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BS EN 4352:2004

Current

Current

The latest, up-to-date edition.

Aerospace series. Bolts, double hexagon head with lockwire holes, relieved shank, long thread, in heat resisting nickel base alloy NI-PH2601 (Inconel 718), MoS2 coated. Classification. 1 550 MPa (at ambient temperature) / 425°C

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

16-12-2004

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

Gives the characteristics of double hexagon headed bolts with lockwire holes, relieved shank and long thread, in NI-PH2601, 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 NI-PH2601, MoS2 coated, for aerospace applications. Classification: 1 550 MPa ) / 425 °C )

Committee
ACE/12
DevelopmentNote
Supersedes 97/710476 DC (02/2003)
DocumentType
Standard
Pages
12
PublisherName
British Standards Institution
Status
Current
Supersedes

Standards Relationship
I.S. EN 4352:2005 Identical
NS EN 4352 : 2ED 2005 Identical
NF EN 4352 : 2005 Identical
NBN EN 4352 : 2005 Identical
SN EN 4352 : 2003 Identical
DIN EN 4352:2006-03 Identical
EN 4352:2004 Identical
NEN EN 4352 : 2006 Identical
UNI EN 4352 : 2005 Identical

ISO 5855-2:1999 Aerospace MJ threads Part 2: Limit dimensions for bolts and nuts
EN 3833:2004 Aerospace series - Bolts, MJ threads, in heat resisting nickel base alloy NI-PH2601 (Inconel 718), passivated - Classification: 1 550 MPa (at ambient temperature) / 650 °C - Technical specification
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

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