EN 3892:2001
(Main)Aerospace series - Titanium alloy TI-W64001 - Filler metal for welding
Aerospace series - Titanium alloy TI-W64001 - Filler metal for welding
This standard specifies the requirements relating to:
Titanium alloy TI-W64001
Filler metal for welding
for aerospace applications.
Luft- und Raumfahrt - Titanlegierung TI-W64001 - Schweißzusatz
Diese Norm legt die Anforderungen an:
Titanlegierung TI-W64001
Schweißzusatz
für Anwendungen in der Luft- und Raumfahrt fest.
Série aérospatiale - Alliage de titane TI-W64001 - Métal d'apport de soudage
Aerospace series - Titanium alloy TI-W64001 - Filler metal for welding
General Information
- Status
- Published
- Publication Date
- 19-Jun-2001
- Withdrawal Date
- 30-Dec-2001
- Technical Committee
- ASD-STAN - Aerospace
- Drafting Committee
- ASD-STAN/D 4 - Metallic
- Current Stage
- 9093 - Decision to confirm - Review Enquiry
- Start Date
- 01-Jun-2017
- Completion Date
- 28-Jan-2026
Relations
- Effective Date
- 28-Jan-2026
- Effective Date
- 28-Jan-2026
- Referred By
EN 4877-002:2023 - Aerospace series - Filler metals for welding - Part 002: Authorized filler metals - Effective Date
- 28-Jan-2026
Overview
EN 3892:2001 is a European standard developed by the European Committee for Standardization (CEN) that specifies the technical requirements for Titanium alloy TI-W64001 filler metal used in welding applications within the aerospace industry. This standard ensures the quality, consistency, and performance of filler metals critical for aerospace components, where titanium alloys are valued for their high strength-to-weight ratio, corrosion resistance, and temperature stability.
As part of the aerospace series of metallic material standards, EN 3892:2001 aligns with related standards to provide comprehensive guidelines on material properties, production methods, testing, and certification processes. It supports manufacturing safety and reliability, key criteria in aerospace engineering.
Key Topics
Material Designation
Defines the chemical composition and physical attributes of the titanium alloy TI-W64001, including key elements such as aluminum, vanadium, nitrogen, and others within specified limits to maintain alloy integrity.Filler Metal Specifications
Details forms (filler wire and rods), production methods (cold drawing), and delivery conditions (cold-drawn and annealed) to ensure consistent welding performance.Technical Requirements
Covers heat treatment, mechanical properties such as proof stress and tensile strength, dimensional tolerances, and testing protocols for residual stress, internal defects, and batch uniformity to meet aerospace quality standards.Testing and Quality Control
Mandates adherence to test conditions outlined in related standards (e.g., EN 3879 for filler metals) for comprehensive product qualification, defect inspection, and marking criteria to ensure traceability and conformity.Normative References
Connects with other important aerospace standards including EN 2043 (qualification of semi-finished products), EN 3879 (technical specifications for filler metals), and EN 4500-4 (rules for drafting titanium standards).
Applications
The requirements set out in EN 3892:2001 apply primarily to the aerospace sector, where the welding of titanium alloys is prevalent for manufacturing structural components, engine parts, and airframe assemblies. The standard is essential for:
- Aerospace manufacturers producing welded titanium parts requiring high mechanical reliability.
- Quality assurance teams ensuring compliance with European aerospace materials regulations.
- Engineers selecting appropriate filler metals to optimize performance and durability of welded joints under extreme operational conditions.
- Suppliers and fabricators aiming to certify their products and processes under recognized European standards.
Related Standards
EN 3892:2001 is part of a broader framework for aerospace metallic materials and should be considered alongside:
- EN 2043 – General requirements for qualification of semi-finished aerospace metallic products (excluding forgings and castings)
- EN 3879 – Technical specification for weld filler metals used in aerospace applications
- EN 4258 – Organization and linkage of aerospace metallic material standards
- EN 4500-4 – Drafting and presentation rules for titanium and titanium alloy standards
These complementary standards provide a holistic approach for aerospace manufacturers to ensure the integrity and performance of metallic materials used in critical aerospace structures.
Keywords: EN 3892:2001, titanium alloy TI-W64001, filler metal for welding, aerospace standard, titanium welding wire, aerospace materials, titanium alloy welding, European aerospace standard, CEN titanium alloy, aerospace manufacturing standards
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Frequently Asked Questions
EN 3892:2001 is a standard published by the European Committee for Standardization (CEN). Its full title is "Aerospace series - Titanium alloy TI-W64001 - Filler metal for welding". This standard covers: This standard specifies the requirements relating to: Titanium alloy TI-W64001 Filler metal for welding for aerospace applications.
This standard specifies the requirements relating to: Titanium alloy TI-W64001 Filler metal for welding for aerospace applications.
EN 3892:2001 is classified under the following ICS (International Classification for Standards) categories: 49.025.30 - Titanium. The ICS classification helps identify the subject area and facilitates finding related standards.
EN 3892:2001 has the following relationships with other standards: It is inter standard links to EN 4258:2024, EN 4632-006:2013, EN 4877-002:2023. Understanding these relationships helps ensure you are using the most current and applicable version of the standard.
EN 3892:2001 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)
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.Aerospace series - Titanium alloy TI-W64001 - Filler metal for weldingLuft- und Raumfahrt - Titanlegierung TI-W64001 - SchweißzusatzSérie aérospatiale - Alliage de titane TI-W64001 - Métal d'apport de soudageAerospace series - Titanium alloy TI-W64001 - Filler metal for welding49.025.30TitanTitaniumICS:Ta slovenski standard je istoveten z:EN 3892:2001SIST EN 3892:2002en01-januar-2002SIST EN 3892:2002SLOVENSKI
STANDARD
EUROPEAN STANDARDNORME EUROPÉENNEEUROPÄISCHE NORMEN 3892June 2001ICS 49.025.30English versionAerospace series - Titanium alloy TI-W64001 - Filler metal forweldingSérie aérospatiale - Alliage de titane TI-W64001 - Métald'apport de soudageLuft- und Raumfahrt - Titanlegierung TI-W64001 -SchweißzusatzThis 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 EuropeanStandard the status of a national standard without any alteration. Up-to-date lists and bibliographical references concerning such nationalstandards 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 translationunder the responsibility of a CEN member into its own language and notified to the Management Centre has the same status as the officialversions.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 STANDARDIZATIONCOMITÉ EUROPÉEN DE NORMALISATIONEUROPÄISCHES KOMITEE FÜR NORMUNGManagement Centre: rue de Stassart, 36
B-1050 Brussels© 2001 CENAll rights of exploitation in any form and by any means reservedworldwide for CEN national Members.Ref. No. EN 3892:2001 ESIST EN 3892:2002
Page 2EN 3892:2001ForewordThis 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 hasreceived the approval of the National Associations and the Official Services of the member countries ofAECMA, prior to its presentation to CEN.This European Standard shall be given the status of a national standard, either by publication of an identicaltext or by endorsement, at the latest by December 2001, and conflicting national standards shall bewithdrawn at the latest by December 2001.According to the CEN/CENELEC Internal Regulations, the national standards organizations of the followingcountries are bound to implement this European Standard: Austria, Belgium, Czech Republic, Denmark,Finland, France, Germany, Greece, Iceland, Ireland, Italy, Luxembourg, Netherlands, Norway, P
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