ORDER OF THE GOVERNMENT OF THE REPUBLIC OF KAZAKHSTAN

of January 23, 2012 No. 156

About approval of regulations of serviceability of airfields (helidromes) of civil aviation

According to the subitem 28) of article 13 of the Law of the Republic of Kazakhstan of July 15, 2010 "About use of airspace of the Republic of Kazakhstan and activities of aircraft" the Government of the Republic of Kazakhstan DECIDES:

1. Approve the enclosed regulations of serviceability of airfields (helidromes) of civil aviation.

2. This resolution becomes effective after ten calendar days from the date of the first official publication.

Approved by the Order of the Government of the Republic of Kazakhstan of January 23, 2012 No. 156

Regulations of serviceability of airfields (helidromes) of civil aviation of the Republic of Kazakhstan

Section 1. Airfields.

1. General provisions

1. This Regulations of serviceability of airfields (helidromes) of civil aviation of the Republic of Kazakhstan (further - NGEA GA of RK) are developed according to the Law of the Republic of Kazakhstan of July 15, 2010 "About use of airspace of the Republic of Kazakhstan and activities of aircraft", and also taking into account standards and recommended practice International Civil Aviation Organization (further - the ICAO standard).

2. NGEA GA of RK determine the main minimum requirements to airfields (helidromes), used for the purpose of civil aviation, including to airfields (helidromes) of joint use and joint basing.

3. Airfields (helidromes) shall be designed, be under construction and develop on the approved authorized body in the field of civil aviation (further - authorized body) to the master plans developed by the specialized organizations.

4. In each airfield (helidrome) there is approved master plan taking into account perspective of development of airfield (helidrome) approved with bodies of the state architectural construction supervision. The master plan of airfield (helidrome) is reviewed at least once in five years.

5. Approval of construction of buildings and constructions in the terminal area and the adjacent territory is made by authorized body in accordance with the established procedure based on the conclusion on projects of development and the layout of the cities (settlements) in the territory or in areas where there are airfields (helidromes). Preparation of the conclusions is made by project civil aviation organizations.

6. Upon termination of construction the builder receives from the specialized organization which is under authority of authorized body, exact coordinates and height of construction object in the WGS-84, system provided in the standardized aeronautical format for inclusion of construction object in the state register of electronic data on the area and obstacles.

7. The airfield (helidrome) can be allowed to operation by civil air vehicles only after its compliance to requirements of NGEA GA of RK is established. Temporary departures from requirements of NGEA GA of RK are allowed in compensation cases by the measures providing the equivalent level of aviation safety. The owner (operator) of airfield (helidrome) in these cases attracts the specialized organizations to preparation and approval by authorized body the conclusion confirming ensuring equivalent level of aviation safety.

8. The administration of the airports (helidromes) bears responsibility for provision and reliability of aeronautical data of airfield (helidrome) in aeronautical information service.

9. These NGEA GA of RK do not include provisions on the organization of control and air traffic control in airfields and in areas of airfields, requirements to structure of control offices of air traffic maintenance (further - Department of Internal Affairs) airfield, to application, tasks and configuration the EXPERT of the Department of Internal Affairs. Also rules of establishment of airfield schemes of flights and determination of minima of airfields for take off and landing of air vehicles and organizational requirements to airfield services do not enter.

10. Compliance of characteristics and parameters of airfield (helidrome) to requirements of these NGEA GA of RK is determined by the Technique of assessment of conformity to regulations of the validity of airfields (helidromes) to the operation of civil air vehicles approved by the Government of the Republic of Kazakhstan.

11. In these NGEA GA of RK the following main terms and determinations are used:

1) automatic direction finder - the equipment which provides automatic measurement and display on indicators of control offices of Department of Internal Affairs of bearing (azimuth) of the air vehicles radiating radio signals on channels of air telecommunication of OVCh of the range for flight servicing of air vehicles in the terminal area (helidrome);

2) the intermediate place of expectation - the certain place intended for mission control where the driving air vehicles and vehicles stop and are expected before receipt of the subsequent permission to movement continuation, from the relevant control office;

3) threshold value of the luminance contrast for day conditions of tool measurements (background brightness more than 10 cd/m 2), are accepted by equal 0,05;

4) fly-by-wire - the flight which is carried out in conditions when the attitude of the air vehicle and its location are determined by crew fully or partially by flight and navigation instruments;

5) atmospheric pressure - force with which the atmosphere on the Earth's surface presses. On sea-level atmospheric pressure is on average close 1013, 25 hPa (Mbar) that is equivalent to pressure of column of mercury 760 mm high;

6) relative air humidity - the relation of the actual absolute humidity to absolute humidity for saturation condition at the same temperature. It is expressed as a percentage;

7) airfield - certain site terrestrial or surface of the water (including buildings, constructions and the equipment), intended fully or partially for arrival, departure and movement on this surface of air vehicles;

