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BS EN 3741:2004

Current

Current

The latest, up-to-date edition.

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

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

05-01-2004

€140.23
Excluding VAT

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.

Committee
ACE/12
DevelopmentNote
Supersedes 91/80684 DC (03/2003)
DocumentType
Standard
Pages
10
PublisherName
British Standards Institution
Status
Current
Supersedes

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.

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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