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: 1275 MPa (at ambient temperature) / 550°C. Technical specification

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

05-30-2008

Publisher

British Standards Institution

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

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

This standard specifies the characteristics, qualification and acceptance requirements for self-locking thin wall salvage inserts with MJ threads in NI-PH2601 (NI P100HT). Classification: 1 275 MPa ) / 550 °C ).

Committee	ACE/12
DocumentType	Standard
Pages	22
PublisherName	British Standards Institution
Status	Current

Standards	Relationship
EN 3915 : 2008	Identical

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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BS EN 3915:2008

Current

Table of Contents

Abstract

Scope

General Product Information

International Equivalents

Standards Referencing This Book

Category

Subcategory

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