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I.S. EN 2882:2006

I.S. EN 2882:2006

Superseded

Superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

View Superseded by
superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

AEROSPACE SERIES - NUTS, HEXAGONAL, SELF-LOCKING, WITH COUNTERBORE AND CAPTIVE WASHER, IN STEEL, CADMIUM PLATED, MOS[2] LUBRICATED - CLASSIFICATION: 1100 MPA (AT AMBIENT TEMPERATURE)/235 DEGREE C

Available format(s)

Hardcopy , PDF

Superseded date

30-11-2023

Language(s)

English

Published date

01-01-2006

Publisher

National Standards Authority of Ireland

Preview

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.

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

Describes characteristics for hexagon nuts, with counterbore and captive washer, with a self-locking feature achieved by forming the upper portion out-of-round, in steel, cadmium plated, MoS[2] lubricated, classification 1100 MPa/235 degree C.

DocumentType
Standard
Pages
9
PublisherName
National Standards Authority of Ireland
Status
Superseded
SupersededBy

Standards Relationship
DIN EN 2882:2008-02 Identical
BS EN 2882:2006 Identical
UNI EN 2882 : 2008 Identical
NBN EN 2882 : 2006 Identical
NS EN 2882 : 1ED 2006 Identical
SN EN 2882 : 2007 Identical
NEN EN 2882 : 2006 Identical
NF EN 2882 : 2006 Identical
EN 2882:2006 Identical
ONORM EN 2882 : 2007 Identical

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 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
ISO 8538:1999 Aerospace Nuts, hexagonal, self-locking, with counterbore and captive washer, with MJ threads, classifications: 1 100 MPa (at ambient temperature)/235 degrees C, 1 100 MPa (at ambient temperature)/315 degrees C and 1 100 MPa (at ambient temperature)/425 degrees C Dimensions

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Hardcopy - English
PDF - English
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