This document defines the requirements for a two-components, high corrosion inhibiting epoxy primer.
The coating shall be suitable for use on suitably prepared metallic substrates, chromic acid anodised, or conversion coated aluminium alloys and other suitably prepared substrates.

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    • Standard
      18 pages
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This document specifies the requirements for a two-components flexible polyurethane topcoat to be applied over EN 4687 and/or EN 4688 primers mainly for exterior aerospace applications.
The primer and the finish tested to this document will be from the same manufacturer applied in accordance with (i.a.w.) their instructions/Table 1.

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    • Standard
      20 pages
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This document defines the requirements for a two-components, chromate and lead-free primer.
The coating shall be suitable for use on fibre reinforced composite materials, titanium and corrosion resistant steels and other suitably prepared corrosion resistant substrates.

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      17 pages
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This document specifies the electrolytic cadmium plating of parts and fasteners in steel of tensile strength Rm (max.)  1 450 MPa, copper, copper alloys and nickel alloys, whose temperature in service does not exceed 235 °C.

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      20 pages
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This standard specifies requirements for the durability testing of coatings most commonly used for space applications, i.e.:
-   Thin film optical coatings
-   Thermo-optical and thermal control coatings (the majority are paints, metallic deposits and coatings for stray light reduction)
-   Metallic coatings for other applications (RF, electrical, corrosion protection)
This standard covers testing for both ground and in-orbit phases of a space mission, mainly for satellite applications.
This sta...
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      43 pages
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This standard specifies requirements for the durability testing of coatings most commonly used for space applications, i.e.:
-   Thin film optical coatings
-   Thermo-optical and thermal control coatings (the majority are paints, metallic deposits and coatings for stray light reduction)
-   Metallic coatings for other applications (RF, electrical, corrosion protection)
This standard covers testing for both ground and in-orbit phases of a space mission, mainly for satellite applications.
This sta...
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This standard specifies several chemical methods of passivation for corrosion resisting steels (austenitic, ferritic, martensitic and precipitation hardenable) and of decontamination for nickel or cobalt base alloys.

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      13 pages
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This document describes the electrical contact resistance testing method applicable to conductive and non-conductive coatings applied on test specimens made of conductive materials (unless otherwise specified) for aerospace applications. An objective of this practice is to define and control many of the known variables in such a way that valid comparisons of the contact properties of materials can be made.This test may be locally destructive depending on the process tested.

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    • Standard
      9 pages
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This standard specifies several chemical methods of passivation for corrosion resisting steels (austenitic, ferritic, martensitic and precipitation hardenable) and of decontamination for nickel or cobalt base alloys.

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    • Standard
      13 pages
      English language
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This document describes the electrical contact resistance testing method applicable to conductive and non-conductive coatings applied on test specimens made of conductive materials (unless otherwise specified) for aerospace applications. An objective of this practice is to define and control many of the known variables in such a way that valid comparisons of the contact properties of materials can be made.
This test may be locally destructive depending on the process tested.

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    • Standard
      9 pages
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This standard specifies the requirements for an intermediate coat to be applied over a primer for aerospace applications and with a topcoat for aerospace applications on top. The properties specified in this document are obtained on defined aluminium alloy test pieces prepared in accordance with EN 3837 and EN ISO 3270 and painted with primer listed in Table 1. Topcoat listed in Table 1 is to be applied on intermediate coat to this document. The ability of the material to be used for a specific ...view more

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      17 pages
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This document defines the requirements for hexavalent chromium free anodizing of aluminium and
aluminium alloys for corrosion protection, bonding and painting.
Hard anodizing and plasma electrolytic anodizing (micro-arc oxidation) are not covered by this
document.
The purpose of this document is to give design, quality and manufacturing requirements. It does not give
complete in-house process instructions; these are given in the processors detailed process instructions.

