EN 3831:2004
Current
Current
The latest, up-to-date edition.
Aerospace series - Inserts, thickwall, self-locking, MJ threads, in heat resisting steel FE-PM3801 (17-4PH), MoS2 coated
Published date
10-11-2004
Publisher
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Foreword
1 Scope
2 Normative references
3 Required characteristics
4 Insert definition
5 Designation
6 Marking
7 Technical specification
This standard specifies the characteristics of self-locking, thickwall inserts, in FE-PM3801, MoS2 coated, for aerospace applications.Maximum test temperature: 350 °C
| Committee |
ASD-STAN
|
| DevelopmentNote |
Supersedes PREN 3831 (11/2003)
|
| DocumentType |
Standard
|
| PublisherName |
Comite Europeen de Normalisation
|
| Status |
Current
|
| Supersedes |
| Standards | Relationship |
| NEN EN 3831 : 2006 | Identical |
| DIN EN 3831:2005-09 | Identical |
| BS EN 3831:2004 | Identical |
| NS EN 3831 : 2ED 2005 | Identical |
| NBN EN 3831 : 2005 | Identical |
| PN EN 3831 : 2005 | Identical |
| NF EN 3831 : 2005 | Identical |
| I.S. EN 3831:2005 | Identical |
| DS EN 3831 : 2005 | Identical |
| UNE-EN 3831:2004 | Identical |
| BS EN 4015:2004 | Aerospace series. Inserts, thickwall, self-locking. Installation and removal procedure |
| I.S. EN 4014:2005 | AEROSPACE SERIES - INSERTS, THICKWALL, SELF-LOCKING - DESIGN STANDARD |
| I.S. EN 4015:2005 | AEROSPACE SERIES - INSERT, THICKWALL, SELF-LOCKING - INSTALLATION AND REMOVAL PROCEDURE |
| BS EN 4014:2004 | Aerospace series. Inserts, thickwall, self-locking. Design standard |
| EN 4014:2004 | Aerospace series - Inserts, thickwall, self-locking - Design standard |
| EN 4015:2004 | Aerospace series - Inserts, thickwall, self-locking - Installation and removal procedure |
| ISO 5855-2:1999 | Aerospace — MJ threads — Part 2: Limit dimensions for bolts and nuts |
| ISO 5855-1:1999 | Aerospace — MJ threads — Part 1: General requirements |
| EN 4015:2004 | Aerospace series - Inserts, thickwall, self-locking - Installation and removal procedure |
| PREN 3906 : 200P1 | AEROSPACE SERIES - MARTENSITIC CORROSION RESISTING STEEL FE-PM3801 - AIR MELTED - SOLUTION TREATED - BAR - D <= 50 MM - FOR THE MANUFACTURE OF FASTENERS - 1100 MPA <= R[M] <= 1300 MPA |
| EN 2491:2011 | Aerospace series - Molybdenum disulphide dry lubricants - Coating methods |
| EN 4014:2004 | Aerospace series - Inserts, thickwall, self-locking - Design standard |
| EN 3899:2004 | Aerospace series - Inserts, thickwall, self-locking, MJ threads, in heat resisting steel FE-PM3801 (17-4PH) - Technical specification |
| EN 2424:2008 | Aerospace series - Marking of aerospace products |
| TR 3198 : 2013 | AEROSPACE SERIES - MANUFACTURERS' IDENTIFICATION MONOGRAMS AND MARKS FOR EN AEROSPACE PRODUCTS |
Summarise
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