EN 2435-001:2006
Withdrawn
A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.
Aerospace series - Paints and varnishes - Corrosion resistant chromated two component cold curing primer - Part 001: Minimum requirements
18-09-2024
21-06-2006
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Withdrawn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 |
SN EN 2435-001 : 2006 | Identical |
UNI EN 2435-001 : 2008 | Identical |
NS EN 2435-001 : 1ED 2006 | Identical |
NF EN 2435-001 : 2006 | Identical |
UNE-EN 2435-001:2006 | Identical |
I.S. 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 |
UNI EN 2434-004 : 2011 | AEROSPACE SERIES - PAINTS AND VARNISHES - TWO COMPONENT COLD CURING POLYURETHANE FINISH - PART 004: HIGH FLEXIBILITY |
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 |
UNI EN 2434-001 : 2011 | AEROSPACE SERIES - PAINTS AND VARNISHES - TWO COMPONENT COLD CURING POLYURETHANE FINISH - PART 001: BASIC REQUIREMENTS |
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 |
UNI EN 4476 : 2012 | 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 |
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