EN 2436-001:2006
(Main)Aerospace series - Paints and varnishes - Corrosion resistant chromate-free two component cold curing primer - Part 001: Basic requirements
Aerospace series - Paints and varnishes - Corrosion resistant chromate-free two component cold curing primer - Part 001: Basic requirements
This standard specifies the basic requirements for a two component, cold curing, chromate-free epoxy or polyurethane, corrosion resistant primer which can be used with or without a finish for aerospace applications.
The properties specified in this standard are obtained on defined aluminium alloy test pieces prepared in accordance with EN 3837, process A and ISO 3270. The ability of the material to be used for a specific application (e.g. alternative substrate, alternative primer, specific drying conditions etc.) shall be determined by supplementary tests to confirm that the requirements of this standard are met.
Luft- und Raumfahrt - Beschichtungsstoffe - Korrosionsbeständiger Zweikomponenten-Grundanstrich, kalthärtend chromatfrei - Teil 001: Grundlegende Anforderungen
Diese Norm legt die Mindestanforderungen an einen korrosionsbeständigen, chromatfreien, kalthärtenden Zweikomponenten Primer auf Epoxid oder Polyurethanharzbasis fest, der mit oder ohne Deckbeschichtung in der Luft und Raumfahrt verwendet werden kann.
Die in dieser Norm festgelegten Eigenschaften werden anhand definierter Probenkörper aus Aluminiumlegie¬rung ermittelt, die gemäß EN 3837, Verfahren A und ISO 3270 vorbereitet werden. Die Eignung des für eine bestimmte Anwendung zu verwendenden Materials (z. B. alternativer Trägerwerkstoff, alternativer Primer, bestimmte Trocknungsbedingungen usw.) ist durch zusätzliche Prüfungen bestimmen, um nachzuweisen, dass die Anforderungen dieser Norm erfüllt werden.
Série aérospatiale - Peintures et vernis - Peinture primaire anti-corrosion sans chromate à deux composants polymérisant à température ambiante - Partie 001 : Exigences générales
Aeronavtika - Barve in laki - Dvokomponentni temeljni premaz, korozijsko obstojen, brez kroma, ki se suši pri sobni temperaturi - 001. del: Osnovne zahteve
General Information
- Status
- Published
- Publication Date
- 20-Jun-2006
- Withdrawal Date
- 30-Dec-2006
- 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
- 11-Feb-2026
Relations
- Effective Date
- 09-Feb-2026
- Effective Date
- 09-Feb-2026
- Refers
EN 2334:1997 - Aerospace series - Chromic-sulphuric acid pickle of aluminium and aluminium alloys - Effective Date
- 28-Jan-2026
- Effective Date
- 28-Jan-2026
- Effective Date
- 28-Jan-2026
Overview
EN 2436-001:2006 defines the basic requirements for a two-component, cold-curing, chromate-free, corrosion-resistant primer intended for aerospace applications. The primer can be an epoxy (Type A) or polyurethane (Type B) system and may be used with or without a finish coat. Properties in this standard are obtained on defined aluminium-alloy test pieces prepared in accordance with EN 3837 (process A) and ISO 3270. Where the primer is to be used on alternative substrates or under different processing conditions, supplementary testing is required to confirm compliance.
Key Topics
- Scope and classification: Primer types are classified by chemical reaction mechanism - Type A (epoxy with amino activator) and Type B (hydroxyl resin with polyisocyanate activator).
- Formulation and application: The standard describes the form of product (base, activator, thinner if required) and instructs mixing in whole-number proportions by volume or weight as per manufacturer guidance. Typical dry film thickness is 20 ± 5 µm.
- Testing regime:
- Batch release tests: Tests marked with * in the standard's tables are required for batch acceptance.
- Qualification tests: Full set of tests in Tables 1–5 must be completed for product qualification.
- Representative tests referenced include adhesion, scratch resistance, viscosity/fineness, VOC and density checks, and drying characteristics.
- Environmental and durability requirements: The standard sets performance checks for exposure and resistance, including:
- Resistance to fluids (e.g. tri-n-butyl phosphate to EN 2379 G2 for 24 h at (70 ± 2) °C) with no blistering or lifting.
- Water exposure (water to ISO 3696 Grade 2 for 336 h) with no film defect.
- Corrosion resistance assessed by neutral salt spray test (1 000 h) with limits on blistering, detachment, pitting and corrosion near scribe lines.
- Referenced test methods and documentation: EN 3840 (technical specification), EN 3837 (surface preparation), EN 2334 (pickling), ISO 3270 (conditioning), ISO 1513 and TR 7000-9 are among the normative references.
