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AMC and GM to the rules of the air — Issue 1, Amendment 6

AMC and GM to the rules of the air — Issue 1, Amendment 6

Utgivare
Europeiska unionens byrå för luftfartssäkerhet
Antagen
2022-12-20
Utfärdat genom
ED Decision 2022/024/R
Språk
engelska
Ämnesord
Rules of the air
Källa
www.easa.europa.eu
Endast på engelskaEuropeiska unionens byrå för luftfartssäkerhet har inte publicerat någon svensk version av detta dokument. Texten nedan återges på engelska, så som den publicerats av Europeiska unionens byrå för luftfartssäkerhet.

‘AMC and GM to SERA — Issue 1, Amendment 6’

The Annex to ED Decision 2013/013/R is amended as follows: The text of the amendment is arranged to show deleted, new or amended text as shown below: (a) deleted text is struck through; (b) new or amended text is highlighted in blue; (c) an ellipsis ‘[…]’ indicates that the remaining text is unchanged.

AMC1 SERA.6005(c) Requirements for communications, SSR transponder and electronic conspicuity in U-space airspace

MEANS OF TRANSMISSION OF INFORMATION AND INFORMATION TO BE TRANSMITTED

(a) Manned aircraft should transmit information through one or more of the following means to continuously make themselves electronically conspicuous to U-space service providers: (1) A certified ADS-B OUT system compliant with ICAO Annex 10 Volume IV Chapter 5 (Mode-S Extended Squitter). (2) A certified ADS-B OUT system compliant with ICAO Annex 10 Volume III Chapter 12 (Universal Access Transceiver) 12 months after its implementation and deployment for that purpose in all Member States. (3) A system that transmits the information specified in Appendix 1 to this AMC using: (i) a short-range device (SRD) 860 frequency band, and the information is transmitted in compliance with the format as documented in technical specification ADS-L 4 SRD-860; (ii) standardised mobile telecommunication network services coordinated for aerial use in the relevant decisions of the Electronic Communication Committee (ECC) of the European Conference of Postal and Telecommunications Administrations (CEPT), and the information is transmitted in compliance with the format as documented in technical specification ADS-L 4 MOBILE. The aircraft operator using application-based service should ensure that all other applications or functions that might run in the background are switched off or made inactive to limit in-flight transmissions to only those necessary to minimise interference through unpredictable data upload. This option becomes applicable 6 months after the publication of the technical specification ADS-L 4 MOBILE. The systems used for transmission in accordance with points (3)(i) and (ii) should bear an appropriate CE marking, and be either installed on the aircraft with the installation approved by the competent authority or carried on board the aircraft as non-installed equipment. (b) The information specified in Appendix 1 to this AMC, and which is transmitted through a system referred to in points (3)(i) and (ii), shall be transmitted in a machine-readable format accessible to U-space service providers without any restrictions.

Appendix 1 to AMC1 SERA.6005(c) Requirements for communications, SSR transponder and electronic conspicuity in Uspace airspace

ADS-L MESSAGE GENERATION FUNCTION

(a) This AMC details the minimum set of parameters that should be transmitted, and a set of parameters that may be optionally transmitted. (b) All parameters should originate from a position source or from the system configuration. Each ADS-L message should include an identifier unique to the transmission source.

TRANSMITTED PARAMETERS

TABLES FOR REQUIRED PARAMETERS

TABLES FOR OPTIONAL PARAMETERS

TRANSMISSION RATE

The position and velocity/track parameters should be transmitted at a rate of at least 1 Hz. The transmission of other parameters may be less frequent than 1 Hz, but not less frequent than 0.1 Hz.

ERROR CONTROL

There should be at least a digital error detection technique at one level of the transmission (e.g. cyclic redundancy check (CRC)). No specific error-control means are prescribed.

SECURITY

The transmission should be protected to ensure security and confidentiality of the exchanged parameters.

POSITION SOURCE

The horizontal and vertical position and velocity/track parameters should primarily be based on a GNSS source.

GM1 SERA.6005(c) Requirements for communications, SSR transponder and electronic conspicuity in U-space airspace

POSITION SOURCE

It is recommended that the GNSS position source process more than one constellation and/or use SBAS augmentation if available.

USE OF THE ‘HARDWARE AND SOFTWARE DAL’ PARAMETER

The development assurance parameter is a provision to indicate the system’s hardware and software development assurance levels (DALs), if applicable. Further information on DAL determination and use may be found in aeronautical standards for certification of software and hardware items, such as ED-80 and ED-12().

