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PREN 4035 : 200P1

Withdrawn
Withdrawn

A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.

View Superseded by
withdrawn

A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.

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

Withdrawn date

16-12-2023

Language(s)

English

Publisher

Aerospace & Defence Industries Association of Europe

1 Scope
2 Normative references
3 Symbols
4 Required characteristics
5 Designation
6 Marking
7 Technical specification

Gives 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 oscillations and only slow rotations under load. They consist of: - a rod end comprising: - circumferential groove to identify location; - either shields or seals; - 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 degree C to +150 degree C.

Committee
C1
DocumentType
Draft
Pages
7
ProductNote
Superseded by EN 4035:2006
PublisherName
Aerospace & Defence Industries Association of Europe
Status
Withdrawn
SupersededBy

Standards Relationship
DIN EN 4035:2006-09 Identical

ISO 1132:1980 Rolling bearings — Tolerances — Definitions
ISO 5855-2:1999 Aerospace MJ threads Part 2: Limit dimensions for bolts and nuts
PREN 3315 : 200P2 AEROSPACE SERIES - TITANIUM ALLOY TI-P64001 - SOLUTION TREATED AND AGED - FORGINGS - D[E] <= 75 MM
ISO 8075:1985 Aerospace Surface treatment of hardenable stainless steel parts
ISO 3353:1992 Aerospace — Rolled threads for bolts — Lead and runout requirements
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

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Hardcopy - English
PDF - English
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