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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Superseded

Superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

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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Superseded date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

Superseded by

I.S. EN 2882:2023

Language(s)

English

Published date

01-01-2006

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.

€33.00
Excluding VAT

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Superseded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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