40
TH
GAZETTE OF INDIA: EXTRAORDINARY
WART
n-8EC. 3(ii)1
MINISTRY OF CIVIL AVIATION NOllFICAllON
New Del Delhi hi the 14th 14th Jan Januar uary, y, 20 I0
Aircraft S.O.84(E). exercise supersession of the notification of the Government of India in 1934 Ministry of Civil Aviation n u m b e r S.O. 1589(E), dated the 30 th J u n e , 2008 expedient so to do for Central Government being of opinion that it is necessary under: safety of aircraft operations hereby direct
1. No building
c o n s t r u c t e d or erected s t r u c t u r e shall no tree shall planted any land within II from Civil limits specified in Annexure Aeronautical communication stations listed Annexure Defence Aerodromes IIIA,IIIB, IIIC, IIID IIIE without obtaining 'No Objection Certificate' Fo
th
purpose of issuing of No Objection Certificate referred to iri paragraph
(a)
No responsible for issuing th Airports Authority of India shall behalf of Central Government Objection Certificate respect of all civil Private aerodromes in India including the State Government aerodromes aerodromes where civil commercial flights Annexure IlIA; listed operating (b) for Defence aerodromes, defence authorities shall responsible for issuing No Objection Certificate subject to accordance with this notification other restriction 'No condition which such authorities deemed fit for issuing Objection Certificate'. 3.
s t r u c t u r e higher than the height specified in Annexure No building II no tree which is likely to grow ordinarily shall be constructed or erected grows higher than II shall be height specified in the said Annexure radius of tw enty kilometers from planted on any land within aerodrome reference point. developed In respect of Aerodromes which required to constr ucted structure where he height of existing building tree o n a n y land within he limits specified in Annexure Annexure II, exceeds the height specified this notification, the owner or the person having control of such building, structure tree shall reduce the height thereof within period of one m o n t h from date specified height. of publication of notification this egard so to exceed Where owner or the person having control over building or .structure height within State tree fails to reduce period specified in para 4, other concerned authority shall t-r: esponsible for Government authorities taking action in respect such building, structure tree; building structure including tower, installation chimney that is constructed erected or
m-rr I
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tree that is grown shall be considered responsible for removal
41
this notification violation of the provisions contained illegal authorities referred to above shall reduction of height thereof.
6.
airstrips specified in case of Government Private civil aerodromes present, civil schedule operations Annexure III B where, taking place possibility of s u c h operations taking place for r e a s o n s including there is terrain penetrating obstacle airspace restrictions, permanent structures limitation surface, national security, etc., he provisions of this notification shall be operational usage of applicable on the basis of th aerodrome reference code that aerodrome or strip.
7. Each Aerodrome Operator shall be responsible for preparing zoning m a p s conformity with he provisions of this notification with digitized data in WGS871' Coordinates indicating al latest features a r o u n d airport. [F. No AV AV-20036/66/2000 -20036/66/2000-AAI] ALOK SINHA Jt. Secy
ANNEXURE-I
The Land area specified below shall be completely free from al obstacles provided hereunder: 1. meters Th land comprising within Runway strip of uniform width of meters beyond each either side of centerline which extends to extremity of Runway along extended .centerline of Runway for a Instrumen runway code 4.
2.,
Th land comprising within he Runway strip of uniform width of 75 meters meters beyond each on either side of centerline which extends to extremity of Runway along extended centerline of Runway Ior 2 for n o n - I n s t r u m e n t r u n w a y code 4. instrument Runway code
3.
Th
4.
Runway strip land comprising within uniform width of 30 meters either side of centerline which extends to meters beyond each extremity of Runway end along extended centerline of Runway for a I n s t r u m e n t runway code
5.
a p p r o a c h funnel of rectangular area of land enclosed within Runway within maximum distance of 300 meters from extremity of he Runway meters either side of the extended Runway centerline for either side of extended Runway centerline for code 45 meters 2. code
land comprising within he Runway strip of uniform width 40 meters terline which extends to 60 meters beyond each either side of extremity of Runway along extended centerline of the Runway for a non I n s t r u m e n t runway code
42
6.
TH
In
GAZETTE OF INDIA: EXTRAORDINARY
.\J '/1
SEC. 3(ii)
aerodrome, where
(a) Very High Frequency Omni Radio Range (VOR)/Distance Measuring Equipments (DME)/Very High Frequ ency Dire ction Finder (VHF DF) available, land within the facilities meters r a d i u s of he facility; (b) Localizer facilities
available, th
area bounded
namely:
(i)
(ii) (iii) (iv)
a line 300 meters in
nearest of direction of approach runway whichever is great from localizer a n t e n n a perpendicular to th runway; a line from th centerline of localizer a n t e n n a both side parallel to he runway; a line containing centre of localizer ennas perpendicular to runway;
a r e a within circle of 75 meters radius with centr a n t e n n a system;
(c) GLIDE PATH facilities namely (i)
following,
line
facility;
available,
meters in th
area bounded
direction of approach from
middl
of
following,
glide path
line containing glide p a t h a n t e n n a perpendicular runway; (iii) n e a r edge of the runway from he glide path; (iv) a line meters in directions away from the runway parallel to it;
(ii)
(d) Locators r a d i u s of
of
land within Markers Beacons fa cilities available, meters of he site of th markers locator beacons;
(e)
available, Air Surveillance Radar facilities structure will level of 3 meters below pedestal permitted on the l a n d above to distance of meters from Radar a n t e n n a ; height
(f)
Air Routes Surveillance Radar facilities available, no structure will be permitted land above he level of 5 meters below the pedestal to th distance of 200 meters from Radar a n t e n n a ; height
(g)
Secondary Surveillance Radar are available, th distance in respect of he Air height restriction shall be he same Surveillance Radar or Air Routes Surveillance Radar, depending u p o n operational usage;
(h) Microwave Link facilities
available, meters corridor of line of th azimuth 10 meters below from either side of the dir flight in vertical plane; the direct line
[ 'lWT II
3(ii) ]
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43
3ffiTmDJT .
(i)
avail able Ultra H i g h Frequency (UHF) Link facilities of zimuth meters on either side of direct line of th direct line of sight in th vertical plane; meters below from
Ul
-route Beacons facilities meters a r o u n d antenna;
(k)
Remote Receiver facilities meters site
available> land within
orridor 10
radius
radius
available, land within
1525
purpose of this Annexure
Explanation .-
(a) "Runway Strip" means way, if provided, intended:
defined area included
r u n w ay
(i) to reduce the risk of damage to aircraft r u n n i n g of (ii) to protect aircraft Dying over it during take operations;
stop
runway; of or landing
"Runway Code" m e a n s Runway Code, in relation to the dimension (b) Table below of Runway strip, specified in column (1) DIMENSION OF RUNWAY STRIP
Runway Code
(1) 1. 2. 3. 4.
