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BS EN 4421:2007

Current

Current

The latest, up-to-date edition.

Aerospace series. Studs, in titanium alloy TI-P64001, MoS2 coated, with serrated locking ring in corrosion resisting steel. Strength class: 1100 MPa(at ambient temperature)

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

31-08-2007

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

Specifies the characteristics of studs in TI-P64001, MoS[2] coated, with serrated locking ring in corrosion resisting steel for aerospace applications.

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

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

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