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 EN 2436-004:2006

Publication date:   Mar 28, 2008

General information

90.93 Standard confirmed   Jun 1, 2017

CEN

ASD-STAN Aerospace

European Norm

49.040   Coatings and related processes used in aerospace industry

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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.

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PUBLISHED
EN 2436-004:2006
90.93 Standard confirmed
Jun 1, 2017