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BSI - BS EN 4322

Bolts, double hexagon head with lockwire holes, relieved shank, long thread, in titanium alloy TI-P64001, anodized, MoS2 coated Strength class: 100 MPa (at ambient temperature)

inactive
Organization: BSI
Publication Date: 4 March 2003
Status: inactive
Page Count: 12
ICS Code (Bolts, screws, studs): 49.030.20

Document History

BS EN 4322
December 15, 2004
Bolts, double hexagon head with lockwire holes, relieved shank, long thread, in titanium alloy TI-P64001, anodized, MoS2 coated - Strength class: 1 100 MPa (at ambient temperature)
A description is not available for this item.
BS EN 4322
March 4, 2003
Bolts, double hexagon head with lockwire holes, relieved shank, long thread, in titanium alloy TI-P64001, anodized, MoS2 coated Strength class: 100 MPa (at ambient temperature)
A description is not available for this item.

References

This document references:
ISO 4095 - Aerospace - Bihexagonal Drives - Wrenching Configuration - Metric Series
Published by ISO on March 15, 1998
This International Standard specifies the metric wrenching configuration dimensions of bihexagonal drives. This is a design standard.
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:
EN 2424 - Aerospace series - Marking of aerospace products
Published by CEN on May 1, 2008
A description is not available for this item.
This document references:
EN 2491 - Aerospace series - Molybdenum disulphide dry lubricants - Coating methods
Published by CEN on June 1, 2011
This European Standard defines the coating methods and characteristics of molybdenum disulphide dry film lubricants which may be applied to parts in titanium, titanium alloys, steel, corrosion...
This document references:
EN 3813 - Aerospace series - Titanium alloy TI-P64001 (Ti-6Al-4V) - Annealed - Bar and wire for forged fasteners - De ≤ 50 mm
Published by CEN on January 1, 2013
This standard specifies the requirements relating to: Titanium alloy Ti-6Al-4V Annealed Bar and wire for forged fasteners De ≤ 50 mm for aerospace applications.
This document references:
EN 3818 - Aerospace series - Bolts, MJ threads, in titanium alloy TI-P64001 - Strength class: 1 100 MPa (at ambient temperature) - Technical specification
Published by CEN on May 1, 2019
This European standard specifies the characteristics, qualification and acceptance requirements for bolts with MJ threads in TI-P64001, for aerospace applications. Strength class: 1 100 MPa1. It is...
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