EN 4535-2:2009

Aerospace series - Bushes, flanged in aluminium alloy with self-lubricating liner, elevated load - Part 2: Dimensions and loads - Inch series

This standard specifies the characteristics of bushes flanged in aluminium alloy with self-lubricating liner
elevated load for aerospace applications.
The bushes are intended for use in fixed or moving parts of the aircraft structure and control mechanisms.
They shall be used in the temperature range - 55 °C to 121 °C.

Luft- und Raumfahrt - Buchsen mit Flansch aus Aluminiumlegierung, mit selbstschmierender Beschichtung, erhöhte Belastung - Teil 2: Maße und Belastungen - Inch-Reihe

Die vorliegende Norm legt die Eigenschaften von Buchsen mit Flansch aus Aluminiumlegierung, mit selbstschmierender Beschichtung, erhöhter Belastung, für die Anwendung in der Luft- und Raumfahrt fest.
Die Buchsen sind für den Einsatz in starren oder beweglichen Teilen der Luftfahrzeugstruktur und der Betätigungsvorrichtungen vorgesehen.
Sie sind für den Einsatz im Temperaturbereich von - 55 °C bis 121 °C bestimmt.

Série aérospatiale - Bagues à épaulement en alliage d'aluminium à garniture autolubrifiante, charge élevée - Partie 2 : Dimensions et charges - Série en inches

Aeronavtika - Puše s prirobnico iz aluminijeve zlitine s samomazalno oblogo, serija za večje obremenitve - 2. del: Mere in nosilnosti - Colski tip

General Information

• Status: Withdrawn
• Publication Date: 09-Jun-2009
• Withdrawal Date: 06-Sep-2016
• ICS: 49.035 - Components for aerospace construction
• Technical Committee: ASD-STAN - Aerospace
• Drafting Committee: ASD-STAN/D 3 - Mechanical
• Current Stage: 9093 - Decision to confirm - Review Enquiry
• Completion Date: 30-Jun-2017
• Ref Project: SIST EN 4535-2:2009 - Aerospace series - Bushes, flanged in aluminium alloy with self-lubricating liner, elevated load - Part 2: Dimensions and loads - Inch series

Relations

• Replaced By: EN 4535-2:2016 - Aerospace series - Bushes, flanged in aluminium alloy with self-lubricating liner, elevated load - Part 2: Dimensions and loads - Inch series
• Effective Date: 04-Feb-2015

Standards Content (Sample)

SLOVENSKI STANDARD
01-september-2009
$HURQDYWLND3XãHVSULUREQLFRL]DOXPLQLMHYH]OLWLQHVVDPRPD]DOQRREORJR
VHULMD]DYHþMHREUHPHQLWYHGHO0HUHLQQRVLOQRVWL&ROVNLWLS
Aerospace series - Bushes, flanged in aluminium alloy with self-lubricating liner, elevated
load - Part 2: Dimensions and loads - Inch series
Luft- und Raumfahrt - Buchsen mit Flansch aus Aluminiumlegierung, mit
selbstschmierender Beschichtung, erhöhte Belastung - Teil 2: Maße und Belastungen -
Inch Reihe
Série aérospatiale - Bagues à épaulement en alliage d'aluminium à garniture
autolubrifiante, charge élevée - Partie 2 : Dimensions et charges - Série en inches
Ta slovenski standard je istoveten z: EN 4535-2:2009
ICS:
49.025.20 Aluminij Aluminium
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.