(c) (i)
Length
(Meter)
(2)
Width Extending laterally either side Runway Centre Line
(Meter) (3)
<800 800<1200 1200 <1800 1800 above
"Approach funnel'>,
Length beyond Runway
End/ Stopway
(Meter)
Width Extending laterally ei t h e r side of Runway Centre Line
(4)
(Meter) (5)
60
40
Length beyond Runway
End/ Stopway
(Meter) (6)
75 50 50
relation to
a n I n s t r u m e n t runway code area s h a p e of 4, m e a n s longer parallel side 4800 meters isosceles trapezium having long (2400 meters on either side of th th extended centerline runway) smaller parallel side meters long (150 meters runway), where the smaller either side of the extended centerline of meters longer parallel sides placed distance of runway of 15060 meters respectively, from th right angles to extended centerline;
44
TIlE GAZElTE OF INDIA: EXTRAORDINARY
IPART
n-SEC. 3(ii»)
(ii)
2, m e a n s a n I n s t r u m e n t runway (precision) code area s h a p e of isosceles trapezium having the longer parallel side 4 6 5 0 meters long 9 2 3 2 5 meters either side of the extended centerline of smaller parallel side where th smaller longer th runway) 15060 meters distance meters parallel sides are placed right angles to respectively, from runway extended centerline;
(iii)
2, m e a n s a n I n s t r u m e n t runway (non precision) code area he s h a p e of isosceles trapezium having the longer parallel side meters long (450 meters on either side the extended centerline smaller parallel side 150meters long (7 meters he runway) either side of the extended centerline of smaller runway) where distance meters longer parallel sides are placed 2560 meters respectively, from runway right of th angles to extended centerline;
(iv)
4,means non-Instrument runway code in the s h a p e isosceles trapezium having longer parallel side meters long either side of the extended centerline runway) (375 meters meters long (75 meters on either side of smaller parallel side runway) where the smaller the extended centerline of longer distance of parallel sides are placed meters 3060 meters runway respectively, from right angles to of extended centerline;
(v)
I n s t r u m e n t runway code 2, m e a n s a r e a in shape longer parallel side 580 meters long isosceles trapezium having th either side of 9290 meters runway) extended centerline longer parallel sides where he smaller placed distance meters runway 2560 meters respectively, from right angles to the extended centerline;
(vi)
I n s t r u m e n t runway code 1, m e a n s area shape isosceles trapezium having longer parallel side 320 meters long (160 meters on either side of the extended centerline runway) smaller parallel side meters long (3 meters either side of runway) where the smaller longer the extended centerline of 1660 meters parallel sided placed distance of 30 meters respectively, from runway right angles to of extended centerline he diagrams of Runway strip and approach I n s t r u m e n t runway code 1, non-Instrument funnel Appendix; runway code have been shown
(d)
"Instrument runway" means runway served by visual non-visual aids providing directional guidance a d e q u a t e for a straight in approach intended for th operation of aircraft using i n s t r u m e n t approach procedures;
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45
(i)
Non-precision approach runway- An i n s t r u m e n t runway served by providing visual aids non-visual ai least directional guidance adequate fora straight-in approach,
(ii)
i n s t r u m e n t runway Precision approach runway, category MLS served by I n s t r u m e n t Landing System a n d / visual aids intended for operations with lower t h a n decision height meters either a visibility runway less t h a n 8 0 0 m e t e r s visual range not less t h a n meters,
(iii)
Precision approach runway, ategory II- An i n s t r u m e n t runway MLS served by I n s t r u m e n t Landing System visual aids intended for operations with decision height lower t h a n 60 meters meters runway visual range riot less lower t h a n than 350 meters,
(iv)
Precision approach runway category served by Instrument Landing System a n d / surface of he runway a n d -
i n s t r u m e n t runway MLS to along
A-
ended for operations with decision height lower than no decision height runway visual range less t h a n meters, eters, B-intended for operations with decision height lower than 15 meters, runway visual range less t h a n 200 meters no decision height less t h a n 5 0 meters, c- intended for operations with no decision height runway visual range limitations
(e)
"Non-Instrument runway m e a n s runway intended for operations of he aircraft using visual approach procedure
(D
"Very
(g)
" I n s t r u m e n t Landing System" m e a n s th facility which erves to help craft to make th runway conditions of poor safe landing visibility comprises of th followin component facilities amely :
High Frequen cy Omni Radio Range, Terminal Very High er Frequen cy Omni Radio Range Doppler High Frequency facilities operating in Omni Radio Range" m e a n s Very High to 11 MHz radiate signals Frequency b a n d of frequencies 11 an instrument its cockpit when whereby aircraft with th help t u n e d to ground equipment frequency automatically gets direction with resp to th facility elps craft to navigate fa cility; predetermined course airport served by home to
Localizer facility which radiates Very High Frequency (i) by ircraft guide it onto the centerline of which when picked is norm ally s i t u a t e d a b o u t runway in the horizontal d; meters from he runw
46
,!,HE G A Z E l T E OF
INDIA:
EXTRAORDINARY
PART
II
SEC.
3(ii)1
(ii} is Glide Path facility radiates Ultra High Frequency signals runway normally s i t u a t e d a b o u t 275 meters to 305 meters from meters from threshold meters to offset a b o u t terline of the runway provides th glide angle information to help of a n i n s t r u m e n t in the cockpit which landing aircraft with glide p a t h frequency indicates whether when t u n e d to aircraft flying down along the correct glide angle;
O u t e r Marker or O u t e r Locator facility operating on 75 MHz Very High Frequency band is normally installed along the extended distance between nautical centerline the runway produces radiation pattern miles (1 nautical mile := 1853 meters) to indicate the landing aircraft, the pre-determined distance from threshold along the I n s t r u m e n t Landing System glide p a t h ; (iii.)
(h)
(i)
"Radar" includes (i)
Air Surveillance Radar which is r a d a r facility serving traffic within aerodrome to scan th to 60 nautical miles of the aerodrome;
(ii)
Secondary Surveillance Radar Air Routes Surveillance Radar distance is h i g h ' power long-range r a d a r covering it s c a n s traffic to nautical miles approximately larger distance than Air Surveillance Radar;
Communication/ Navigational facilities include
Note 1: An located
(i)
Microwave Link which is intelligence/data is carried to
(ii)
Ultra High F r e q u e n c y Lin which operating in Ultra High Frequency Band;
(iii)
Beacons which radio transmitters operating in the Medium to KLHz radiating omni Frequency band from directionally in the horizontal plane aircraft equipped suitable cockpit i n s t r u m e n t with location et automatically with respect to this facility;
(iv)
Remote Receivers which radio receiving s t a t i o n s (HF Band) installed remote site away from factory or industrial a r e a s to avoid interference link m a n - m a d e static, etc.
equipment
installation required for
radio facility whereby mostly Air Traffic Control Display site;
radio
navigation
relay facility
must
[ 'lWT II
3(ii) ]
47
(a) i)
that portion of the strip within: 75 meters of th Runway centerline where
i) (b)
is 3 or 4, r
meters of the Runway
Runway code
terline where Runway code is
runway safety a r e a taxiway strip or within distances specified in Annex 14 of guidelines th International Civil Aviation Organisation; or
(c)
which would endanger clearway shall be frangible and mounted low
aircraft in the air, possible.
Note 2 Any equipment or installation required for ir navigation purposes which strip of precision approach Runway category I, II or near must be located which II of I n s t r u m e n t Landing System (a).
(b) (i)
(ii) (iii)
is situated meters of th
that portion of the strip within the 77.5 code number is Runway centerline where code letter is is situated within 240 meters from of strip within meters of th extended Runway centerline where Runway code is or 4: or 45 meters of the extended Runway centerline where Runway code is 2: inner approach surface, penetrates th th mner transitional surface or balked landing surface,
and shall be frangible
mounted
low
possible
NOTE 3. Location of Navigational Aids shall be determined provisions of Annex-1 0 of guidelines of International Civil Aviation Organisation.
SJOM
•
strip
Rw 4650'
00M
rc
·
)R REO S I O N CODE 1 & 2 · EClSIO NON
(:ODE
approaci funnel of instrument Rw
>50000'
code
-JJ
-' CJ
:> L-'
1&
L-' ""l
.-
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Me---
-==-..::-._
§ E Z ~ J
..
L-'
s:
OR Pf;E: IS ION AP COD,, :U OR NON f'll CISION APP CODE H<2
000M
2S00
;:0
S2
:> ;:0
-<
Rw strip
approach funnel of non instrumen Rw
code 3&4 II
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49
ANNEXURE-II permissible elevations shall be calculated based u p o n Th height Annex 14 obstacle limitation surfaces, the radio navigation aids based on Annex 10 operational requirements for minimum altitudes of various s e g m e n t s of published instrument approach procedures based on Document 8168, VOl II of International Civil Avi ation Organisation.
1.
Based
Annex 14 Obstacle Limitation surface
1.1
Take-off climb surface dimensions of take-off climb surface shall table given below except t h a t be less than the dimensions specified in if runway is m e a n t for takeoff, a lesser length may be adopted for takeoff climb surface where s u c h lesser length would be consistent with procedural measures adopted to govern he outward flight aeroplanes, namely:
under:
Table obstacle limitation surfaces Dimensions slopes (RUNWAYS MEANT FOR TAKE-OFF) Code Number
Surface dimensions*
(1) TAKE-OFF CLIMB ength of inner edge Distance from runway Divergence (each
side)
Final width
(2) meters meters 0%
380 meters
(4)
(3) 18
80 meters meters
meters meters
12.05%
10
1200meters 1800 meters ** 15000 meters
580 meters
2500 meters 1600 meters 2% 4% 5% measured horizontally. All dimensions ** 1800 meters when the intended track includes changes of heading greater than 15 degree for operations conducted in IMC, VMC by _niggL Length Slope
__
1.
Transitional Surface
1.2.1 Th
o u t e r limit transitional surface is determined by it with the plane containing inner horizontal surface transitional surfaces are given below, namely :
intersection slopes of
1.2.2 (i) (ii)
Precisionapproach Runway Non precision
(Iii)
Non-Instrument runway
175 GI/1
14.3% (1:7) 14.3% (1:7) for code 3 & 4 "20% (1:5) for code 14.3% (1:7) for code 3 & 4. 0% (1:5) for od 1 & 2;
50
THE GAZEITE OF INDIA: EXTRAORDINARY
IP.-\RT
II-SEC. 3(ii)1
1.2.3 The slope of the transitional surface shall be measured in a vertical. plane right angles to the center line of th Runway;
point 1.2.4 The elevation of a lower edge shall be (a) along side of a p p r o a c h surface, equal to th elevation approach point; surface (b) along strip, equal to elevation of nearest point of center line of Runway or its extension;
1.3 Approach Surface 1.3
Th approach surface shall established for each .Runway strip in direction of intended landing of th aeroplanes limits slopes given in table below:
1.3.1.1.
Instrument runway (diver gence 15 on either side) for Code No.1 Length of Inner edge - 1 5 0 mete meters for Code No.3 and 30 Distance from Threshold meters Table
RUNWAY ,.
Code
No.
Length (meter)
1.
<800
2.
