EN 2435-001:2006
Withdrawn
Aerospace series - Paints and varnishes - Corrosion resistant chromated two component cold curing primer - Part 001: Minimum requirements
06-21-2006
09-18-2024
Foreword
1 Scope
2 Normative references
3 Definitions
4 Classification
5 Required characteristics
6 Designation
Annex A (normative) Test methods
This standard specifies the minimum requirements for a two-component, chromated epoxy or polyurethane, corrosion resistant primer 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, procedure A and ISO 3270. The ability of the material to be used for a specific application (e.g. alternative substrate, specific drying conditions, etc.) shall be determined by supplementary tests to confirm that the requirements of this standard are met.
| Committee |
ASD-STAN
|
| DevelopmentNote |
Supersedes PREN 2435-1. (08/2006)
|
| DocumentType |
Standard
|
| PublisherName |
Comite Europeen de Normalisation
|
| Status |
Withdrawn
|
| Supersedes |
| Standards | Relationship |
| PN EN 2435-001 : 2010 | Identical |
| DIN EN 2435-001:2007-04 | Identical |
| BS EN 2435-001:2006 | Identical |
| NBN EN 2435-001 : 2006 | Identical |
| NEN EN 2435-001 : 2006 | Identical |
| NS EN 2435-001 : 1ED 2006 | Identical |
| NF EN 2435-001 : 2006 | Identical |
| I.S. EN 2435-001:2006 | Identical |
| UNE-EN 2435-001:2006 | Identical |
| BS EN 2434-004:2010 | Aerospace series. Paints and varnishes. Two component cold curing polyurethane finish High flexibility |
| PREN 4835 : DRAFT 2017 | AEROSPACE SERIES - INSTALLATION AND REMOVAL REQUIREMENTS FOR RING LOCKED FITTING AND REDUCER, 24 DEGREES CONE UP TO 35000 KPA (5080 PSI) - INCH SERIES |
| I.S. EN 2434-001:2010 | AEROSPACE SERIES - PAINTS AND VARNISHES - TWO COMPONENT COLD CURING POLYURETHANE FINISH - PART 001: BASIC REQUIREMENTS |
| I.S. EN 2434-004:2010 | AEROSPACE SERIES - PAINTS AND VARNISHES - TWO COMPONENT COLD CURING POLYURETHANE FINISH - PART 004: HIGH FLEXIBILITY |
| BS EN 4476:2011 | Aerospace series. Paints and varnishes. Cold curing intermediate coat |
| EN 2434-004:2010 | Aerospace series - Paints and varnishes - Two component cold curing polyurethane finish - Part 004: High flexibility |
| 14/30310865 DC : 0 | BS EN 4835 - AEROSPACE SERIES - INSTALLATION AND REMOVAL REQUIREMENTS FOR RING LOCKED FITTING AND REDUCER, 24 DEGREE CONE UP TO 35000 KPA (5080 PSI) - INCH SERIES |
| BS EN 2434-001:2010 | Aerospace series. Paints and varnishes. Two component cold curing polyurethane finish Basic requirements |
| EN 4476:2011 | Aerospace series - Paints and varnishes - Cold curing intermediate coat |
| EN 2434-001:2010 | Aerospace series - Paints and varnishes - Two component cold curing polyurethane finish - Part 001: Basic requirements |
| I.S. EN 4476:2011 | AEROSPACE SERIES - PAINTS AND VARNISHES - COLD CURING INTERMEDIATE COAT |
| PREN 2379 : 200P1 | AEROSPACE SERIES - FLUIDS FOR ASSESSMENT OF NON-METALLIC MATERIALS |
| PREN 3840 : 200P2 | AEROSPACE SERIES - PAINTS AND VARNISHES - TECHNICAL SPECIFICATION |
| PREN 3837 : 200P1 | AEROSPACE SERIES - PAINTS AND VARNISHES - NATURE AND METHOD FOR SURFACE PREPARATION OF TEST PIECES IN ALUMINIUM ALLOYS |
| ISO 1518:1992 | Paints and varnishes — Scratch test |
| ISO 2409:2013 | Paints and varnishes — Cross-cut test |