Applications
This standard is targeted at manufacturers, suppliers and end-users in the aerospace industry who specify or validate primers for airframe and related structures. It supports:
- Selection and qualification of chromate-free, corrosion-resistant primers for aluminium alloys
- Batch release and ongoing quality control of two-component cold-curing primer systems
- Demonstration of adhesion, corrosion protection and compatibility with subsequent finishes or direct exposure
Related Standards
- EN 3840 - Aerospace paints and varnishes: technical specification
- EN 3837 - Surface preparation and test-piece nature
- EN 2334 - Chromic-sulphuric acid pickle of aluminium alloys
- EN 2379 - Fluids for assessment of non-metallic materials
- EN 4385 - Organisation of aerospace non-metallic materials standards
- ISO 3270, ISO 1513 and TR 7000-9
Practical value: EN 2436-001:2006 provides a prescriptive baseline for chromate-free aerospace primers, helping manufacturers and users ensure consistent corrosion protection, adhesion and regulatory-aligned batch qualification for aluminium-based aerospace substrates.
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Frequently Asked Questions
EN 2436-001:2006 is a standard published by the European Committee for Standardization (CEN). Its full title is "Aerospace series - Paints and varnishes - Corrosion resistant chromate-free two component cold curing primer - Part 001: Basic requirements". This standard covers: This standard specifies the basic requirements for a two component, cold curing, chromate-free epoxy or polyurethane, corrosion resistant primer which can be used with or without a finish for aerospace applications. The properties specified in this standard are obtained on defined aluminium alloy test pieces prepared in accordance with EN 3837, process A and ISO 3270. The ability of the material to be used for a specific application (e.g. alternative substrate, alternative primer, specific drying conditions etc.) shall be determined by supplementary tests to confirm that the requirements of this standard are met.
This standard specifies the basic requirements for a two component, cold curing, chromate-free epoxy or polyurethane, corrosion resistant primer which can be used with or without a finish for aerospace applications. The properties specified in this standard are obtained on defined aluminium alloy test pieces prepared in accordance with EN 3837, process A and ISO 3270. The ability of the material to be used for a specific application (e.g. alternative substrate, alternative primer, specific drying conditions etc.) shall be determined by supplementary tests to confirm that the requirements of this standard are met.
EN 2436-001:2006 is classified under the following ICS (International Classification for Standards) categories: 49.040 - Coatings and related processes used in aerospace industry. The ICS classification helps identify the subject area and facilitates finding related standards.
EN 2436-001:2006 has the following relationships with other standards: It is inter standard links to ISO 1513:1992, ISO 3696:1987, EN 2334:1997, EN 3840:2007, EN 4588:2007. Understanding these relationships helps ensure you are using the most current and applicable version of the standard.
EN 2436-001:2006 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.Aeronavtika - Barve in laki - Dvokomponentni temeljni premaz, korozijsko obstojen, brez kroma, ki se suši pri sobni temperaturi - 001. del: Osnovne zahteveLuft- und Raumfahrt - Beschichtungsstoffe - Korrosionsbeständiger Zweikomponenten-Grundanstrich, kalthärtend chromatfrei - Teil 001: Grundlegende AnforderungenSérie aérospatiale - Peintures et vernis - Peinture primaire anti-corrosion sans chromate à deux composants polymérisant à température ambiante - Partie 001 : Exigences généralesAerospace series - Paints and varnishes - Corrosion resistant chromate-free two component cold curing primer - Part 001: Basic requirements49.040Prevleke in z njimi povezani postopki, ki se uporabljajo v letalski in vesoljski industrijiCoatings and related processes used in aerospace industryICS:Ta slovenski standard je istoveten z:EN 2436-001:2006SIST EN 2436-001:2009en,de01-julij-2009SIST EN 2436-001:2009SLOVENSKI
STANDARD
EUROPEAN STANDARDNORME EUROPÉENNEEUROPÄISCHE NORMEN 2436-001June 2006ICS 49.040 English VersionAerospace series - Paints and varnishes - Corrosion resistantchromate-free two component cold curing primer - Part 001:Basic requirementsSérie aérospatiale - Peintures et vernis - Peinture primaireanti-corrosion sans chromate à deux composantspolymérisant à température ambiante - Partie 001 :Exigences généralesLuft- und Raumfahrt - Anstrichstoffe -Korrosionsbeständiger Zweikomponenten-Grundanstrich,kalthärtend chromatfrei - Teil 001: GrundlegendeAnforderungenThis European Standard was approved by CEN on 9 March 2006.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 Central Secretariat 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 Central Secretariat has the same status as the officialversions.CEN members are the national standards bodies of Austria, Belgium, Cyprus, Czech Republic, Denmark, Estonia, Finland, France,Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Romania,Slovakia, Slovenia, Spain, Sweden, Switzerland and United Kingdom.EUROPEAN COMMITTEE FOR STANDARDIZATIONCOMITÉ EUROPÉEN DE NORMALISATIONEUROPÄISCHES KOMITEE FÜR NORMUNGManagement Centre: rue de Stassart, 36
B-1050 Brussels© 2006 CENAll rights of exploitation in any form and by any means reservedworldwide for CEN national Members.Ref. No. EN 2436-001:2006: ESIST EN 2436-001:2009
Fluids for assessment of non-metallic materials1)
EN 3837, Aerospace series — Paints and varnishes — Nature and method for surface
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