EN 3899:2004
Current
The latest, up-to-date edition.
Aerospace series - Inserts, thickwall, self-locking, MJ threads, in heat resisting steel FE-PM3801 (17-4PH) - Technical specification
10-11-2004
Foreword
1 Scope
2 Normative references
3 Terms and definitions
4 Quality assurance
4.1 Qualification
4.2 Acceptance
4.2.1 Purpose
4.2.2 Conditions
4.2.3 Responsibility
4.2.4 Inspection and test report
5 Requirements
Annex A (normative) Definition of test block
Annex B (normative) Assembly for rotational resistance test
Annex C (normative) Axial tensile strength test
Annex D (normative) Assembly for reusability test
This standard specifies the characteristics, qualification and acceptance requirements for self-locking thickwall inserts with MJ threads, in FE-PM3801, for aerospace applications. It is applicable whenever referenced.
| Committee |
ASD-STAN
|
| DevelopmentNote |
Supersedes PREN 3899 (11/2003)
|
| DocumentType |
Standard
|
| PublisherName |
Comite Europeen de Normalisation
|
| Status |
Current
|
| Supersedes |
| Standards | Relationship |
| BS EN 3899:2004 | Identical |
| DIN EN 3899:2007-02 | Identical |
| PN EN 3899 : 2006 | Identical |
| SN EN 3899 : 2005 | Identical |
| NF EN 3899 : 2005 | Identical |
| NEN EN 3899 : 2006 | Identical |
| NS EN 3899 : 2ED 2005 | Identical |
| UNE-EN 3899:2004 | Identical |
| I.S. EN 3899:2005 | Identical |
| NBN EN 3899 : 2005 | Identical |
| UNI EN 3899 : 2006 | Identical |
| I.S. EN 3831:2005 | AEROSPACE SERIES - INSERTS, THICKWALL, SELF-LOCKING, MJ THREADS, IN HEAT RESISTING STEEL FE-PM3801 (17-4PH), MOS[2] COATED |
| BS EN 3831:2004 | Aerospace series. Inserts, thickwall, self-locking, MJ threads, in heat resisting steel FE-PM3801 (17-4PH), MoS<sub>2</sub> coated |
| EN 3831:2004 | Aerospace series - Inserts, thickwall, self-locking, MJ threads, in heat resisting steel FE-PM3801 (17-4PH), MoS2 coated |
| ISO 5855-2:1999 | Aerospace MJ threads Part 2: Limit dimensions for bolts and nuts |
| 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 4014:2004 | Aerospace series - Inserts, thickwall, self-locking - Design standard |
| ISO 3452:1984 | Non-destructive testing — Penetrant inspection — General principles |
| ISO 7481:2000 | Aerospace — Nuts, self-locking, with maximum operating temperature less than or equal to 425 degrees C — Test methods |
| PREN 9133 : 200P1 | AEROSPACE SERIES - QUALITY MANAGEMENT SYSTEMS - QUALIFICATION PROCEDURE FOR AEROSPACE STANDARD PRODUCTS |
| PREN 2638 : 200P1 | AEROSPACE SERIES - ALUMINIUM ALLOY 2024-T3 - EXTRUDED BAR AND SECTION - 1,2 <= (A OR D) <= 150 MM - WITH COARSE PERIPHERAL GRAIN CONTROL |
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