800<1200 1200<1800 1800
Above
Precision approach Runway Second First Se ction Section Length Length
(Meter)
(Meter)
Slope 3000 .5 3000 2.5%
Non Precision approach First Section length
(Meter)
Slope
Slope
Slope
12000**
2500 3.33% 2500 3.33%
12000*
3000
.5%
3000 2%
3000
3600
3000
:5
"Total length of approach surface for code No. 3 precision shall be 15000
3600 2.5% 3600 .5
Horizontal Section
(Meter)
8400** 8400**
non
(precision
eters.
Total length of approach surfac shall be 15000 meters. 1.3.1.2.
Second Section Length
(meter)
.33% 3600
2%
R ~ n w a y
for Precision approach Runway Code No. 1
Non -Instrumental runway Length of Inner edge for Code No.3 and
meters for code No.1 and
15
meters
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Distance from Threshold
51
meters Table
RUNWAY
01 VERGENCE
SI
Code
No.
Length
No. 1. 2. 3. 4.
Metre)
Length
(Meter)
<800 800<1200 1200<1800 1800 above
2500 3000 3000
0_
10%
ON
EITHER
Section slope % % 3.33% 2.5%
1.3. i.3.
Aerodrome where there are more than on runway with over-lapping approach a r e a s a n d associated surface, most stringent of tw would be applicable criteria.
1.3.1.4.
runway approach, he physical extremities of for determining shall only be considered. displaced threshold the In case permissible height shall be calculated based approach surface displaced transitional surface with respect to runway extremity threshold which ever is more restrictive. However in c a s e the threshold been displaced to obstacles of permanent nature, which taken likely to be remov d, the displaced threshold will reference point.
1.3.1.5.
Aerodromes, where the proposals for runway extension exist, requisite surface shall be determined from proposed extension existing runway strip/ associated clearway, well from lower of applicable two elevations shall be permitted
1.3.1.6.
elevation of the associated Runway e x t r e m i t y / d i s p l a c e d threshold/ proposed extension of Runway shall be the datum for s u r f ce appro
1.3.1.7.
slope of containing
1.4
approach surface shall centerline of the runway.
measured in
vertical plane
Inner. Horizontal Surface
1.4.1 Dimensions permissible heights table below:
Inner Horizontal Surface
DIMENSIONS AND PERMISSIBLE HEIGHTS RUNWAY
given in
INNER HORIZONTAL SURFACE
INSTRUMENT
Code
Length
Radius
Height
No. 1.
(Meter)
(Meter)
(Meter)
<800
3500*
NON -INSTRUMENT Radius
(Meter) 2000*
Height JMeter)
52
TH
2. 3. 4.
IP\RT I I - S r . Co 3(ii)1
GAZETTE OF I N D I A ' EXTRAORDINARY
800<1200 1200<1800 1800 above
2500*
3500*
4000** 4000**
4000** 4000**
*Radius shall be measured from
** Radius shall be measured from th
Aerodrome Reference Point. extremities of the Runway
1.4.1.1.
Th reference datum for Inner-Horizontal Surface shall be Explanation to this Aerodrome elevation defined in clause (g) of notification.
1.4.2.
4, Fo Runway code Inner Horizontal Surface shall be th composite pattern, which consists of two circular areas centered two ends with radius of 4000 meters These areas shall be joined shown in Appendix-A. elliptical shape tangentially to form
1.4.3.
Where it is required to protect two or more widely spaced long runways, even more complex pattern involving four or more circular areas formed. These areas should be joined tangentially Inner Horizontal Surface shall be defined by by straight lines the external limits of the resulting pattern.
1.4.4.
When two aerodromes are close to each other with overlapping circuits Inner Horizontal Surface will be drawn prescribed in para 1.4.2. he inner horizontal surface of these two aerodromes shall be joined common Inner Horizontal Surface. tangentially to form
1.4.5.
In case of common horizontal surface serving two aerodromes, the tw elevation of Inner Horizontal Surface will be th lower of aerodromes.
1.5.
Conical Surface
1.5.1.
Th conical surface shall be projected upwards and outwards from he slope 5% (1:20) of th periphery of the Inner Horizontal Surface. conical surface shall be measured in vertical plane perpendicular to periphery of Inner Horizontal Surface. he outer limits table below: permissible heights of th conical surface given in Table
OUTER LIMITS AND PERMISSBLE HEIGHTS OF CONICAL SURFACE RUNWAY Code No.
Length (Meter)
INSTRUMENT RUNWAY Precision Runway
Nonprecision Runway
NON-INSTRUMENT RUNWAY Horizontal Distance of Conical Surface beyond
Maximum Height above Inner Horizontal
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Inner Horizontal Surface
53
..
-_
Surface
(Meter)
(Meter)
1. 2. 3. 4.
<800 800<1200 1200<1800 1800 above
1200 2000 2000
10 10
1200 1500 2000
10
The reference datum for Conical Surface shall be defined in this Annexure.
1100 1500 2000
10
aerodrome elevation
Note: Where
conical surface lies below part of Inner Horizontal Surface approach/ take cliinb surface, th permissible heights shall be lowest of applicable surfaces.
1.6
Outer Horizontal Surface
1.6.1. Th
Outer Horizontal Surface shall extend to 15000 meters from th Aerodrome Reference Point for Aerodrome with runway code
1.6.2. In case of Aerodrome with Runway Code-Z, the Outer Horizontal Surface shall extend to 14740 meters from Aerodrome Reference Point for Instrument runways 13740 meters for Non-Instrument runways. 1.6.3. Where
combined Outer Horizontal Surface IS established for two Outer Horizontal Surface shall be centered on th Aerodromes, Aerodrome Reference Point of th Aerodrome of higher category.
1.6.4. Outer Horizontal
for Aerodrome with runway code No. 1
be
established. 1.6.5. he Outer Horizontal Surface, would be defined such that Conical Surface may continue to be extended 5% slope to point wherein the permissible maximum height 300 meters (above aerodrome elevation) is reached thereafter this surface is maintained upto 15 Kilometers from Aerodrome Reference Point. Construction (s) protruding above these area be permitted. Obstructions existing in surfaces shall normally
shouldbe marked
lighted.
1.6.6. In order to avoid abrupt vertical changes in surfaces, th surfaces beyond 1:7 from edges of conical surfaces will slope laterally approach take off surfaces between th permissible heights of 50 meters to meters. 1.6.7. Th datum for Outer Horizontal Surface shall be defined in this Annexure.
1.7. Th
Inner approach, inner transitional
aerodrome elevation
balked landing surfaces (OFZ)
54
THE GAZEITE OF INDIA: E X T R A O ~ I N A R Y
(PART I 1 - 8 E c . 3(ii)]
. 1.7.1 Obstacles free zone shall established for precision approach Category II III operations. The zone shall kept free from fixed objects other than light weight frangible mounted aids to navigationwhich m u s t .near Runway to perform their functions, from transient objects such aircraft vehicles when Runway is being used for Category II III operations. 1.7.2 The dimensions
given below:
slopes of
Obstacles free zone (Code 3
Note: Obstacles free zone for Runway code No.1
4)
established.
1.7.2.1
he Inner approach surface 12 meters Width Distance from Thresholdmeters meters Length
Slope
2%
1.7.2.2 The inner transitional surface Slope33.3% 1.7.2.3 Balked Landing surface Length of the Inner edge, Distance from Threshold
Divergence Slope
18
meters meters
10%
3.33%
1.8. Th
obtained from the competent No Objection Certificate needs to requested height of authority in all cases wherein structure etc. more than meters above reference datum distance of to Reference point. Kilometers from
2.
Based
2.1
Very
Annex 10 (Navigational Aids)
High Frequency O m n i R a d i o Range (VOR) Terminal Very H i g h Frequency Omni Radio Range (TVOR), Very High Frequency Omni Radio Range Distance Measuring Equipment (VOR DME)": An a r e a beyond meters from radius of facility no c t u r e shall sustain vertical angle greater than 1. degree the center of th Very High Frequency Omni horizontal plane passing through Radio Range counterpoise from counterpoise.
2.2
Stand alone Distance Measuring Equipment- Beyond 150 me,ters no steel towers, power lines, metal buildings shall protrude elevation angle of degree measured from the base of Distance Measuring Equipment antenna.
