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Commission Implementing Regulation (EU) No 1207/2011 of 22 November 2011 laying down requirements for the performance and the interoperability of surveillance for the single European sky (Text with EEA relevance)
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This Regulation lays down requirements on the systems contributing to the provision of surveillance data, their constituents and associated procedures in order to ensure the harmonisation of performance, the interoperability and the efficiency of these systems within the European air traffic management network (EATMN) and for the purpose of civil-military coordination.
1.This Regulation shall apply to the surveillance chain constituted of:
(a)airborne surveillance systems, their constituents and associated procedures;
(b)ground-based surveillance systems, their constituents and associated procedures;
(c)surveillance data processing systems, their constituents and associated procedures;
(d)ground-to-ground communications systems used for distribution of surveillance data, their constituents and associated procedures.
2.This Regulation shall apply to all flights operating as general air traffic in accordance with instrument flight rules within the airspace provided for in Article 1(3) of Regulation (EC) No 551/2004 of the European Parliament and of the Council(1) with the exception of Articles 7(3) and 7(4) which shall apply to all flights operating as general air traffic.
3.This Regulation shall apply to air traffic service providers which provide air traffic control services based on surveillance data, and to communication, navigation or surveillance service providers which operate systems laid down in paragraph 1.
For the purpose of this Regulation, the definitions in Article 2 of Regulation (EC) No 549/2004 shall apply.
The following definitions shall also apply:
‘surveillance data’ means any data item, time stamped or not, within the surveillance system that pertains to:
aircraft 2D position;
aircraft vertical position;
aircraft attitude;
aircraft identity;
24-bit ICAO aircraft address;
aircraft intent;
aircraft velocity;
aircraft acceleration;
‘operator’ means a person, organisation or enterprise engaged in or offering to engage in an aircraft operation;
‘ADS-B’ means automatic dependent surveillance — broadcast, a surveillance technique in which aircraft automatically provide, via a data link, data derived from on-board navigation and position-fixing systems;
‘ADS-B Out’ means the provision of ADS-B surveillance data from an aircraft transmit perspective;
‘harmful interference’ means interference that prevents the achievement of the performance requirements;
‘surveillance chain’ means a system composed of the aggregation of airborne and ground-based constituents used to determine the respective surveillance data items of aircraft, including the surveillance data processing system, if deployed;
‘cooperative surveillance chain’ means a surveillance chain requiring both ground and airborne components to determine surveillance data items;
‘surveillance data processing system’ means a system that processes all surveillance inputs received to form a best estimate of the current aircraft surveillance data;
‘aircraft identification’ means a group of letters, figures or a combination thereof which is either identical to, or the coded equivalent of, the aircraft call sign to be used in air-to-ground communications, and which is used to identify the aircraft in ground-to-ground air traffic services communications;
‘State aircraft’ means any aircraft used for military, customs and police purposes;
‘transport type State aircraft’ means fixed wing State aircraft that are designed for the purpose of transporting persons and/or cargo;
‘extrapolate’ means to project, predict or extend known data based upon values within an already observed time interval;
‘coasted’ means extrapolated for a period longer than the ground surveillance systems update period;
‘time of applicability’ means the time at which the data item has been measured by the surveillance chain or the time for which it has been calculated by the surveillance chain;
‘accuracy’ means the degree of conformity of the provided value of a data item with its actual value at the time when the data item is output from the surveillance chain;
‘availability’ means the degree to which a system or component is operational and accessible when required for use;
‘integrity’ means the degree of undetected (at system level) non-conformity of the input value of the data item with its output value;
‘continuity’ means the probability that a system will perform its required function without unscheduled interruption, assuming that the system is available at the initiation of the intended operation;
‘timeliness’ means the difference between the time of output of a data item and the time of applicability of that data item.
1.Air navigation service providers shall ensure seamless operations within the airspace under their responsibility and at the boundary with adjacent airspaces by applying appropriate minimum requirements for the separation of aircraft.
2.Air navigation service providers shall ensure that systems referred to in points (b), (c) and (d) of Article 2(1) are deployed as necessary to support the minimum requirements for the separation of aircraft applied in accordance with paragraph 1.
3.Air navigation service providers shall ensure that the output of the surveillance chain referred to in Article 2(1) complies with the performance requirements set out in Annex I provided that the airborne constituent functions used are compliant with the requirements set out in Annex II.
