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: 30-Oct-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
SIST EN 2436-004:2009
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
SIST EN 2436-004:2009 en,de

2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.

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SIST EN 2436-004:2009
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SIST EN 2436-004:2009
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.
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SIST EN 2436-004:2009
EN 2436-004:2006 (E)
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

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SIST EN 2436-004:2009
EN 2436-004:2006 (E)
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.
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SIST EN 2436-004:2009
EN 2436-004:2006 (E)
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 —

Part 004: High flexibility
EN 3840, Aerospace series — Paints and varnishes — Technical specification

EN 4385, Aerospace series — Non-metallic materials — General organisation of standardisation — Links be-

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

standards — Part 9: Paints and varnishes
1) Published as ASD Prestandard at the date of publication of this standard.
2) Publis
...