I.S. EN 3741:2005
Current
The latest, up-to-date edition.
AEROSPACE SERIES - NUTS, CLIP, METRIC - INSTALLATION HOLES AND ASSEMBLY
Hardcopy , PDF
English
01-01-2005
For Harmonized Standards, check the EU site to confirm that the Standard is cited in the Official Journal.
Only cited Standards give presumption of conformance to New Approach Directives/Regulations.
Dates of withdrawal of national standards are available from NSAI.
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.
DocumentType |
Standard
|
Pages |
9
|
PublisherName |
National Standards Authority of Ireland
|
Status |
Current
|
Supersedes |
Standards | Relationship |
NEN EN 3741 : 2006 | 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 |
BS EN 3741:2004 | 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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