8) the terminal area (helidrome) - airspace over airfield (helidrome) and the area adjoining to it in the established borders the horizontal and vertical planes. The specified borders of airfield (helidrome) are established by body of Department of Internal Affairs according to the technique approved by authorized bodies in spheres civil and (or) state aviation;

9) aerodrome environs - the site of the land surface with radius of 46 kilometers from checkpoint of airfield;

Refusal of electric utility service of object of airfield - having rummaged 10) in electric utility service on board of uninterruptible power supply, exceeding the most allowed time;

11) airfield fire - any fire, excepting fires established on the air vehicle which is specially held for use as aeronautical means;

12) atmospheric pressure in airfield - value of atmospheric pressure in millimeters of mercury (mm Hg), in millibars (Mbar) or hectopascals (hPa) at the level of threshold runway strips (further - the runway);

13) aerodrome movement area - specially prepared part of airfield intended for take-off, landing and taxing of air vehicles consisting of the maneuvering area and the platform (platforms);

14) system of the light-signal equipment of airfields - set of the light-signal devices placed in airfield according to certain scheme, the electrical equipment and remote-control equipment intended for ensuring take-off, landing approach, landing and taxing of air vehicles;

15) airfield movement - all movement on airfield maneuvering areas, and also flights of all air vehicles in the terminal area. The air vehicle is considered carrying out flights in the terminal area: when it enters aerodrome traffic circuit, leaves it or is in its limits;

16) the aerodrome additional radio marker beacon - the equipment which provides marking of separate obstacles or other characteristic points in approach zone of airfield;

17) airfield coverings - the designs perceiving loadings and impacts from air vehicles, operational and natural factors which include the top and lower coat of airfield covering;

18) top coat of airfield covering (referred to as "covering" - directly perceiving loadings from wheels of air vehicles, impact of natural factors (variable temperature moisture conditions, repeated freezing and defrosting, influence of solar radiation, wind erosion), thermal and mechanical impacts of air-gas streams of the aircraft engines and mechanisms intended for aerodrome operation and also impact of deicing chemical means;

19) the lower coat of airfield covering (which is referred to as the artificial basis), providing transfer of loads of the soil basis together with covering which in addition to the bearing function can carry out also draining, antimuding, thermoisolating, protivopuchinny, waterproofing and other functions;

20) the generalized characteristic of flatness of airfield covering (R) - the number expressing impact of roughnesses of airfield covering on aircraft design in case of its movement on this covering;

21) checkpoint of airfield (further - KTA) - the point determining the geographic location of airfield;

22) aerodrome elevation - the absolute altitude of vertex of landing strip (strips);

23) the located take-off distance (further - RDV) airfield - the amount of the located take-off run (further - RDR) and lengths of clear area if it is provided;

24) the located accelerate stop distance (further - RDPV) airfield - the amount of the located take-off run (LTOR) and length of end stopway if it is provided;

25) the located take-off run (LTOR) of airfield - the runway length which appears located and suitable for running start of the airplane making take-off;

26) landing distance available (further - RPD) airfield - the runway length which appears located and suitable for airplane run after landing;

27) the Department of Internal Affairs control office - the workplace of the dispatcher of Department of Internal Affairs equipped with the necessary equipment for air traffic control;

28) aircraft observation - assessment of one or several meteorological elements made onboard the air vehicle which is in flight;

29) classification number of the air vehicle (further - ACN) - the number expressing relative impact of the air vehicle on artificial covering for the established category of standard durability of the basis;

30) omnidirectional OVCh azimuthal radio beacon (VOR) - the equipment which works in the OVCh-range and radiates the signals allowing to determine onboard AF azimuth of the air vehicle concerning radio beacon installation site;

31) primary measuring transducer of meteosize (further - the sensor) - the measuring transducer of meteosize costing to the first in metering circuit. The measuring transducer of meteosize - the gage of meteoparameters intended for development of signal, measuring information in the form convenient for transfer, further transformation, processing and (or) storage, but which is not giving in to direct perception by the meteoobserver;

32) main runway - The runway in airfield located, as a rule, in prevailing wind direction and having the extreme length;

33) signs - the devices established over earth level for display to their panels of information in the form of texts, symbols, letters or digits or their combinations, necessary for the organization of land movement in airfield of air vehicles and/or vehicles which depending on circumstances can be as with permanent information the transferring only one message and with the variable information providing possibility of transfer of several in advance determined messages or, if necessary, the termination of transfer of any information;

34) the helidrome raised over surface - site on the design towering above the ground intended for arrival and departure of helicopters;

35) surface level heliport - the helidrome located on terrestrial or surface of the water;

36) the taxiway (T) - the part of airfield of airfield which is specially prepared for taxing of air vehicles;

37) height of the lower bound of clouds (further - VNGO) - distance down between land surface (water) and the lower bound of the lowest cloud cover;

38) side band of safety (further - BPB) - the site adjacent to edge of artificial covering and prepared so that to provide transition from artificial covering to abutting surface;

39) airfield of joint basing - the airfield intended for flight servicing and permanent placement of the air vehicles which are under authority of different departments;

