ASD-STAN/D 5 - Non-Metallic

This document provides means of compliance with the “Direct Remote Identification” requirements set
in Regulation (EU) 2019/945 on Unmanned Aircraft Systems.
“Direct remote identification” means a system that ensures the local broadcast of information about a
UA in operation.
More specifically, this document addresses drone’s capability to be identified during the whole duration
of the flight, in real time and with no specific connectivity or ground infrastructure link, by existing
mobile devices when within the broadcasting range. Such functionality, based on an open and
documented transmission protocol (described in this document) contributes to address security threats
and to support drones’ operators’ obligations with respect to citizens’ fundamental rights to privacy
and protection of personal data. It can be used by law enforcement people, critical infrastructure
managers, and public to get an instantaneous information on the drone flying around, providing various
information such as UA serial number, UA navigation data and operational status, UAS Operator
registration number and position as defined in the Delegated Regulation (EU) 2019/945.
Since Regulation (EU) 2019/945 requires DRI information to be broadcasted using an “open and
documented protocol”, this document does not define technological measures to protect the
confidentiality and integrity of the data broadcasted.

This European Standard specifies the properties of acrylonitrile-butadiene rubber (NBR)  ), mineral oil resistant, hardness 50 IRHD, for aerospace applications.

This European Standard specifies the properties of acrylonitrile-butadiene rubber (NBR)  ), low temperature resistant, hardness 70 IRHD, for aerospace applications.

This European Standard defines the test method for the determination of the operability of a cured sealant during and after submission to a bending load at low temperatures (low-temperature flexibility).

This European Standard specifies the properties of acrylonitrile-butadiene rubber (NBR)  ), mineral oil resistant, hardness 90 IRHD, for aerospace applications.

This European Standard specifies the properties of acrylonitrile-butadiene rubber (NBR)  ), fuel and synthetic oil resistant, hardness 70 IRHD, for aerospace applications.

This European Standard specifies the properties of acrylonitrile-butadiene rubber (NBR)  ), fuel and synthetic oil resistant, hardness 80 IRHD, for aerospace applications.

This European Standard specifies the properties of acrylonitrile-butadiene rubber (NBR)  ), fuel and synthetic oil resistant, hardness 50 IRHD, for aerospace applications.

This European Standard specifies the properties of chloroprene rubber (CR)  ) heat resistant, hardness 80 IRHD, for aerospace applications.

This European Standard specifies the properties of chloroprene rubber (CR)  ) heat resistant, hardness 70 IRHD, for aerospace applications.

This European Standard specifies the properties of acrylonitrile-butadiene rubber (NBR)  ), fuel and synthetic oil resistant, hardness 70 IRHD, for aerospace applications.

This European Standard specifies the properties of acrylonitrile-butadiene rubber (NBR)  ), fuel and synthetic oil resistant, hardness 50 IRHD, for aerospace applications.

This European Standard specifies the properties of acrylonitrile-butadiene rubber (NBR)  ), fuel and synthetic oil resistant, hardness 60 IRHD, for aerospace applications.

This European Standard specifies the properties of acrylonitrile-butadiene rubber (NBR)  ), mineral oil resistant, hardness 70 IRHD, for aerospace applications.

This European Standard specifies the properties of acrylonitrile-butadiene rubber (NBR)  ), mineral oil resistant, hardness 60 IRHD, for aerospace applications.

This European Standard specifies the properties of acrylonitrile-butadiene rubber (NBR)  ), low temperature resistant, hardness 60 IRHD, for aerospace applications.

This European Standard specifies the requirements relating to anaerobic polymerisable threadlocking compounds having a torque strength of 16 Nm for aerospace applications.

This European Standard specifies the requirements relating to universally available and high light transmission, chemically tempered float glass plies, for aerospace applications.

This European Standard defines a qualitative method for the determination of the ream and surface ripple in glass transparencies for aircraft applications.

This European Standard defines the requirements for the determination of the flatness of monolithic glass transparencies for aircraft applications. The method is designed to eliminate the effect of the glass deflecting under its own weight, thus eliminating false results.

This European Standard specifies the requirements relating to anaerobic polymerisable threadlocking compounds having a torque strength of 19 Nm for aerospace applications.

This European Standard specifies the requirements relating to universally available and high light transmission, thermally tempered float glass plies, for aerospace applications.

This European Standard specifies the requirements relating to anaerobic polymerisable threadlocking compounds having a torque strength of 2 Nm for aerospace applications.

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.

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 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.

This European Standard specifies the properties of chloroprene rubber (CR)  ) heat resistant, hardness 50 IRHD, for aerospace applications.

This European Standard specifies the properties of chloroprene rubber (CR)  ) heat resistant, hardness 40 IRHD, for aerospace applications.

This European Standard specifies the properties of chloroprene rubber (CR)  ) heat resistant, hardness 60 IRHD, for aerospace applications.