4.If an air navigation service provider identifies an aircraft whose avionics exhibit a functional anomaly, he shall inform the operator of the flight of the deviation from the performance requirements. The operator shall investigate the matter before the next flight is initiated and any rectification necessary shall be introduced in line with normal maintenance and corrective procedures for the aircraft and its avionics.
1.Air navigation service providers shall ensure that all surveillance data transferred from their systems identified in points (b) and (c) of Article 2(1) to other navigation service providers complies with the requirements set out in Annex III.
2.Air navigation service providers when transferring surveillance data from their systems identified in points (b) and (c) of Article 2(1) to other air navigation service providers, shall establish formal arrangements with them for the exchange of the data in accordance with the requirements set out in Annex IV.
3.Air navigation service providers shall ensure that, by 2 January 2020 at the latest, the cooperative surveillance chain has the necessary capability to allow them to establish individual aircraft identification using downlinked aircraft identification made available by aircraft equipped in accordance with Annex II.
4.Operators shall ensure that:
(a)aircraft operating flights referred to in Article 2(2) with an individual certificate of airworthiness first issued on or after 8 January 2015 are equipped with secondary surveillance radar transponders having the capabilities set out in Part A of Annex II;
(b)aircraft with a maximum certified take-off mass exceeding 5 700 kg or having a maximum cruising true airspeed capability greater than 250 knots, operating flights referred to in Article 2(2), with an individual certificate of airworthiness first issued on or after 8 January 2015 are equipped with secondary surveillance radar transponders having, in addition to the capabilities set out in Part A of Annex II, the capabilities set out in Part B of that Annex;
(c)fixed wing aircraft with a maximum certified take-off mass exceeding 5 700 kg or having a maximum cruising true airspeed capability greater than 250 knots, operating flights referred to in Article 2(2), with an individual certificate of airworthiness first issued on or after 8 January 2015 are equipped with secondary surveillance radar transponders having, in addition to the capabilities set out in Part A of Annex II, the capabilities set out in Part C of that Annex.
5.Operators shall ensure that by 7 December 2017 at the latest:
(a)aircraft operating flights referred to in Article 2(2), with an individual certificate of airworthiness first issued before 8 January 2015, are equipped with secondary surveillance radar transponders having the capabilities set out in Part A of Annex II;
(b)aircraft with a maximum certified take-off mass exceeding 5 700 kg or having a maximum cruising true airspeed capability greater than 250 knots, operating flights referred to in Article 2(2), with an individual certificate of airworthiness first issued before 8 January 2015 are equipped with secondary surveillance radar transponders having, in addition to the capabilities set out in Part A of Annex II, the capabilities set out in Part B of that Annex;
(c)fixed wing aircraft with a maximum certified take-off mass exceeding 5 700 kg or having a maximum cruising true airspeed capability greater than 250 knots, operating flights referred to in Article 2(2), with an individual certificate of airworthiness first issued before 8 January 2015 are equipped with secondary surveillance radar transponders having, in addition to the capabilities set out in Part A of Annex II, the capabilities set out in Part C of that Annex.
6.Operators shall ensure that aircraft equipped in accordance with paragraphs 4 and 5 and having a maximum certified take-off mass exceeding 5 700 kg or having a maximum cruising true airspeed capability greater than 250 knots operate with antenna diversity as prescribed in paragraph 3.1.2.10.4 of Annex 10 to the Chicago Convention, Volume IV, Fourth Edition including all amendments up to No 85.
7.Member States may impose carriage requirements in accordance with point (b) of paragraph 4 and point (b) of paragraph 5 to all aircraft operating flights referred to in Article 2(2) in areas where surveillance services using the surveillance data identified in Part B of Annex II are provided by air navigation service providers.
8.Air navigation service providers shall ensure that, before putting into service the systems referred to in points (b), (c) and (d) of Article 2(1), they are implementing the most efficient deployment solutions taking into account the local operating environments, constraints and needs as well as airspace users capabilities.
1.By 5 February 2015 at the latest Member States shall ensure that a secondary surveillance radar transponder on board any aircraft flying over a Member State is not subject to excessive interrogations that are transmitted by ground-based surveillance interrogators and which either elicit replies or whilst not eliciting a reply are of sufficient power to exceed the minimum threshold level of the receiver of the secondary surveillance radar transponder.
