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BS EN 4036:2006

BS EN 4036:2006

Superseded

Superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

View Superseded by
superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.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 and threaded shank in corrosion resisting steel, reduced internal radial clearance. Dimensions and loads

Available format(s)

Hardcopy , PDF

Superseded date

16-03-2021

Language(s)

English

Published date

30-06-2006

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

Describes the characteristics of adjustable rod ends with self-aligning double row ball bearing with reduced internal radial clearance and threaded shank in corrosion resisting steel, 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 with reduced internal radial clearance and threaded shank in corrosion resisting steel, 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Superseded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 4036 : 2007 Identical
NS EN 4036 : 1ED 2006 Identical
I.S. EN 4036:2006 Identical
UNI EN 4036 : 2007 Identical
SN EN 4036 : 2006 Identical
NF EN 4036 : 2006 Identical
NBN EN 4036 : 2006 Identical
EN 4036:2006 Identical
DIN EN 4036:2007-06 Identical
NEN EN 4036 : 2006 Identical

PREN 2226 : 200P1 AEROSPACE SERIES - STEEL FE-PM 3501 (X105CRMO17) - HARDENED AND TEMPERED - HAND AND DIE FORGINGS D[E] <= 150 MM
ISO 5855-2:1999 Aerospace MJ threads Part 2: Limit dimensions for bolts and nuts
PREN 2030 : 200P1 AEROSPACE SERIES - STEEL FE-PM3501 (X105CRMO17) - HARDENED AND TEMPERED - BARS D[E] <= 150 MM
ISO 8074:1985 Aerospace Surface treatment of austenitic stainless steel parts
PREN 3490 : 200P2
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
TR 3775 : 4 AEROSPACE SERIES - BOLTS AND PINS - MATERIALS
EN 2067:1996/AC:1996 AEROSPACE SERIES - ROD ENDS WITH SELF-ALIGNING BALL BEARINGS - TECHNICAL SPECIFICATION
PREN 2136 : 2 AEROSPACE SERIES - STEEL FE-PM42 - 900 MPA <= R[M] <= 1100 MPA - BARS D[E] <= 100 MM
ISO 3353-1:2002 Aerospace Lead and runout threads Part 1: Rolled external threads

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