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BSI - BS EN 2882

Nuts, hexagonal, self-locking, with counterbore and captive washer, in steel, cadmium plated, MoS2 lubricated - Classification: 1 100 MPa (at ambient temperature) / 235 °C

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Organization: BSI
Publication Date: 31 August 2006
Status: active
Page Count: 10
ICS Code (Nuts): 49.030.30

Document History

BS EN 2882
November 30, 2023
Aerospace series - Nut, hexagonal, self-locking, with counterbore and captive washer, in steel, cadmium plated, MoS2 lubricated - Classification: 1 100 MPa (at ambient temperature) / 235 °C
A description is not available for this item.
BS EN 2882
August 31, 2006
Nuts, hexagonal, self-locking, with counterbore and captive washer, in steel, cadmium plated, MoS2 lubricated - Classification: 1 100 MPa (at ambient temperature) / 235 °C
A description is not available for this item.

References

This document references:
ISO 5858 - Aerospace - Nuts, Self-Locking, with Maximum Operating Temperature Less Than or Equal to 425 Degrees Celsius - Procurement Specification
Published by ISO on November 15, 1999
This International Standard specifies the required characteristics for metric self-locking nuts, with MJ threads, for use in aerospace construction at a maximum temperature less than or equal to 425...
This document references:
ISO 8538 - Aerospace - Nuts, Hexagonal, Self-Locking with Counterbore and Captive Washer, with MJ Threads, Classifications: 1 100 MPa (at Ambient Temperature)/235 Degrees Celsius, 1 100 MPa (at Ambient Temperature)/315 Degrees Celsius and 1 100 MPa (at Ambient Temperature)/425 Degrees Celsius - Dimensions
Published by ISO on February 1, 1999
A description is not available for this item.
This document references:
ISO 5855-2 - Aerospace - MJ Threads - Part 2: Limit Dimensions for Bolts and Nuts
Published by ISO on October 15, 1999
This part of ISO 5855 specifies limit dimensions of MJ threads for bolts and nuts of nominal diameter 1,6 mm to 39 mm for aerospace construction.
This document references:
BS EN 2133 - Aerospace series — Cadmium plating of steels with specified tensile strength ≤ 1 450 MPa, copper, copper alloys and nickel alloys
Published by BSI on December 31, 2020
A description is not available for this item.
This document references:
BS EN 2424 - Aerospace series - Marking of aerospace products
Published by BSI on July 31, 2008
A description is not available for this item.
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