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3(ii)
55
Localizer
2.3.1. Beyond area specified in Annexure object should sustain front of antenna, the centre of antenna array. degrees
within ±-1 0 degrees azimuth in angle of elevation more than 0.75
within.±. 10 degrees to .±. 2.3.2. Beyond areas specified in Annexure degrees azimuth front of antenna an object should angle of sustain elevation more t h a n 2.4. Annexure within .:t degrees azimuth in front of Beyond th area specified glide path antenna, building/ structure should not. tend angle of antenna base. elevation of more than 1.1 degree
.5
Air Surveillance Radar :
Beyond 5 0 0 m e l e r s from particular Radar site th height of permissible increased the rate of 0.05 meter per meter, to structures point wherein th height of th permissible structure does protrude above th line below farthest point drawn from a point 10 minimum sector altitude center of antenna pedestal, considering the Minimum (from Radar site) to Sector Altitude (MSA) in that particular sector. Beyond above stated point no point 10 large object would be permitted to protrude above th line drawn from below he minimum sector altitude the farthest point (from Radar site) to th center of antenna pedestal depending on th Minimum Sector Altitude that structure / s in isolation or collectively particular sector. Large object means subtending azimuth angle of .4 degree or above Radar antenna. In case of cluster of buildings wherein two a d j a c e n t buildings subtends gap between .4 degree on the antenna pedestal, the entire azimuth angle of less than object. Diagrammatic representation is cluster should be considered
Appendix-B. .6
Air Route Surveillance Radar:
Beyond 200 meters from particular Radar site th height of permissible be increased the rate of .0 meter to point structures protrude above wherein the height of permissible structure does angle of elevation of more than .5 degree angle equal to antenna pedestal antenna tilt angle during last flight inspection whoever is higher. Beyond line above stated point, no large object would be permitted to protrude above drawn at an angle of .5 degree from antenna pedestal angle equal to Large during last flight inspection whichever is high er antenna tilt angl object means structure subtending azimuth angle of 0.4 degree or above two between Radar antenna. In case of cluster of buildings wherein the adjacent buildings s u b t ends azimuth angle of less than .4 degr ee antenna pedestal, th entire cluster should be considered obj ect. on Diagrammatic representation is Appendix -C.
2.7
Secondary Surveillance Radar
56
TH
GAZETIE OF INDIA: EXTRAORDINARY
IPART II-SEC. 3(ii)1
Same Air Surveillance Radar / Air Route Surveillance Radar depending on operational usage. control system (ASMGCS) Advance Surface Movement Guidance No structure s h o u l d built on the relevant area of the airport surface which sensors of line of sight between blocks of Advance Surface control system case relevant operational a r e a Movement Guidance there is operational structure safety/security requirement to airport surface which obstruct line of sight between Surface Movement Radar (SMR) a n t e n n a / sensors, Airports Authority of India (AAI) would a u g m e n t system to meetcontrol system Advance Surface Movement Guidance operational requirement.
Indian
Uplink Station (INLUS)/Indian National Reference Station (INRES) of GP Aided Ge Augmented Navigation (GAGAN) System No structure will be permitted to protrude the above the plane inclined elevation angle of degree from horizontal surface drawn level of antenna of Indian Land Uplink Station Indian National Reference Station of GPS Aided p a r t of Global Navigation Satellite Ge Augmented Navigation system which is System (GNSS) .9
Land
2.10 Communication Navigation Surveillance (CNS) Simulation study structure made within aerodrome surface in In case required to obstruction from Communication Navigation operational interest which creates to study Surveillance point of view, a simulation study could be carried impact of this s t r u c t u r e on the performance of the relevant facility in case s t u d y confirms that i m p a c t would not hamper operability of facility, s u c h s t r u c t ur e could be permitted within the aerodrome boundary.
3.
Operational criteria based
Document 8168, Vol II
In order to achi eve he lowest possible operating minima for aircraft operation, is essary to protect only th Annex 14 Obstacle Limitation Surfaces also to eguard the Procedure for Air Navigation Service (PANS) Operations (OPS) (Doc u m e n t 8168) Surfaces Considerations need to be given to objects which pe etrate th Procedure for Air Navigation Service Operations Surface, regardless Such wh they penetrate Annex 14 Obstacle Limitation Surfaces. obst acle result in operational penalty like higher Obstruction Clearance Altitude introduction of longer approach segment Height (OCA/H) Therefore, while examining th cases issue of No Objection Certificate from considerations of Annex 14 An provided ill. p a r a 10 criteria erational criteria needs to be considered based on the provisions of above, th to be ensur ed that minimum altitude of he Document 8168, Vol. II. ne a p p r o a c h procedures p r o p o s ed instrum following segment of publish ed no infringed by the propos ed construction eith within the Obstruction Limit Surface (OLS) or outside of it. (i) (ii)
Minimum Sector Altitude (MSA) Minimum Holding Altitude (MHA)
['lWT I I
-
(iii) (iv) (v)
~
cqrrn
3(ii)]
CfiT
3lWtmUT
57
Minimum Vectoring Altitude (MVA) Minimum Altitudeof Initial intermediate Segments Circling) for all aircraft categor ies. OCAjH (Straight-in
Note:
civil aerodromes in India I n s t r u m e n t approach ro cedures of all AlP India u n d e r th section Aerodrome. In th have been published in published procedures, th minimum altitudes of th various segments of procedures have been specified. i n s t r u m e n t approa 1.
2.
th riteria are applied Th minimum obstacle clearance (ICAO) Document provisions of International Civil Aviation NM 8168 Vol. II. Normally, for minimum sector altitudes (applicable upto from facility on which procedure is designed), m i n i m u m vectoring for initial approach altitudes, minimum holding altitudes obstacle cl e a r a n ce of 1000 feet is applied
3. Final approach a r e a s of er High Frequ ency Omni Radio Range (VOR)j No Directional Beacon (NOB) have been illustrated in Appendix-D 4.
Shielding Benefit
Shielding principles employed with respect to n a t u r a l indicated below e r r a i n j duly authorized existing obstacles which penetrate above obstacle limitation surfaces described a n d a s contained in this document, subject to aeronautical study, if considered necessary by competent authority. 4.1
Aerodrome
Ground Aids (AGA) parameters
lying 4.1.1 The following criteria shall be applied for the purpose of s t r u c t u r e with respect shielding benefits for he proposed building to existing n a t u r a l terrain Zbuilding structures. 4.1.2
principle of shielding will area.
be applied in
transitional surface
4.1.3 The principle of shielding shall applied the approach areas inner edge of runway strip. beyond 4000 meters of in 4.1.4 Th principle of shielding shall appli ed Surface (IHS) beyond radius of 3000 meters from strip.
4.1.5 The principle of shielding shall also be applied horizontal surfaces. shielding benefit is to provid ed wit.h r hori zontal pl s t r u c t u r e s j atural terrain in of ach of obstacle away from
.1.6 Th
'J
Inner Horizontal nearest runway
conical
oute
pect authorized op projected from
pl
58
TH
towards the runway 10 slope having Inner s negative slope shall benefit of Horizonta l, Surface applicable Aerodrome upto 300.0 meters from n e a r e s t Runway end or Referenc Point the case !pay be In case of approach surface the benefit of negative slope shall be applicable upto 4000 meters from Outer Horizontal surfaces, case of Conical n e a r e s t runway end. shielding benefit of negative slope shall be restricted to same surface.
ii
11
I'
I
GAZETTE OF INDIA-: EXTRAORDINARY
II
1,11 _
provided for determining following guidelines shielding benefit would be applicable:
.1.7 I' \
I ,.'
[.
i/1
'
-iY
l\ '1
{i
', ,-Ii
II
,'
t-,
(ii) d ' i ; ~
,JI ;
<1
d
-11
!(!' j l
praw
runway Neg
s. (1
111
:)JL II r' 4.1.7 .2
hj
-~
(iii) ,,
,I
\.
th highest point
reference terrain/obstacle of.all runways ,for ,obst$.cles Iocated within the Inner Horizontal Surface, Conical th Outer Horizontal Surface. lines areas bound within The shielding benefit will cover from
1: (i)., face of o b s t a c l e located within approach i. runway, the negative shielding shall be applicable to that articular runway only area shall drawn by joining highest point reference terrain/ obstacle to of nearest runway end. The dimension of th same area shall the dimension .pana
' i ~ . 6 , a n d ~ p a . . r a i 4 . 1 . 7
111·) '1111_'
I
"Iii
I,
,I
f,jll'
I, ffi-w ay. f r o m t h e runway (Horizontal. plane
'. 11)1
'-,J
II
,j
Inne r, HQri4ontal Surface. Conical obstacles located in Aerodrome Reference Outer Horizontal Surface, draw a l i n e from
(i)
;:
ive slope) I
. o . b s t a c l ~ . .'1
.areas where
,-
( )/\ Il'ow
L7
l
)I
11
,'\I. !I ! oftheobstacle. ,' , " 1 " r- \Y. extremities obstacle away from line d r a w n a s .perpana 4.1.7-.2 (i), runway parallel to line from th obstacle located in approach surface, draw ne s t r u ri wa ie '1 .t th c e n t r e o f t h e obstacle.
projection of Draw obstacle away from the runway parallel to para line drawn (iii) benefit of horizontalvplan shall be applicable to ' I,; (V obstacles l o c a t e d b e l o w t h e p r o j e o t i o n I i n e r i r a w r u a s p e r para 4.1.7.2 indicated in Appendix-E (ii iv) '" ' ," '' ii i II I I '" isolated towers, chimney, ,8;J'all.-r s k e l e t a l o b s t n ;t ctions power lines masts, electric pylons, telephone poles will provide shielding. (iv)
.. 1· '
I'
1
shielding benefit it s h a l l- be ensured that 4.1.9. While providing various segments th published instrument minimum altitude, adversely affected. I. approach procedures
[mTT
1 1 - ~ ' 3 ( l i ) ]
:
cqffif CflT
59
Communication Navigation Surveillance {CNS) Parame ters
4.
i
'
II I
IT'
I
navigational Aids Surveillance facilities shielding fi could 'be provided to he s t r u c t u r e s in cases wherein such structures in their shadow of highest existing authorized s t r u c t u r e . /terrain of Sli.Eia ' for thIs both th u r p o s e is defined as an area falling 'below a line drawn from to extremities existingauthorized s b : u c t u r e j t e r r a i ~ y f : ure, to ) : n a n e xtrapolation of facility pl ,ne ind frorn th aid)9 (. Fo
5.