40) visibility vertical - the maximum distance from the Earth's surface to the level from which vertically objects on earth's surface are visible down;

41) water heliport - the helidrome located on water and held for use specially equipped helicopters which are carrying out regular flights about waters or the interrupted take-off with movement on water;

42) glide path - the flight profile established for decrease in air vehicles on final approach;

43) localizer heading line curvature - heading line shift concerning its midposition;

44) the uglomestny characteristic of GRM - dependence of size of difference of depth of modulation in points of the action area of radio beacon from angular provision of these points concerning glide path;

45) size "D" - the largest size of the size of the helicopter with rotating bearing and Vpptami's helmsmen. This size is measured, as a rule, from limiting and front point bearing rotating VPPTA, to limiting-back point of the helmsman VPPTA;

46) the circle "D" - the imagined circle provided that the site is not round which diameter is equal to the size "D" of the biggest helicopter which is operated on this helipad;

47) aim circle is the point for exact landing located so that the chair of the pilot was located directly over it in case of the guaranteed lack of obstacles in either direction in case of rotation bearing and the helmsman VPPTA;

48) the DME/N system transponder - the equipment providing acceptance and relaying of onboard demand signals by which propagation time onboard AF the distance to the transponder is determined;

49) final stage of go-around - stage of go-around at which climb to the minimum safety of flight height established according to the scheme for repeated landing approach or for exit from the terminal area is performed;

50) clear area (further - SZ) - the rectangular site which is under control of services of the airport terrestrial or surface of the water, adjoining the end of the located take-off run, chosen or prepared as the site suitable for initial climb by the air vehicle to set value;

51) the landing strip which is not equipped - the runway intended for the air vehicles which are carrying out contact approach;

52) the landing strip equipped - one of the following types of the runway intended for the air vehicles which are carrying out instrument landing approach:

Runway of instrument landing approach - The runway equipped with visual means and any type not of visual means providing, at least, guidance of the air vehicle in approach direction;

Runway of precision approach of the I category - The runway equipped with the radio beacon system and visual means intended for landing approach up to the height of decision making at least 60 m and or in case of visibility at least 800 m or in case of visible range on the runway at least 550 m;

Runway of precision approach of the II category - The runway equipped with the radio beacon system and visual means intended for landing approach up to the height of decision making less than 60 m, but at least 30 m and in case of visible range on the runway at least 300 m;

Runway of precision approach of III category - The runway equipped with the radio beacon system operating to and along all surface of the runway and intended:

IIIA - for landing approach and landing with decision making height less than 30 m or without altitude limitation of decision making and in case of visible range on the runway at least 175 m;

IIIB - for landing approach and landing with decision making height less than 15 m or without altitude limitation of decision making and in case of visible range on the runway less than 175 m, but at least 50 m;

IIIC - for landing approach and landing without altitude limitations of decision making and visible range to the runway;

53) airfield radio engineering system of short-range navigation - the equipment which provides issue of these current values of azimuth and slant range aboard the air vehicle concerning installation of land radio beacon;

54) artificial covering - top coat of the airfield clothes which are directly perceiving loadings and impacts from air vehicles, operational and natural factors;

55) separate locator beacon - the equipment which provides the drive of the air vehicle on airfield (helidrome), accomplishment of intermediate approach and landing approach;

56) wind speed - the motion speed of air of rather earth's surface: In meteorological data when ensuring take off and landing average and maximum wind speeds are given;

57) the average speed of wind - average values of the measured instantaneous velocity of wind in 2 and 10 min.;

58) the maximum speed of wind (rushes) - the greatest value of instantaneous velocity of wind in the expired 10 min. or 2 min.

59) linear fire - three or more fires placed with small intervals on the cross line which at distance seem short light strip;

60) landing point - design point of crossing of nominal glide path with the runway;

the "landing point" determined above is point of reference, but not obligatory tangency point of surface of the runway the air vehicle.

61) the local control adjusting station (GBAS) - the equipment of land functional amendment to the global navigation satellite system;

62) roadside - the site adjacent to edge of artificial covering of elements of airfield (the runway, taxiway (further - RD), etc.) and prepared in such a way that to provide transition from artificial covering to abutting soil surface;

63) obstacle - all motionless (temporary or permanent) and mobile objects or their parts which are placed in the zone intended for movement of air vehicles on surface. Objects or their parts which tower over the conditional surface intended for safety control of air vehicles in flight or are out of such established surfaces and by results of assessment constitute danger to air navigation;

64) zone, free from obstacles - airspace over inner surface of landing approach, inner transitional surfaces and the surface of balked landing and part of the flying strip limited to these surfaces which no motionless obstacles, except the fragile objects necessary for the air navigation purposes support;

65) the sector (Union of Right Forces), free from obstacles, - the sector with a radius of 210 °C, providing free takeoff flight path for each type of the helicopter operated on the helipad in which the arrangement of obstacles higher than the level of the helipad is forbidden. Horizontal extent of the sector from the helipad for helicopters of class 1 and 2 (on flight technical characteristics) depends on characteristics of the helicopter with one non-running engine;

