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Homepage>BS Standards>49 AIRCRAFT AND SPACE VEHICLE ENGINEERING>49.030 Fasteners for aerospace construction>49.030.20 Bolts, screws, studs>BS EN 3725:2004 Aerospace series. Screws, pan head, six lobe recess, normal shank, long thread, in titanium alloy TI-P64001, anodized, MoS<sub>2</sub> coated. Strength class: 1100 MPa (at ambient temperature)
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immediate downloadReleased: 2004-01-05
BS EN 3725:2004 Aerospace series. Screws, pan head, six lobe recess, normal shank, long thread, in titanium alloy TI-P64001, anodized, MoS<sub>2</sub> coated. Strength class: 1100 MPa (at ambient temperature)

BS EN 3725:2004

Aerospace series. Screws, pan head, six lobe recess, normal shank, long thread, in titanium alloy TI-P64001, anodized, MoS<sub>2</sub> coated. Strength class: 1100 MPa (at ambient temperature)

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Standard number:BS EN 3725:2004
Pages:12
Released:2004-01-05
ISBN:0 580 45188 7
Status:Standard
DESCRIPTION

BS EN 3725:2004


This standard BS EN 3725:2004 Aerospace series. Screws, pan head, six lobe recess, normal shank, long thread, in titanium alloy TI-P64001, anodized, MoS2 coated. Strength class: 1100 MPa (at ambient temperature) is classified in these ICS categories:
  • 49.030.20 Bolts, screws, studs
This standard specifies the characteristics of pan head screws with six lobe recess, threaded to head, in TI-P64001, anodised, MoS2 coated, for aerospace applications. Strength class: 1 100 MPa NOTE Taking account of the recess geometry, the strength class to be used for the seating torque calculation shall not be greater than 900 MPa.
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