Conduct of Aeronautical Study ,'
The following
II ,'
request fo Authority India •
,:
l.
mined
")
J'
I'
,.
aeronautica l' study afte Recommendations approval of the ompetent authority shall be considered by Airp6r f\\ 6rit'y of India for issuing No Objection Certificate for the height sought
I'
The follo wing steps shall ermissible 'igHt' Certificate for U i l d i n g / i r ~ l
!,
I
(fir
(hi)
nnex
he
'-I
,j
ible' h'elgn ts
ITi
~ t i n g
site of
•
'"
o'
l a ' t i o ' n s
J; :
;.
or .1
rnaximu Objection
tli ,f
I' J.i
p;6'po secl
p t i l I d i r t g ~ / i h s t a l l a t i of the a: rodr h1
r.1
-r i-.
I,
Ji-r
1
aH
oylt tfre zoning operator, where Annex 14 surfaces have been drawn. 'If hh location is permissibfe pplk abie heigHts r6'ach' rf k: l:l: surface, transitional tfac surface shall be calculated. sitc '{s
~ r k e d
t'
on
lo h'ld
£Rtf
~ i d e " t h e
the height shall be determined 'k's relevant surface (transitional, Inner Horizontal Surfa ce" Conical or Outer Horizontal Surface ; "' l' 1. [1,11 :,1 4"
lf
iI
""[li
1,1
tl /i t
1( I , l ' : )
'.'J,f/ ,.
)wr;[
,i
(i
,'
distance site proposed of from an rv ililci hc Iacilit cOffimuhlCa'ti j'riaviga t1 6ri i3:i" id applicabl heights based on the provisions as' contained in para Determine
..
[1
Illl
1,
',
I,
'1
,
''''tt
(i)
pe take
An ex 14 Cr te ia
11
..
I-
I
Y"
'A
tI
r.
by a p ed
l'
.
'I Procedure for determining
.1 .2
,'II
I
'l
,I
6.1.1
oc'J sse/c' by'l Airports
to 'case 'basis,
Aeronautical study shall be undertaken approved agency guidelines.
(iv)
'6.1
]f rl lt: 1(
snalr
t i c a 1 " s t u d y
f"
\
df
cl
"
'i
11 -lll
I'
\lJ:
llli
idelines ar provided !i.1r cb
'the (iii)
,(
·a
he .. ~ ~ r
te e II.
60
THE GAZETfE OF INDIA: EXTRAORDINARY
6.1.3.
\PAR
II
C, 3(ii»)
above two criterion shall be The permissible height from lowest applicable to specific surface/individual communication /navigational id surveillance facility
Procedure for Air Navigation Service Operations (PANS OPS) Criteria
6.2
After having determined the permissible heights based on the Annex 14 Obstruction Limit Surface (OLS) criteria Annex criteria, it shall Procedure for Air Navigation Service further be e n s u r e d that Operations (PANS OPS) Surfaces are infringed the minimum
i)
p u b l i s h e d / proposed segments f. i n s t r u m e n t approach altitudes procedures are fully protected. This p a r a 3. also been referred to
ii)
obstacles located even outside the limits of Annex 14 OLS, it shall be e n s u r e d that Procedure for Air Navigation Service Operations (PANS OPS) Surfaces he published i n s t r u m e n t approach procedures penetrated.
iii)
final approach a r e a for Fo consideration of obstacle clearance in secondary a r e a shall proposed construction he criteria of primary be applicable
iv)
Procedure for Air Navigation Service Operations (PANS limits of OPS) Surfaces extend to NM from facility [Very High Frequency Non Directional Beacon (NDB)] serving Omni Radio Range (VOR) which procedure is designed. This is to e n s u r e t h a t aerodrome based minimum sector altitudes minimum vectoring altitudes the proposed constructions adversely affected
Fo
6.3 Th Annex 10 lowest height determined based Annex 14 Procedure for Air Navigation Service Operations (PANS OPS) shall be permissible height of the proposed building/ installations for which NO Objection Certificate is to be issued.
Explanation,----- Description of Annex 14 Obstacle Limitation Surface for diagrams in respect purpose of this Annexure shall be given h e r e u n d e r given in Appendix-F -1 to F-5. thereof shall be (a)
Conical Surface surface sloping u p w a r d s periphery of th i n n e r horizontal surface.
o u t w a r d s from
The limits of the conical surface shall c o m p r i s e : .t
(i)
(ii)
lower edge coincident with the periphery of th
u p p e r edge located surface.
specified height above
i n n e r horizontal surface;
i n n e r horizontal
srm
II ~
" @ U : S
3(ii) ]
The slope of perpendicular to
61
conical surface shall be measured in periphery of the inner horizontal surface.
vertical
plane
(b)
Inner horizontal surface surface located horizontal plane above aerodrome ts environs. The radius of o u t e r limits of i n n e r horizontal surface shall be measured from a reference point or points established fo s u c h purpose. Inner approach surface rectangular portion of approach surface (c) immediately preceding th threshold. The limits of i n n e r a p p r o a c h surface shall comprise: (i)
the intersection of lower edge beginning side of the approach surface with extending down the side inner horizontal surface of th a p p r o a c h surface with inner edge of a p p r o a c h surface runway from there along th strip parallel to length of center line.
u p p e r edge located in the plane of th
(ii)
(d)
Inner transitional surface closer to the runway. Th limits of (i)
inner horizontal surface.
transitional surface surface similar to inner transitional surface shall comprise:
of th inner approach surface lower edge beginning th inner side of th inner approach surface to extending down edge of t h a t surface, from there along the strip parallel to the runway balked landing surface from centerline to th inner edge of th point where he side of th balked anding surface to there side intersects th inner horizont al surface;
u p p e r edge locat ed in the plane of the inner horizontal surface.
(ii)
(e)
Balked landing surface An inclined plane located specified distance after the threshold extending between the inner transitional surface. The limits of the balked anding surface shall comprise: (i)
inner edge h o r i z o n t a l and perpendicular to the centre line of ecified distance after the threshold; located runway
(ii)
tw
(iii)
diverging sides originating inner edge he e n d s of th uniformly specified rate from th vertical plane containing th centre line of the runway; located in the plane of th o u t e r edge arallel to he inner edge inner horizontal surface.
(f) he surface shall be established for a runway meant Take -off climb surface limits of th take-off climb surface shall comprise: for take-off.
62
TH
GAZETIE OF INDIA: EXTRAORDINARY
PART I I - S E C.
3(ii)1
(i)
i n n e r edge horizontal perpendicular to centre line runway located either 'specified distance beyon d runway of th lear wa when such is provided its length exceeds the specified dista
(ii)
divergin ends of i n n e r edge tw sides originating specified rate from take-off to cified final width uniformly continuing thereafter at that width for remainder of take-off climb surface; length of 1
(iii) ;"
(g) ,
erod rome
(h)
perpendi c u l a r to
o u t e r edge horizontal track. evation
highest- point
elevation
Aerodrome Reference Point
specified
- o f f
landing area
geographical location of
designed
Aerodrome.
(i)
Threshold- T h e b e g i n n i n g of that portion of
U)
Displaced Threshold-
(k)
:'
I
,
threshold-
r u n w a y usable Tor landin g'.
located a t t h e
xtremity of
L
runway
An object of low m a s t designed to break, distort Frangible Object minimum hazard to aircraft. I impact to present
yield /.
,
mobile objects, Obstacle- All fixed(whether temporary or permanent) p a r t s hereof, that located on an area intended for surface movement or aircraft defined surface (indicated in Annexure IV) intended to that extend above , protect aircraft in-flight. (1)
(m)
airspace Obstacle Free Zone (OFZ)ve balked landing surface inner transitional surfaces bounded these surfaces', which is not penetratec t h a n low m a s t frangible mounted one, required for
(n}
defined rectangular area Runway landing take off aircraft. I
inner approach surface, t h a t portion of strip fi obstacle o t h e r purposes ir navigati I,
"
land aerodrome prepared for th
(0) Runway ) area symmetrical a b o u t th extended Safety Area adjacent to strip primaril runway cent erline of ended to reduce risk of damage to overrunnin runway. oplane undershooting "j
I
(p) Runway Strip
intended .:-
he ri , To To protect (ii) (i)
defined area included th
r u n w a y a n d s t o p - w a y , if provided, I,
damage a i r c r ~ f t r u n n i n g off flyin over it during a k
runway;
in
I'
[mrr I
I
-
~
63
~ ( i i ) ]
R U N W A Y STRIP
DIMENSION ..
