Name: EN 4421:2007
Brand: CEN

Aerospace series - Studs, in titanium alloy TI-P64001, MoS2 coated, with serrated locking ring in corrosion resisting steel - Strength class: 1 100 MPa (at ambient temperature)

Published date

20-06-2007

Publisher

Comite Europeen de Normalisation

Foreword
1 Scope
2 Normative references
3 Required characteristics
  3.1 Configuration - Dimensions - Tolerances - Masses
  3.2 Materials
  3.3 Surface treatment
4 Designation
5 Marking
6 Technical specification

This standard specifies the characteristics of studs in TI P64001, MoS2 coated, with serrated locking ring in corrosion resisting steel for aerospace applications.Strength class: 1 100 MPa )

Committee	ASD-STAN
DevelopmentNote	Supersedes PREN 4421. (08/2007)
DocumentType	Standard
PublisherName	Comite Europeen de Normalisation
Status	Current
Supersedes	PREN 4421 : 200P1

Standards	Relationship
NBN EN 4421 : 2007	Identical
BS EN 4421:2007	Identical
DIN EN 4421:2008-02	Identical
NS EN 4421 : 1ED 2007	Identical
SN EN 4421 : 2008	Identical
I.S. EN 4421:2007	Identical
NEN EN 4421 : 2007	Identical
UNE-EN 4421:2007	Identical
UNI EN 4421 : 2008	Identical
NF EN 4421 : 2007	Identical

ISO 5855-2:1999	Aerospace MJ threads Part 2: Limit dimensions for bolts and nuts
ISO 3353:1992	Aerospace — Rolled threads for bolts — Lead and runout requirements
EN 2424:2008	Aerospace series - Marking of aerospace products
EN 4458:2005	Aerospace series - Studs, MJ threads, in titanium alloy TI-P64001, MoS2 coated, with serrated locking ring in corrosion resisting steel - Strength class: 1 100 MPa (at ambient temperature) - Technical specification
PREN 3311 : 200P2	AEROSPACE SERIES - TITANIUM ALLOY TI-P64001 - ANNEALED - BAR FOR MACHINING - D <= 150 MM
SAE AMS 5604 : 2016	STEEL, CORROSION RESISTANT, SHEET, STRIP, AND PLATE, 16.5CR - 4.0NI - 4.0CU - 0.30CB, SOLUTION HEAT TREATED, PRECIPITATION HARDENABLE