EN 3832:2004
Aerospace series - Bolts, double hexagon head, relieved shank, long thread, in heat resisting nickel base alloy NI-PH2601 (Inconel 718) - Classification: 1 550 MPa (at ambient temperature) / 650 degrees C

Standard No.
EN 3832:2004
Release Date
2004
Published By
European Committee for Standardization (CEN)
Latest
EN 3832:2004
Replace
prEN 3832-2003

EN 3832:2004 Referenced Document

  • ASD-STAN prEN 2952-1995 Aerospace Series Heat Resisting Alloy NI-PH2601 Solution Treated and Cold Worked Bar for Forged Fasteners D Less Than or Equal to 50 mm 1270 MPa Less Than or Equal to Rm Less Than or Equal to 1550 MPa (Edition P 3)
  • ASD-STAN prEN 3666-1995 Aerospace Series Heat Resisting Alloy NI-PH2601 Solution Treated and Cold Worked Bar for Forged Fasteners D Less Than or Equal to 50 mm 1550 MPa Less Than or Equal to Rm Less Than or Equal to 1830 MPa (Edition P 2)
  • EN 2424:1995 Aerospace Series - Marking of Aerospace Products
  • EN 3833:2003 Aerospace series - Bolts, MJ threads, in heat resisting nickel base alloy NI-PH2601 (Inconel 718) - Classification: 1 550 MPa (at ambient temperature) / 650 degrees C - Technical specifications
  • ISO 3353-1:2002 Aerospace - Lead and runout threads - Part 1: Rolled external threads
  • ISO 4095:1998 Aerospace - Bihexagonal drives - Wrenching configuration - Metric series
  • ISO 5855-2:1999 Aerospace - MJ threads - Part 2: Limit dimensions for bolts and nuts

EN 3832:2004 history

  • 2004 EN 3832:2004 Aerospace series - Bolts, double hexagon head, relieved shank, long thread, in heat resisting nickel base alloy NI-PH2601 (Inconel 718) - Classification: 1 550 MPa (at ambient temperature) / 650 degrees C
  • 2003 EN 3832:2003 Aerospace series - Bolts, double hexagon head, relieved shank, long thread, in heat resisting nickel base alloy NI-P100HT (Inconel 718) - Classification: 1 550 MPa (at ambient temperature) / 650 degrees C



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