SIST EN 3890:2004
(Main)Aerospace series - Steel FE-WM1502 (X11CrNiMoVN12-3) - Filler metal for welding
- Abstract
This standard specifies the requirements relating to:
Steel FE-WM1502 (X11CrNiMoVN12-3)
Filler metal for welding
for aerospace applications.
- Status
- Published
- Publication Date
- 30-Apr-2004
- Technical Committee
- I08 - Imaginarni 08
- Current Stage
- 6060 - National Implementation/Publication (Adopted Project)
- Start Date
- 01-May-2004
- Due Date
- 01-May-2004
- Completion Date
- 01-May-2004
SIST EN 3890:2004 is the Slovenian adoption of EN 3890:2001 for aerospace filler metal. It specifies the requirements for steel FE-WM1502 (X11CrNiMoVN12-3) used as filler metal for welding in aerospace applications.
What does SIST EN 3890:2004 specify?
SIST EN 3890:2004 specifies the requirements for a welding filler metal identified as steel FE-WM1502 (X11CrNiMoVN12-3) for aerospace applications. It is a material standard, so it focuses on the identity of the product, how it is made, how it is supplied, and which inspection and qualification rules apply.
The document is organized around:
- scope and normative references
- material designation and chemical composition
- melting method, product form, production method, and dimensions
- technical specification and delivery condition
- characteristics, inspection items, notes, and product qualification
The standard uses EN 3879 for detailed filler-metal technical requirements and EN 2043 for product qualification.
What are the key requirements of SIST EN 3890:2004?
The standard defines a specific aerospace filler metal and then ties most detailed controls to referenced aerospace material rules. In practice, that means producers and purchasers can use one document to identify the product, check how it must be made, and see which inspections and qualification steps apply.
- Material designation and chemistry - The standard names the material as FE-WM1502 (X11CrNiMoVN12-3) and gives a chemical composition table. For users, this is the basis for ordering, traceability, and verifying that the product matches the intended alloy.
- Melting method - Clause 3 requires the material to be air melted. This matters because the melting route is part of the defined material condition and therefore part of acceptance.
- Product form and production route - Clauses 4.1 to 4.3 specify filler wire and filler rods produced by cold drawing, with controlled dimensions. That tells manufacturers what forms are covered and what production route they must follow.
- Technical specification - Clause 5 points to EN 3879. In practice, EN 3879 carries the detailed technical rules, so this standard works as the grade-specific identifier and EN 3879 provides the broader welding filler-metal framework.
- Delivery condition - Clauses 6.1 and 6.2 require the filler metal to be supplied cold drawn and annealed with delivery condition code U. Buyers and quality teams use this to check that the supplied condition matches the order.
- Use condition - Clause 7 states the use condition as the delivery condition. That links the supplied state directly to the intended use state, which helps avoid ambiguity in procurement and welding preparation.
- Characteristics and inspection items - The characteristics section lists property and inspection headings such as proof stress, tensile strength, elongation, hardness, bending, impact strength, external defects, residual stress, internal defects, batch uniformity, marking inspection, and dimensional inspection. For practice, this means the product is controlled not only by chemistry and supply condition but also by inspection and material consistency.
- Product qualification - Clause 100 points to EN 2043 and says the qualification programme is to be agreed between manufacturer and purchaser. This matters when the material is being approved for aerospace use and both sides need a defined qualification plan.
What terms does SIST EN 3890:2004 define?
- FE-WM1502 - The material designation used for the specified aerospace welding filler metal.
- X11CrNiMoVN12-3 - The steel grade designation associated with FE-WM1502.
- Filler wire - A wire form of welding filler metal covered by the standard.
- Filler rods - A rod form of welding filler metal covered by the standard.
- Air melted - The required melting method for the material.
- Cold drawn - The production method used to make the filler metal.
- Delivery condition code U - The code used for the specified supplied condition.
- Product qualification - The approval process for the product under EN 2043.
Who uses SIST EN 3890:2004?
SIST EN 3890:2004 is used by aerospace materials manufacturers, welding filler-metal producers, purchasers, quality managers, and test laboratories. They use it to specify the alloy, control production, verify delivery condition, and plan qualification and inspection for welding applications.
It is also relevant for organizations that accept aerospace materials against a standard, because it gives the reference points for chemistry, form, production route, and inspection.
What changed in SIST EN 3890:2004 from the previous edition?
SIST EN 3890:2004 is identical to EN 3890:2001.
Which standards are used with SIST EN 3890:2004?
- EN 2043 - Provides the general requirements for semi-finished product qualification, which the standard uses for product qualification.
- EN 3879 - Provides the technical specification for aerospace filler metals for welding, including the detailed inspection and defect requirements referenced throughout the standard.
- EN 4258 - Gives the general organization of aerospace metallic material standards and the links between types of EN standards.
- EN 4500-5 - Gives the drafting and presentation rules for aerospace steel material standards.
What does the SIST EN 3890:2004 document contain?
The document contains the material designation for FE-WM1502 (X11CrNiMoVN12-3), a chemical composition table, and entries for melting method, product form, production method, dimensions, delivery condition, and delivery condition code. It also contains a characteristics section that organizes the controlled properties and inspection items used for acceptance and qualification.
Several items in the characteristics area are cross-referenced to EN 3879, including defect checks, residual stress, batch uniformity, marking inspection, and dimensional inspection. The final qualification line points to EN 2043 and notes that the qualification programme is agreed between manufacturer and purchaser.
Relations
- Effective Date
- 28-Jan-2026
- Effective Date
- 28-Jan-2026
Get Certified
Connect with accredited certification bodies for this standard

BUREAU VERITAS Certification Germany
Bureau Veritas certification in Germany.

