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 of HECTARE 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 by International Civil Aviation Organization (further - the ICAO standard).

2. NGEA of HECTARE 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 around airfield 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 the project organizations of civil aviation.

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 aircrafts only after its compliance to requirements of NGEA of HECTARE of RK is established. Temporary departures from requirements of NGEA of HECTARE of RK are allowed in compensation cases by the measures providing the equivalent level of safety of flights. 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 safety of flights.

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

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

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

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

1) automatic radio 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 aircrafts radiating radio signals on channels of air telecommunication of OVCh of the range for ensuring flights of aircrafts around airfield (helidrome);

2) the intermediate place of expectation - the certain place intended for traffic control where the driving aircrafts 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 brightness contrast for day conditions of tool measurements (background brightness more than 10 cd/m 2), are accepted by equal 0,05;

Weeds 4) on devices - the flight which is carried out in conditions when the space provision of the aircraft and its location are determined by crew fully or partially by flight and navigation devices;

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

6) humidity of air relative - the attitude of the actual absolute humidity towards 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 aircrafts;

8) the area of airfield (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 control point 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 aircraft 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 (gp) at the level of threshold runway strips (further - the runway);

13) the working area of airfield - specially prepared part of the airfield intended for take-off, landing and taxing of aircrafts 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 electric equipment and the equipment of remote control intended for ensuring take-off, landing approach, landing and taxing of aircrafts;

15) airfield movement - all movement on airfield maneuvering areas, and also flights of all aircrafts around airfield. The aircraft is considered carrying out flights around airfield: when it enters airfield circle of flights, leaves it or is in its limits;

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

17) airfield coverings - the designs perceiving loadings and impacts from aircrafts, operational and natural factors which include the upper and lower layer of airfield covering;

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

19) the lower layer 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) control point of airfield (further - KTA) - the point determining the geographic location of airfield;

22) height of airfield - the absolute height of the highest point of landing strip (strips);

23) the located take-off distance (further - RDV) airfield - the amount of the located running start distance (further - RDR) and lengths of free zone if it is provided;

24) the located distance of the interrupted take-off (further - RDPV) airfield - the amount of the located running start distance (LRSD) and length of trailer strip of braking if it is provided;

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

26) the located landing distance (further - RPD) airfield - length of the runway 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) observation from aircraft board - assessment of one or several meteorological elements made onboard the aircraft which is in flight;

29) classification number of the aircraft (further - ACN) - the number expressing relative impact of the aircraft 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 aircraft azimuth concerning radio beacon installation site;

31) primary measuring converter of meteosize (further - the sensor) - the measuring converter of meteosize costing to the first in measuring chain. The measuring converter 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 the direction of the dominating winds and having the greatest length;

33) signs - the devices established over earth level for display to their panels of information in the form of texts, symbols, letters or figures or their combinations, necessary for the organization of land movement in airfield of aircrafts 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 - the platform on the design towering above the ground intended for arrival and departure of helicopters;

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

36) the rulezhny path (RP) - the part of the airfield of airfield which is specially prepared for taxing of aircrafts;

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

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

39) airfield of joint basing - the airfield intended for ensuring flights and permanent placement of the aircrafts 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 the land surface are visible down;

41) hydrohelidrome - 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 aircrafts on final stage of landing approach;

43) curvature of the line of rate of course radio beacon - the shift of the line of rate concerning its average provision;

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 ВППта, to limiting-back point of the helmsman ВППта;

46) the circle "Д" - the imagined circle provided that the platform 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 any direction in case of rotation bearing and the helmsman ВППта;

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

49) final stage of leaving on the second circle - leaving stage on the second circle on which ascent to the minimum safety of flight altitude established according to the scheme for repeated landing approach or for exit from the area of airfield is performed;

50) free zone (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 running start distance, chosen or prepared as the site suitable for initial ascent by the aircraft to the established value;