Code
Length
No.
(Meter)
Width Extending laterally either side of Runway .Centre Line
(Meter)
1. 2.
(q)
<800
Length beyond Runway End'; Stopway
(Meter)
Length beyond Runway
30
30
75
60
(Meter)
I
75
800 <120
4
1200<1800 1800 above
Clea
y
control which
Width Extending laterally either side of Runway CentreLine
6.0
15 15
End/ Stopway (Meter)
60
defin ed rectangular a r e ~ on the ound: or water u n d e r appropriate authority selected Of prepared suitable area over aeroplane make portion of it initialclimb to specified height. t
I
'
.
(f)
Stopway defined rectangular area on the ground suitable area in which available prepared aircraft
anabandoned. take..:6ff.
(s) Take-Off R
~ n w a y
j w a y i n t e n d e
of take off be stopped in case of
to take-offonly.
,
(t) Obstacle Clearance Altitude/Height (OCA/H) - Th lowest altitude or .lowest height above relevant runway threshold or aerodrome elevation of elevation applicable used in establishing compliance with appropriate clearance criteria, II
-
(u)
Declare (i)
I
Dista n: ces:-,. ;:t e Off Available (TORA) : - T h e length of declared ae:roplan,e taking pf av ailable suitable for theground of I
(ii) ..
Take Of Distance Available (TODA):he length 'of take-off clearway, if provided available plus the length
I.
(iii) ,
Accelerate Stop Distance Available (ASDA):- he length of take-off available plus length of stopway, if provided. If
(iv) I,.
Landing Distance Available (LDA):- Th suitable for available ground
length of runway declared aeroplane landing
a r e a of defined dimensions about localizer (V Criti dal Area- Critical area is glide p a t h a n t e n n a where vehicles including aircraft excluded during I n s t r u m e n t Landing System (ILS) operations'. he critical area is protected because presence of vehicles a n d / aircraft inside its b o u n d a r y will cause I n s t r u m e n t Landing System (ILS) signal unacceptable discrepancies to space.
THE GAZETfE OF INDIA:
64
LIST OF
S. NO.
AIRPORT
STATE
ANNEXURE-III-A AAI OPERAT IONAL AERODROMES COORD.
ELEV. (IN MTRS.)
RUNWAY ORIENTA TION
DIMENSION (IN MTRS.)
OWNER
235326N 911421E 104926 072!037E
1403
18/36
2286X45
AAI
04122
1204 x
AAI
230414.4N 0723737.3
57.44
05123
3505 x 45
AAI
204152N 0770332E 314216N 0744811E
305
10128
1219 x 45
AAI
16/34
3289 x 45
AAI
582
09/27
2286 x 45
887
04/22
1829 x 45
AAI
759
08/26
1830 x 45
AAI
13
07125
1920x45
523
2/30
LAT/
LONG (IN DEGREES) 1
AGARTALA
TRJPURA
2
AGATTI
LAKSHWADEEP ISLANDS (U.T.) GUJARAT
AHEMDABAD (SVBPI AIRPORT)
7
9 10
II
12 13
AKOLA
MAHARASHTRA
AMRlTSAR (RAJA SANSI) AURANGABAD CHIK.AL THANA) BARAPANI 'SHILLONG BELGAUM (SAMBRA) BHAVNAGAR
PUNJAB
BHOPAL RAJA BHOJ AIRPORT BHUBNESHWAR (BIJU PATNAIK AIRPORT) CHENNAI
14
COIMBATORE (PEELAMEDU) COOCH BEHAR
15
CUDDAPAH
16
17 18 19 20
DELHIIGI AIRPORT (PALAM)
MAHARASHTRA EGHALAYA K{\RNATAKA GUJARAT MADHYA PRADESH RISSA
215941.7N 0801031.8E
15.84
TAMIL NADU
1I0149N 0770230E
404
WEST BENGAL
261949N 0892815E
41.5
ANDRA PRADESH DELHI
1431N 07847E
ASSAM
UWAHATI (LGBI AIRPORT)
283407.42N 0770643.69E
2045
AAI
45 AAI
TAMIL NADU
DIBRUGARH (MOHANBARI) DIMAPUR
231711N 0772017.4
44.5
UTTARAKHAND
".
195152N 0752351E 254210N 0915152E 155127N 0743707E 214513N 0721128E
229.5
201448N 0854906E
DEHRADUN (JOLLYGRANT)
[PART n - 8 E C . 3(ii))
EXTRAORDINARY
/4/32
2243
1381 x 45
AAI
07/25 12/30
3658 X 45 2032 X 45
AAI
OS /23
OS/23
45
AAI
04/22
2290 x 45 1069 x 30
AAI
131
11/29
\098 x 18
AAI
227
10/28 09/27
3RIOx45 2813 x 45 42RO x 60 40 x 45
DIAL
11129
.IV
AAI
301125N 07RI054E 272851.7N 0950104.%
550
OR/26
110
OS/2J
NAGALAND
255258N 093462RE
144
12/30
2290 x 45
1\1\1
ASSAM
260617.RN 913507.7E
49.21
02120
2743 x 45
1\1\1
IR29x 45
II\F
21
GAYA
BIHAR
244451N 084564I
110
0128
22R6 45
1\1\1
22
HUBLI
KI\ RNI\TAKA
1521 39N 0750508E
659
08126
1674 x 30
1\1\1
23
HYDERABAD (BEGUMPET)
I72709N 0782750E
531
09/27
3103x45
1\1\1
24
IMPHAL (TULIHAL)
ANDRA PRI\DESH MI\NIPUR
244549N 0935411E
774.2
04/22
2746 x 45
1\1\1
'qf'T
25
26
I
1
-
~
3(ii) ]
INDORE DEVI AI-liLYABAI HOLKAR AIRPORT JABALPUR
65 224321.9N 0754823 .4
560.8
07125
2750 x 45
AAI
PRADESH MADHYA PRADESH
231058N 0800343E
495
06/24
1988x45
AAI
264926N 0754812E 215451N 0840303E 190548N 0725004E
385
9/27
2797 x 45
AAI
228
06/24
1882x45
AAI
51
727 x 45 1143 x 30 1372 x 45
AAI
211852N 701610E 230642N 0700605E 320954N 0761542E 2626 25N 0802153E 449 ION 0795512E 110817N
16/34 08/26 OS/23
29
OS/23
1524 x 30
AAI
759.6
15/33
1372 x 45
AAI
125
10128
1082 x 45
AAI
217.4
0 11 9
1829
45
AAI
104
10/28
2860 x 45
AAI
606.5
07125
1372 x 45
AAI
0lRl19L
36 27 x 46 2399 x 46
AAI
MADHYA
27
JAIPUR (SANGANER)
RAJASTHAN
28
JHARSUGUDA
ORISSA
29
MUMBA1 (JUHU)
MAHARASHTRA
30
KESHOD
GUJARAT
31
KANDLA
GUJARAT
32
GAG GAL (KANGRA)
HIMACHAL
33
KANPUR (CIVIL)
PRADESH UTTAR
PRADESH 34 35
KHAJURAHO
MADHYA
CALlCUT
PRADESH KERALA
(KOZHlKODE) KOLHAPUR
MAHARASHTRA
163955N 0741729E
37
KOLKATA (NSCBI AIRPORT)
WEST BENGAL
22391 I. ON 0882657.25
KULLU-MANALl (BHUNTAR)
HIMACHAL
NORTH
ASSAM
39
LAKHIMPUR
LU CKNOW
0lUI9R
1088.8
16/34
1128
30
AAI
100
04122
2286 x 45
AAI
122
09127
2742 x 45
AAI
305120N 0755706E
ti4
12/30
1463 x 30
AAI
315237N 0770919E 271726N 0940549£
(LlLABARI) 40
AAI
075570lE
36
38
.74
264543N
41
LUDHIANA
UTTAR PRADESH PUNJAB
42
MADURAI
TAMILNADU
09500lN
136
09127
1-826
x 45
AA!