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.

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.

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.

This standard defines the test equipment, apparatus and media required for determination of the smoke density according to EN 2825 and the concentration of the gas components in the smoke according to EN 2826 due to pyrolitic decomposition of solid materials and composite materials of up to 25 mm in thickness under the influence of radiant heat only or with simultaneous flame application.
This test method applies exclusively to materials whose specific standard requires this type of test. It cannot be substituted for the statutory tests required for a final specific use of the material concerned.
NOTE   The smoke gas density and the gas components in the smoke are determined according to the specific environmental and test conditions defined in this standard, in EN 2825 and EN 2826. No studies have been made up to now to determine whether the results can be transferred to differing conditions, particularly to actual fire conditions. The inhalatory toxical risk and irritancy affect cannot be assessed by merely measuring the concentration of individual gas components in the smoke.

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 products intended for use in aerospace applications.

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.

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 applications.

This European Standard defines a test method for determination of the smoke density due to pyrolitic decomposition of solid materials and composite materials of up to 25 mm in thickness under the influence of radiant heat only or with simultaneous flame application.
The test results enable a comparison of the smoke production of different materials or material configurations under the conditions specified in this standard.
NOTE 1   The smoke gas density is determined according to the specific environmental and test conditions defined in EN 2824 and this standard. No studies have been made up to now to determine whether the results can be transferred to differing conditions, particularly to actual fire conditions.
NOTE 2   The burning behaviour - and consequently the smoke density - of aerospace materials are not only influenced by the type of material but also to a large extent by the configuration, the specific surface and mass, the combination with other materials, the means of joining as well as the processing technique.

This European Standard defines a test method to determine the concentration of certain gas components due to pyrolitic decomposition of solid materials and composite materials under the influence of radiant heat only or with simultaneous flame application.
NOTE 1   The gas components in the smoke are determined according to the specific environmental and test conditions defined in EN 2824 and this standard. No studies have been made up to now to determine whether the results can be transferred to different conditions, particularly to actual fire conditions. The inhalatory toxical risk and irritancy affect cannot be assessed by merely measuring the concentration of individual gas components in the smoke.
NOTE 2   The burning behaviour and consequently the gas components in the smoke of aerospace materials are not only influenced by the type of material but also to a large extent by the configuration, the specific surface and mass, the combination with other materials, the means of joining as well as the processing technique.
NOTE 3   These influences shall be taken into account in the preparation of tests, the selection of test specimens and the interpretation of test results.

This European Standard specifies the requirements for a two component polyurethane finish to be applied over a primer for interior and exterior aerospace applications, where maximum resistance to normal operational fluids is required.
The properties specified in this European 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 2435-002. 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.

This European Standard specifies the requirements for a two component polyurethane finish to be applied over a primer mainly for exterior aerospace applications, offering high flexibility
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 prEN 2435-002. 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.

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 prEN 2435-03. 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.

This standard defines the technical requirements for the qualification, manufacture, inspection and the delivery of paints and varnishes for use in aerospace applications. It shall be applied in conjunction with the EN material specification.

This standard describes a procedure of ageing to assess the resistance of a coated panel (metallic or organic substrate) to a temperature cycle (cold, hot, hot and wet) for aerospace purposes.
This test deals with the assessment of the capability of the paint to support modification of internal stresses without any crack formation, peeling or other defects due to modification of the mechanical properties of the paint system.

This standard specifies the requirements for a two component polyurethane top coat to be applied over top coats in line with EN 2434 to provide an anti slip surface for walkway/step areas in aerospace applications.
The paint shall be formulated to meet the requirements of this standard or alternatively shall consist of material approved to and complying with the requirements the appropriate parts of EN 2434 together with a non-metallic anti slip agent.

This standard describes a method of measurement of the electrical resistance of electrically conducting surface coatings on non-conductive parts and samples for aerospace applications.
If electrical contact areas are provided, the method is also applicable on electrical conducting layers over coated with non-conducting layers.

This standard specifies the method of test for determining the infrared reflectance of paints and varnishes.
The test procedure determines the amount of energy reflected by the material in the range of wavelengths between 700 nanometres and 2 400 nanometres with respect to that of a standard reflectance material.
The procedure is applicable to products intended for use in aerospace applications.

This standard specifies the requirements for a two component polyurethane, abrasion resistant coating available in a range of colours and levels of gloss, to be applied over a primer for aerospace applications offering resistance to wear on sliding surfaces and resistance to impact from solid particles.
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 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.

This standard defines the requirements for manufacture, inspection and testing of narrow woven fabrics for aerospace applications.

This standard defines the requirements for manufacture, inspection and testing of wide woven fabrics for aerospace applications.

This standard defines the general requirements for the determination of warp bow of narrow woven fabrics by measurement testing.

This standard specifies the procedure for determination of the sliding friction behaviour of an anti slip coating.