Name: EN 4323:2004
Brand: CEN

Aerospace series - Screws, 100° countersunk head, six lobe recess, threaded to head, in titanium alloy TI-P64001, anodized, MoS2 coated - Classification: 900 MPa (at ambient temperature) / 350 °C

Published date

10-11-2004

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 screws with 100° countersunk head with six lobe recess, threaded to head, in TI-P64001, anodized, MoS2 coated, for aerospace applications.Classification: 900 MPa ) / 350 °C )

Committee	ASD-STAN
DevelopmentNote	Supersedes PREN 4323 (12/2003)
DocumentType	Standard
PublisherName	Comite Europeen de Normalisation
Status	Current
Supersedes	PREN 4323 : 200P1

Standards	Relationship
NBN EN 4323 : 2005	Identical
NEN EN 4323 : 2006	Identical
NS EN 4323 : 2ED 2005	Identical
I.S. EN 4323:2005	Identical
PN EN 4323 : 2005	Identical
SN EN 4323 : 2003	Identical
UNI EN 4323 : 2007	Identical
UNE-EN 4323:2004	Identical
BS EN 4323:2004	Identical
NF EN 4323 : 2005	Identical
DIN EN 4323:2006-03	Identical

ISO 5855-2:1999	Aerospace MJ threads Part 2: Limit dimensions for bolts and nuts
EN 3911:2010	Aerospace series - Six lobe recess - Geometrical definition
EN 2491:2011	Aerospace series - Molybdenum disulphide dry lubricants - Coating methods
EN 3818:2004	Aerospace series - Bolts, MJ threads, in titanium alloy TI-P64001 - Strength class: 1 100 MPa (at ambient temperature) - Technical specification
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