INSTALLED SYSTEMS

(a) Certified ADS-B OUT systems compliant with ICAO Annex 10 that are implemented and deployed for that purpose in all Member States.

The systems may be installed in accordance with CS-ACNS (Subpart D Section 4) or CS-STAN (Standard Change CS-SC005 INSTALLATION OF AN ADS-B OUT SYSTEM COMBINED WITH A TRANSPONDER SYSTEM), or AMC 20-24. The installation of the system should be approved by the competent authority. (b) Systems using an SRD 860 frequency band or standardised mobile telecommunication network services coordinated for aerial use in Europe. The installation of a system in an aircraft, for which EASA is the competent authority for the aircraft design, should be performed in accordance with the EASA aircraft design change processes or in accordance with CS-STAN (CS-SC0051 INSTALLATION OF ‘FLARM’ EQUIPMENT, and CS-SC0057 INSTALLATION OF AN ELECTRONIC CONSPICUITY (EC) FUNCTION). (c) The installation of a system in an aircraft, for which an aviation competent authority is the authority for the aircraft design, should be performed in accordance with the aircraft design change processes defined by the relevant authority. Aviation competent authorities may make use of recognised standards (e.g. CS-STAN) for technically similar installations in aircraft specified in Annex I to Regulation (EU) 2018/1139.

DECLARATION OF COMPLIANCE

The manufacturer of a system referred to in points (a)(3)(i) and (ii) of AMC1 SERA.6005(c) may declare conformity of its system with point SERA.6005(c). The declaration should be supported by technical documentation showing compliance. Alternatively, the manufacturer may voluntarily ask for a technical evaluation of its system by a competent authority. Such declarations of conformity and technical evaluations may be used by aircraft operators to demonstrate to competent authorities compliance with point SERA.6005(c).

NON-INSTALLED EQUIPMENT

(d) The carriage of non-installed equipment on board the aircraft, for which EASA is the competent authority for the aircraft design, should comply with the applicable air operations requirements (points CAT.GEN.MPA.140, NCC.GEN.130, NCO.GEN.125, and SPO.GEN.130). The carriage of non-installed equipment on board the aircraft, for which an aviation competent authority is the authority for the aircraft design, should comply with the applicable air operations requirements defined by the relevant authorities. Aviation competent authorities may make use of the relevant EASA requirements for similar kinds of air operations with aircraft specified in Annex I to Regulation (EU) 2018/1139. (e) The equipment should be set up on board the aircraft in such a way so as to limit transmission obscuration by the airframe, human body, or other structures and at the same time maximise the visibility of the transmitting antennas, including those on the ground.

MOBILE TELECOMMUNICATION SERVICES FOR AERIAL USE

(f) National and international roaming agreements rely on standardised roamed services (SMS, voice streaming, etc.), which cannot be automatically presumed for aerial services. Only the mobile telecommunication services concluded by the standardisation bodies for aerial use

could be used by manned aircraft to make themselves electronically conspicuous to U-space service providers. (g) There are country-specific restrictions for the aerial use of certain mobile telecommunication frequencies. Therefore, the frequencies used by aerial mobile telecommunication services should be consistent with the relevant decisions of the Electronic Communication Committee (ECC) of the European Conference of Postal and Telecommunications Administrations (CEPT) as implemented by national telecommunication authorities.

MILITARY AND STATE AIRCRAFT OPERATIONS

(h) Although the amendment to Implementing Regulation (EU) No 923/2012 introduced by Implementing Regulation (EU) 2021/666 does not apply to military and State aircraft operations and training, these aircraft may fully or partially operate in the U-space airspace. Military and State organisations may reserve the right not to be electronically conspicuous to U-space service providers, taking both security and safety requirements into account. (i) At national level, coordination between authorities in charge of civil and military/State aircraft should assess the risk of electronically non-conspicuous military and State aircraft operating in U-space airspace and may specify means by which the presence and or location of such aircraft may be communicated by the relevant operational units. (j) In determining the designation of an area as U-space airspace, States should consider operations and training conducted with manned military and State aircraft in the airspace concerned and the ability or otherwise to be conspicuous, whether for technical or operational reasons.

SAFEGUARDS FOR CONTINUOUS TRANSMISSION

(k) U-space service providers may use the provisions of Article 18(h) of Implementing Regulation (EU) 2021/664 to inform the competent authority about any known irregularities in the continuous transmission of the systems that make manned aircraft electronically conspicuous to U-space service providers, particularly if such irregularities may negatively affect the provision of air traffic information services as referred to in Article 11 of that Regulation. (l) Manned aircraft that operate in U-space airspace should use the provisions of Regulation (EU) No 376/2014 for reporting any known irregularities in the continuous transmission of the systems used for making them electronically conspicuous to U-space service providers. (m) The competent authority should, in case of an urgent safety problem, determine a corrective action (including directives or recommendations) to be taken by a natural or a legal person, where this is necessary to safeguard the safety of traffic information service.