66) board of uninterruptible power supply - the distribution device providing in case of refusal working source of electrical power automatic connection of consumers of electricity to reserve source;

67) flashing light with condenser discharge - the lamp making light exposures of high intensity and extremely short duration in case of transmission of flash-over of high tension through the gas concluded in tube;

68) visual flight - the flight which is carried out in conditions when the attitude of the air vehicle and its location are determined by crew visually by the natural horizon and terrestrial reference points;

69) visibility - visibility for the aviation purposes represents the greatest of the following sizes:

the greatest distance at which it is possible to differentiate and identify the black object of the acceptable sizes located near the earth in case of its observation on light background;

the greatest distance at which it is possible to differentiate and identify fires luminous intensity about 1000 candelas (cd) on dark background;

70) sensitive zone KRM (GRM) - the space located behind critical zone KRM (GRM) in which control of statement on the parking and (or) by movement of vehicles, including air vehicles, for prevention of emergence of unacceptable hindrances to signal of ILS is exercised;

71) nominal provision of heading line - provision of center line of rate in case of which it matches with center line of the runway;

72) critical zone of course, glide-path radio beacons (further - KRM GRM) - space around localizer (glide-path) radio beacon in which the parking or movement of vehicles, including air vehicles, can cause unacceptable changes of parameters of radio beacon;

73) the azimuthal characteristic of localizer (further - KRM) - dependence of size of difference of depth of modulations (KPM ILS). (ILS - the ground equipment of blind landing system of meter wave range working by the principle of ILS) in points of the action area of radio beacon from angular provision of these points concerning heading line;

74) difficult meteoconditions - visibility of 2000 m and less and (or) height of the lower bound of clouds of 200 m and below in case of their total quantity more than two octants;

75) system of fires of small intensity - system of airfield fires in which landing lights less than 10 000 cd have luminous intensity;

76) system of fires of high intensity - system of airfield fires in which landing lights at least 10 000 cd have luminous intensity;

77) the safety area - certain zone of helidrome around zone of final approach and take-off (further - FATO), free from obstacles, except the obstacles necessary for the air navigation purposes, and FATO intended for reduction of danger of damage of helicopters in case of inadvertent exit out of limits;

78) zone of safe landing - zone limited by the line and fires of perimeter;

79) the touchdown zone - the site of the runway behind its threshold intended for the first contact of the runway with the landing airplanes;

80) radio engineering landing system the landing system equipment (further - OSP) - the equipment which provides the drive of the air vehicle on airfield, accomplishment of intermediate approach and landing approach;

81) final approach - stage of instrument landing approach at which exit in alignment of the runway and decrease in the air vehicle for the purpose of landing is made;

82) the landing radar - the equipment which provides terrestrial monitoring behind keeping of heading line and glide path air vehicles on base leg and management of their advisory approach of dispatchers;

83) radio beacon landing system on devices (PMC or ILS) - the ground equipment of landing system of meter wave range working by the principle of ILS (ICAO standard);

84) the main taxiway - the taxiway which is located, as a rule, along the runway and providing taxing of air vehicles from one end of the runway to another;

85) the maneuvering area - part of airfield, excepting platforms, intended for take-off, landing and taxing of air vehicles;

86) marker - the object established over earth level for designation of obstacle, border, the direction, zone;

87) alternate aerodrome on route - airfield in which the air vehicle will be able to make landing if in flight time along route it appeared in emergency or emergency environment;

88) arrival airfield - the airfield specified in flight plan and in task for flight as airfield of the planned landing;

89) alternate aerodrome of destination - airfield where the air vehicle if it is impossible or inexpedient to make aerodrome landing of the planned landing can follow. The airfield from which the departure of the air vehicle is made can also be alternate aerodrome on route or alternate aerodrome of destination for this air vehicle;

90) meteorological range of visibility (Ministry of Internal Affairs) - the maximum distance at which the brightness contrast of absolutely black surface against the background of the saturated (maximum) brightness of mist or fog reaches threshold (minimum) value;

91) meteorological data - the meteorological report, the forecast and any other message concerning the actual or expected meteorological conditions;

92) representativeness of meteorological observations - typicalness (pokazatelnost) of the meteorological data for condition of the atmosphere determined (measured) in airfield;

93) meteorological sizes (meteosizes) - the general name of number of characteristics of condition of air and some atmospheric processes. Treat them: atmospheric pressure, temperature and air humidity, speed and wind direction, meteorological range of visibility, overcast (quantity, form and height of the lower bound), quantity and type of rainfall, fog, thunder-storms, blizzards and so forth;

94) the roadside strengthened - paved roadside, intended for prevention of hit of foreign objects in engines of air vehicles and jet erosion of soil surface;

95) means of objective control - the equipment which provides automatic registration of negotiations on channels of air telecommunication, and also on channels of interaction of dispatchers of Department of Internal Affairs in real time during all duration of flights, including registration of meteoinformation;

