration
Table 1 — Dimensions, tolerances and mass (1 of 2)
∅D
b
∅d b b l
∅d ∅d B C ∅D2 ∅D
3 1 2 1
Type of
Diameter
thread
0 0 +0,254 0 0 +0,127
a
Limit deviation ±0,254
code UNIJF-3A
−0,203 −0,05 0 −0,203 −0,127 0
Bearing
diameter
(0 (0 (+0.010 (0 (0 (+0.005
Δ Δ
nominal max. (±0.010)
dmp ds
−0.008) −0.002) 0) −0.008) −0.0050) 0)
7,249 4,826 5,232 12,700 5,588 8,000 14,288 6,604 1,575 38,100
03 0.3125-24
(0.2854) (0.1900) (0.206) (0.500) (0.220) (0.315) (0.5625) (0.2600) (0.062) (1.500)
8,837 6,350 6,756 15,062 6,731 9,700 18,796 7,899 49,225
04 0.3750-24
(0.3479) (0.2500) (0.266) (0.593) (0.265) (0.382) (0.7400) (0.3110) (1.938)

7,938 8,331 12,850
(0.3125) (0.328) (0.506)
10,287 20,650 23,012 9,398 53,980
2,362
0.4375-20
(0.4050) (0.813) (0.9060) (0.3700) (2.125)
9,525 9,931 13,250 (0.093)
9,017
(0.3750) (0.391) (0.522)
0 (0.355)
−0,013
11,875 11,113 11,506 22,225 15,540 25,400 11,074 61,925
07 0.5000-20
(0.4675) (0.4375) (0.453) (0.875) (0.612) (1.0000) (0.4360) (2.438)
0 (0
−0.0005)
14,958 12,700 −0,013 13,106 23,800 10,439 18,290 28,575 13,741 66,675
08 0.6250-18
(0.5889) (0.5000) (0.516) (0.937) (0.411) (0.720) (1.1250) (0.5410) (2.625)
(0
3,175
−0.0005) (0.125)
18,019 15,875 16,281 30,480 14,656 21,540 34,925 16,840 73,025
10 0.7500-16
(0.7094) (0.6250) (0.641) (1.200) (0.577) (0.845) (1.3750) (0.6630) (2.875)

19,050 19,456 32,512 16,002 24,260 39,688 19,736 85,725
(0.7500) (0.766) (1.280) (0.630) (0.955) (1.5625) (0.7770) (3.375)
21,046 3,962
0.8750-14
(0.8286) (0.156)
22,225 22,631 35,560 16,129 28,300 44,450 95,250
(0.8750) (0.891) (1.400) (0.635) (1.114) (1.7500) (3.750)

25,400 25,806 21,488 32,050 53,975
...