SS-EN-4595 Aerospace series - Paints and varnishes - Two component cold curing polyurethane finish - Subsonic erosion resistance

SS-EN-4595 - 2013 EDITION - CURRENT


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This standard specifies the requirements for a two component polyurethane, topcoat, with a medium degree of resistance to erosion by the effects of rain, available in a range of colours and levels of gloss, to be applied over a primer for aerospace applications on areas where rain erosion at subsonic speeds may be a problem e.g. leading edges and air intakes. The properties specified in this standard are obtained on defined aluminium alloy test pieces prepared in accordance with EN 3837 Procedure A and EN 23270 and painted with primer to EN 2435. 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.

To find similar documents by classification:

49.020 (Aircraft and space vehicles in general Including aircraft performance, flight dynamics, etc. Air transport, see 03.220.50)

49.040 (Coatings and related processes used in aerospace industry Coatings for general use, see 25.220)

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Designation Name

SS-EN 4595:2013

Revision Level

2013 EDITION

Status

Current

Publication Date

Jan. 14, 2013

Language(s)

English

Page Count

20

International Equivalent

EN 4595:2013(IDT)