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1. 3T-1-Kr 14 URTI tic16 ITT 3TTUTfl ACTT :

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(35F ITT4*NuT-ta)

3771=1 * T.f-45rr

1

(2)

2

(3)

60 RIO 80 4-WO

30 1 0 60 "1:0

10% 10%

380 580 H10

1600 RIO 2500 140

3tfr4

(4)

180 TO

60 1 );)

12.05%

12-0-1-30

1800 1#0 **

15000 TO

2% 6c11-1 5% 4%

3-Truirql cr1 ITrcrl—Acr)K s3i ► d`l #

** 1800 RIO Ji 3T15It-qc1 34.--d-ta. Tiff -4 . fcnu Try

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1.2 •(-1c16 (1i ti)

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- 14.3% (1:7)

(ii) EfrojT, - 14.3% (1 :7) -fg 3 AT 4 fcTl

- 20% (1:5) -Yg- 13T 2

(iii) Jucr) ,<uf arm TT4 - 14.3% (1:7) 3 311-T 4 4) e'cll!.

- 20%(1:5)132

10 THE GAZETTE OF INDIA : EXTRAORDINARY

I PART II—SEC. 3001

1.2.2 tictsliul ‘`-1(16 acifri A ITig trra-- . a cii$4 ul ITT IttirraiT 14 YILIt I

1.2.3 3^-K4-1 f•-1 1-.1 -cri4 6

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(41cA) #0 ( 4:1)6'()

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(4-1)c.‹) .&-d1 GC11 ,-1 --dt ZaT4

(41 c) (ii rA) 1. <800 3000 12000 ** 2500

2.5% 3% 3.33%

2. 800 < 1200 3000 12000** 2500 2.5% 3.33% 3.33%

3. 1200 < 1800 3000 3600 3000 3600 8400 *

2% 2.5% 2% 2.5%

4. 1800 3R 3000 3600 3000 3600 8400* ,314.t 2% 2.5% 2% 2.5%

* mis 'it 3 3t 4 (trf 311-T mu Tiffe. A&-al 15000 *0 04111 ** tir7/1 cols T01 311T 2 TraT A T-7 15000 RIO g),IW I

1 .3.1 .2 itT-d4arcuf 'UM R-4a

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3 3ft 4 rciu

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1.3

[mr II-111ur 3(11)]

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wr-i-aft

-4a WO • -

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(Wfi) * 3TIT 10% tici-f)

*o s -drf (ifta) itaIR 601.4

1. <800 1600 5%

2. 800 < 1200 2500 4% 3. 1200< 1800 3000 3.33%

4. 3000 2.5% 1800 3h .3.)LK

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1T2T RTRT Pcit0-11-1 A qz-a/ ,< f501„5, erTrr mir

TT-Krf . 4 -RI' co44 i-rr 34-0-Ti -&Trri

1.3.1.6 ti504, t9'k 5T .3-10-1/ fd-MTRFJ eltigcs/ q- Frr-dT f-d-R?i-R-, 140 Tra-g Pciu 3T1 TTl I

1.3.1.7 to 5 Gcli-f A 1111:1 di) I *- 347141Zj5 1-tclfcoR t

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`111(1) erciof '1(-1E; cbl 3771173 3'IrT 39tT 31 -cq

AT-614cfrtuf itictr,tuf

Plac41

(4)CA)

5 R:NXIT elsili sqf

(TW) (4)o•c) cA) 1. <800 3500 * 45 2000* 45

2. 800 < 1200 3500 * 45 2500 * 45

3. 1200< 1800 4000** 45 4000** 45 4. 4000** 45 4000* * 45 1800 3th- ilt-R

12

THE GAZETTE OF INDIA: EXTRAORDINARY IPART II—Sec. 3(ii)J

* frii* lug UERIOTT*-0#kiiic **.zw.1

** Tarr R--4 *Eh* wrut

1.4.1.1"1-1WfT3T ¶U tiO4 aTTUTT VT 34f 3173- 9r -III Pitz- t--)I.1

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era 3traTi t9) a-)7 fW-e•-• T;41-TT TdITT 31-1M-R- (34-11-)

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5c11 -3T-0 cr;) rr fi t1415iracr) <)L4 t ,711-1Iurm

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(i-ficA) Th-Ti" *R-16 d;c11 (i.11) ( 6.)

