EN 2680:2006

Current

Current The latest, up-to-date edition.

Aerospace series - Nuts, anchor, self-locking, floating, self-aligning, two lug, in alloy steel, cadmium plated, MoS2 lubricated, metric series - Classification: 900 MPa (at ambient temperature) / 235 °C

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Published date: 17-05-2006

Publisher: Comite Europeen de Normalisation

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Table of Contents - (Show below) - (Hide below)

Foreword
1 Scope
2 Normative references
3 Required characteristics
4 Designation
5 Marking
6 Technical specification

Abstract - (Show below) - (Hide below)

This standard specifies the characteristics of self-locking, floating, self-aligning, two lug anchor nuts, in alloy steel, cadmium plated, MoS2-lubricated.Classification: 900 MPa / 235 °C

General Product Information - (Show below) - (Hide below)

Committee	ASD-STAN
Development Note	Supersedes PREN 2680. (06/2006)
Document Type	Standard
ISBN
Pages
Published
Publisher	Comite Europeen de Normalisation
Status	Current
Supersedes	PREN 2680 : 200P3

National Adoptions - (Show below) - (Hide below)

Equivalent Standard(s)	Relationship
NS EN 2680 : 1ED 2006	Identical
DIN EN 2680:2007-02	Identical
BS EN 2680:2006	Identical
UNE-EN 2680:2006	Identical
PN EN 2680 : 2006	Identical
UNI EN 2680 : 2007	Identical
I.S. EN 2680:2006	Identical
NF EN 2680 : 2006	Identical
SN EN 2680 : 2006	Identical
NEN EN 2680 : 2006	Identical
NBN EN 2680 : 2006	Identical

Standards Referencing This Book - (Show below) - (Hide below)

EN 9100:2009	Quality Management Systems - Requirements for Aviation, Space and Defense Organizations
ISO 8788:2000	Aerospace Nuts, metric Tolerances of form and position
ISO 5855-2:1999	Aerospace MJ threads Part 2: Limit dimensions for bolts and nuts
EN 2491:2011	Aerospace series - Molybdenum disulphide dry lubricants - Coating methods
ISO 12273:2010	Aerospace Nuts, anchor, self-locking, floating, self-aligning, two lug, with MJ threads, classifications: 900 MPa (at ambient temperature)/235 degrees C, 900 MPa (at ambient temperature)/315 degrees C and 900 MPa (at ambient temperature)/425 degrees C Dimensions
ISO 5858:1999	Aerospace Nuts, self-locking, with maximum operating temperature less than or equal to 425 degrees C Procurement specification
EN 2133:2010	Aerospace series - Cadmium plating of steels with specified tensile strength ≤ 1 450 MPa, copper, copper alloys and nickel alloys
EN 2424:2008	Aerospace series - Marking of aerospace products
ISO 9001:2015	Quality management systems — Requirements
TR 3791 : 3	AEROSPACE SERIES - MATERIALS FOR SELF-LOCKING NUTS, THREADED INSERTS AND SCREW THREAD INSERTS OF TEMPERATURE CLASSES <= 425 DEGREES C

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