The present document is applicable to deployed non-cooperative sensor as a constituent of an Advanced Surface
Movement Guidance and Control System (A-SMGCS).
The present document provides a European Standard for manufacturers, Air Navigation Service Providers and/or
Airport Operators, who have to demonstrate and declare compliance of their systems and constituents to the Essential
Requirements (ERs) of Annex VIII of Regulation (EU) 2018/1139 [i.7].
NOTE 1: The ERs in Annex VIII of Regulatio...
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The present document is applicable to deployed non-cooperative SMR sensor as a constituent of an Advanced Surface
Movement Guidance and Control System (A-SMGCS).
NOTE 1: Generic requirements for a non-cooperative sensor are defined in ETSI EN 303 213-4-1 [1].
The present document provides a European Standard for manufacturers, Air Navigation Service Providers and/or
Airport Operators, who have to demonstrate and declare compliance of their systems and constituents to the Essential
Requireme...
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The present document is applicable to Advanced Surface Movement Guidance and Control System (A-SMGCS)
Surveillance Service. This system provides enhanced surveillance functionalities, as well as a display to controllers with
accurate and unambiguous identity and position information on the entire manoeuvring and movement area of
aerodromes.
The present document provides a European Standard for manufacturers, Air Navigation Service Providers and/or
Airport Operators, who have to demonstrate ...
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REN/ERM-TGAERO-37-1

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The present document is applicable to the Advanced Surface Movement Guidance and Control System (A-SMGCS)
airport safety support service. This service is based on the A-SMGCS surveillance service (as specified in ETSI
EN 303 213-1 [3]) and provides safety net functionalities to controllers with timely, accurate and unambiguous
information and alerts covering the entire manoeuvring and movement area of aerodromes.
The present document provides a European Standard for manufacturers, Air Naviga...
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The present document is applicable to the Advanced Surface Movement Guidance and Control System (A-SMGCS)
Routing Service. This service is based on the A-SMGCS surveillance service as specified in ETSI EN 303 213-1 [3]
and generates individual routes for mobiles based on the trajectory start and end points and known constraints (e.g.
standard taxi routes, taxiway closures). In most cases these trajectory points for aircraft are the assigned runway holding
point and parking stand, or for vehi...
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The present document specifies technical characteristics and methods of measurements for the following equipment:
1) Interrogators transmitting in the 1 030 MHz band, used in Mode S multilateration equipment in an Advanced
Surface Movement Guidance and Control System (A-SMGCS).
2) Receivers, receiving in the 1 090 MHz band, used in Mode S multilateration equipment in an Advanced
Surface Movement Guidance and Control System (A-SMGCS).
Antennas for this equipment are external and passive with...
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1.1   General
Part 001 of EN 4533 examines the termination of optical fibre cables used in aerospace applications. Termination is the act of installing an optical terminus onto the end of a buffered fibre or fibre optic cable. It encompasses several sequential procedures or practices. Although termini will have specific termination procedures, many share common elements and these are discussed in this document. Termination is required to form an optical link between any two network or system comp...
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This document specifies a method to determine the effects of thermal shock on an optical fibre or cable.

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This European standard establishes uniform requirements for Packaging for the Common Functional
Modules (CFM) within an Integrated Modular Avionic (IMA) system. It comprises the module physical
properties and the Module Physical Interface (MPI) definitions together with guidelines for IMA rack
and the operational environment.
The characteristics addressed by the Packaging Standard are:
Interchangeability:
 For a given cooling method all modules conforming to the packaging standard will fu...
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The purpose of this MOAA standard is to define a set of open architecture standards,
concepts & guidelines for Advanced Avionics Architectures (A3).
The three main goals for the MOAA Standards are:
— Reduced life cycle costs,
— Improved mission performance,
— Improved operational performance.
The MOAA standards are organised as a set of documents including:
— A set of agreed standards that describe, using a top down approach, the Architecture overview to all
interfaces required to implem...
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This European Standard establishes uniform requirements for design and development of software
architecture for modular avionics systems.

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      321 pages
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This European Standard establishes uniform requirements for design and development of software
architecture for modular avionics systems.

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      321 pages
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This European standard establishes uniform requirements for Packaging for the Common Functional
Modules (CFM) within an Integrated Modular Avionic (IMA) system. It comprises the module physical
properties and the Module Physical Interface (MPI) definitions together with guidelines for IMA rack
and the operational environment.
The characteristics addressed by the Packaging Standard are:
Interchangeability:
 For a given cooling method all modules conforming to the packaging standard will fu...
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    • Standard
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The purpose of this MOAA standard is to define a set of open architecture standards,
concepts & guidelines for Advanced Avionics Architectures (A3).
The three main goals for the MOAA Standards are:
— Reduced life cycle costs,
— Improved mission performance,
— Improved operational performance.
The MOAA standards are organised as a set of documents including:
— A set of agreed standards that describe, using a top down approach, the Architecture overview to all
interfaces required to implem...
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The present document specifies technical characteristics and methods of measurements for monostatic X-band radar
sensors intended for the surveillance of airport surface movement traffic with the following characteristics:
• Operating in one or both of the following frequency ranges:
- 9 000 MHz to 9 200 MHz and 9 300 MHz to 9 500 MHz utilizing modulated or unmodulated pulses.
• Transmitter Peak Envelope Power up to 100 kW.
• The transceiver-antenna connection is using a hollow metallic rec...
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This document specifies the general characteristics, conditions for qualification, acceptance and quality assurance for a fibre optic cable with a 9/125 µm, SM fibre core, and 1,8 µm outside cable diameter and of semi loose buffer construction.

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This document specifies a method to determine the ability of an optical fibre or cable to withstand impact under specified environmental conditions.

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This document specifies the general characteristics, conditions for qualification, acceptance and quality assurance for a fibre optic cable with a 62,5/125 µm, MM fibre core, and 900 µm outside cable diameter and of semi-loose buffer construction for "inside avionics box" equipment fibre harnessing.

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This European Standard specifies two methods of determining the fluid resistance of a fibre optic interconnection device.
It shall be used together with EN 3745-100 and EN 3909.

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