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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: 1 550 MPa (at ambient temperature) / 650 °C

Published date

10-11-2004

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

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 )

Committee
ASD-STAN
DevelopmentNote
Supersedes PREN 3832. (12/2003)
DocumentType
Standard
PublisherName
Comite Europeen de Normalisation
Status
Current
Supersedes

Standards Relationship
PN EN 3832 : 2005 Identical
I.S. EN 3832:2005 Identical
BS EN 3832:2004 Identical
DIN EN 3832:2005-09 Identical
NS EN 3832 : 2ED 2005 Identical
NBN EN 3832 : 2005 Identical
NF EN 3832 : 2005 Identical
NEN EN 3832 : 2006 Identical
DS EN 3832 : 2005 Identical
UNE-EN 3832:2004 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
ISO 4095:1998 Aerospace — Bihexagonal drives — Wrenching configuration — Metric series
PREN 3666 : 200P2 AEROSPACE SERIES - HEAT RESISTING ALLOY NI-PH2601 - SOLUTION TREATED AND COLD WORKED - BAR FOR FORGED FASTENERS - D <= 50 MM - 1550 MPA <= R[M] <= 1830 MPA
EN 2424:2008 Aerospace series - Marking of aerospace products
ISO 3353-1:2002 Aerospace — Lead and runout threads — Part 1: Rolled external threads
PREN 2952 : 200P3 AEROSPACE SERIES - HEAT RESISTING ALLOY NI-PH2601 - SOLUTION TREATED AND COLD WORKED - BAR FOR FORGED FASTENERS - D <= 50 MM - 1270 MPA <= R[M] <= 1550 MPA

Sorry this product is not available in your region.