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BS EN 4322:2004

BS EN 4322:2004

Current

Current

The latest, up-to-date edition.

Aerospace series. Bolts, double hexagon head with lockwire holes, relieved shank, long thread, in titanium alloy TI-P64001, anodized, MoS2 coated. Strength class: 1100 MPa (at ambient temperature)

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

12-15-2004

Publisher

British Standards Institution

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

Describes the characteristics of double hexagon headed bolts with lockwire holes, relieved shank and long thread, in TI-P64001, anodized, MoS[2] coated, for aerospace applications.

Committee
ACE/12
DevelopmentNote
Supersedes 97/710475 DC (03/2003)
DocumentType
Standard
Pages
12
PublisherName
British Standards Institution
Status
Current
Supersedes

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 )

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

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Hardcopy - English
PDF - English
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