ORDER OF THE MINISTRY OF TRANSPORT OF THE RUSSIAN FEDERATION

of October 20, 2014 No. 297

About approval of the Federal aviation rules "Radio Engineering Ensuring Flights of Aircrafts and Aviation Telecommunication in Civil Aviation"

List of amending documents

According to Item 2 of article 69 of the Federal Law of March 19, 1997 No. 60-FZ "The air code of the Russian Federation" (The Russian Federation Code, 1997, No. 12, Art. 1383; 1999, No. 28, Art. 3483; 2004, No. 35, Art. 3607, No. 45, Art. 4377; 2005, No. 13, Art. 1078; 2006, No. 30, Art. 3290, Art. 3291; 2007, No. 1 (p. I), Art. 29, No. 27, Art. 3213, No. 46, Art. 5554, No. 49, Art. 6075, No. 50, Art. 6239, Art. 6244, Art. 6245; 2008, No. 29 (p. I), Art. 3418, No. 30 (p. II), Art. 3616; 2009, No. 1, Art. 17, No. 29, Art. 3616; 2010, No. 30, Art. 4014; 2011, No. 7, Art. 901, No. 15, Art. 2019, Art. 2023, Art. 2024, No. 30 (p. I), Art. 4590, No. 48, Art. 6733, No. 50, Art. 7351; 2012, No. 25, Art. 3268, No. 31, Art. 4318, No. 53 (p. I), Art. 7585; 2013, No. 23, Art. 2882, No. 27, Art. 3477; 2014, 16, of the Art. 1830, of the Art. 1836) and for the purpose of implementation of standards and recommended practice of International Civil Aviation Organization I order to No.:

1. Approve the enclosed Federal aviation rules "Radio Engineering Ensuring Flights of Aircrafts and Aviation Telecommunication in Civil Aviation".

2. Declare invalid the order of Federal aeronautical Service of November 26, 2007 No. 115 "About approval and enforcement of the Federal aviation rules "Radio Engineering Ensuring Flights of Aircrafts and Aviation Telecommunication" (registration No. 10622) is registered by the Ministry of Justice of the Russian Federation on December 6, 2007.

Approved by the Order of the Ministry of Transport of the Russian Federation of October 20, 2014 No. 297

Federal aviation rules "Radio Engineering Ensuring Flights of Aircrafts and Aviation Telecommunication in Civil Aviation"

I. General provisions

1.1. The federal aviation rules "Radio Engineering Ensuring Flights of Aircrafts and Aviation Telecommunication in Civil Aviation" (further - Rules) establish procedure for the organization of radio engineering ensuring flights of aircrafts and aviation telecommunication in civil aviation for the purpose of requirements satisfaction of users of airspace of the Russian Federation, bodies of servicing of air traffic, safety of air traffic, are developed according to Item 2 of article 69 of the Federal Law of March 19, 1997 No. 60-FZ "The air code of the Russian Federation" (The Russian Federation Code, 1997, No. 12, Art. 1383; 1999, No. 28, Art. 3483; 2004, No. 35, Art. 3607, No. 45, Art. 4377; 2005, No. 13, Art. 1078; 2006, No. 30, Art. 3290, Art. 3291; 2007, No. 1 (p. I), Art. 29, No. 27, Art. 3213, No. 46, Art. 5554, No. 49, Art. 6075, No. 50, Art. 6239, Art. 6244, Art. 6245; 2008, No. 29 (p. I), Art. 3418, No. 30 (p. II), Art. 3616; 2009, No. 1, Art. 17, No. 29, Art. 3616; 2010, No. 30, Art. 4014; 2011, No. 7, Art. 901, No. 15, Art. 2019, Art. 2023, Art. 2024, No. 30 (p. I), Art. 4590, No. 48, Art. 6733, No. 50, Art. 7351; 2012, No. 25, Art. 3268, No. 31, Art. 4318, No. 53 (p. I), Art. 7585; 2013, No. 23, Art. 2882, No. 27, Art. 3477; 2014, No. 16, the Art. 1830, the Art. 1836) (further - the Air code) and for the purpose of implementation of standards and recommended practice of International Civil Aviation Organization (ICAO).

1.2. These rules are obligatory for management and execution by all physical persons and legal entities performing and providing aeronautical servicing of users of airspace of the Russian Federation and performing operation of means of radio engineering ensuring flights of aircrafts and aviation telecommunication in civil aviation.

II. Organization of radio engineering ensuring flights of aircrafts and aviation telecommunication

2.1. The persons performing and providing aeronautical servicing of users of airspace of the Russian Federation and performing operation of means of radio engineering ensuring flights of aircrafts and aviation telecommunication in civil aviation perform complex of actions for aeronautical servicing of users of airspace and bodies of servicing of air traffic (further - bodies of Department of Internal Affairs) regarding provision of information from watch facilities, radio navigation and landing, and also providing with aviation telecommunication (further - radio engineering ensuring flights of aircrafts (RTOP)).