2.For the purpose of paragraph 1, the sum of such interrogations shall not cause the secondary surveillance radar transponder to exceed the rates of reply per second, excluding any squitter transmissions, specified in paragraph 3.1.1.7.9.1 for Mode A/C replies and in paragraph 3.1.2.10.3.7.3 for Mode S replies of Annex 10 to the Chicago Convention, Volume IV, Fourth Edition.
3.By 5 February 2015 at the latest Member States shall ensure that the use of a ground based transmitter operated in a Member State does not produce harmful interference on other surveillance systems.
4.In the event of disagreement between Member States regarding the measures detailed in paragraphs 1 and 3 the Member States concerned shall bring the matter to the Commission for action.
1.Air navigation service providers shall assess the level of performance of ground based surveillance chain before putting them into service as well as regularly during the service, in accordance with the requirements set out in Annex V.
2.Operators shall ensure that a check is performed at least every two years, and, whenever an anomaly is detected on a specific aircraft, so that the data items set out in point 3 of Part A of Annex II, in point 3 of Part B of Annex II and in point 2 of Part C of Annex II, if applicable, are correctly provided at the output of secondary surveillance radar transponders installed on board their aircraft. If any of the data items are not correctly provided then the operator shall investigate the matter before the next flight is initiated and any rectification necessary shall be introduced in line with normal maintenance and corrective procedures for the aircraft and its avionics.
3.Member States shall ensure that the assignment of 24-bit ICAO aircraft addresses to aircraft equipped with a Mode S transponder complies with Chapter 9 and its appendix of Annex 10 to the Chicago Convention, Volume III, Second Edition including all amendments up to No 85.
4.Operators shall ensure that on board the aircraft they are operating, any Mode S transponder operates with a 24-bit ICAO aircraft address that corresponds to the registration that has been assigned by the State in which the aircraft is registered.
1.Member States shall ensure that, by 7 December 2017 at the latest, State aircraft operating in accordance with Article 2(2) are equipped with secondary surveillance radar transponders having the capability set out in Part A of Annex II.
2.Member States shall ensure that, by 1 January 2019 at the latest, transport-type State aircraft with a maximum certified take-off mass exceeding 5 700 kg or having a maximum cruising true airspeed capability greater than 250 knots, operating in accordance with Article 2(2) are equipped with secondary surveillance radar transponders having in addition to the capability set out in Part A of Annex II, the capability set out in Part B and Part C of that Annex.
3.Member States shall communicate to the Commission by 1 July 2016 at the latest the list of State aircraft that cannot be equipped with secondary surveillance radar transponders that comply with the requirements set out in Part A of Annex II, together with the justification for non-equipage.
Member States shall communicate to the Commission by 1 July 2018 at the latest the list of transport-type State aircraft with a maximum certified take-off mass exceeding 5 700 kg or having a maximum cruising true airspeed capability greater than 250 knots, that cannot be equipped with secondary surveillance radar transponders that comply with the requirements set out in Part B and Part C of Annex II, together with the justification for non-equipage.
The justification for non-equipage shall be one of the following:
(a)compelling technical reasons;
(b)State aircraft operating in accordance with Article 2(2) that will be out of operational service by 1 January 2020 at the latest;
(c)procurement constraints.
4.Where State aircraft cannot be equipped with secondary surveillance radar transponders as specified by paragraphs 1 or 2 for the reason set out in point (c) of paragraph 3 Member States shall include in the justification their procurement plans regarding these aircraft.
5.Air traffic service providers shall ensure that the State aircraft identified in paragraph 3 can be accommodated, provided that they can be safely handled within the capacity of the air traffic management system.
6.Member States shall publish the procedures for the handling of State aircraft which are not equipped in accordance with paragraphs 1 or 2 in national aeronautical information publications.
7.Air traffic service providers shall communicate on an annual basis to the Member State that has designated them their plans for the handling of State aircraft which are not equipped according with paragraphs 1 or 2. Those plans shall be defined by taking into account the capacity limits associated with the procedures referred to in paragraph 6.
1.Member States shall ensure that, by 5 February 2015 at the latest, a safety assessment is conducted by the parties concerned for all existing systems referred to in points (b), (c) and (d) of Article 2(1).
2.Member States shall ensure that any changes to the existing systems referred to in points (b), (c) and (d) of Article 2(1) or the introduction of new systems are preceded by a safety assessment, including hazard identification, risk assessment and mitigation, conducted by the parties concerned.