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2000

2000

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60

100

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1200 60 700 35

2. 800 < 1200 1200 60 1100 55

3. 1200 < 1800 1500 75 1500 75

4. 1800 31 -T 2000 100 2000 100

['ITT 11-13133' 3(ii)

$ ,<-1 3Tf r ii 3T d - III 14fit flU YTTR- icrci ► cb ► vc #01 tzTT -raTTR4-1-

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1.6 1.-ge Oft tici6

1.6.1 fa d-) R--q4 fit 3 30 4 t ar r ar-ffY (3fr Q.ti) fa (tr

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3TOZ:f S;r4 51ift I

1.6.7 3-1TratT T1 7:121Tf'cir gC 4-I TER-Vp4 u I

1.7 Iftue tritaal .aruRpr Agir *106 (3TI ucu *6)

1 . 7 1 uci)- rot! 94* II 3#Z III cltilc1-1) 3T-dft .311R i2TttiTcf situ 154*

11 3T2T-d-r III ATTIciR a-) fffti Gni 37;i=n-r fir Judi g (-11 311 Ch) fd4-11-1

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1.7.2 3T1 U 1-t) (UTUT 11c1-cI 43) (cr))g 3 34 4) d 3TgT14 30 6c11-I eirlr.) F6,1! flU

12.13-1u11 *0 1 3k 2 31 U1W 2.1TfZr-a Rff f)u WA #1

1.7.2.1 lituft

60

14

1 ilE GAZETTE OF INDIA : EXTRAORDINARY I P %Ft r II—SEc. 3(0

900 4-1)(!7

FT7 .7%

1.7.2.2ftt rifitaff

6r1ki 33.3%

1.7.2.3 sticetzsg Ag-IT titie

1-Wr TO A 120 4-71c.‹

3T< 180 -44‘Tc;

10%

6c11-i 3.33%

1.8 T.104 Eqz tr 20 f---0 1:ThU "5",t tre0 tzTr 3-Trtith 150 1:11-dT t 3; r.4 ark et 31 ft f i T&PT cr-J:rruT-u ci-).<- 3*fraT 614I I

2. 3977-4W 10 tT WM-TRU (PdTh7:4ici-f -edur)

2.1 3u-IfM 31317-4t / itzx ,3-TrOM 31 24-41 /3ik

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ct) uT faNIT tf 150 3TT# IcTITTT I

2.3 ri CII*JR

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ct)1 c)ur cla-tf cr)) 'f- TFT

24

1 a! TW fart 1-1 31ft fd-FOuT EMI Ur-6-11 a') Ti#4 of ca-)7 8

f5 41 34T f-07-&3-1, 3TTUTT Li.< 1.1 rthr 31-rtIth cb)ur ch

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2.5 UER . 1.1 ,tsvc .

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[ %;PT II-0rS 3(ii) 1.117-6 tI4141 : 3M1111731"

16

THE GAZETTE OF INDIA : EXTRAORDINARY I PART I I-SEC. 3(01

alf-d-Y?:r cue) 2 r8 4:1) ch)ur r J-1(-111 f aid

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18

THE GAZETTE OF INDIA : EXTRAORDINARY I PART II—Sec. 3001

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3Tait.4-rAtit7r (111 14)

V. c1 I-I t.T1 1:12T gTt4Vrq

(Itz-{ 14) Tdificc

(1,11--d-- 14) f44- Trizr

1 &IR ar--i-Trter4 Td-t th--{ - 1009I4N 7.68 09/27 3400 x 45 I:1A

3t-g-r(Tir3rtarff) 0762425E

2 3T74,1 cra-vr 17 1 426N 617 09/27 4260x60 . ,osii 3T---i-Trtt-4 Tat f:-1,31) JV 0782544E 317T, Ill-MIGII

tn 131155.92N 914.68 09/27 4000x45 47--1- 3T--- Tit-zr Td-t cr)-1 6cr, -IA JV 774219.70E 37-87, a cl-I6cve)

