EN 3528:2013
Aerospace series - Steel X2NiCoMo18-8-5 (1.6359) - Vacuum induction melted and vacuum arc remelted - Solution treated and precipitation treated - Bar - a or D = 150 mm - 1 750 MPa = Rm = 2 000 MPa

Standard No.
EN 3528:2013
Release Date
2013
Published By
European Committee for Standardization (CEN)
Latest
EN 3528:2013
Replace
FprEN 3528-2011
Scope
This standard specifies the requirements relating to:Steel X2NiCoMo18-8-5 (1.6359) Vacuum induction melted and vacuum arc remelted Solution treated and precipitation treated Bar a or D ≤ 150 mm 1 750 MPa ≤ Rm ≤ 2 000 MPa for aerospace applications.

EN 3528:2013 Referenced Document

  • EN 4050-4:2012 Aerospace series - Test method for metallic materials - Ultrasonic inspection of bars, plates, forging stock and forgings - Part 4: Acceptance criteria
  • EN 4258:1998 Aerospace series - Metallic materials - General organization of standardization - Links between types of EN standards and their use
  • EN 4500-005:2012 Aerospace series - Metallic materials - Rules for drafting and presentation of material standards - Part 005: Specific rules for steels
  • EN 4700-002:2010 Aerospace series - Steel and heat resisting alloys - Wrought products - Technical specification - Part 002: Bar and section

EN 3528:2013 history

  • 2013 EN 3528:2013 Aerospace series - Steel X2NiCoMo18-8-5 (1.6359) - Vacuum induction melted and vacuum arc remelted - Solution treated and precipitation treated - Bar - a or D = 150 mm - 1 750 MPa = Rm = 2 000 MPa



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