EUROPEAN STANDARD
EN 4535-2
NORME EUROPÉENNE
EUROPÄISCHE NORM
June 2009
ICS 49.035
English Version
Aerospace series - Bushes, flanged in aluminium alloy with self-
lubricating liner, elevated load - Part 2: Dimensions and loads -
Inch series
Série aérospatiale - Bagues à épaulement en alliage Luft- und Raumfahrt - Buchsen mit Flansch aus
d'aluminium à garniture autolubrifiante, charge élevée - Aluminiumlegierung, mit selbstschmierender Beschichtung,
Partie 2 : Dimensions et charges - Série en inches erhöhte Belastung - Teil 2: Maße und Belastungen - Inch
Reihe
This European Standard was approved by CEN on 23 April 2009.
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 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 Management Centre has the same status as the
official versions.
CEN members are the national standards bodies of Austria, Belgium, Bulgaria, Cyprus, Czech Republic, Denmark, Estonia, Finland,
France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal,
Romania, Slovakia, Slovenia, Spain, Sweden, Switzerland and United Kingdom.
EUROPEAN COMMITTEE FOR STANDARDIZATION
COMITÉ EUROPÉEN DE NORMALISATION
EUROPÄISCHES KOMITEE FÜR NORMUNG
Management Centre: Avenue Marnix 17, B-1000 Brussels
© 2009 CEN All rights of exploitation in any form and by any means reserved Ref. No. EN 4535-2:2009: E
worldwide for CEN national Members.

Contents Page
Foreword . 3
1 Scope . 4
2 Normative references . 4
3 Terms and definitions . 4
4 Requirements . 4
4.1 Configuration, dimensions and mass . 4
4.2 Surface roughness . 4
4.3 Materials. 4
4.4 Surface treatment . 5
5 Designation . 20
6 Marking . 20
7 Technical specification . 20
8 Design recommendation . 20

Foreword
This document (EN 4535-2:2009) has been prepared by the Aerospace and Defence Industries Association of
Europe - Standardization (ASD-STAN).
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 December 2009, and conflicting national standards shall be withdrawn at the
latest by December 2009.
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.
Attention is drawn to the possibility that some of the elements of this document may be the subject of patent
rights. CEN [and/or CENELEC] shall not be held responsible for identifying any or all such patent rights.
This standard was reviewed by the Domain Technical Coordinator of ASD-STAN's Mechanical Domain.
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, Cyprus, Czech Republic,
Denmark, Estonia, Finland, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania,
Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Romania, Slovakia, Slovenia, Spain, Sweden,
Switzerland and the United Kingdom.
1 Scope
This standard specifies the characteristics of bushes flanged in aluminium alloy with self-lubricating liner
elevated load for aerospace applications.
The bushes are intended for use in fixed or moving parts of the aircraft structure and control mechanisms.
They shall be used in the temperature range – 55 °C to 121 °C.
2 Normative references
The following referenced documents are indispensable for the application 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 2101, Aerospace series — Chromic acid anodizing of aluminium and wrought aluminium alloys
EN 2284, Aerospace series — Sulphuric acid anodizing of aluminium and wrought aluminium alloys
EN 2311, Aerospace series — Bushes with self-lubricating liner — Technical specification
EN 2318, Aerospace series — Aluminium alloy AL-P2024- — T3511 — Extruded bars and sections — 1,2 mm ≤
a or D ≤ 150 mm
EN 2424, Aerospace series — Marking of aerospace products
1)
TR 4475, Aerospace series — Bearings and mechanical transmissions for airframe applications — Vocabulary
ISO 2768-1, General tolerances — Part 1: Tolerances for linear and angular dimensions without individual
tolerance indications
3 Terms and definitions
For the purposes of this document, the terms and definitions given in TR 4475 apply.
4 Requirements
4.1 Configuration, dimensions and mass
According to Figures 1 and 2 and Tables 1, 2, 4 and 5. Dimensions apply after surface treatment. Dimensions
and tolerances are expressed in millimetres (inches).
General tolerances shall be ISO 2768-m in accordance with ISO 2768-1.
4.2 Surface roughness
According to Figures 1 and 2.
4.3 Materials
Bush: Aluminium alloy according to EN 2318.

