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BS EN 4322:2004 | British Standards

Standards Shop | ICS 49 | ICS 49.030 |  ICS 49.030.20

49.030.20 Bolts, screws, studs

Aerospace series. Bolts, double hexagon head with lockwire holes, relieved shank, long thread, in titanium alloy TI-P64001, anodized, MoS<sub>2</sub> coated. Strength class: 1100 MPa (at ambient temperature)

Aerospace series. Bolts, double hexagon head with lockwire holes, relieved shank, long thread, in titanium alloy TI-P64001, anodized, MoS<sub>2</sub> coated. Strength class: 1100 MPa (at ambient temperature)

BS EN 4322:2004

Aerospace series. Bolts, double hexagon head with lockwire holes, relieved shank, long thread, in titanium alloy TI-P64001, anodized, MoS2 coated. Strength class: 1100 MPa (at ambient temperature)


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ISBN: 0580450945

Keywords:
Surface treatment, Anodizing, Fasteners, External-thread fasteners, Dimensional tolerances, Dimensions, Bolts, Titanium alloys, Marking, Aircraft components, Threaded fasteners, Molybdenum inorganic compounds, Sulfides, Designations, Coatings, Bihexagonal-head fasteners, PDF
Publication Date15 Dec 2004
Product SKU30097232
ISBN0580450945
BSI CodeBS EN 4322:2004
No. of pages12
ReplacesBS EN 4322:2003
PublisherBritish Standards Institution
Identical National Standard to:
  • EN 4322:2004




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