4 1FTiti, [MI 37Kgra-47 1409N 475 09/27 2237x45 f.-1,71) 07748E

5 Th--- 1-6-th 1510I9N 502 13/31 1600 x 30 cMt1T-141'‹ .-f si 0763837E

6 11- 7 41,T1.tIc1 225003N 5.18 05/23 1700x30 1:1,-`11 0694552E

7 74:7117 2249N 08610E 141.7 08/26 1220 x 45 1:101'/ $.11.<q.5u5

.31-0sitE 1 1 1-41

UU31-r- g Kr .1. ..4fct f+-11--ra.W . et 71-dt

0,44 TiO

utRorl-- TT7:1 Tfirli-c1c1 ,

3Taii-7IA-Ul7T

(f%-th #)

12e1 7I--1 t.TTU7:12-1.

f4--d'-- -TTER- glO7F (RE--{ 14)

ZfTF4-icci

( 14)

1 3707. fl&R-1,7 234443N 334 01/19 1190x27 2.L73TT 0924822E

2 3TT ci r-117U7l 611Iie 2340N ()870 1 E 98 10/28 1826 x 45 alyrt

3 *71=r7" 1:1%1:1 4 Ile 25 1 547N 24 09/27 1097x30 uu3T1 0884754E

4 .-.4--414 4411c4 223022N 3 18/36 861 x 30 ut-T34-r 0881748E

5 220000N 274 06/24 1448X45 um-fr- 0820400E 17/35 1455X45

6 LI cl-v“.-11 Si l'C'gt-J5 222736N 129 17/35 2221X45 arari-- 1)864237E

7 aFT(1-11c1--i.t) 241604N- • 145 06/24 1008 x 30 ar3TT ±,31•0-f . 0721218E

8 .\I- TegT 37-4.-Tcfr 1550N 142 04/23 915X30 a-T3IT 7930E

9 Tr-8-4-r 4-161•<1 2131N 08020E 311.16 05/23 1966 x 45 Cj73TT

10 31-41 -3(-K-11 gtVT 244 15/33 1295 x 45 a-334 2529N (371=11 07834E:

3.TtN)

11 3TM=1,4 151 3-a-tr 2I55N 228 06/24 1890X45 0173-1-1 08403E

12 -71 11&1- 1-d- R 261 8N 59 09/27 1 525X 152 1231T 8718E

13 ic1I 7 15.t Ng-Tr 241828N 24 03/21 900X30 ut-T3T11 92()()33E

14 c64-11e1T( --- -r 24()754N . 39 01/19 1372 x 30 a-731-if 0914851E

15 l'scti Titzr Ai--vr . 2I5125N 32A 10/28 890X30 ugylt 761959E

16 4rat f-171 240342N 29

18/36 915X30 CILT3T1t 913627E

17 V"a72.-1H 2636N 480 03/21 1219 x 30 Cfg34 fct)1---Ill6 07449E

[ 1PT H 300

wir17 I gl 4 1 : arPrairn.

27

18 RT-diZTR 250935N 0755056E 244258N 0782503E 2500 ,10N 880750E

273 08/26 1220 x 38 a334-1 co 61

19 TM/ cra-ZT 367 10/28 1890 x 45 tr731-1 cl riciT‹

20 . 24 11/29 I 099X30 ai34 HMI `4d1:1 GIII1c1

21 1 3141Y9't (.116K 260701N 0851854E

171IN 07833E

243915N 810546E

53 11/29 1219 x 30 L31-1

22 31W1 552 14/32 914 x 23 LIT34 -II ±1c1

23 ttT 7.7;ravr 424 17/35 1538X18 aryrt

24 2806N 9523E

157 17/35 1006X 18 aryl Intl tiit 3Th-urr41 lial

tiiiYar 25 trif-g4- I I 5759N 0794843E

43 07/25 1222 x 30 ugarl

26 2658N , 8450E

79 10/28 1097X30 mut ,ticr\qici 616K

27 311W11:1 2608N 8945E

40 05/23 1829X45 unit V4t1

28 irri (til-6.3111) ----—cr1 283504N 0771229E

212 12/30 1180 x 45 1re3rr

29 1:ftlfLAT 243345N 0805116E

319 11/29 1062X30 , 27311 '<ichli

30 Rird9-1-4 125424N 0790406E

233 07/25 793 x 150 ggarr ckt

31 31Tg-a-vr 175452N 0793608E

284 09/27 1859 x 45 UCT311 clkl1e1

,jqlT - IIt 11<4 1-111-14(71-11 tIlti)