1) Published as ASD Technical Report at the date of publication of this standard.
Liner: Self-lubricating wear resistant material consistent with the requirements of EN 2311.
4.4 Surface treatment
Code R: Chromic acid anodizing according to EN 2101, type A or Sulphuric acid anodizing according to EN 2284,
type A.
Key
a
Chamfer machined before bonding
b
Chamfer or radius at manufacturers option
c
Chamfer machined after bonding
d
Manufactory optional
Figure 1 — Configuration — Type D

Table 1 — Dimensions and tolerances — Type D
d D D g g l f a R
1 1 2 2 1 α
0 0 0
+ 0,25
Diameter
± 0,013
− 0,025 − 0,51 − 0,13
a
Nominal
code
max. max. max. ± 2°
diameter
0 0 0
+ 0.010
( )
( ) (± 0.0005) () ( )
− 0.0010 − 0.020 − 0.005 0
6,350 6,388 9,550 19,05
(0.2500) (0.2515) (0.3760) (0.750)
7,938 7,976 11,140 20,64
(0.3125) (0.3140) (0.4386) (0.813)
9,525 9,563 12,730 22,23
(0.3750) (0.3765) (0.5012) (0.875)
11,113 11,151 14,321 23,81
(0.4375) (0.4390) (0.5638) (0.938)
12,700 12,738 15,913 25,40 0,70 0,70
(0.5000) (0.5015) (0.6265) (1.000) (0.028) (0.028)
14,288 14,326 17,506 28,58 1,60
(0.5625) (0.5640) (0.6892) (1.125) (0.063)
15,875 15,913 20,681 31,75
(0.6250) (0.6265) (0.8142) (1.250)
17,463 17,501 22,268 34,93
(0.6875) (0.6890) (0.8767) (1.375)
0,50
19,050 19,088 23,858 38,10 to
(0.7500) (0.7515) (0.9393) (1.500) 0,70
1,20 0,13
15°
(0.047) (0.005)
22,225 22,263 27,038 41,28 (0.020
to
(0.8750) (0.8765) (1.0645) (1.625)
0.030)
25,400 25,438 30,221 44,45
(1.0000) (1.0015) (1.1898) (1.750)
28,575 28,613 33,396 47,63
(1.1250) (1.1265) (1.3148) (1.875)
31,750 31,788 36,571 50,80
(1.2500) (1.2515) (1.4398) (2.000)
34,925 34,963 39,746 53,98 1,00 1,00
(1.3750) (1.3765) (1.5648) (2.125) (0.039) (0.039)
38,100 38,138 44,508 57,15 2,39
(1.5000) (1.5015) (1.7523) (2.250) (0.094)
41,275 41,313 47,683 60,33
(1.6250) (1.6265) (1.8773) (2.375)
44,450 44,488 50,858 63,50
(1.7500) (1.7515) (2.0023) (2.500)
50,800 50,838 57,208 69,85
(2.0000) (2.0015) (2.2523) (2.750)
a
Diameter code corresponds to nominal diameter d in 1/16 inch.

