Standard

NS-EN 2436-004:2006

Nov 2006 Published

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Language English

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Abstract

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.

Document information

Standard from SN
Published: 1 November 2006
Edition: 2006-07
Version: 1
Document type: NAT
ISBN:

ICS 49.040
National Committee ASD-STAN

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Adopted from: EN 2436-004:2006 , 0

NS-EN 2436-004:2006

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Abstract

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