Mg it 04-II-Ncri-f il&21 +Pi cf,

. 3TeitTA47T (fg-th -11)

al • •

(111U 4) EirdRIT4

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(41c.< 4)

1. 3TI1TK1 soot ri-avf 270932N 167.7 05/23 2744X45 34 7 EAT

775730E 2. $eivelia Jai.< cra-Vf 252626N 97.2 12/30 2477X45 34.1 7 7tF

814409E 3. ticiiir 31'UIItJC19T 281035N 250 05/23 914 x 45 3Trf u ucff

0944824E . aTrrtiriT ' T45-47 thrrff 264108N 126 18/36 2744 x 45 31Tt 7 7r5

(ffr&ge) 0.-isccr)

0881948E 5. 125703N 888 09/27 3306 x 45 4,,,r

(QV U wg) 0773957E

. IF ±Isifld 231713N 78 05/23 2515 x 45 34 U0:5

(tviiiir) 06940 15E 7. RTYR,21R 280418N 215 05/23 2746 x 45 3Trf U Uch. *Thik(-

(27 2 2ff) 0731225E 8. wan •"-&. flf-+Td. sfa71 3040N 314 11/29 2744 x 45 311 U um

07647E 9. 31Tffff ga-VI 2800N 244 07/25 1001 x 27 3T1 u acff aqK syt

09411 E 10. Ji of n cif 152247.41N7t-- 46 08/26 3430 x 45 td1

(so)reTg) 0734940.05E 11. 1 ,(xgv. Rcii II 264429N 78 11/29 2744 x 45 3T g [scu

0832709E 12. 4 Cii MK 4W T1 . 261730N 188 06/24 2744 x 45 3T1 .7 71:6-

0781341E 13. Aird*-{ TIM-MR 2653N 236 04/22 2744 x 45 31T 7 7W

07052E 14. i4-1 51711, 74 Cb-T 234132N 291 18/36 2042 x 45 3T u

0745024E 14Locii/ t

Adz 15.

22. 11c.N11<.

23. Filc•

24. o114k (t)I:1111.).

341•7..1 SIC;RI

25.

26.

IPART 11-SEC. 3001 28 THE GAZETTE OF INDIA : EXTRAORDINARY

26125N 0730308E 2644N 09411E 2624N 08025E 3408N 07733E 2007N 07355E 321402N 0753802 E 1138549N 0924406E

183458N 0735513E 245448N (1925851E 3359N 07447 E 2643N 09247 E 174316N 0831329E

217 05/23 2743 x 45 3T1 U TT

91 04/22 2652 x 45 um

124 09/27 2744 x 45 7 M

1256 07/25 2922 x 45 7 PLE

598 09/27 3000 x 45 u m

312 01/19 2744 x 45

5 04/22 3414 x 45

592 10/28 2535 x 45

3Trt7 LTEff

103 06/24 1785 x 45 7 Q4)

656.5 13/31 3658 x 45 u t_to

70 05/23 2744 x 45 u ut-t-)

3 05/23 1829 x 45 • 10/28 3048 x 45

3tTrdET - III gt u 3r-AR. rrf r titirt

WriTiO 3NTR dt.IT . 1T1

(sm./ UfT

84) (seetigI URI 84)

1 2749'45.5" 7810'42"

2 ITTT IR" 1.T.1 317 1926'00" 8452'08" • •

1509'54.4" 7652'50" ac'.?13ii3TRfiatili-ks,(11-ET aril) 4 1 a-41-311311 .041.11 1,.t (e. c•'') 2833'09.84" 7747'15.61"

5 a- 1303rwauff(u--cr t.i) 2811'20.422" 7406'41.267" -qct-)1 2

6 fr.Tcrii ,(cr)fl 4-31131 1VaU11-:(Utj 2820'51.2" 7639'20.2"

7 M-3T)-3TIVatill- (TO. 0) 1718. 48.8" 7648'11"

8 ..31c11c11114 -211-dbl3TR/0131=ft (CT.0 2741'39.6" 7942'44.7"

9 U-fat 2153'47.6" 8402'19.5"

10 TT Ti aciT3iT3TIV:chTE.,1(CYU 0) 1247'15.1" 7942'44.7"

11 2534'1.7" 8733'20.6" TT65K

12 u;i-at`A 2118'53" 7016'10"

13

14

RIPTIT-T v; u=iadr).