51) the landing strip which is not equipped - the runway intended for the aircrafts which are carrying out visual landing approach;

52) the landing strip equipped - one of the following types of the runway intended for the aircrafts which are carrying out landing approach on devices:

The runway of landing approach on devices - The runway equipped with visual means and any type not of visual means providing, at least, targeting of the aircraft in the direction of landing approach;

Runway of exact landing approach of the I category - The runway equipped with the radio beacon-type 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 visibility range on the runway at least 550 m;

Runway of exact landing approach of the II category - The runway equipped with the radio beacon-type 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 visibility range on the runway at least 300 m;

Runway of exact landing approach of III category - The runway equipped with the radio beacon-type 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 restriction on height of decision making and in case of visibility range on the runway at least 175 m;

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

IIIC - for landing approach and landing without restrictions on height of decision making and visibility range to the runway;

53) airfield radio engineering system of near navigation - the equipment which provides issue of these current values of azimuth and inclined range aboard the aircraft concerning installation of land radio beacon;

54) artificial covering - the upper layer of the airfield clothes which are directly perceiving loadings and impacts from aircrafts, operational and natural factors;

55) separate drive radio station - the equipment which provides the aircraft drive on airfield (helidrome), accomplishment of prelanding maneuver and landing approach;

56) wind speed - the speed of movement of air of rather land surface: In meteorological information when ensuring take off and landing average and maximum speeds of wind 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 - settlement point of intersection of nominal glide path with the runway;

the "landing point" determined above is reference point, but not obligatory point of contact of surface of the runway with the aircraft.

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, rulezhny path (further - RD), etc.) and prepared in such a way that to provide transition from artificial covering to adjacent 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 aircrafts on surface. Objects or their parts which tower over the conditional surface intended for safety of aircrafts 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 the internal surface of landing approach, internal transitional surfaces and the surface of the interrupted landing and part of the flight 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 trajectory of take-off 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 idle engine;

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

67) pulse fire with the condenser category - the lamp making flashes of light of high intensity and extremely short duration in case of transmission of electric discharge of high voltage through the gas concluded in tube;

68) flight visual - the flight which is carried out in conditions when the space provision of the aircraft 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 aircrafts, for prevention of emergence of unacceptable hindrances to ILS signal is exercised;

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

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

73) the azimuthal characteristic of course radio beacon (further - KRM) - dependence of size of difference of depths of modulation (KPM ILS). (ILS - the land equipment of system of instrument landing of meter wave band working by the principle of ILS) in points of the action area of radio beacon from angular provision of these points concerning the line of rate;

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 fires less than 10 000 cd have luminous intensity;

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

77) the safety area - certain zone of helidrome around zone of final stage of landing 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) landing zone - the site of the runway behind its threshold intended for the first contact of the runway with the landing airplanes;

80) radio engineering system of landing the equipment of system of landing (further - SMALLPOX) - the equipment which provides the aircraft drive on airfield, accomplishment of prelanding maneuver and landing approach;

81) final stage of landing approach - stage of landing approach on devices at which exit in alignment of the runway and decrease in the aircraft for the purpose of landing is made;

82) the landing radar - the equipment which provides control from the earth of keeping of the line of rate and glide path by aircrafts on prelanding straight line and management of their landing approach according to teams of dispatchers;

83) radio beacon-type system of instrument landing (PMC or ILS) - the land equipment of system of landing of meter wave band working by the principle of ILS (ICAO standard);

84) the main rulezhny path - the rulezhny path which is located, as a rule, along the runway and providing taxing of aircrafts 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 aircrafts;

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

87) reserve airfield on route - airfield in which the aircraft will be able to make landing if during flight along route it appeared in emergency or emergency environment;

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

89) reserve airfield of destination - airfield where the aircraft if it is impossible or inexpedient to make landing in airfield of the planned landing can go. The airfield from which the aircraft departure is made can also be reserve airfield on route or reserve airfield of destination for this aircraft;

