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BS EN 4424:2006

BS EN 4424:2006

Current

Current

The latest, up-to-date edition.

Aerospace series. Rod-ends, adjustable single fork and threaded shank with engagement: 1,5 x thread diameter in titanium alloys. Dimensions and loads

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

06-30-2006

Publisher

British Standards Institution

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

Describes the characteristics of rod-ends for flight control rods. - a single fork; - a threaded shank comprising; - a circumferential groove to identify engagement; - an optional longitudinal groove for locking purpose. These rod-ends are intended for use with control rods or rods for aircraft structures.

This standard specifies the characteristics of rod-ends for flight control rods. a single fork; a threaded shank comprising; a circumferential groove to identify engagement; an optional longitudinal groove for locking purpose. These rod-ends are intended for use with control rods or rods for aircraft structures.

Committee
ACE/12
DocumentType
Standard
Pages
10
PublisherName
British Standards Institution
Status
Current

Standards Relationship
SN EN 4424 : 2006 Identical
UNI EN 4424 : 2008 Identical
I.S. EN 4424:2006 Identical
NBN EN 4424 : 2006 Identical
DIN EN 4424:2007-03 Identical
EN 4424:2006 Identical
NS EN 4424 : 1ED 2006 Identical
NF EN 4424 : 2006 Identical
NEN EN 4424 : 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
EN 2601 : 1996 AEROSPACE SERIES - FORK ENDS, ADJUSTABLE - TECHNICAL SPECIFICATION
PREN 3315 : 200P2 AEROSPACE SERIES - TITANIUM ALLOY TI-P64001 - SOLUTION TREATED AND AGED - FORGINGS - D[E] <= 75 MM
TR 3775 : 4 AEROSPACE SERIES - BOLTS AND PINS - MATERIALS
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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