Aerospace series. Nuts, clip, metric. Installation holes and assembly

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

05-01-2004

Publisher

British Standards Institution

Foreword
1 Scope
2 Normative references
3 Principle
4 Design instructions
  4.1 Support design
      4.1.1 Installation A: "on flank of support"
      4.1.2 Installation B: "with slot"
      4.1.3 Dimensions
  4.2 Type of installation
      4.2.1 Installation A
      4.2.2 Installation B
5 Indication on drawings
  5.1 Definition drawing
  5.2 Assembly drawing
6 Designation

Provides the characteristics of the installation holes required for the utilization of clip nuts with design configuration to EN-Standards for aerospace applications.

This standard specifies the characteristics of the installation holes required for the utilization of clip nuts with design configuration to EN-Standards for aerospace applications.

Committee	ACE/12
DevelopmentNote	Supersedes 91/80684 DC (03/2003)
DocumentType	Standard
Pages	10
PublisherName	British Standards Institution
Status	Current
Supersedes	91/80684 DC : DRAFT OCT 1991 BS EN 3741:2003

Standards	Relationship
NEN EN 3741 : 2006	Identical
I.S. EN 3741:2005	Identical
NBN EN 3741 : 2005	Identical
SN EN 3741 : 2005	Identical
DIN EN 3741:2005-09	Identical
EN 3741:2004	Identical
NS EN 3741 : 2ED 2005	Identical
UNI EN 3741 : 2005	Identical
NF EN 3741 : 2005	Identical

EN 3726:2004

Aerospace series - Nuts, self-locking, clip, in heat resisting steel FE-PA2601 (A286), MoS2 coated - Classification: 1 100 MPa (at ambient temperature) / 425 °C

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BS EN 3741:2004

Aerospace series. Nuts, clip, metric. Installation holes and assembly

Table of Contents

Abstract

Scope

General Product Information

International Equivalents

Standards Referencing This Book

Category

Subcategory