3.During the assessments identified in paragraphs 1 and 2, the requirements set out in Annex VI shall be taken into consideration as a minimum.
Before issuing an EC declaration of conformity or suitability for use provided in Article 5 of Regulation (EC) No 552/2004, manufacturers of constituents of the systems referred to in Article 2(1) of this Regulation or their authorised representatives established in the Union, shall assess the conformity or suitability for use of those constituents in compliance with the requirements set out in Annex VII.
However, certification processes complying with Regulation (EC) No 216/2008 of the European Parliament and of the Council(2), shall be considered as acceptable procedures for the conformity assessment of constituents if they include the demonstration of compliance with the applicable interoperability, performance and safety requirements of this Regulation.
1.Air navigation service providers which can demonstrate or have demonstrated that they fulfil the conditions set out in Annex VIII shall conduct a verification of the systems referred to in points (b), (c) and (d) of Article 2(1) in compliance with the requirements set out in Part A of Annex IX.
2.Air navigation service providers which cannot demonstrate that they fulfil the conditions set out in Annex VIII shall subcontract to a notified body a verification of the systems referred to in points (b), (c) and (d) of Article 2(1). This verification shall be conducted in compliance with the requirements set out in Part B of Annex IX.
3.Certification processes complying with Regulation (EC) No 216/2008 shall be considered as acceptable procedures for the verification of systems if they include the demonstration of compliance with the applicable interoperability, performance and safety requirements of this Regulation.
1.Air navigation service providers shall ensure that all personnel concerned are made duly aware of the requirements laid down in this Regulation and that they are adequately trained for their job functions.
2.Air navigation service providers shall:
(a)develop and maintain operations manuals containing the necessary instructions and information to enable all personnel concerned to apply this Regulation;
(b)ensure that the manuals referred to in point (a) are accessible and kept up to date and that their update and distribution are subject to appropriate quality and documentation configuration management;
(c)ensure that the working methods and operating procedures comply with this Regulation.
3.Operators shall take the necessary measures to ensure that the personnel operating and maintaining surveillance equipment are made duly aware of the relevant provisions of this Regulation, that they are adequately trained for their job functions, and that instructions about how to use this equipment are available in the cockpit where feasible.
4.Member States shall ensure compliance with this Regulation including the publication of the relevant information on surveillance equipment in the national aeronautical information publications.
1.For the specific case of approach areas where air traffic services are provided by military units or under military supervision and when procurement constraints prevent compliance with Article 5(3), Member States shall communicate to the Commission by 31 December 2017 at the latest, the date of compliance of the cooperative surveillance chain that shall not be later than 2 January 2025.
2.Following consultation with the Network Manager and not later than 31 December 2018, the Commission may review the exemptions communicated under paragraph 1 that could have a significant impact on the EATMN.
1.Aircraft of specific types with a first certificate of airworthiness issued before 8 January 2015 that have a maximum take off mass exceeding 5 700 kg or a maximum cruising true airspeed greater than 250 knots that do not have the complete set of parameters detailed in Part C of Annex II available on a digital bus on-board the aircraft may be exempted from complying with the requirements of point (c) of Article 5(5).
2.Aircraft of specific types with a first certificate of airworthiness issued before 1 January 1990 that have a maximum take off mass exceeding 5 700 kg or a maximum cruising true airspeed greater than 250 knots may be exempted from complying with the requirements of Article 5(6).
3.The Member States concerned shall communicate to the Commission by 1 July 2017 at the latest, detailed information justifying the need for granting exemptions to these specific aircraft types based on the criteria of paragraph 5.
4.The Commission shall examine the requests for exemption referred to in paragraph 3, and, following consultation with the parties concerned, shall adopt a decision.
5.The criteria referred to in paragraph 3 shall include the following:
(a)specific aircraft types reaching the end of their production life;
(b)specific aircraft types being produced in limited numbers;
(c)disproportionate re-engineering costs.
This Regulation shall enter into force on the 20th day following its publication in the Official Journal of the European Union.
Article 4, Article 5(1) and (2) and Article 7(1) shall apply from 13 December 2013.
This Regulation shall be binding in its entirety and directly applicable in all Member States.
Done at Brussels, 22 November 2011.
For the Commission
The President
José Manuel Barroso
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