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BS EN 3832:2004

Current

Current

The latest, up-to-date edition.

Aerospace series. Bolts, double hexagon head, relieved shank, long thread, in heat resisting nickel base alloy NI-PH2601 (Inconel 718). Classification: 1550 MPa (at ambient temperature) / 650°C

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

06-01-2005

$325.41
Including GST where applicable

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 relieved shank and long thread, in NI-PH2601, for aerospace applications.

Committee
ACE/12
DevelopmentNote
Supersedes 91/76640 DC (02/2003)
DocumentType
Standard
Pages
12
PublisherName
British Standards Institution
Status
Current
Supersedes

This standard specifies the characteristics of double hexagon headed bolts with relieved shank and long thread in NI-P100HT for aerospace applications. Classification: 1 550 MPa ) / 650 °C )

Standards Relationship
I.S. EN 3832:2005 Identical
DIN EN 3832:2005-09 Identical
NS EN 3832 : 2ED 2005 Identical
NBN EN 3832 : 2005 Identical
EN 3832:2004 Identical
NF EN 3832 : 2005 Identical
NEN EN 3832 : 2006 Identical
UNE-EN 3832:2004 Equivalent

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
ISO 4095:1998 Aerospace — Bihexagonal drives — Wrenching configuration — Metric series
EN 2424:2008 Aerospace series - Marking of aerospace products
ISO 3353-1:2002 Aerospace — Lead and runout threads — Part 1: Rolled external threads

$325.41
Including GST where applicable