Fotnoter

  1. Annex to ED Decision 2022/024/R Page 1 of 9
  2. AMC and GM to SERA — Issue 1, Amendment 6
  3. Annex to ED Decision 2022/024/R Page 3 of 9
  4. AMC and GM to SERA — Issue 1, Amendment 6
  5. Figure 1: The scope of the ADS-L message generation function (dashed line) as specified in Appendix 1 to AMC1 to SERA.6005(c)
  6. Required/ Data type Parameter Remarks Source optional
  7. Unique identifier / Should be included in Required Configuration Aircraft address address each transmission Address type Required See the table below Configuration Time Timestamp Required Position source
  8. Aircraft category Required See the table below Configuration
  9. Emergency Pilot-in-command Emergency status Optional See the table below status inputs Latitude Required Reference WGS-84 Position source Longitude Required Reference WGS-84 Position source Position Reference WGS-84 GNSS altitude Required Height Above Ellipsoid Position source (HAE) Ground speed Required Alternatively, north- Position source Velocity/track south, east-west Ground track Required Position source velocities
  10. Annex to ED Decision 2022/024/R Page 4 of 9
  11. AMC and GM to SERA — Issue 1, Amendment 6
  12. Vertical rate Required Position source Velocity accuracy Optional See the table below Position source To facilitate Version Required Configuration interoperability Design assurance Optional See the table below Configuration Horizontal position 95 % confidence Required Position source accuracy See table below Capabilities and Vertical position 95 % confidence Required Position source status accuracy See the table below Containment radius (Rc) Navigation integrity Optional Position source See table below Probability that Rc is Source integrity level Optional exceeded Configuration See the table below
  13. Data type Values
  14. Reserved ICAO Address type Unique identifier Reserved
  15. Parameter Values
  16. No emitter category information available Light fixed-wing (<7 031 kg / 15 500 lb) Small to heavy fixed-wing (≥7 031 kg / 15 500 lb) Light rotorcraft Heavy rotorcraft Glider/sailplane Lighter-than-air Ultralight Aircraft category Hang-glider Paraglider Parachutist/skydiver/wingsuit eVTOL/UAM UAS ‘open’ category UAS ‘specific’ category UAS ‘certified’ category Model plane Reserved
  17. Parameter 95 % horizontal accuracy bound
  18. EPU ≥ 926 m (0.5 NM) EPU < 926 m (0.5 NM) EPU < 555.6 m (0.3 NM) EPU < 185.2 m (0.1 NM)
  19. Annex to ED Decision 2022/024/R Page 5 of 9
  20. AMC and GM to SERA — Issue 1, Amendment 6
  21. EPU < 92.6 m (0.05 NM) EPU < 30 m EPU < 10 m EPU < 3 m
  22. Data type 95 % geometric altitude accuracy
  23. Unknown or > 150 m ≤ 150 m Vertical position accuracy ≤ 45 m ≤ 15 m
  24. Parameter Values
  25. No emergency General emergency Lifeguard/medical emergency Minimum fuel (Energy) Emergency status No communications Unlawful interference Downed aircraft Reserved
  26. Parameter Horizontal Figure of Merit for rate (HFOMr) values
  27. Unknown or ≥ 10 m/s < 10 m/s Velocity accuracy < 3 m/s < 1 m/s
  28. Parameter Software and hardware DAL
  29. n/a D Design assurance C B
  30. Parameter Rc
  31. ≥ 20 NM < 20 NM < 8 NM < 4 NM < 2 NM Navigation integrity < 1 NM < 0.6 NM < 0.2 NM < 0.1 NM < 75 m < 25 m
  32. Annex to ED Decision 2022/024/R Page 6 of 9
  33. AMC and GM to SERA — Issue 1, Amendment 6
  34. Parameter Probability of exceeding Rc
  35. Unknown or > 1E-3 / FH ≤ 1E-3 / FH Source integrity level ≤ 1E-5 / FH ≤ 1E-7 / FH
  36. Annex to ED Decision 2022/024/R Page 7 of 9
  37. AMC and GM to SERA — Issue 1, Amendment 6
  38. Annex to ED Decision 2022/024/R Page 8 of 9
  39. AMC and GM to SERA — Issue 1, Amendment 6
  40. Annex to ED Decision 2022/024/R Page 9 of 9