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      22 pages
      English language
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This standard specifies the method of test for evaluating the tendency of paints and varnishes towards sedimentation of their pigments. The procedure describes a method where the pigmented paint is allowed to settle at a specified temperature and for a specified time. The procedure is not applicable to products which possess a pot life inferior to the specified measuring time.

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    • Standard
      5 pages
      English language
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      1 day

This document defines the requirements for hexavalent chromium free anodizing of aluminium and aluminium alloys for corrosion protection, bonding and painting.
Hard anodizing and plasma electrolytic anodizing (micro-arc oxidation) are not covered by this document.
The purpose of this document is to give design, quality and manufacturing requirements. It does not give complete in-house process instructions; these are given in the processors detailed process instructions.

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    • Standard
      22 pages
      English language
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This document specifies the requirements for an intermediate coat to be applied over a primer for aerospace applications and with a topcoat for aerospace applications on top.
The properties specified in this document are obtained on defined aluminium alloy test pieces prepared in accordance with EN 3837 and EN ISO 3270 and painted with primer listed in Table 1. Topcoat listed in Table 1 is to be applied on intermediate coat to this document. The ability of the material to be used for a specific...
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This document defines the requirements for hexavalent chromium free anodic electrodeposition of organic coatings on aluminium and aluminium alloys for corrosion protection of parts. The purpose of this standard is to give design, quality and manufacturing requirements. It doesn’t give complete in-house process instructions; these shall be given in the processor detailed process instructions.

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    • Standard
      18 pages
      English language
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      1 day

This document specifies the method of test for evaluating the tendency of paints and varnishes towards sedimentation of their pigments.
The procedure describes a method where the pigmented paint is allowed to settle at a specified temperature and for a specified time.
The procedure is not applicable to products which possess a pot life inferior to the specified measuring time.

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    • Standard
      5 pages
      English language
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This document defines the nature of and the surface preparation method for test pieces in aluminium alloys intended for testing paints and varnishes used for aerospace applications. 2 Normative

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    • Standard
      10 pages
      English language
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This document defines the requirements for hexavalent chromium free anodic electrodeposition of organic coatings on aluminium and aluminium alloys for corrosion protection of parts.
The purpose of this standard is to give design, quality and manufacturing requirements. It doesn’t give complete in-house process instructions; these shall be given in the processor detailed process instructions.

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    • Standard
      18 pages
      English language
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      1 day

This document defines the nature of and the surface preparation method for test pieces in aluminium alloys intended for testing paints and varnishes used for aerospace applications.

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    • Standard
      10 pages
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This standard specifies the method of test for determining the solar absorptance of paints and varnishes.
The test procedure determines the amount of energy reflected by the material in the range of wavelengths at which there is energy from the sun hitting the Earth’s surface, and with the aid of a standard solar spectrum it allows a calculation to determine the solar absorptance which can then be used to determine the efficiency of solar heat reflecting paints.
The procedure is applicable to ...
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      6 pages
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The purpose of the proposed Standard is to summarise the (general) corrosion protection requirements applicable to the materials, surface treatments, finishing and manufacturing processes used for space flight hardware.
It contains the minimum requirements necessary to guarantee and verify the suitability of materials, coatings systems and processes for corrosion control of space rated products.
The Standard classifies the corrosion environments and requires the issuing of a Corrosion Prevention...
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    • Standard
      34 pages
      English language
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The purpose of the proposed Standard is to summarise the (general) corrosion protection requirements applicable to the materials, surface treatments, finishing and manufacturing processes used for space flight hardware.
It contains the minimum requirements necessary to guarantee and verify the suitability of materials, coatings systems and processes for corrosion control of space rated products.
The Standard classifies the corrosion environments and requires the issuing of a Corrosion Prevention...
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      34 pages
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This European Standard defines the coating methods and characteristics of aluminium pigmented coatings to EN 4473 which may be applied to fasteners in titanium, titanium alloys, heat resisting nickel base or cobalt base alloys and corrosion resisting steels.