96) fire - the light device from the set svetoraspredeleniye curve;

97) subsystem of fires - group of fires of system of the light-signal equipment of one functional purpose;

98) fire refusal - decrease for any reason of average luminous intensity in ordered angles of dispersion more than for 50% in comparison with the normalized luminous intensity of new fire;

99) the platform - the part of airfield of airfield prepared and intended for placement of air vehicles for the purpose of landing and disembarkation of passengers, loading and unloading of baggage, mail and loads and also for accomplishment of other types of servicing;

100) the action area of radio beacon - area of airspace in which the radio beacon ensures normal functioning of the corresponding onboard receiver;

101) the end safety area (further - KZB) - the zone symmetrized on both sides from continuation of center line of the runway and adjoining the end of flying strip, intended first of all for reduction of risk of damage in case of landing with falling short to the runway or in case of runway overrun;

102) end stopway - specially prepared rectangular site at the end of the located take-off run intended for stop of the air vehicle in case of the interrupted take-off;

103) fragile object - the object of small weight which is structurally intended to collapse, be deformed or be bent in case of shock impact to constitute the minimum danger to the air vehicle;

104) marking sign (marking) - symbol or group of the symbols located on surface of airfield for transfer of aeronautical information;

105) mountain airfield - the airfield located on the area with the crossed relief and relative excesses of 500 m and more in radius of 25 km from checkpoint of airfield and also the airfield located at the height of 1000 m and more above sea level;

106) effective intensity - the effective intensity of flashing light equal to intensity of fire of permanent radiation of the same color to which the same visible range is provided under identical conditions of observation.

107) the soil bases - the planned and condensed local and imported soil intended for perception of the loadings distributed through design of airfield covering;

108) classification number of covering (PCN) - the number expressing bearing capacity of artificial covering for operation without restrictions;

109) stall (further - MS) - the prepared area in airfield intended for placement of the air vehicle for the purpose of its servicing;

110) helidrome - airfield or certain surface segment on construction, intended fully or partially for arrival, to departures of movement of helicopters on this surface;

111) critical zone for helidromes - zone, adjacent to the helicopter, within which the fire needs to be localized for the purpose of temporary preserving integrity of the fuselage and providing zone for evacuation of persons which are onboard;

112) the located takeoff distance (TODAH) of helidrome - length of zone of final approach and take-off plus length of helicopter strip, free from obstacles (if it is provided), which appears located and suitable for take-off completion by helicopters;

113) the located accelerate stop distance (RTODAH) of helidrome - length of zone of final approach and take-off which appears located and suitable for completion of the interrupted take-off by helicopters with class 1 flight technical characteristics;

114) landing distance available (LDAH) of helidrome - length of zone of final approach and take-off plus any additional zone which appears located and suitable for completion by helicopters of maneuver of landing from the established height.

115) helideck - the site located on floating or motionless sea design held for use by helicopters;

116) land RD for helicopters - land RD, held for use only by helicopters;

117) the stall (S) of the helicopter - aircraft parking place which is intended for the parking of the helicopter and if it is provided accomplishment of air taxiing, for landing and lead of the helicopter;

118) temporary airfield - the airfield intended for flight servicing of air vehicles during certain period of year and which does not have fixed constructions and the equipment, but being subject to accounting and registration in accordance with the established procedure;

119) the place of expectation at the runway - the certain place intended for protection of the runway, the surfaces of restriction of obstacles, critical zones RMS of landing in which the driving air vehicles and vehicles stop and are expected if there is no other specifying from the relevant control office;

120) broadening of the runway - part of the landing strip intended for providing turn of air vehicles;

121) visible range on the runway (the reduced abbreviation in English of RVR) - distance within which the aircraft pilot, being on center line of landing strip, can see marking signs on the surfaces of landing strip or fires limiting landing strip or the center line designating it;

122) pressure specified to runway threshold level - the atmospheric pressure measured in installation site of primary measuring transducer and specified to runway threshold level;

123) runway threshold - start of the segment of the runway of airfield which can be used for landing of air vehicles;

124) fires of protection of the runway - the light-signal system intended for the warning of pilots or transport drivers of possibility of departure on the operating runway;

125) the displaced runway threshold - the landing strip threshold which is not matching with its beginning;

126) airfield - part of airfield on which one or several flying strips, taxiways, platforms and platforms of special purpose are located;

127) flying strip - the part of airfield of airfield including landing strip and end stopways if they are provided, intended for ensuring take off and landing of air vehicles, reduction of risk of damage of the air vehicles which are rolled out of runway limits, and safety of the air vehicles which are flying by over it in takeoff time and landings;

128) alternate aerodrome in case of take-off - the airfield in which the air vehicle (further - AF) can make landing if in it there is need soon after take-off and is not possible to use departure airfield;

129) the landing strip (LS) - the main part of flying strip of airfield intended for providing takeoff run and run after landing of the air vehicle;