90) meteorological visibility range (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 haze or fog reaches threshold (minimum) value;

91) meteorological information - the meteorological report, the forecast and any other message concerning the actual or expected weather 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 humidity of air, speed and direction of wind, meteorological visibility range, cloudiness (quantity, form and height of the lower bound), quantity and type of rainfall, fog, thunder-storms, blizzards and so forth;

94) the roadside strengthened - roadside with the artificial covering intended for prevention of hit of foreign objects in engines of aircrafts 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 the set angles of dispersion more than for 50% in comparison with the normalized luminous intensity of new fire;

99) the platform - the part of the airfield of airfield prepared and intended for placement of aircrafts 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 airborne receiver;

101) the end safety area (further - KZB) - the zone symmetrized on both sides from continuation of the axial line of the runway and adjoining the end of flight 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 rolling-out out of runway limits;

102) trailer strip of braking - specially prepared rectangular site at the end of the located running start distance intended for aircraft stop 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 aircraft;

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 control point 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 fire equal to intensity of fire of permanent radiation of the same color to which the same visibility 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 the bearing capability of artificial covering for operation without restrictions;

109) the parking lot (further - MS) - the prepared platform in airfield intended for placement of the aircraft for the purpose of its servicing;

110) helidrome - airfield or certain site of the surface 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 take-off distance (TODAH) of helidrome - length of zone of final stage of landing 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 distance of the interrupted rise (RTODAH) of helidrome - length of zone of final stage of landing 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) the located landing distance (LDAH) of helidrome - length of zone of final stage of landing 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) vertopaluba - the platform 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 parking lot (PL) of the helicopter - the parking lot of the aircraft which is intended for the parking of the helicopter and if it is provided taxing accomplishment by air, for landing and lead of the helicopter;

118) temporary airfield - the airfield intended for ensuring flights of aircrafts 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 aircrafts 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 aircrafts;

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

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

123) runway threshold - the beginning of the site of the runway of airfield which can be used for landing of aircrafts;

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) the airfield - part of airfield on which one or several flight strips, rulezhny paths, platforms and platforms of special purpose are located;

127) flight strip - the part of the airfield of airfield including landing strip and trailer strips of braking if they are provided, intended for ensuring take off and landing of aircrafts, reduction of risk of damage of the aircrafts which are rolled out of runway limits, and safety of the aircrafts which are flying by over it during take off and landing;

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

129) the landing strip (LS) - the main part of flight strip of airfield intended for ensuring running start in case of take-off and run after landing of the aircraft;

130) zone of take off and landing - airspace from the level of airfield up to the height of the second echelon inclusive in the borders providing maneuvering of the aircraft in case of take-off and landing approach;

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

132) fire of permanent radiation - fire having permanent intensity of radiation 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 the maneuver of leaving on the second circle shall be begun. In cases if before achievement of this height by the commander of the aircraft the necessary visual contact with reference points for continuation of landing approach was not come or if aircraft provision 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 supplies and the requirement to their switchings;

136) the international airfield - airfield from which flights of aircrafts 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 the axial line of the runway in the direction of landing approach at distance of 7500 m from runway threshold;

138) point of "B" ILS - the point on glide path located over continuation of the axial line of the runway in the direction of landing approach 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 axis of the runway and at distance of 900 m from runway threshold in the direction of course beacon;

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

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

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

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

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

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

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

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

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

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

151) the ranging equipment DME (DME/N) - the equipment providing acceptance of onboard signals of request and radiation of signals of the answer by which distribution time onboard AF inclined range to control point (zero indication range) of radio beacon installation site is determined;

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

153) ILS glide path tilt angle - corner between straight line which represents average glide path of ILS and the 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 depths of modulation is equal to 0,0875 (0,175);

