Aerospace series - Paints and varnishes - Corrosion resistant chromate-free two component cold curing epoxy primer - Part 006: High corrosion resistance for military application

This standard defines the requirements for a two component, chromate and lead free epoxy, high corrosion resistant primer.
The coating shall be suitable for use on chromic acid anodised or conversion coated aluminium alloys, fibre reinforced composite materials and other suitably prepared substrates.

Luft- und Raumfahrt - Beschichtungsstoffe - Korrosionsbeständiger Zweikomponenten-Primer, kalthärtend, chromatfrei - Teil 006: Hoher Korrosionsschutz für militärische Anwendung

Diese Norm legt die Anforderungen an einen chromat  und bleifreien Zweikomponenten Primer auf Epoxidharzbasis mit hoher Korrosionsbeständigkeit fest.
Die Beschichtung muss für die Anwendung bei mit Chromsäure anodisierten oder mit einer Konver¬sionsschutzschicht überzogenen Aluminiumlegierungen, faserverstärkten Verbundwerkstoffen und bei ande¬ren auf geeignete Weise vorbereiteten Trägerwerkstoffen geeignet sein.

Série aérospatiale - Peintures et vernis - Peinture primaire anti-corrosion sans chromate à deux composants polymérisant à température ambiante - Partie 006 : Haute résistance à la corrosion pour applications militaires

Aeronavtika - Barve in laki - Dvokomponentni temeljni premaz, korozijsko obstojen, brez kroma, ki se suši pri sobni temperaturi - 006. del: Visoka korozijska odpornost, za vojaško uporabo

General Information

Status
Published
Publication Date
03-May-2009
Technical Committee
I13 - Imaginarni 13
Current Stage
6060 - National Implementation/Publication (Adopted Project)
Start Date
17-Apr-2009
Due Date
22-Jun-2009
Completion Date
04-May-2009

EN 2436-006:2006 - Overview

EN 2436-006:2006 is a CEN aerospace standard specifying a two-component, chromate- and lead‑free, cold‑curing epoxy primer formulated for high corrosion resistance in military applications. The primer is intended for use on chromic acid anodised or conversion‑coated aluminium alloys, fibre‑reinforced composite materials and other suitably prepared substrates. The standard sets material, performance, testing and batch release requirements to ensure consistent corrosion protection for aerospace structures.

Key topics and technical requirements

  • Material scope: Two‑component epoxy system (base + activator ± thinner), chromate‑free and lead‑free, designed for aerospace corrosion protection.
  • Application parameters: Typical dry film thickness 25 ± 5 µm; components mixed in whole‑number ratios per manufacturer instructions; cold (room temperature) curing.
  • Classification:
    • Type I - standard solvent content
    • Type II - low VOC (≤ 350 g/L)
    • Class A - standard pigments
    • Class B - low infrared reflective pigments
  • Batch release & qualification: Qualification requires testing of a minimum of three batches; batch acceptance tests are defined for production control.
  • Delivery and physical tests: Non‑volatile matter, VOC (Type II), flash point, density, fineness of grind, sedimentation, flow time, pot life and appearance checks.
  • Film performance tests: Cross‑cut adhesion, scratch resistance, bend/cupping/slow deformation tests, colour and IR reflectance as agreed with purchaser.
  • Environmental and corrosion resistance: Thermal exposure, humidity/condensation, water immersion, neutral salt spray (e.g., 3 000 h Procedure B or 1 000 h Procedure A/C as specified), alternate immersion, and filiform corrosion resistance - all with defined acceptance criteria (e.g., limits on blistering, scribe corrosion and adhesion).
  • Resistance to fluids: Exposure to system fluids such as hydraulic oil (NATO H‑515) with specified performance limits.
  • Relevant test standards: Normative references include EN 3837 (surface preparation), EN 2435‑005/EN 2434‑005 (related aerospace coating standards) and numerous ISO methods for paint testing.

Practical applications and users

  • Primary users: Aerospace and defence manufacturers, paint formulators, military procurement/specification engineers, maintenance/repair organizations, qualified coating applicators and quality assurance teams.
  • Use cases: Primer specification for structural airframe components, repairs and new builds that require chromate‑free corrosion protection suitable for military performance demands and environmental exposure.

Related standards

  • EN 2435‑005 - chromated two‑component cold‑curing epoxy primer (comparator)
  • EN 2434‑005 - related top‑coat system referenced for filiform testing
  • EN 3837 - surface preparation for aluminium substrates
  • ISO/EN test methods for salt spray, humidity, adhesion, VOC and other coating properties

This standard supports transition to chromate‑free aerospace primers while preserving high corrosion resistance required for military applications. Keywords: EN 2436‑006:2006, chromate‑free epoxy primer, aerospace coatings, high corrosion resistance, military primer, two‑component cold curing.

Standard

SIST EN 2436-006:2009

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14 pages
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Frequently Asked Questions

SIST EN 2436-006:2009 is a standard published by the Slovenian Institute for Standardization (SIST). Its full title is "Aerospace series - Paints and varnishes - Corrosion resistant chromate-free two component cold curing epoxy primer - Part 006: High corrosion resistance for military application". This standard covers: This standard defines the requirements for a two component, chromate and lead free epoxy, high corrosion resistant primer. The coating shall be suitable for use on chromic acid anodised or conversion coated aluminium alloys, fibre reinforced composite materials and other suitably prepared substrates.

This standard defines the requirements for a two component, chromate and lead free epoxy, high corrosion resistant primer. The coating shall be suitable for use on chromic acid anodised or conversion coated aluminium alloys, fibre reinforced composite materials and other suitably prepared substrates.

SIST EN 2436-006:2009 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.

You can purchase SIST EN 2436-006:2009 directly from iTeh Standards. The document is available in PDF format and is delivered instantly after payment. Add the standard to your cart and complete the secure checkout process. iTeh Standards is an authorized distributor of SIST standards.

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 - 006. del: Visoka korozijska odpornost, za vojaško uporaboLuft- und Raumfahrt - Beschichtungsstoffe - Korrosionsbeständiger Zweikomponenten-Primer, kalthärtend, chromatfrei - Teil 006: Hoher Korrosionsschutz für militärische AnwendungSérie aérospatiale - Peintures et vernis - Peinture primaire anti-corrosion sans chromate à deux composants polymérisant à température ambiante - Partie 006 : Haute résistance à la corrosion pour applications militairesAerospace series - Paints and varnishes - Corrosion resistant chromate-free two component cold curing epoxy primer - Part 006: High corrosion resistance for military application49.040Prevleke 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 2436-006:2006SIST EN 2436-006:2009en,de01-junij-2009SIST EN 2436-006:2009SLOVENSKI
STANDARD
EUROPEAN STANDARDNORME EUROPÉENNEEUROPÄISCHE NORMEN 2436-006July 2006ICS 49.040 English VersionAerospace series - Paints and varnishes - Corrosion resistantchromate-free two component cold curing epoxy primer - Part006: High corrosion resistance for military applicationSérie aérospatiale - Peintures primaire anti-corrosion sanschromate à deux composants polymérisant à températureambiante - Partie 006 : Haute résistance à la corrosionpour applications militairesLuft- und Raumfahrt - Anstrichstoffe -Korrosionsbeständiger Zweikomponenten-Grundanstrich,kalthärtend chromatfrei - Teil 006: Hoher Korrosionsschutzfür militärische AnwendungThis European Standard was approved by CEN on 27 February 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 2436-006:2006: ESIST EN 2436-006:2009

1) Published as ASD Prestandard at the date of publication of this standard. SIST EN 2436-006:2009
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