130) takeoff area and landings - airspace from the level of airfield up to the height of the second echelon inclusive in the borders providing maneuvering of the air vehicle in case of take-off and landing approach;

131) balked landing - landing which accomplishment stops below the minimum safe height of flight of obstacles;

132) fire of permanent radiation - fire having permanent emission power in case of observation from motionless point;

133) the sector of limited obstacles (further - SOP) - sector 150 ° in which obstacles can be located provided that height of these obstacles is limited;

134) decision making height - the established relative height at which overshoot maneuvre shall be begun. In cases if before achievement of this height by the aircraft commander the necessary visual contact with reference points for continuation of landing approach was not come or if provision of the air vehicle in space or parameters of its movement do not ensure safety of landing;

135) category of reliability of electric utility service - the characteristic of utility power system determining the number of independent power sources and the requirement to their switchings;

136) the international airfield - airfield from which flights of air vehicles to the states which are not agreement parties about civil aviation and about use of airspace are performed;

137) point of "A" ILS - the point on glide path located over continuation of center line of the runway in approach direction at distance of 7500 m from runway threshold;

138) point of "B" ILS - the point on glide path located over continuation of center line of the runway in approach direction at distance of 1050 m from runway threshold;

139) point of "C" ILS - point through which there passes continuation of the decreasing rectilinear part of nominal glide path at the height of 30 m over the horizontal plane passing through runway threshold;

140) point of "D" ILS - the point located at the height of 4 m over runway center line and at distance of 900 m from runway threshold in the direction of the localizer beacon;

141) point of "E" ILS - the point located at the height of 4 m over runway center line and at distance of 600 m from the end of the runway in the direction of runway threshold;

142) obstruction light of small intensity of type A - fire with permanent radiation of red color and the maximum intensity at least 10 cd;

143) obstruction light of small intensity of type B - fire with permanent radiation of red color and the maximum intensity at least 32 cd;

144) obstruction light of small intensity of type C - flashing light of yellow/blue color and the maximum intensity from 40 cd to 400 cd;

145) obstruction light of small intensity like D - flashing light with radiation of yellow color and effective intensity from 200 cd to 400 cd;

146) obstruction light of average intensity of type A - flashing light with radiation of white color and effective intensity of 20000/2000 cd;

147) obstruction light of small intensity of type B - flashing light with radiation of red color and effective intensity of 2000 cd;

148) obstruction light of small intensity of type C - fire with permanent radiation of red color and effective intensity of 2000 cd;

149) obstruction light of high intensity of type A - flashing light with radiation of white color and effective intensity of 200000/20000/2000 cd;

150) obstruction light of type B - flashing light with radiation of white color and effective intensity of 100000/20000/2000 cd;

151) the range-metering equipment DME (DME/N) - the equipment providing acceptance of onboard demand signals and radiation of signals of the answer, by which propagation time onboard AF slant range to checkpoint is determined (zero - range indication), radio beacon installation sites;

152) glide path of ILS (or radio beacon landing system (further - RMS) - locus in the vertical plane passing through center line of the runway in which the difference of depth of modulations is equal to zero and which constitute the smallest corner with horizontal plane;

153) glide slope angle of ILS - corner between straight line which represents average glide path of ILS and horizontal plane;

154) the semi-sector (sector) of glide path of ILS - the sector in the vertical plane containing glide path and limited by the loci next to glide path in which the difference of depth of modulations is equal to 0,0875 (0,175);

155) to floor the sector (sector) of rate of ILS - the sector in horizontal plane containing heading line and limited by the loci next to heading line in which for KPM ILS the difference of depth of modulations is equal to 0,0775 (0,155);

156) reference point of ILS (or RMS) (the T point) - the point at certain height located over crossing of runway center line and threshold of the runway through which there passes continuation of the decreasing straight section of glide path of ILS;

157) NOTAM - the notice distributed by means of telecommunication and containing information on enforcement, condition or change of any aeronautical equipment, servicing and rules or information on danger, the timely prevention of which is important for the personnel connected with accomplishment of flights;

158) radio beacon landing system of the I category (PMC-I or ILS-I) - landing system which provides data for control of the air vehicle from action area border to point in which the heading line crosses glide path at the height of 60 m or less over the horizontal plane which is at the level of runway threshold;

159) radio beacon landing system of the II category (PMC-II or ILS-II) - landing system which provides data for control of the air vehicle from action area border to point in which the heading line crosses glide path at the height of 15 m or less over the horizontal plane which is at the level of runway threshold;

160) radio beacon landing system of III category (PMC-III or ILS-III) - landing system which provides data for control of the air vehicle from action area border to the surface of the runway and along it.

2. Data of airfield and physical characteristics of airfields

Classification of airfields and paved landing strips

12. For airfield the class and class is determined by each paved landing strip (further - IVPP). The class of airfield is determined:

1) in the airfields having one runway - class IVPP;

2) in the airfields having two or more artificial landing strips - class IVPP, having the extreme length.

For the airfields providing the international flights, besides, the specification symbol shall be determined.

