Name: EN 4424:2006
Brand: CEN

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

Published date

06-14-2006

Publisher

Comite Europeen de Normalisation

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

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	ASD-STAN
DevelopmentNote	Supersedes PREN 4424. (08/2006)
DocumentType	Standard
PublisherName	Comite Europeen de Normalisation
Status	Current
Supersedes	PREN 4424 : 200P1

Standards	Relationship
NBN EN 4424 : 2006	Identical
NEN EN 4424 : 2006	Identical
NS EN 4424 : 1ED 2006	Identical
I.S. EN 4424:2006	Identical
PN EN 4424 : 2010	Identical
SN EN 4424 : 2006	Identical
UNI EN 4424 : 2008	Identical
UNE-EN 4424:2006	Identical
BS EN 4424:2006	Identical
NF EN 4424 : 2006	Identical
DIN EN 4424:2007-03	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