2.2. Treat watch facilities:

the survey radar route (further - ORL-T);

the survey radar airfield (further - ORL-A);

the secondary radar (further - VRL);

the landing radar (further - PRL);

radar station of the overview of the airfield (further - OLP radar Station);

multiposition watch system airfield (further - MPSN-A);

multiposition watch system shirokozonny (further - MPSN-Sh);

land station of contractual automatic dependent observation (further - AZN-K);

land station of broadcasting automatic dependent observation (further - AZN-V);

automatic radio direction finder (further - ARP);

video surveillance equipment.

2.3. ORL-T is intended for detection and determination of coordinates (azimuth range) of aircrafts in extra airfield zone (on airways and out of routes) with the subsequent information transfer about air situation in the centers (Items) of Department of Internal Affairs for the purposes of control and ensuring air traffic control.

The ORL-T antenna system is adjusted rather true meridian. The period of updating of information constitutes no more than ten seconds.

ORL-T is recommended to be placed so that overlapping of airways of this area by the action area of the radar at height from lower to the upper controlled airspace of echelons was provided.

2.4. ORL-A is intended for detection and determination of coordinates (azimuth range) of aircrafts around airfield with the subsequent information transfer about air situation in the centers (Items) of Department of Internal Affairs for the purposes of control and ensuring air traffic control. The period of updating of information constitutes no more than six seconds.

ORL-A is recommended to be placed so that the continuous radar overview of controlled airspace around airfield was provided.

Lack of radar information from ORL-A in 3 - 5 reviews in a row from the aircraft making maneuver of turn or being on the site with the tangential direction of speed is allowed. The ORL-A antenna system is adjusted rather magnetic meridian.

Radar information of ORL-A can be used for the purposes of control and air traffic control in extra airfield zone (on airways and out of routes) in district control centers of air traffic. In this case the coordinate information (azimuthal) intended for the district center is recalculated rather true meridian by the equipment of processing of ORL-A or the equipment of air traffic control of the district center or other special equipment.

2.5. VRL is intended for detection, determination of coordinates (azimuth range), request and acceptance of the additional information from the aircrafts equipped with defendants with the subsequent issue of information in the centers (Items) of Department of Internal Affairs.

VRL intended for ensuring flights of aircrafts on airways and out of routes shall have the period of updating of information no more than ten seconds, and in airfield zone - no more than six seconds.

2.6. PRL is intended for detection and control of flight of the aircraft on trajectory of landing approach.

PRL is located in airfield and is adjusted so that to provide the overview in the sector which begins in the point located at distance of 150 m from landing point in the direction of landing. The corner on azimuth of this sector shall constitute 5 ° rather axial line of landing strip (further - the runway), and place corner from -1 ° to +6 °.

In the presence on the same direction of landing of PRL and radio beacon-type system of tool calling of the aircraft on landing of the line of rate and glide path of these means shall match on the site from point of entry in glide path to near drive radio station with marker radio beacon or 1000 m from runway threshold.

2.7. To OLP radar Station it is intended for control and traffic control of the aircrafts, special motor transport, technical means and other objects which are on the working area of airfield (the maneuvering area and the platform, the runway, rulezhny paths and places of parking of aircrafts).

2.8. MPSN-A is intended for determination of location and traffic control of the aircrafts, special motor transport, technical means and other objects equipped with defendants, which are on landing straight line and working area of airfield (the maneuvering area and the platform, the runway, rulezhny paths and places of parking of aircrafts).

2.9. 24-bit addresses are appropriated to the land radio radiating equipment installed on airfield vehicles, obstacles or stationary devices of detection of the purposes in the mode S which is used for observation.

The procedure for assignment of the 24-bit address to the land radio radiating equipment installed on airfield vehicles, obstacles or stationary devices of detection of the purposes in the mode S is given in appendix No. 1 to these rules.

2.10. MPSN-Sh is intended for determination of location and traffic control of the aircrafts equipped with the onboard defendants working in the international range (in the A/C modes and S), in the upper and lower airspace.

2.10.1. MPSN-A and MPSN-Sh can be united in the integrated multiposition watch system.

2.11. AZN-K is intended for observation of aircrafts in case of acceptance of information from board of the aircraft having the agreement on transfer of this information to governing body of air traffic.

Information on location is created onboard the aircraft and transferred on data lines of the following types:

satellite data line;

data line in very high-frequency (further - OVCh) the range;

data line in high-frequency (further - VCh) the range;

other data lines.

