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: 1 100 MPa (at ambient temperature)

Standard No.

EN 3725:2004

Release Date

2004

Published By

European Committee for Standardization (CEN)

Latest

EN 3725:2004

Replace

prEN 3725-2003

EN 3725:2004 Referenced Document

• EN 2424:1995 Aerospace Series - Marking of Aerospace Products
• EN 2491:1997 Aerospace Series - Molybdenum Disulfide Dry Lubricants - Coating Methods
• EN 3818:2004 Aerospace series - Bolts, MJ threads, in titanium alloy TIP64001 - Strength class: 1 100 MPa (at ambient temperature) - Technical specification
• EN 3905:2008 Aerospace series - Six lobe recesses for bolts - Technical specification
• EN 3911:2010 Aerospace series - Six lobe recess - Geometrical definition*， 2023-12-24 Update
• ISO 3353-1:2002 Aerospace - Lead and runout threads - Part 1: Rolled external threads
• ISO 5855-2:1999 Aerospace - MJ threads - Part 2: Limit dimensions for bolts and nuts

EN 3725:2004 history

• 2004 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: 1 100 MPa (at ambient temperature)
• 2003 EN 3725:2003 Bolts, pan head, six lobe recess, normal shank, long thread, in titanium alloy TI-P64001, MoS2 coated - Classification: 1 100 MPa (at ambient temperature)