EN 2436-004:2006

Aerospace series - Paints and varnishes - Corrosion resistant chromate-free two component cold curing primer - Part 004: High corrosion and fluid resistance with surface preparation tolerance

This standard specifies the basic requirements for a two component, cold curing, chromate-free epoxy or polyurethane, high corrosion and fluid resistant primer with improved tolerance to the standard of surface preparation 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 D 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-Primer, kalthärtend chromatfrei - Teil 004: Hohe Beständigkeit gegen Korrosion und Flüssigkeiten mit Oberflächentoleranzen

Diese Norm legt die Mindestanforderungen an einen chromatfreien, kalthärtenden Zweikomponenten Primer auf Epoxid  oder Polyurethanharzbasis mit hoher Beständigkeit gegen Korrosion und Flüssigkeiten und einer verbesserten Oberflächentoleranz 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 nach EN 3837, Verfahren D 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 - Peintures primaire anti-corrosion sans chromate à deux composants polymérisant à température ambiante - Partie 004 : Haute résistance à la corrosion et aux fluides avec tolérance à la préparation de surface

Aeronavtika - Barve in laki - Dvokomponentni temeljni premaz, korozijsko obstojen, brez kroma, ki se suši pri sobni temperaturi - 004. del: Visoka odpornost proti koroziji in tekočinam s toleranco pri pripravi površine

General Information

• Status: Published
• Publication Date: 18-Jul-2006
• Withdrawal Date: 30-Jan-2007
• ICS: 49.040 - Coatings and related processes used in aerospace industry
• Technical Committee: ASD-STAN - Aerospace
• Drafting Committee: ASD-STAN/D 5 - Non-Metallic
• Current Stage: 9093 - Decision to confirm - Review Enquiry
• Completion Date: 01-Jun-2017
• Ref Project: SIST EN 2436-004:2009 - Aerospace series - Paints and varnishes - Corrosion resistant chromate-free two component cold curing primer - Part 004: High corrosion and fluid resistance with surface preparation tolerance

Standards Content (Sample)

SLOVENSKI STANDARD
01-julij-2009
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Aerospace series - Paints and varnishes - Corrosion resistant chromate-free two
component cold curing primer - Part 004: High corrosion and fluid resistance with surface
preparation tolerance
Luft- und Raumfahrt - Beschichtungsstoffe - Korrosionsbeständiger Zweikomponenten-
Primer, kalthärtend chromatfrei - Teil 004: Hohe Beständigkeit gegen Korrosion und
Flüssigkeiten mit Oberflächentoleranzen
Série aérospatiale - Peintures et vernis - Peintures primaire anti-corrosion sans
chromate à deux composants polymérisant à température ambiante - Partie 004 : Haute
résistance à la corrosion et aux fluides avec tolérance à la préparation de surface
Ta slovenski standard je istoveten z: EN 2436-004:2006
ICS:
49.040 Prevleke in z njimi povezani Coatings and related
postopki, ki se uporabljajo v processes used in aerospace
letalski in vesoljski industriji industry
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.

EUROPEAN STANDARD
EN 2436-004
NORME EUROPÉENNE
EUROPÄISCHE NORM
July 2006
ICS 49.040
English Version
Aerospace series - Paints and varnishes - Corrosion resistant
chromate-free two component cold curing primer - Part 004:
High corrosion and fluid resistance with surface preparation
tolerance
Série aérospatiale - Peintures et vernis - Peintures Luft- und Raumfahrt - Anstrichstoffe -
primaires anti-corrosion sans chromate à deux composants Korrosionsbeständiger Zweikomponenten-Grundanstrich,
polymérisant à température ambiante - Partie 004 : Haute kalthärtend chromatfrei - Teil 004: Hohe Beständigkeit
résistance à la corrosion et aux fluides avec tolérance à la gegen Korrosion und Flüssigkeiten mit
préparation de surface Oberflächentoleranzen
This 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 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 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 translation
under the responsibility of a CEN member into its own language and notified to the Central Secretariat has the same status as the official
versions.
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 STANDARDIZATION
COMITÉ EUROPÉEN DE NORMALISATION
EUROPÄISCHES KOMITEE FÜR NORMUNG
Management Centre: rue de Stassart, 36  B-1050 Brussels
© 2006 CEN All rights of exploitation in any form and by any means reserved Ref. No. EN 2436-004:2006: E
worldwide for CEN national Members.

Contents Page
Foreword.3
0 Introduction.4
1 Scope .4
2 Normative references .4
3 Definitions .5
4 Classification.5
5 Batch release and qualification testing.5

Foreword
This European Standard (EN 2436-004:2006) has been prepared by the AeroSpace and Defense Industries
Association - Standardization (ASD-STAN).
After enquiries and votes carried out in accordance with the rules of this Association, this Standard has re-
ceived the approval of the National Associations and the Official Services of the member countries of ASD,
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 January 2007, and conflicting national standards shall be withdrawn at
the latest by January 2007.
Attention is drawn to the possibility that some of the elements of this document may be the subject of patent
rights. CEN [and/or CENELEC] shall not be held responsible for identifying any or all such patent rights.
According to the CEN/CENELEC Internal Regulations, the national standards organizations of the following
countries are bound to implement this European Standard: Austria, Belgium, Cyprus, Czech Republic, Den-
mark, Estonia, Finland, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxem-
bourg, Malta, Netherlands, Norway, Poland, Portugal, Romania, Slovakia, Slovenia, Spain, Sweden, Switzer-
land and the United Kingdom.
0 Introduction
This standard is part of a series of EN non-metallic materials standards for aerospace applications. The gen-
eral organisation of this series is described in EN 4385.
This standard is a level 3 document as defined in EN 4385.
Definition of subcase numbering in Tables 2 to 5 is given in TR 7000-9.
1 Scope
This standard specifies the basic requirements for a two component, cold curing, chromate-free epoxy or
polyurethane, high corrosion and fluid resistant primer with improved tolerance to the standard of surface
preparation 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 D 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.
2 Normative references
The following referenced documents are indispensable for the application of this document. For dated refer-
ences, only the edition cited applies. For undated references, the latest edition of the referenced document
(including any amendments) applies.
)
EN 2379, Aerospace series — Fluids for assessment of non-metallic materials
EN 3837, Aerospace series — Paints and varnishes — Nature and method for surface preparation of test
)
pieces in aluminium alloys
EN 2434-004, Aerospace series — Paints and varnishes — Two component cold curing polyurethane finish —
1)
Part 004: High flexibility
1)
EN 3840, Aerospace series — Paints and varnishes — Technical specification
EN 4385, Aerospace series — Non-metallic materials — General organisation of standardisation — Links be-
1)
tween types of standards
ISO 1513, Paints and varnishes — Examination and preparation of samples for testing
ISO 3270, Paints and varnishes and their raw materials — Temperature and humidities for conditioning and
testing
ISO 3696, Water for analytical laboratory use — Specification and test methods
TR 7000-9, Aerospace series — Non-metallic materials — Rules for the drafting and presentation of material
2)
standards — Part 9: Paints and varnishes

1) Published as ASD Prestandard at the date of publication of this standard.
2) Publis
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