13. Class IVPP is determined by runway length in standard conditions on the table 1 of appendix 1.

The specification symbol of the airfields providing the international flights is determined by the table 2 of appendix 1.

Geometrical sizes of elements of airfield

14. In airfield for each direction of take off and landing the following takeoff and landing distances shall be established:

1) located take-off run (LTOR);

2) located take-off distance (LTOD);

3) located accelerate stop distance (LASD);

4) landing distance available (LDA).

If on the runway take-off from RD which do not adjoin runway end faces is provided, then the corresponding takeoff distances shall be established.

The procedure for determination of the located distances is given in appendix 2.

15. The flying strip (further - LP) including the runway both equipped, and not equipped, shall stretch behind each end of the runway or behind end stopway (further - KPT) if it is provided, for distance at least 60 m for the runway of classes A, B, B, G, D and 30 m for the runway of class E.

16. The flying strip including the equipped runway shall stretch in cross direction on both sides from runway center line and its continuation (throughout LP) for distance at least:

1) 150 m for the runway of classes A, B, B, G;

2) 75 m for the runway of classes D and E.

17. The flying strip including not equipped runway, except for reserve unpoved runway shall stretch in cross direction on both sides from runway center line (throughout LP) for distance at least:

1) 80 m for the runway of classes A and B;

2) 70 m for the runway of class B;

3) 65 m for the runway of class G;

4) 55 m for the runway of class D;

5) 40 m for the runway of class E.

18. The part of LP (which includes the equipped or not equipped runway) located on both sides from runway center line (throughout LP) shall be planned and prepared so that to minimize risk of damage of the air vehicle in case of landing with falling short or runway overrun.

The planned part of LP shall stretch from runway center line for distance at least:

1) 80 m for the runway of classes A and B;

2) 70 m for the runway of class B;

3) 65 m for the runway of class G;

4) 55 m for the runway of class D;

5) 40 m for the runway of class E.

19. The soil surface of the planned part of LP in places of interface to artificial coverings of elements of airfield (IVPP, side bands of safety, taxiways, KPT, etc.) shall be located flush with them.

20. The part of LP located before threshold of IVPP shall be strengthened on width at least width of IVPP for the purpose of prevention of erosion from streams of AF gases and protection of the landing air vehicles against blow about end face of IVPP on distance is at least:

1) 60 m for IVPP of class A;

2) 50 m for IVPP of classes B and B;

3) 30 m for IVPP of classes G and D.

For the existing runways strengthening which width decreases to 2/3 width of the runway at the end of strengthening is allowed.

21. Within the planned part of LP there shall not be objects, except for the objects having easy and fragile design which on the functional purpose shall be on this part of LP (for example, visual means, monitoring antenna of localizer, flashers of the landing radar (further - PRL), etc.). On the planned part of LP there shall not be mobile objects (for example, snowplows) in usage time of the runway for take-off or landing.

Instructive material concerning availability of temporary obstacles in flying strip is given in appendix 3.

22. Ranging from border of the planned part to border of LP shall not be, objects, except those which functional purpose requires their placement near the runway and does not allow placement in other place (GRM, PRL, starting control office, weather measuring instruments).

In these limits new shall not be placed or increase in sizes the existing objects unless placement new or increase in sizes of the existing object:

1) it is necessary for ensuring takes off and landing of air vehicles or;

2) will not make adverse effect on aviation safety of AF.

23. Width of the runway shall be on all length of constant at least:

1) 60 m for the runway of class A;

2) 45 m for the runway of class B;

3) 42 m for the runway of class B;

4) 35 m for the runway of class G;

5) 28 m for the runway of class D;

6) 21 m for the runway of class E.

For IVPP of class A intended for operation of AF with wing span to 75 m and track on external aviatires to 10,5 of m and the smaller sizes, equal 45 m are allowed to accept the minimum width of the runway. At the same time side bands of safety of such width that the distance from axis of IVPP to external edges of everyone of side bands of safety was at least 30 m shall be provided.

For IVPP of class A intended for operation of AF of index 7 with wing span more than 75 m, the general width of IVPP with side bands of safety shall be at least 75 m, and the distance from axis of IVPP to external edges of each of them shall be at least 37,5 of m.

At the same time side bands of safety shall have biases, comparable to IVPP, and maintain the loading created by airplane in case of rolling-out without causing in it constructive damages, or loading of land vehicles which can move on roadside.

24. In the absence of RD adjoining the end site of IVPP or at its insufficient durability for turn of AF broadening of IVPP at the left or to the right of it shall be provided. Width of IVPP in places of broadening shall be at least:

1) 75 m for IVPP of classes A, B, B;

2) 45 m for IVPP of classes G and D.

25. The long edged profile of the runway with indication of the actual biases shall be given in the Instruction for production of flights for each runway.