KARNATAKA
0780522E 125743N 0745323.9E
102.6
09127
1625 x 45 2450 x 45
AAI
09/27 14/32
3489 x 45
MIAL
2925 x 45
JV
OS/23 09/27 14/32
AAI
09127
348 x 45 1740x30 3200 x 45 1957 x 45
10/28
1097 x 8.4
AAI
51.18
07125
1954 x 45
AAI
5.18
09/27
1372 x 45
AAI
313
06/24
1955 x 45
AAI
45
OS/23
1750 x 45
AAI
OS/2
1846 x 45
AAI
2713
AAI
(AMOUSn
43
MANGALORE
(BAJPE) 44 45 46
MUMBAI (CSI AIRPORT) MYSORE NAGPUR
MAHARASHTRA
KARNATAKA MAHARASHTRA
SONEGAON) 47 48 49 50
PANTNAGAR PATNA PORBANDAR RAIPUR (MANA)
UTTARAKHAND
BIHAR GUJARAT
CHATTISGARH
080530lE
06/24
190527N 0725200E 121345N 0763930E 210528N 0790259E 290156N 0792827E 253537N 0850531E 13859N 0693932E 211049N 0814425E 170630N 0814916E
716 308.45 23
51
RAJAHMUNDARY
ANDHRA PRADESH
52
RAJKOT
GUJARAT
221834N 0704645E
133.4
53
RANCH! (BIRSA MUNDA AIRPORT)
JHARKHAND
231851N 0851915E
646
175 GI/10-9
3/31
.,
45
MIHAN
JV
66
T I l E GAZETTE OF INDIA : EXTRAORDINARY
54
SALEM
TAMILNADU
55 56
SHIMLA (JUBBARHATTl) SHOLAPUR
HIMACHAL PRADESH MAHARASHTRA
57
SURAT
GUJARAT
58
TIRUPATHI
59
TIRUCHIRAPALL! (TRlCHY)
ANDHRA PRADESH TAMILNADU
60 ...
61 62
63 64
104557N
3(ii»)
300
04/22
1829 x 45
AAI
1540
14/32
1189 x 23
AAI
481
15/33
1365 x 45
AAI
04/22
2250 x 45
AAI
106.75
08/26
2286 x 45
AAI
85
09127
1864 x 45
AAI
14/32
AAi
10128
3398 x 45 1224 x 45
0784253E
THlRUVANANTHA ·PURAM
KERALA
TUTICORIN (TOOTHKUDI) UDAIPUR (MAi'IARANA PRATAP AIRPORT) VADODARA
TAMILNADU RAJASTHAN
VARANASI (BABATPUR) VlJAYAWADA
65
1I4647N 0780355E 310454N 0770407E 173735N 0755606E 210647N 0724435E 133759N 0793230E
IPART I I - S E c .
GUJARAT .P. ANDHRA PRADESH
082847N 0765511E 084317N 0780140E 243702N 0735343E
25.6
10/28
1350 x 30
AAI
509
08/26
2281 x 45
AAI
221946N 0731310E 252703N 0825138E 16)135N 0804754E
37
04122
2469 x 45
AAI
80
09127
2206 x 45
AAI
21
08/26
1745 x 45
AAI
STATE GOVERNMENT OWNED OPERATIO NAL AIRPORTS S. NO.
AIRPORT
STATE
COORD. LAT/
AIZAWL (LENGPUl) DIU
UNION TERRITORY
LONG. (IN DEGREES) 235016.88N 0923736.38E 204247N 0705514E
ELEV. (IN MTRS.)
RUNWAY ORIENTA TION
DIMENSIO N (IN MTRS.)
4.9
OS/23
1826 x 45 1069x25
U.T.
13/31
RUNWAY ORIENTA TION,
D1MENSIO N (IN MTRS.)
OWNER
.68
09127
3400 x 45
PVT
617
09/27
4260x60
PVT
OWNER
PRIVATE AIRPORTS S. NO.
AIRPORT
3
COORD. LAT/
COCI-IIN
2
STATE
INTERNATIONAL AIRPORT LTD( CIAL) HYDERABAD INTERNATIONAL AIRPORT(HIAL) SHAMSABAD BENGALURU INTERNATIONAL AIRPORT (BIAL) DEVANHALLJ
KERALA
ANDHRA PRADESH
171426N 0782544E
KARNATAKA
J31155.92N 774219.70E
5
VIDYANAGAR
ANDHRA PRADESH KARNATAKA
6
MUNDRA
GUJARAT
JAMSHEDPUR
./HARKHAND
PUTTAPARTHY
LONG. (IN DEGREES) 100914N 0762425E
1409N 07748E 151019N 0763837 225003N 0694552E 2249N 08610E
ELEV. (IN MTRS.)
JV
914,68
isrn
4000x45
PVT JV
475
09127
2237x45
PVT
502
13131
1600x 30
PVT
.18
OS/23
1700x30
PVT
141.7
08/26
1220x 45
PVT.
'm'T I
I
-
~
67
3(ii)]
ANNEXURE-BIB LIST OF AERODROMES CONTROLLED BY AAI NO
AIRPORT
STATE
AIZAWL (TURIAL)
MIZORAM
ASANSOL
EST BENGAL
BALURGHAT
WEST BENGAL
BEHALA
WEST BENGAL
23022N 0881748E
BILASPUR
CHATIISGARH
20000N 0820400E 222736N 0864237E 241604N 0721218 1550N 7930E 2131N 08020E
HAKULlA DEESA (PALANPUR)
JHARKHAND GUJARAT
DONAKONDA
ANDHRA PRADESH
GONDIA
MAHARASHTRA
10
JHANSI
UTIAR PRADESH
II
JHARSUGUDA
ORiSSA
12
JOGBANI
BIHAR
13
KAILASHAHAR
TRlPURA
14
KAMALPUR
TRIPURA
15
KHANDWA
16
KHOWAI
MADHYA PRADESH TRIPURA
17
K1SHANGARH
18
KOTA
RAJASTHAN
19
LALITPUR
20
MALDA
MADHYA PRADESH WEST BENGAL
21
MUZZAFARPUR
BIHAR
NADIRGUL
ANDRA PRADESH
.PANNA
MADHYA PRADESH
22 23 24
COORD. LAT LONG. (IN DEGREES) 34443N 0924822E 2340N 08701E 251547N 0884754E
RAJASTHAN
ELEV. (IN MTRS.)
RUN\VAY ORIENTA TION
DIMENSIO N (IN MTRS.)
OWNER
34
01/19
1190x27
AAI
98
10/28
1826 x
AAI
24
09127
1097x30
AAI
18/36
861
AAI
1448X45 1455X45 2221X45
AAI
129
06/24 17/35 17/35
145
06/24
1008 x3
AAI
14
04123
311.1
274
30
AAI
915X30
AAI
05123
1966
AAI
244
15/3
1295 x 45
2155N 08403E 2618N 8718E 241828N 920033E 240754N 091485 IE 215125N 761959E 240342N 913627E
228
06/24
1890X45
AAI (UNDER ARMY) AAI
09/27
1525X 152
AAI
24
03/21
900X30
AAI
39
01/1
1372 x 30
AAI
329
10/28
890X30
AAI
29
18/36
915X30
AAI
2636N 07449E
480
03121
1219 x 30
AAI
250935N 0755056E 244258N 0782503E 50040N 880750E
273
08/26
1220
AAI
367
10128
1890 45
24
11 /29
1099X30
AAI
53
11
/29
1219 x 30
AAI
2529N 07834E
6070lN 0851854E
45
38
IN 07833E 243915N 810546E
552
14/32
914 x 23
AAJ
424
17/35
1538XI8
AAI
2806N 9523E
157
17/35
1006XI8
AAI
115759N 0794843E
43
07125
1222 x 30
AAI
10/28
1097X30
AAI
40
OS/23
1829X45
AAI
212'
12/30
1180 x 45
AAI
171
PASSIGHAT
ARUNACHAL PRADESH
25
PONDICHERRY
PONDICHERRY
26
RAXAUL
BIHAR
2658N 8450E
27
RUPSI
ASSAM
2608N 8945E
28
DELI'll (SAFDARJUNG)
DELHI
283504N
68
TH
29
SATNA
30
VELLORE
31
WARANGAL
GAZETTE OF INDIA: EXTRAORDINARY
-
WART
MADHYA PRADESH TAMIL NADU
243345N 0805116E
319
11/29
125424N 0790406E
233
ANDHRA PRADESH
175452N 0793608E
284
II- S e c . 3(ii)J
1062X30
AAI
07/25
793 x
AAI
09/27
1859 x 45
ISO
AAI
ANNEXURE - I I I e LIST OF DEFENCE AERODROMES S. NO.
AIRPORT
AGRA
STATE
A
Y
DIMENSION (IN MTRS .)