The accepted information on land communication networks is transferred to governing body of air traffic under control of which at present time there is aircraft.

2.12. AZN-V is intended for observation of aircrafts in case of acceptance of information from aircraft board on its location, and also other additional information transferred on data line (further - LPD) in the broadcasting mode.

LPD of the "S" VRL mode, LPD of expanded skvitter ("1090ES") and others belong to such data lines.

2.13. ARP is intended for issue of information on bearing on the aircraft concerning radio direction finder antenna installation site on signals of onboard radio stations in the centers (Items) of Department of Internal Affairs.

2.14. The equipment of video surveillance is intended for observation by means of television, teplovizorny and other visual means in the conditions of limited visibility behind aircrafts, vehicles and other objects on the airfield maneuvering area, and also behind the aircrafts making take off and landing.

2.15. For the purpose of elimination of ambiguity (conflict) in case of consolidation and exchange of information individual system codes of the region (SAC) and system identification code (SIC) are assigned for watch facilities.

The procedure for purpose of system codes of identification of watch facilities of civil aviation of the Russian Federation in format of the ASTERIX protocol is given in appendix No. 2 to these rules.

2.16. Treat means of radio navigation and landing:

omnidirectional OVCh radio beacon azimuthal (further - RMA);

omnidirectional ultrahigh-frequency (further - UVCh) radio beacon ranging (further - RMD);

radio engineering system of near navigation (further - RSBN);

separate drive radio station (further - OPRS);

marker radio beacon (further - MRM);

the equipment of system of landing (further - SMALLPOX);

radio beacon-type system of tool calling of the aircraft on landing (further - RMS);

the global navigation satellite system (further - GNSS).

2.17. RMA of the range of OVCh is intended for measurement of azimuth of the aircraft concerning radio beacon installation site when flying the aircraft on airways and around airfield.

RMA is used by aircrafts for landing approach on devices if RMA is located on the axial line of the runway (in runway alignment) or away from the axial line, but at the same time:

if the line of way of final stage of landing approach crosses continuation of the axial line of the runway, then the point of intersection shall be at distance at least 1400 m from runway threshold, and the angle of crossing shall not exceed 30 ° for the schemes of landing approach intended only for aircrafts of category A and B, and 15 ° - for other schemes;

if the line of way of final stage of landing approach does not cross continuation of the axial line of the runway before threshold, then the corner between the line of way of final stage of landing approach and continuation of the axial line of the runway shall be less than 5 °, and at distance of 1400 m from runway threshold the line of way of final stage of landing approach shall pass not further 150 m from continuation of the axial line of the runway.

Note: RMA is considered to the runway located in alignment if the magnetic traveling corner (further - MPU) differs in the last straight line of landing approach from MPU of bedding of the runway used for landing on corner no more than 5 °.

2.18. RMD of the range of UVCh is intended for measurement of range of the aircraft concerning radio beacon installation site when flying aircrafts on airways and around airfield.

RMD used together with glissadny radio beacon is intended for determination by range aircrafts to runway threshold in points where comparison of the established flight altitude with indications of the onboard altimeter is required. In this case RMD is navigation and landing (RMD-NP).

Where the RMD antenna is not combined with RMA providing targeting in the area of way, the maximum discrepancy between the direction from control point in which information on range to runway threshold is required, on RMA and on RMD shall not exceed 23 °.

2.19. RSBN is intended for determination of azimuth and range of the aircraft on board and on the earth concerning installation site of land radio beacon.

2.20. OPRS is intended for designation of the checkpoint on trass (flight route), the drive of the aircraft equipped with the corresponding equipment to the area of airfield, accomplishment of prelanding maneuver and keeping of the direction of flight of the aircraft along runway axis.

MRM for informing crew of the aircraft on flight of the fixed point can be part of OPRS.

The OPRS installation in airfield is performed on continuation of axis of the runway on removal from runway threshold to 10 km. The OPRS installation away from continuation of axis of the runway or sideways from the runway is allowed. At the same time the corner between prelanding straight line and continuation of the axial line of the runway shall not exceed 10 °, and the point of their crossing shall be at a distance of at least 2000 m from runway threshold.

2.21. SMALLPOX consists of two drive radio stations with MRM (distant and near) and it is intended for the aircraft drive to the area of airfield, accomplishment of prelanding maneuver and landing approach.

Distant drive radio station (further - DPRS) and MRM are intended for the aircraft drive the area of airfield, accomplishment of prelanding maneuver, keeping of rate of landing.

Near drive radio station (further - BPRS) and MRM are intended for keeping of rate of landing of the aircraft.

