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I.S. EN 2866:2009

Current
Current

The latest, up-to-date edition.

AEROSPACE SERIES - NUTS, ANCHOR, SELF-LOCKING, FLOATING, ONE LUG, WITH COUNTERBORE, IN STEEL, CADMIUM PLATED, MOS[2] LUBRICATED - CLASSIFICATION: 1110 MPA (AT AMBIENT TEMPERATURE)/235 DEGREE C
Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

01-01-2009

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 the characteristics of one lug, floating anchor nuts, with counterbore and self-locking feature achieved by forming the upper portion out-of-round, in steel, cadmium plated, MoS[2] lubricated.

DocumentType
Standard
Pages
9
PublisherName
National Standards Authority of Ireland
Status
Current

Standards Relationship
EN 2866 : 2009 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
ISO 3224:1998 Aerospace Nuts, anchor, self-locking, floating, single lug, with counterbore, 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
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
TR 3791 : 3 AEROSPACE SERIES - MATERIALS FOR SELF-LOCKING NUTS, THREADED INSERTS AND SCREW THREAD INSERTS OF TEMPERATURE CLASSES <= 425 DEGREES C
EN 2542:2008 Aerospace series - Steel FE-PL1502 (25CrMo4) - Annealed - Bar and wire - De ≤ 40 mm - For prevailing torque nuts
EN 2543 : 2009 AEROSPACE SERIES - STEEL FE-PL1502 (25CRMO4) - ANNEALED - SHEET AND STRIP - 0,3 MM <= A <= 2 MM - FOR PREVAILING TORQUE NUTS

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