OWNER
IAF
97.2
12/30
2477X45
JAF
281035N 0944824E 264108N 0881948E 125703N 0773957E 23J713N 0694015
250
05/23
914 x 45
IAF
126
18/36
2744 x 4
IAF
888
09/27
3306 x 45
HAL
78
05/23
2515 x 45
IAF
2804I8N 0731225E 3040N 07647E 2800N 09411E 152247.4IN 0734940.05E 264429N 0832709E ,' 261730N 0781341E 653N 07052E 234l 32N 0745024E
215
05/23
274 x 45
IAF
314
11/29
2744 x 45
IAF
244
07125
1001
x 27
IAF
46
08/26
3430 x 45
NAVY
78
11/29
2744 x 45
IAF
188
06124
2744 x 45
IAF
236
04/22
2744 x 45
IAF
291
18/36
2042 x 45
IAF/CE
26125N 0730308E 2644N 09411E 2624N 08025E 3408N 07733E 2007N 07355£ 2 1402N 0753802E 1138549N 0924406E
217
05/23
2743 x 45
IAF
91
04/22
2652
45
IAF
124
09127
2744 x 45
IAF
3256
07125
2922 x 45
IAF
598
09/27
000 x 45
tAF
312
01/19
2744 x 45
IAF
04122
3414x45
INDIAN NAVY
BAGDOGRA (SILIGURI) BENGLURU (HAL)
WEST BENGAL
GUJARAT
7
BHUJ (RUDRAMATA) BIKANER (NAL)
8
CHANDIGARH
UNION TERRITORY
DAPARlJO
ARUNACHAL PRADESH OA
KARNATAKA
RAJASTHAN
UTTAR PRADESH MADHYA PRADESH
12
GWALIOR
13
JAISALMER
14
JAMMU
IS
JODHPUR
RAJASTHAN
16
JORHAT
ASSAM
17 18
KANPUR (CHAKERI) LEH
UTTAR PRADESH J&K
19
OZAR (NASIK)
MAHARASHTRA
0
PATHANKOT
PUNJAB
PORT BLAIR (VEER SAVARKAR AIRPORT) PUNE (LOHEGAON)
ANDAMAN ISLAND
ASSAM
24
SILCHAR (KHUMBIGRAM) SRINAGAR
J&K
25
TEZPUR
ASSAM
26
VISHAKAPATNAM
ANDHRA PRAQESH
23
W
2744X45
ARUNACHAL PRADESH
22
N
05/23
ALONG
21
~
ORIENTA TION
167.7
3
GORAKHPUR
R
MTRS.)
270932N 775730E 252626N 814409E
ALLAHABAD
GOA (DABOLlM)
ELEV. (IN
UTTAR PRADESH UTTAR PRADESH
2
10
COORD. LAT LONG. (IN DEGREES)
RAJASTHAN
MAI-IARASHTRA
183458N 0735513E 45448N 0925851E 3359N 07447E 2643N 09247E 174316N 0831329E
592
IAF
10/28
2535 x4
06/24
1785 45
IAF
13/31
3658 x 45
JAF
70
05/23
2744
IAF
3
05/23
1829x 45 3048 x 45
103 1656.5
10/28
45
NAVY
69
3(ii) ]
'qpT
Annexure III D
S t a n d a l o n e Aeronautical C o m m u n i c a t i o n S t a t i o n s
S. No.
Station
1.
Aligarh
Behrampur Bellary
of the Facility
CVORjDME(HP)
Coord N (WGS 84
DVORjDME(HP) DVO Rj DME(HP
Bikaner
DVO
Coord E ( W G S 84
2 7 4 9 ' 45.5"
19
MSSR
Bikaner- Lunka
Lunka
Coordinates
Name
~ 0 0 "
1509'54.4"
;84"
42
8 4 5 2 ' 08
7 6 5 2 ' 50 77 47' 15 .61"
7406'
DME(HP)
Chillarki
CVORjDME(HP)
20.422" 28 20"51.2"
Gulbarga
DVORjDME(HP)
17 18' 48.8"
Jalalabad
CVORjDME(HP)
2 7 4 1 ' 39.6
7 9 4 2 ' 44.7"
NDB
2153' 47.6
19.5"
DVORjDME(HP)
12
arsuguda
41.267" 7 6 3 9 ' 20.2"
48'11"
10
Kanchipuram
11
Katihar
NDB
34'1.7"
12
Keshod
NDB
2118'53"
7016' 10
13
Khammam
NDB
17
8 0 0 8 ' ,15"
14
Kishanganj
NDB
2606'
15
Pratapgarh
DVORjDME(HP)
16
Rajamuridri
NDB
17
Sakras
18 19
21
Sikndrabad
5.1"
45
7 9 4 2 ' 44.7" 8733' 20.6"
5"
87 56' 30.3"
13.65"
7 4 4 4 ' 38.16"
1706'31"
81
18"
CVORjDME(HP)
2 7 5 0 ' 54.4"
7 7 0 0 ' 29.6
CVORjDME(HPj
ILl"
7 6 4 9 ' 9.6"
CVORjDME(HP)
2 8 2 3 ' 36.2" 2.5':
Songarh
NDB
Tuticorin
NDB
0 8 4 3 32.2"
Vikarabad
NDB
1 7 2 0 ' 3.8"
21
7 7 4 2 ' 29.2" 73 33' 57.4"
7801'
.5" .5"
THE GAZETTE OF INDIA:
70
JPART
EXTRAORDINARY
II-SE C. 3(ii»)
Annexure JIJ
aerodromes fo
List
which Governmentltas given "in-principle" approval ......
for
settfnz
aerodrames Elevati-
ocation
S.
S t a t e l Union
am
No.
Territory
atitude (North)
Madhy
Dabra
49' 42 .8"N
Pradesh
Navi
2,
on
ah ar sh
Mumbai
18°59
ik im
Pakyon
27 °1 3'
est Bengal
Durgapur
,.
58. 2691N
37' .... ..
33" N
7.7" N
ongitud} (East)
78
(feet)
,t,
' 1.7/'
07 °04' 18"E °35'
Meters
.7927
°14' 32 .5"E
Dimen-
/w
Directi-
on
sions Meters
(feet)
240
R09/27
3000x45
5.00
R08/26
700x60
1321.27
R02/20
1700x30
85
R16/34
33 15x45
..
..
... ./
,-
0.) . <..,.i ~.
":.-""" ;:...
:'J C!
"\.,':r -' ro
Ii:::
...;:;1
I .\
-,
.. ())
..
..
(!)
(l) 1 , - : ~ ~
(lJ
c:: Ii
0.
cr:: . ~ ~ . - . _
..
rv ,..,
c;
If
['l1lTf 1I-<9US 3(ii)] Appendix A-2
--
,.---------
-----
----
---.
----
OUTE CONICAL UTER TRA NSITIO AL OUTE
HORI ZANT AL SURFACE From Rw rom Rw
xtremi ty
trip
48
- - - -
-
-
-
,._ -
----
--
-
---{
-
-
-
-
-
-otfTER -eON E:At- - , 1 - --,-- ---,- -,
/
-
-
---,-,--
-
.
...
-
.
_
-
-
"f'lt:..
_
-
-
-.--.-
-
-
-
-
-
-
-
'
-
-
-
-
-
-
72
TH
GAZ ETI'E
INDIA : EXTRAORDINARY
AR
I 1 - 8 Ec. 3(ii»)
AppcndixB
-- --
loje ==o.O) m/mtr ..
..
.....
..J
00
Fig 1
Criteria
for height restriction with re spect to
Beyond Point ll obstructions having azimuth w i d t h less than degree .4 Antenna RADAR can be permitted line this above Subjected other ondi in para .5 restrictions ( r o m AG &. PAN-OPS
mT
I
I
-
~
73
3(ii)]
ppendixC
A
Angle ~ i 1 t angle of the antenna or 0.5 degree whichever is higher
5m lo Je=o .o:;
/m tr
Beyond Point ll obstructions having a z i m u t h w i d t h less than degree ON RADAR A n t e n n a ca be p e r m i t t e d above this line s u b j e c t e d o t h e r conditions para in from restrictions AG &. PA -OPS
------(0
..
00
ig
175 GI/10
Criteria for height restriction with respect to ARSR
GAZETTE OF INDIA: EXTRAORDINARY
TH
74
.\
cr.:
0'::
;J;l
?.
--
Cl
...
,-
&:
Ul
f\)
ro
-,....
..:\
2:
,...;.
- :>
(Y')
2:
,,
'/
r.i
,
2:-
·J
[ mrr II
3(ii) ] Ap endix
r I I
I CONI Al
I I
I
I !
I INNER HORiZQl\lTAL SURFACE
Coward' N i i W A ~
l l h l ~ n
.... 1.iw
Iop,
Bldg roviding shielding
CONICAL UR ACE
INNER f-IORIZONTAl SURFACE
U ~ ! F A C E
76
THEGAZETIE
OF INDIA: EXTRAOR[)INARY
[Pxn'r
II-SEC.
Appendix
Diagrams of Obstacle limitation Surfaces, ILS Critical Areas and Shielding Benefits
Approach
s « t ( ~ A - A
Transitional
Sectlon B-B
J(ii)1
['qfTf I
I
-
~
77
3(ii)]
AppendIx I"-:l
I
.. .;
Balked landing
Inner approach Inner transiUonal
Section A-A
" W ~ ' ~ andJng
Section
B-B
Inner approach inner transitional and balked landing obstacle limitation surfaces
-l
IX>
II
OBSTACLE LIMITATION SURFACES Note . - T h e figure shows the obstacle limitation surfaces at an aerodrom with two unways, an instrumentrunway and a non-instrum ent runway Both are also take-off runways . -l
::t
3 "'l
t::'
:>
<,
8(00
Ho,iloolal
plion
<,
:>
"0
lii Co ..
7l Vol
-e
...
- ;ll
..,
Vi t'
("l
::
ol
:::::
.......
l..> -=:
.::;;
'"
Critical Area ..
300m or near en
f the
L-I
of LLZ
wy whichever Is tt>e
reater
..
Runway
1111
20
. ":::I ":::I r:>
:l
Co
,.
'L:
-J
'I:J