DPRS and BPRS in case of hindrances at the main frequencies shall ensure functioning at reserve frequencies of 355 kHz and 725 kHz respectively. One of options of reserve frequencies is for this purpose used:

1 option: DPRS - 725 kHz, BPRS - 355 kHz;

2 option: DPRS - 355 kHz, BPRS - 725 kHz.

Transfer into reserve frequencies is made on specifying of body of Department of Internal Affairs.

On the directions of the runway equipped with RMS, DPRS and BPRS it is recommended to place in MPM PMC installation sites.

On the directions of the runway which are not equipped with RMS, DPRS and BPRS it is recommended to establish on the removals corresponding to placement of MPM PMC, at the same time the BPRS antenna shall be placed no more than on 15 m from the axial line of the runway aside, and the DPRS antenna no more than on 75 m from it.

When the SMALLPOX systems is installed on opposite directions of the same runway and has the identical appropriated frequencies, the measures excluding possibility of concurrent work of both systems or two OPRS at one frequency shall be taken.

2.22. RMS consists of complex of the land and onboard radio engineering equipment and is intended for ensuring obtaining onboard the aircraft and issue to crew and in system of automatic control of information on value and sign of variation from nominal trajectory of decrease, and also for determination of the moments of flight of characteristic points on trajectory of landing approach.

Are part of the RMS land complex course radio beacon (further - KRM), glissadny radio beacon (further - GRM) and MRM.

KRM represents the land radio engineering device radiating in space the radio signals containing information for control of the aircraft of rather landing rate in case of accomplishment of landing approach up to the decision making height.

The KRM antenna is established on continuation of the axial line of the runway, the side shift of the KRM antenna from continuation of the axial line of the runway is not allowed.

GRM represents the land radio engineering device radiating in space the radio signals containing information for control of the aircraft in the vertical plane concerning the established tilt angle of the line of glide path in case of accomplishment of landing approach up to the decision making height.

The GRM antenna is established from runway threshold so that the required height of reference point was provided.

The near (distant) marker radio beacon (further - BMRM, DMRM) represents the land radio engineering device transferring information to crew of the aircraft about flight of MRM established in the fixed point at certain distance from runway threshold.

BMRM is located so that in the conditions of poor visibility began to provide crew of the aircraft with information on proximity uses of visual means of landing approach.

The BMRM antenna no more than 15 m from it are recommended to place at distance 850 - 1200 m from runway threshold on continuation of the axial line of the runway.

DMRM is located so that to provide to crew of the aircraft possibility of check of flight altitude, removal from the runway and functioning of the equipment on final stage of landing approach.

The DMRM antenna no more than 75 m from it are recommended to place at distance 3800 - 7000 m from runway threshold on continuation of the axial line of the runway.

Placement of DMRM (DPRS) and BMRM (BPRS) with departure from these rules taking into account observance of requirements for restriction of high-rise obstacles in flight strip, and also introduction of the compensating measures providing the equivalent level of safety of flights with execution of the conclusion confirming ensuring equivalent level of safety of flights which affirms the senior aviation chief of airfield is allowed.

MRM work at frequency of 75 MHz with modulation of signal:

internal radio marker - 3000 Hz;

BMRM - 1300 Hz;

DMRM - 400 Hz.

Work of MRM with the frequency of modulation of signal of 3000 Hz with publication of information on this departure in documents of aeronautical information is allowed in airfields of joint basing and joint use (not international).

RMS are subdivided into systems I, II, III of categories ICAO (further - PMC-I, PMC-II, PMC-III).

PMC-I provides with information when calling the aircraft on landing from border of the action area of RMS up to the height of decision making, the corresponding 60 m over the horizontal plane passing through runway threshold.

PMC-II provides with information when calling the aircraft on landing from border of the action area of RMS up to the height of decision making corresponding at least 30 m over the horizontal plane passing through runway threshold.

PMC-III provides with information when calling the aircraft on landing from border of the action area of RMS to the surface of the runway and when taxing on the runway after landing.

The GRM equipment shall provide opportunity to establish tilt angle of glide path from 2 to 4 ° concerning horizontal.

The tilt angle of glide path is recommended to be established equal 3 °. The tilt angles of glide path of RMS exceeding 3 ° should be used only when impracticablly otherwise to meet requirements imposed to safe flight of obstacles.

Height of reference point of PMC-I, PMC-II, PMC-III over threshold of the runway shall be (15+3/-0) m. For PMC-I height of reference point of 15 3 m is allowed.

Critical zone KRM represents part of the airfield of airfield 120 m wide in both parties from the axial line the runway and length equal to distance from the KRM antenna system to threshold of the runway of this direction of landing.

The sizes of critical zone KRM in back hemisphere of antenna system are determined according to operational documentation on specific type of the equipment.

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