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EN 3915 : 2008

Current

Current

The latest, up-to-date edition.

Aerospace series - Insert, thin wall, self-locking, MJ threads, in heat resisting nickel base alloy NI-PH2601 (NI-P100HT, Inconel 718), for salvage of components - Classification: 1 275 MPa (at ambient temperature) / 550 °C - Technical specification

Published date

16-04-2008

Foreword
1 Scope
2 Normative references
3 Terms and definitions
4 Quality assurance
  4.1 Qualification
      4.1.1 Purpose
      4.1.2 EN 9133
  4.2 Acceptance
      4.2.1 Purpose
      4.2.2 Conditions
      4.2.3 Responsibility
      4.2.4 Inspection and test report
5 Requirements

This standard specifies the characteristics, qualification and acceptance requirements for self-locking thin wall salvage inserts with MJ threads in NI-PH2601 (NI P100HT).

DevelopmentNote
Supersedes PREN 3915. (05/2008)
DocumentType
Technical Specification
PublisherName
Comite Europeen de Normalisation
Status
Current
Supersedes

Standards Relationship
PN EN 3915 : 2008 Identical
BS EN 3915:2008 Identical
NBN EN 3915 : 2008 Identical
SN EN 3915 : 2008 Identical
I.S. EN 3915:2008 Identical
NS EN 3915 : 1ED 2008 Identical
UNE-EN 3915:2008 Identical
NF EN 3915 : 2008 Identical
DIN EN 3915:2008-12 Identical
NEN EN 3915 : 2008 Identical
UNI EN 3915 : 2008 Identical

NF EN 3916 : 2009 AEROSPACE SERIES - INSERT, THIN WALL - SALVAGE PROCEDURE FOR COMPONENTS
I.S. EN 3916:2008 AEROSPACE SERIES - INSERT, THIN WALL - SALVAGE PROCEDURE FOR COMPONENTS
I.S. EN 3914:2008 AEROSPACE SERIES - INSERT, THIN WALL, SELF-LOCKING, LONG, IN HEAT RESISTING NICKEL BASE ALLOY NI-PH2601 (NI-P100HT, INCONEL 718), SILVER PLATED ON INTERNAL THREAD, FOR SALVAGE OF COMPONENTS
EN 3916:2008 Aerospace series - Insert, thin wall - Salvage procedure for components
NF EN 3914 : 2008 AEROSPACE SERIES - INSERT, THIN WALL, SELF-LOCKING, LONG, IN HEAT RESISTING NICKEL BASE ALLOY NI-PH2601 (NI-P100HT, INCONEL 718), SILVER PLATED ON INTERNAL THREAD, FOR SALVAGE OF COMPONENTS
BS EN 3914:2008 Aerospace series. Insert, thin wall, self-locking, long, in heat resisting nickel base alloy NI-PH2601 (NI-P100HT, Inconel 718), silver plated on internal thread, for salvage of components
EN 3914:2008 Aerospace series - Insert, thin wall, self-locking, long, in heat resisting nickel base alloy NI-PH2601 (NI-P100HT, Inconel 718), silver plated on internal thread, for salvage of components
BS EN 3916:2008 Aerospace series. Insert, thin wall. Salvage procedure for components

ISO 3534:1977 Statistics — Vocabulary and symbols
ISO 5855-2:1999 Aerospace MJ threads Part 2: Limit dimensions for bolts and nuts
EN ISO 4288 : 1997 GEOMETRICAL PRODUCT SPECIFICATIONS (GPS) - SURFACE TEXTURE: PROFILE METHOD - RULES AND PROCEDURES FOR THE ASSESSMENT OF SURFACE TEXTURE
PREN 4376 : 200P1 AEROSPACE SERIES - HEAT RESISTING ALLOY NI-PH2601 (NICR19FE19NB5MO3) - SOLUTION TREATED AND PRECIPITATION TREATED - BAR AND SECTION - D[E] <= 200 MM
ISO 3452:1984 Non-destructive testing — Penetrant inspection — General principles
EN 3298:2008 Aerospace series - Inserts, thin wall, self-locking - Installation and removal procedure
EN 3676:1998 Aerospace series - Inserts, thin wall, self-locking - Design standard
PREN 4377 : 200P1 AEROSPACE SERIES - HEAT RESISTING ALLOY NI-PH2601 (NICR19FE19NB5MO3) - NON HEAT TREATED - FORGING STOCK - A OR D <= 300 MM
PREN 2404 : 2 AEROSPACE SERIES - HEAT RESISTING NICKEL BASE ALLOY NI-P100-HT - SOLUTION TREATED AND PRECIPITATION TREATED - BARS
SAE AMS 4117 : 2015 ALUMINUM ALLOY, ROLLED OR COLD FINISHED BARS, RODS, AND WIRE AND FLASH WELDED RINGS, 1.0MG - 0.60SI - 0.28CU - 0.20CR (6061; -T6, -T651)
SAE AMS QQ A 225/8 : 1998 ALUMINUM ALLOY 6061, BAR, ROD, WIRE, AND SPECIAL SHAPES; ROLLED, DRAWN, OR COLD FINISHED
ISO 8642:2008 Aerospace — Self-locking nuts with maximum operating temperature greater than 425 degrees C — Test methods

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