Table 2 — Mass — Type D
b
Length code
006 007 008 009 010 011 012 014 016 018 020 022 024 028 032
l
Dia-
− 0,10 − 0.004
meter
( )
− 0,40 − 0.016
a
code
4,76 5,56 6,35 7,14 7,94 8,73 9,53 11,11 12,70 14,29 15,88 17,46 19,05 22,23 25,40
(0.188) (0.219) (0.250) (0.281) (0.313) (0.344) (0.375) (0.438) (0.500) (0.563) (0.625) (0.688) (0.750) (0.875) (1.000)
Mass in kg/1 000 pieces ≈
04 1,48 1,57 1,66 1,75 1,84 1,92 2,01 2,19 2,36 — — — — — —
05 1,70 1,80 1,91 2,01 2,12 2,22 2,33 2,54 2,75 2,96 3,17 — — — —
06 1,91 2,03 2,15 2,28 2,40 2,52 2,65 2,89 3,14 3,39 3,63 3,88 4,13 — —
07 2,12 2,26 2,40 2,54 2,68 2,82 2,96 3,25 3,53 3,81 4,09 4,37 4,66 5,22 —
08 2,33 2,49 2,65 2,81 2,97 3,13 3,28 3,60 3,92 4,24 4,55 4,87 5,19 5,83 —
09 2,86 3,03 3,21 3,39 3,56 3,74 3,92 4,27 4,62 4,98 5,33 5,68 6,04 6,74 7,45
10 3,87 4,17 4,48 4,78 5,09 5,39 5,70 6,31 6,91 7,52 8,13 8,74 9,35 10,57 11,79
11 — — 5,20 5,53 5,86 6,19 6,52 7,18 7,84 8,50 9,17 9,83 10,49 11,81 13,14
12 — — 5,97 6,32 6,68 7,04 7,40 8,11 8,83 9,54 10,26 10,97 11,69 13,12 14,55
14 — — 6,71 7,12 7,53 7,94 8,35 9,18 10,00 10,82 11,64 12,46 13,29 14,93 16,57
16 — — 7,46 7,92 8,39 8,85 9,32 10,24 11,17 12,10 13,03 13,96 14,89 16,75 18,61
18 — — — — 11,23 11,75 12,27 13,30 14,34 15,37 16,41 17,44 18,48 20,55 22,62
20 — — — — — — 13,38 14,52 15,66 16,80 17,94 19,08 20,22 22,51 24,79
22 — — — — — — 14,49 15,73 16,98 18,23 19,48 20,72 21,97 24,47 26,96
24 — — — — — — 17,78 19,61 21,45 23,29 25,13 26,97 28,80 32,48 36,16
26 — — — — — — — — 23,00 24,98 26,96 28,94 30,92 34,88 38,84
28 — — — — — — — — 24,55 26,67 28,80 30,92 33,04 37,28 41,52
32 — — — — — — — — 27,66 30,06 32,46 34,87 37,27 42,07 46,88
continued
Table 2 (concluded)
b
Length code
036 040 044 048 052 056 060 064 068 072 076 080 088 096
l
Dia-
− 0,10 − 0.004
meter
( )
− 0,40 − 0.016
a
code
28,58 31,75 34,93 38,10 41,28 44,45 47,63 50,80 53,98 57,15 60,33 63,50 69,85 76,20
(1.125) (1.250) (1.375) (1.500) (1.625) (1.750) (1.875) (2.000) (2.125) (2.250) (2.375) (2.500) (2.750) (3.000)
Mass in kg/1 000 pieces ≈
04 — — — — — — — — — — — — — —
05 — — — — — — — — — — — — — —
06 — — — — — — — — — — — — — —
07 — — — — — — — — — — — — — —
08 — — — — — — — — — — — — — —
09 8,16 — — — — — — — — — — — — —
10 13,01 14,22 — — — — — — — — — — — —
11 14,46 15,79 17,11 — — — — — — — — — — —
12 15,98 17,41 18,84 20,27 — — — — — — — — — —
14 18,22 19,86 21,50 23,15 24,79 — — — — — — — — —
16 20,47 22,33 24,18 26,04 27,90 29,76 31,62 — — — — — — —
18 24,69 26,76 28,83 30,90 32,97 35,04 37,11 39,19 — — — — — —
20 27,07 29,36 31,64 33,92 36,20 38,49 40,77 43,05 45,34 — — — — —
22 29,46 31,95 34,45 36,94 39,44 41,93 44,43 46,92 49,41 — — — — —
24 39,83 43,51 47,18 50,86 54,54 58,21 61,89 65,56 69,24 72,92 76,59 80,27 87,62 —
26 42,80 46,75 50,71 54,67 58,63 62,59 66,55 70,50 74,46 78,42 82,38 86,34 94,26 102,17
28 45,76 50,00 54,24 58,48 62,72 66,96 71,20 75,45 79,69 83,93 88,17 92,41 100,89 109,37
32 51,69 56,49 61,30 66,10 70,91 75,71 80,52 85,33 90,13 94,94 99,74 104,55 114,16 123,77
a
Diameter code corresponds to nominal diameter d in 1/16 inch.
b
Length code corresponds to length l in 1/32 inch.
Table 3 — Loads — Type D
Permissible Radial Axial Permissible Radial Axial

radial load load static load radial load load static load
Diameter Diameter
Length Length
kN kN
a a
code code
code code
Static Dynamic Static Dynamic

b c d b c d
C C C C C C
s 25 a s 25 a
006 2,15 1,92 009 13,09 11,69 54,85
007 3,62
...