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    • Standard
      11 pages
      English language
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This European Standard defines the coating methods and characteristics of aluminium pigmented coatings to EN 4473 which may be applied to fasteners in titanium, titanium alloys, heat resisting nickel base or cobalt base alloys and corrosion resisting steels.

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      11 pages
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This Standard details a test in which pressure‐sensitive tapes are used to assess
the suitability of, for example, coatings, paints, films and other thin materials,
proposed for use on spacecraft and associated equipment.
Surface coatings, such as thermal control paints and corrosion protection
coatings, are affected, both on the ground and after launch, by exposure to the
environment.
It is therefore important that the adhesion of the coating to the relevant
substrate remains at an acceptable l...
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    • Standard
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    • Draft
      23 pages
      English language
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      1 day

This Standard details a test in which pressure‐sensitive tapes are used to assess
the suitability of, for example, coatings, paints, films and other thin materials,
proposed for use on spacecraft and associated equipment.
Surface coatings, such as thermal control paints and corrosion protection
coatings, are affected, both on the ground and after launch, by exposure to the
environment.
It is therefore important that the adhesion of the coating to the relevant
substrate remains at an acceptable l...
view more

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    • Standard
      23 pages
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    • Draft
      23 pages
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This standard specifies the plating of a Zinc-Nickel (12 % to 16 %) alloy on mechanical parts and fasteners in steels (UTS ≤ 1 450 MPa), stainless steels (UTS ≤ 1 450 MPa), copper alloys and aluminium alloys (not applicable for electrical components), as well as the passivation and lubricant finishing that can be associated to them. The Zinc-Nickel process is an electrolytic plating process under controlled current allowing to deposit a Zinc-Nickel layer from, most often, an alkaline electrolyte...view more

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    • Standard
      14 pages
      English language
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This European Standard specifies the plating of a Zinc-Nickel (12 % to 16 %) alloy on mechanical parts and fasteners in steels (Rm ≤ 1 450 MPa), stainless steels (Rm ≤ 1 450 MPa), copper alloys, nickel alloys and aluminium alloys (not applicable for electrical components), as well as the passivation and lubricant finishing that can be associated to them. The Zinc-Nickel process is an electrolytic plating process under controlled current allowing to deposit a Zinc-Nickel layer from, most often, a...view more

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    • Standard
      14 pages
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      1 day

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 supersonic 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 Proced...view more

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    • Standard
      9 pages
      English language
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      1 day

This European 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...view more

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    • Standard
      9 pages
      English language
    • e-Library read for
      1 day

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 Pro...
view more

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    • Standard
      9 pages
      English language
    • e-Library read for
      1 day

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 supersonic 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 P...
view more

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    • Standard
      9 pages
      English language
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      1 day

This European Standard defines the requirement for Tartaric-Sulphuric-Acid (TSA) anodizing of aluminium and wrought alloys for corrosion protection and paint pre-treatment. The purpose of this European Standard is to give design and quality requirements to manufactures.

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    • Standard
      13 pages
      English language
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      1 day

This European Standard defines the requirement for Tartaric-Sulphuric-Acid (TSA) anodizing of aluminium and wrought alloys for corrosion protection and paint pre-treatment.
The purpose of this European Standard is to give design and quality requirements to manufactures.

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    • Standard
      13 pages
      English language
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      1 day

This European Standard specifies a method for the titration and determination of the phosphoric acid content of an hydroalcoholic solution for aerospace applications.
This test method is relevant for the determination of total acidity and phosphoric acid content in a reactive thinner of a wash primer or in metal cleaners.

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    • Standard
      6 pages
      English language
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      1 day

This European Standard defines a test procedure for the determination of the leaching rate of hexavalent chromium from the dry paint film of a chromate containing primer for aerospace use. The rate can be related to requirements either to prescribe the type of primer for an intended use or for the purpose of batch quality consistency.
The procedure is applicable to products intended for use in aerospace applications.

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    • Standard
      9 pages
      English language
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      1 day

This European Standard specifies a method to assess the ability of biocide-containing coatings to prevent the germination of conidiospores of certain fungi known to be capable of proliferating in fuel systems for aerospace applications.

