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CEN
EN 3899:2004

EN 3899:2004

Current

Current

The latest, up-to-date edition.

Aerospace series - Inserts, thickwall, self-locking, MJ threads, in heat resisting steel FE-PM3801 (17-4PH) - Technical specification

Published date

11-10-2004

Publisher

Comite Europeen de Normalisation

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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