155) to floor the sector (sector) of rate of ILS - the sector in the horizontal plane containing the line of rate and limited by the loci next to the line of rate in which for KPM ILS the difference of depths of modulation 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 axis of the runway 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-type system of landing of the I category (PMC-I or ILS-I) - system of landing which provides data for control of the aircraft from action area border to point in which the line of rate 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-type system of landing of the II category (PMC-II or ILS-II) - system of landing which provides data for control of the aircraft from action area border to point in which the line of rate 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-type system of landing of III category (PMC-III or ILS-III) - system of landing which provides data for control of the aircraft 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 landing strips with artificial covering

12. For airfield the class and class by each landing strip with artificial covering is determined (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 greatest length.

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

13. Class IVPP is determined by landing strip 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 take-off and landing distances shall be established:

1) located running start distance (LRSD);

2) located take-off distance (LTOD);

3) located distance of the interrupted take-off (LDITO);

4) located landing distance (LLD).

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

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

15. The flight strip (further - LP) including the runway both equipped, and not equipped, shall stretch behind each end of the runway or behind trailer strip of braking (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 flight strip including the equipped runway shall stretch in the cross direction on both sides from axis of the runway 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 flight strip including not equipped runway, except for the reserve soil runway shall stretch in the cross direction on both sides from runway axis (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 axis (throughout LP) shall be planned and prepared so that to minimize risk of damage of the aircraft in case of landing with falling short or rolling-out out of runway limits.

The planned part of LP shall stretch from runway axis 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 strips of safety, rulezhny paths, KPT, etc.) shall be located flush with them.

20. The part of LP located before IVPP threshold 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 aircrafts against blow about IVPP end face on distance is at least:

1) 60 m for class A IVPP;

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, the control antenna of course radio beacon, angular reflectors 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 flight 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, meteorological measuring devices).

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 aircrafts or;

2) will not make adverse effect on safety of flights 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 in a big way covered up 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 strips of safety of such width that the distance from IVPP axis to external edges of everyone of side strips of safety was at least 30 m shall be provided.

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

At the same time side strips 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 trailer 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. IVPP width 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 longitudinal 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). Lack 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 the KZB cross direction shall stretch in each party from continuation of the axial 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, KZB width, 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, the control antenna of course radio beacon, angular reflectors 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, sharp transitions or abrupt return biases are excluded.

31. The Free Zone (FZ) shall begin at the end of the located distance of running start and its length shall not exceed polovppa of this distance.

Inclusion of requirements to the free zones (FZ) 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 free zone shall stretch for distance at least 75 m in each party from continuation of the axial 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 the axial line of the runway;

2) passing through the point located on the axial line of the runway at the end of the located running start distance.

In certain cases, in case of certain cross and longitudinal biases of the runway, roadsides or LP the lower bound of the plane of free zone, 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 free zone which width, at least, at least width of the runway which it adjoins shall be comparable to runway biases if the average bias of SZ insignificant or is ascending. In case of insignificant (comparable to runway bias) or the ascending average bias of SZ sharp changes of the ascending biases of free zone are not allowed. Separate lowerings of the area, for example the ditches crossing SZ are not excluded.

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

36. The Trailer Strip of Braking (TSB) shall have the same width, as the runway which it adjoins.

Inclusion of requirements to the trailer strips of braking (TSB) 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 the take-off termination, 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 strips 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 scope of wing and track of the chassis 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 chassis 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 chassis track on external aviatires to 9,5 of m, 21 m in case of chassis 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 scope of wing from 65 to 75 m and track of the chassis 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 strips of safety shall be provided (for RD with covering - the strengthened side strips of safety). General width of RD and side strips 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 external engines to 27 m, 39 m for airplanes with index 6 in case of chassis 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 external engines to 36 m, 60 m for airplanes in a big way covered from 75 to 80 m).

41. The distance between the RD axial line 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;

Disclaimer! This text was translated by AI translator and is not a valid juridical document. No warranty. No claim. More info