EN 4035:2006
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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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
19-03-2021
03-05-2006
Foreword
1 Scope
2 Normative references
3 Terms and definitions
4 Symbols and abbreviations
5 Required characteristics
6 Designation
7 Marking
8 Technical specification
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 |
ASD-STAN
|
| DevelopmentNote |
Supersedes PREN 4035. (06/2006)
|
| DocumentType |
Standard
|
| PublisherName |
Comite Europeen de Normalisation
|
| Status |
Superseded
|
| SupersededBy | |
| Supersedes |
| Standards | Relationship |
| BS EN 4035:2006 | Identical |
| I.S. EN 4035:2006 | Identical |
| DIN EN 4035:2006-09 | Identical |
| NS EN 4035 : 1ED 2006 | Identical |
| NBN EN 4035 : 2006 | Identical |
| NF EN 4035 : 2006 | Identical |
| NEN EN 4035 : 2006 | Identical |
| UNE-EN 4035:2006 | Identical |
| SN EN 4035 : 2006 | Identical |
| UNI EN 4035 : 2007 | Identical |
| PN EN 4035 : 2006 | Identical |
| ONORM EN 4035 : 2006 | Identical |
| SN EN 4035:2021 | 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 |
| 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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