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    • Standard
      10 pages
      English language
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      1 day

This European Standard defines a test procedure for the determination of the leaching rate of hexavalent chromium from the dry paint film of a chromate containing primer for aerospace use.
The rate can be related to requirements either to prescribe the type of primer for an intended use or for the purpose of batch quality consistency.
The procedure is applicable to products intended for use in aerospace applications.

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    • Standard
      9 pages
      English language
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      1 day

This European Standard specifies a method to assess the ability of biocide-containing coatings to prevent the germination of conidiospores of certain fungi known to be capable of proliferating in fuel systems for aerospace applications.

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    • Standard
      10 pages
      English language
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      1 day

This European Standard specifies a method for the titration and determination of the phosphoric acid content of an hydroalcoholic solution for aerospace applications.
This test method is relevant for the determination of total acidity and phosphoric acid content in a reactive thinner of a wash primer or in metal cleaners.

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    • Standard
      6 pages
      English language
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      1 day

This standard specifies the method of test for determining the resistance of paints and varnishes to the effects of heat or cold within the limits of - 50 °C to 200 °C.
The test procedure assesses the resistance of paint coatings, varnishes or related products to changes of gloss, colour, blistering, cracking and/or detachment from the substrate as a result of exposure to elevated or sub ambient temperature.
The procedure is applicable to products intended for use in aerospace applications.

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    • Standard
      6 pages
      English language
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This European Standard defines the coating methods and characteristics of molybdenum disulphide dry film lubricants which may be applied to parts in titanium, titanium alloys, steel, corrosion resistant steel and nickel based alloys.

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    • Standard
      9 pages
      English language
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      1 day

This standard defines the method for depositing cadmium layers according to the vacuum deposition process, for use in aerospace construction.
According to this process, cadmium metal is vaporised under vacuum and deposited directly on the base material with an interlayer. The coating produced in this way is ductile and electrically conductive.
This standard is applicable whenever referenced.

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    • Standard
      12 pages
      English language
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This standard defines the general requirements for the determination of drying residues (solid content) (Method A) and residues after ignition (corrosion inhibitor content) (Method B) of primers for aerospace applications.

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    • Standard
      6 pages
      English language
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This standard defines the method for depositing cadmium layers according to the vacuum deposition process, for use in aerospace construction.
According to this process, cadmium metal is vaporised under vacuum and deposited directly on the base material with an interlayer. The coating produced in this way is ductile and electrically conductive.
This standard is applicable whenever referenced.

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    • Standard
      12 pages
      English language
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This European Standard defines the coating methods and characteristics of molybdenum disulphide dry film lubricants which may be applied to parts in titanium, titanium alloys, steel, corrosion resistant steel and nickel based alloys.

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    • Standard
      9 pages
      English language
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      1 day

This European Standard defines the general requirements for the determination of drying residues (solid content) (Method A) and residues after ignition (corrosion inhibitor content) (Method B) of primers for aerospace applications.

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    • Standard
      6 pages
      English language
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      1 day

This European Standard specifies the method of test for determining the resistance of paints and varnishes to the effects of heat or cold within the limits of - 50 °C to 200 °C.
The test procedure assesses the resistance of paint coatings, varnishes or related products to changes of gloss, colour, blistering, cracking and/or detachment from the substrate as a result of exposure to elevated or sub ambient temperature.
The procedure is applicable to products intended for use in aerospace applica...
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    • Standard
      6 pages
      English language
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This European Standard specifies the requirements for a two component polyurethane finish, in a limited range of colours, to be applied over a primer for interior aerospace applications, offering flexibility and high resistance to fluid attack. The properties specified in this European Standard are obtained on defined aluminium alloy test pieces prepared in accordance with EN 3837 and EN 23270 and painted with primer to EN 2435-003. The ability of the material to be used for a specific applicati...view more

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    • Standard
      10 pages
      English language
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      1 day