DIN EN 2436-005:2007-04
Aerospace series - Paints and varnishes - Corrosion resistant chromate-free two component cold curing primer - Part 005: For exterior use with surface preparation tolerance; German and English version EN 2436-005:2006
| Fecha edición: |
2007-04-01
En Vigor
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| Idiomas disponibles: | Alemán, Inglés |
| Resumen: | This standard defines the requirements for a two component, cold curing, chromate-free epoxy or polyurethane, corrosion resistant primer with improved tolerance to the standard of surface preparation for use with a finish for aerospace exterior 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. |
| Keywords: | Aerospace transport|Air transport|Classification|Coating materials|Coatings|Corrosion|Corrosion resistance|Corrosion-resistant|Corrosion-resistant materials|Epoxides|Exterior application|Exterior finishes|Finishing painting|Liquids|Multilingual|Paints|Polyurethane|Priming coats|Properties|Space transport|Specification (approval)|Surface properties|Testing|Tolerances (measurement)|Two-component coatings|Work hardening |
| ICS: | 49.040 - Recubrimientos y procesos relacionados para la industria aeroespacial |
| CTN: | |
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Equivalencia Internacional |
Idéntica EN 2436-005:2006 |
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