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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.

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

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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