Element Materials Technology
Materials testing and product certification.

AQMS Ltd.
AQMS provides ISO certification to SMEs across the UK.
Sponsored listings
Frequently Asked Questions
SIST EN 3890:2004 is a standard published by the Slovenian Institute for Standardization (SIST). Its full title is "Aerospace series - Steel FE-WM1502 (X11CrNiMoVN12-3) - Filler metal for welding". This standard covers: This standard specifies the requirements relating to: Steel FE-WM1502 (X11CrNiMoVN12-3) Filler metal for welding for aerospace applications.
This standard specifies the requirements relating to: Steel FE-WM1502 (X11CrNiMoVN12-3) Filler metal for welding for aerospace applications.
SIST EN 3890:2004 is classified under the following ICS (International Classification for Standards) categories: 49.025.10 - Steels. The ICS classification helps identify the subject area and facilitates finding related standards.
SIST EN 3890:2004 has the following relationships with other standards: It is inter standard links to SIST EN 4258:2024, SIST EN 4632-004:2014. Understanding these relationships helps ensure you are using the most current and applicable version of the standard.
SIST EN 3890:2004 is available in PDF format for immediate download after purchase. The document can be added to your cart and obtained through the secure checkout process. Digital delivery ensures instant access to the complete standard document.
Standards Content (Sample)
SLOVENSKI STANDARD
01-maj-2004
Aerospace series - Steel FE-WM1502 (X11CrNiMoVN12-3) - Filler metal for welding
Aerospace series - Steel FE-WM1502 (X11CrNiMoVN12-3) - Filler metal for welding
Luft- und Raumfahrt - Stahl FE-WM1502 (X11CrNiMoVN12-3) - Schweißzusatz
Série aérospatiale - Acier FE-WM1502 (X11CrNiMoVN12-3) - Métal d'apport de soudage
Ta slovenski standard je istoveten z: EN 3890:2001
ICS:
49.025.10 Jekla Steels
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.
EUROPEAN STANDARD
EN 3890
NORME EUROPÉENNE
EUROPÄISCHE NORM
December 2001
ICS 49.025.10
English version
Aerospace series - Steel FE-WM1502 (X11CrNiMoVN12-3) -
Filler metal for welding
Serié aérospatiale - Acier FE-WM1502 (X11CrNiMoVN12- Luft- und Raumfahrt - Stahl FE-WM1502
3) - Métal d'apport de soudage (X11CrNiMoVN12-3) - Schweißzusatz
This European Standard was approved by CEN on 2 May 2001.
CEN members are bound to comply with the CEN/CENELEC Internal Regulations which stipulate the conditions for giving this European
Standard the status of a national standard without any alteration. Up-to-date lists and bibliographical references concerning such national
standards may be obtained on application to the Management Centre or to any CEN member.
This European Standard exists in three official versions (English, French, German). A version in any other language made by translation
under the responsibility of a CEN member into its own language and notified to the Management Centre has the same status as the official
versions.
CEN members are the national standards bodies of Austria, Belgium, Czech Republic, Denmark, Finland, France, Germany, Greece,
Iceland, Ireland, Italy, Luxembourg, Netherlands, Norway, Portugal, Spain, Sweden, Switzerland and United Kingdom.
EUROPEAN COMMITTEE FOR STANDARDIZATION
COMITÉ EUROPÉEN DE NORMALISATION
EUROPÄISCHES KOMITEE FÜR NORMUNG
Management Centre: rue de Stassart, 36 B-1050 Brussels
© 2001 CEN All rights of exploitation in any form and by any means reserved Ref. No. EN 3890:2001 E
worldwide for CEN national Members.
Foreword
This European Standard has been prepared by the European Association of Aerospace Manufacturers
(AECMA).
After inquiries and votes carried out in accordance with the rules of this Association, this Standard has
received the approval of the National Associations and the Official Services of the member countries of
AECMA, prior to its presentation to CEN.
This European Standard shall be given the status of a national standard, either by publication of an identical
text or by endorsement, at the latest by June 2002, and conflicting national standards shall be withdrawn at
the latest by June 2002.
According to the CEN/CENELEC Internal Regulations, the national standards organizations of the following
countries are bound to implement this European Standard: Austria, Belgium, Czech Republic, Denmark,
Finland, France, Germany, Greece, Iceland, Ireland, Italy, Luxembourg, Netherlands, Norway, Portugal,
Spain, Sweden, Switzerland and the United Kingdom.
...



