Name: EN 4322:2004
Brand: CEN

Aerospace series - Bolts, double hexagon head with lockwire holes, relieved shank, long thread, in titanium alloy TI-P64001, anodized, MoS2 coated - Strength class: 1 100 MPa (at ambient temperature)

Published date

11-10-2004

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 double hexagon headed bolts with lockwire holes, relieved shank and long thread, in TI-P64001, anodized, MoS2 coated, for aerospace applications.Strength class: 1 100 MPa )

Committee	ASD-STAN
DevelopmentNote	Supersedes PREN 4322 (12/2003)
DocumentType	Standard
PublisherName	Comite Europeen de Normalisation
Status	Current
Supersedes	PREN 4322 : 200P1

Standards	Relationship
NBN EN 4322 : 2005	Identical
NEN EN 4322 : 2006	Identical
NS EN 4322 : 2ED 2005	Identical
I.S. EN 4322:2005	Identical
PN EN 4322 : 2005	Identical
SN EN 4322 : 2003	Identical
UNI EN 4322 : 2005	Identical
UNE-EN 4322:2004	Identical
BS EN 4322:2004	Identical
NF EN 4322 : 2005	Identical
DIN EN 4322:2006-03	Identical

ISO 5855-2:1999	Aerospace MJ threads Part 2: Limit dimensions for bolts and nuts
EN 2491:2011	Aerospace series - Molybdenum disulphide dry lubricants - Coating methods
ISO 4095:1998	Aerospace — Bihexagonal drives — Wrenching configuration — Metric series
ISO 3353:1992	Aerospace — Rolled threads for bolts — Lead and runout requirements
EN 2424:2008	Aerospace series - Marking of aerospace products
EN 3813:2013	Aerospace series - Titanium alloy TI-P64001 (Ti-6Al-4V) - Annealed - Bar and wire for forged fasteners - De ≤ 50 mm