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BS EN 4035:2006

BS EN 4035:2006

Superseded

Superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

View Superseded by
superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

Aerospace series. Rod ends, adjustable with self-aligning double row ball bearing in corrosion resisting steel, reduced internal radial clearance and threaded shank in titanium alloy. Dimensions and loads

Available format(s)

Hardcopy , PDF

Superseded date

18-03-2021

Language(s)

English

Published date

31-05-2006

Publisher

British Standards Institution

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

Specifies the characteristics of adjustable rod ends with self-aligning double row ball bearing in corrosion resisting steel with reduced internal radial clearance and threaded shank in titanium alloy, designed to withstand only slow rotations and oscillations under load.

This standard specifies the characteristics of adjustable rod ends with self-aligning double row ball bearing in corrosion resisting steel with reduced internal radial clearance and threaded shank in titanium alloy, designed to withstand only slow rotations and oscillations under load. They consist of: - a rod end comprising: circumferential groove to identify location; 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 or - very high pressure grease, synthetic hydrocarbons, general purpose (code B), operational range - 54 °C to 177 °C (see EN 2067), their field of application when lubricated with code A grease is limited to 121 °C.

Committee
ACE/12
DocumentType
Standard
Pages
12
PublisherName
British Standards Institution
Status
Superseded
SupersededBy

Standards Relationship
ONORM EN 4035 : 2006 Identical
NEN EN 4035 : 2006 Identical
I.S. EN 4035:2006 Identical
DIN EN 4035:2006-09 Identical
NS EN 4035 : 1ED 2006 Identical
SN EN 4035 : 2006 Identical
NBN EN 4035 : 2006 Identical
EN 4035:2006 Identical
UNI EN 4035 : 2007 Identical
NF EN 4035 : 2006 Identical

ISO 5855-2:1999 Aerospace MJ threads Part 2: Limit dimensions for bolts and nuts
PREN 3813 : 200P2 AEROSPACE SERIES - TITANIUM ALLOY TI-P64001 (TI-6AI-4V) - ANNEALED - BAR AND WIRE FOR FORGED FASTENERS - D[E] <= 50 MM
PREN 3315 : 200P2 AEROSPACE SERIES - TITANIUM ALLOY TI-P64001 - SOLUTION TREATED AND AGED - FORGINGS - D[E] <= 75 MM
ISO 1132-1:2000 Rolling bearings — Tolerances — Part 1: Terms and definitions
ISO 8075:1985 Aerospace Surface treatment of hardenable stainless steel parts
EN 2808:1997 Aerospace series - Anodizing of titanium and titanium alloys
EN 2424:2008 Aerospace series - Marking of aerospace products
TR 3775 : 4 AEROSPACE SERIES - BOLTS AND PINS - MATERIALS
EN 3289:1994 Aerospace series - Bearings, airframe rolling - Double row self-aligning ball bearings in corrosion resisting steel - Diameter series 2 - Dimensions and loads
EN 2067:1996/AC:1996 AEROSPACE SERIES - ROD ENDS WITH SELF-ALIGNING BALL BEARINGS - TECHNICAL SPECIFICATION
PREN 3353 : 200P1 AEROSPACE SERIES - TITANIUM ALLOY TI-P63 - SOLUTION TREATED AND AGED - R[M] >= 1100 MPA - BAR AND WIRE FOR FASTENERS MACHINED - D[E] <= 25 MM
ISO 3353-1:2002 Aerospace Lead and runout threads Part 1: Rolled external threads

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Hardcopy - English
PDF - English
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