SIST EN 3886:2002

Aerospace series - Heat resisting alloy NI-WH1303 (NiCo20Cr20Mo5Ti2Al) - Filler metal for welding

This standard specifies the requirements relating to:
Heat resisting alloy NI-WH1303 (NiCo20Cr20Mo5Ti2Al)
Filler metal for welding
for aerospace applications.

Luft- und Raumfahrt - Hochwarmfeste Legierung NI-WH1303 (NiCo20Cr20Mo5Ti2Al) - Schweißzusatz

Diese Norm legt die Anforderungen an:
Hochwarmfeste Legierung NI-WH1303 (NiCo20Cr20Mo5Ti2Al)
Schweißzusatz
für Anwendungen in der Luft- und Raumfahrt fest.

Série aérospatiale - Alliage résistant a chaud NI-WH1303 (NiCo20Cr20Mo5Ti2Al) - Métal d'apport de soudage

Aerospace series - Heat resisting alloy NI-WH1303 (NiCo20Cr20Mo5Ti2Al) - Filler metal for welding

General Information

• Status: Published
• Publication Date: 31-Dec-2001
• ICS: 49.025.15 - Non-ferrous alloys in general
• Technical Committee: SS SPL - Technical Board for the general field
• Current Stage: 6060 - National Implementation/Publication (Adopted Project)
• Start Date: 01-Jan-2002
• Due Date: 01-Jan-2002
• Completion Date: 01-Jan-2002
• Ref Project: EN 3886:2001 - Aerospace series - Heat resisting alloy NI-WH1303 (NiCo20Cr20Mo5Ti2Al) - Filler metal for welding

Overview

EN 3886:2001 (Aerospace series) specifies requirements for the heat‑resisting filler metal NI‑WH1303 (NiCo20Cr20Mo5Ti2Al) used in welding for aerospace applications. Prepared under AECMA and approved by CEN, this standard defines material designation, production and delivery conditions, and references testing and inspection rules applicable to welding filler wires and rods for high‑temperature aerospace components.

Key topics and requirements

• Material designation and chemistry: The standard covers the nickel‑cobalt based heat‑resisting alloy NI‑WH1303 (NiCo20Cr20Mo5Ti2Al) intended as a filler metal for welding.
• Manufacturing and melting: Specifies melting methods such as air melting with vacuum refining to achieve the required cleanliness and alloy consistency.
• Form and production: Defines accepted forms-filler wire and filler rods-and production method (cold drawn).
• Delivery condition: Typical delivery state is cold drawn and annealed; specific delivery codes and use conditions are indicated.
• Technical specification and tests: References EN 3879 for detailed technical specifications for filler metals, including dimensional inspection, marking, batch uniformity (material verification), residual and internal defect criteria, and other inspections.
• Product qualification: Product qualification and any special testing program are to be agreed between manufacturer and purchaser (see EN 2043 for semi‑finished product qualification framework).
• Standard drafting rules: Prepared in accordance with EN 4500‑3 and organized per the EN metallic materials aerospace series guidance (EN 4258).

Applications

• Welding and repair of high‑temperature aerospace components such as turbine parts, hot‑section assemblies, and other engine or airframe elements exposed to elevated temperatures and corrosive environments.
• Use where a nickel‑cobalt based, heat‑resistant filler metal is required to match parent alloys and meet aerospace performance expectations.

Who uses this standard

• Aerospace manufacturers and OEMs specifying welding consumables for engine and hot‑section fabrication.
• Welding consumable producers and material suppliers producing NI‑WH1303 filler wire and rods.
• Quality assurance, procurement and certification teams ensuring compliance with European aerospace material standards.
• Welding engineers and metallurgists selecting filler metals for high‑temperature joining.

Related standards

• EN 3879 - Aerospace series: Filler metals for welding – Technical specification
• EN 2043 - General requirements for semi‑finished product qualification
• EN 4258 - Organization of aerospace material standards
• EN 4500‑3 - Rules for drafting heat‑resisting alloy standards

Keywords: EN 3886:2001, NI‑WH1303, NiCo20Cr20Mo5Ti2Al, filler metal for welding, heat resisting alloy, aerospace welding consumables, CEN, AECMA.

Standards Content (Sample)

2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.Aerospace series - Heat resisting alloy NI-WH1303 (NiCo20Cr20Mo5Ti2Al) - Filler metal for weldingLuft- und Raumfahrt - Hochwarmfeste Legierung NI-WH1303 (NiCo20Cr20Mo5Ti2Al) - SchweißzusatzSérie aérospatiale - Alliage résistant a chaud NI-WH1303 (NiCo20Cr20Mo5Ti2Al) - Métal d'apport de soudageAerospace series - Heat resisting alloy NI-WH1303 (NiCo20Cr20Mo5Ti2Al) - Filler metal for welding49.025.15Neželezove zlitine na splošnoNon-ferrous alloys in generalICS:Ta slovenski standard je istoveten z:EN 3886:2001SIST EN 3886:2002en01-januar-2002SIST EN 3886:2002SLOVENSKI
STANDARD
EUROPEAN STANDARDNORME EUROPÉENNEEUROPÄISCHE NORMEN 3886June 2001ICS 49.025.15English versionAerospace series - Heat resisting alloy NI-WH1303(NiCo20Cr20Mo5Ti2Al) - Filler metal for weldingSérie aérospatiale - Alliage résistant à chaud NI-WH1303(NiCo20Cr20Mo5Ti2Al) - Métal d'apport de soudageLuft- und Raumfahrt - Hochwarmfeste Legierung NI-WH1303 (NiCo20Cr20Mo5Ti2Al) - 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 3886:2001 ESIST EN 3886:2002

Page 2EN 3886:2001ForewordThis 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, Cz
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