26. Each end of LP shall have end safety area (ESA). Absence of KZB on not equipped runways of class E is allowed.

27. In the KZB longitudinal direction shall adjoin the end of LP and stretch behind it for distance at least 90 m.

In cross direction of KZB shall stretch in each party from continuation of center line of the runway for distance at least the planned part of LP established for. In cases when the KZB device of such width is impossible, width of KZB, at least, twice the runway exceeding width is allowed.

28. Within KZB there shall not be objects, except for fragile objects which on the functional purpose shall be there (for example, visual means, monitoring antenna of localizer, flashers of PRL, etc.). On KZB there shall not be mobile objects (for example, snowplows) in usage time of the runway for take-off or landing.

29. The end safety area shall be planned and prepared so that to reduce risk of damage of AF in case of landing with falling short or in case of rolling-out for the runway.

30. The surface of KZB shall not tower over the surface of landing approach or take-off. Longitudinal biases of KZB shall not exceed descending, the bias constituting 5%, and cross - the ascending or descending bias constituting 5%.

Changes of biases as far as it is possible, shall be smooth, abrupt junctions or heavy return grades are excluded.

31. The Clear Area (CA) shall begin at the end of the located take-off run and its length shall not exceed polovppa of this distance.

Inclusion of requirements to the clear areas (CA) does not mean obligatory availability of SZ in airfield. Need of SZ is determined by local conditions and economic feasibility of their device.

32. The clear area shall stretch for distance at least 75 m in each party from continuation of center line of the runway.

33. The surface of SZ shall not act over the conditional plane having the ascending % 1,25 bias, at the same time the lower bound of this plane is the horizontal line:

1) perpendicular the vertical plane containing center line of the runway;

2) passing through the point located on center line of the runway at the end of the located take-off run.

In certain cases, in case of certain cross and longitudinal runway slopes, roadsides or LP the lower bound of the plane of clear area, can be lower than the surface of the runway, roadside or LP. It does not mean that the layout of these surfaces is required. The relief which is located behind the end of LP over the SZ plane, but is lower than the LP level, can not be planned.

34. Characteristics of longitudinal biases of that part of clear area which width, at least, at least width of the runway which it adjoins shall be comparable to runway slopes if the average bias of SZ insignificant or is ascending. In case of insignificant (comparable to runway slope) or the ascending average bias of SZ sharp changes of the ascending biases of clear area are not allowed. Separate lowerings of the area, for example the ditches crossing SZ are not excluded.

35. On surface of clear area availability of obstacles is not allowed. The objects located on functional purpose within clear area shall have easy and fragile design.

36. The End Stopway (ES) shall have the same width, as the runway which it adjoins.

Inclusion of requirements to the end stopways (ES) does not mean obligatory availability of KPT in airfield. Need of the KPT device and length of KPT are determined taking into account local conditions and economic feasibility.

37. KPT shall be prepared so that it could in case of takeoff rejection, sustain the loading created by airplane without causing damage of its design.

38. For the purpose of determination of the minimum parameters: width of RD, side bands of safety of RD, curves of RD, removal of RD from obstacles and other RD - for each RD shall be established indexes of the airplanes operated on data RD of airfield. The index of the airplane is established on wing span and wheel track on external aviatires on appendix 4.

39. Width of RD shall be at least:

1) m 7,0 for AF of index 1;

2) m 10,0 for AF of index 2;

3) m 13,0 for AF of index 3;

4) m 17,0 for AF of index 4 (14 m for airplanes with index 4 in case of wheel track on external aviatires to m 7,5);

5) m 19,0 for AF of index 5;

6) m 22,5 for AF of index 6 (18 m for airplanes with index 6 in case of wheel track on external aviatires to 9,5 of m, 21 m in case of wheel track on external aviatires to m 12,5);

7) m 25,0 for AF of index 7 (m 22,5 for AF of index 7 wing span from 65 to 75 m and wheel track on external aviatires to m 13,5).

40. From two parties of RD intended for taxing of airplanes with index 4, of 5, 6 or 7, side bands of safety shall be provided (for RD with covering - the strengthened side bands of safety). General width of RD and side bands of safety shall be at least:

1) m 27,0 for AF of index 4;

2) m 29,0 for AF of index 5;

3) m 40,5 for AF of index 6 (31 m for airplanes with index 6 in case of distance between axes of outboard engines to 27 m, 39 m for airplanes with index 6 in case of wheel track on external aviatires to m 12,5);

4) m 44,0 for AF of index 7 (m 40,5 for airplanes with index 7 in case of distance between axes of outboard engines to 36 m, 60 m for airplanes with wing span from 75 to 80 m).

41. The distance between center line of RD and motionless obstacles shall be at least:

1) m 25,0 for AF of index 1;

2) m 29,5 for AF of indexes 2, 3;

3) m 38,0 for AF of indexes 4, 5;

4) m 47,5 for AF of index 6;

5) m 57,5 for AF of index 7 (55 m for AF with wing span from 65 to 75 m and wheel track on external aviatires to m 10,5).

The specified distances do not belong to ways of taxing on the platform.

42. The distance between center lines of parallel RD with artificial coverings and without artificial covering shall be at least set values (appendix 5).

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