1715'45" 8008'15"

fcr71-i4i 2606'45" 8756'30.3"

15 crdTtPTd a- 31131Niat.711- (g-U 0) 2402'13.65" 7444'38.16"

16 TrYTT. :('I 1706'31 8149'18"

17 aa311311qatni.(t-rd en) 2750'54.4" 7700'29.6" iich.tti

18 fl44-1c11 d) (TU 2849'11.1" 7649'9.6"

19 E'4311 311 (U.I 2823'36.2" 7742'29.2" fiici)1611

20 . P 3 iad') 2110'2.5" 7333'57.4" ThR-TT

- p,Taa 21 T1 0843'32.2" 7801'32.5"

22 rdcbNIG11 1 /20'3.8 7753'55.5"

Inner

hor i

zon

tal s

urf

ace for

runw

ay c

ode

3 &

4

R P

=R

efe

renc

e P

oin

t

Txf Tr-eV -0 vrrniff wbr

1

2

3TilitffT

25°49'42.8" N

18°49' 33" N

27-° 13'58.2691N

5 1451*(1

-a1A4 17f331 14

4-16h(N

3

4 23°37'27.7" N s411.< 1-1Dr44-1 011Ici

----5- (t) siT CA

(q)

240 809/27 3000X45

5.00 808/26 3700X60

1321.27 802/20 1700X30

85 R16/34 3315X45

078°19'1.7"E

073 04 18 E

088°35

.18.7927E

087 14 32.5 E

[ IMT 11—t9us 300] 17117 k141111 : 37T M:7

29

- III t

3R NI-tall- et tiurwt 4 TEr .-44-reW **-63Trt

3971'1Z7 rd-Eri

OUTER CONICAL OUTER TRANSITIONAL

OUTER HORIZANTAL SURFACE

° From Rwy erktremity

°° From Rwy Aril)

30

THE GAZETTE OF INDIA : EXTRAORDINARY [FART I I—SEC. 3(ii)]

'14 t qltd

Appendix A 2

Line Drawn from Antenna pedestal; to 10 at below MSA at 25 NM

Beyond Point A all obstructions having azimuth width less than 0.4 degree on RADAR Antenna can be permitted above this line Subjected to other conditions

Slo .0.m/mtr in para 2.5 and restrictions from

AGA & PAN-OPS

[ WRT 11—tou5 3(ii) ATTt Wf 7T71:17 : 311711/177 31

tirrfrrEa-

Appendix B

A

500 M

Fig 1 Criteria for height restriction with respect to ASR

A

H

H-3

Beyond Point A all obstructions having azimuth width less than o.4 degree ON RADAR Antenna can be permitted above this line subjected to other conditions in para 2.6 and restrictions from AGA & PAN-OPS

Angle'4'0:angle of the antenna or 0.5 degree whichever is higher

SI4e=0.0m/tntr

32 THE GAZETTE OF INDIA : EXTRAORDINARY 'PART 3001

Appendix C

200 M

Fig 2 Criteria for height restriction with respect to ARSR

H

H - 5

•

7.8VVOR-10,3Vi

VOR or NDB fadlity

3.7km (2.0NM)/VOR

kpO

4.6km (2.SNM)/1.'DB

ite 31'

Appendix D

5 t7

1/1

0 5

it

Nominal fliciht path

\

Runway

FINAL APPROACH AREA OF FOR 88,NDB

34

THE GAZETTE OF INDIA: EXTRAORDINARY {PART II—SEC. 3(11)1

trftfrrtz

Appendix E

;LLUSTRATION OF SHIELDING BENEFITS

..... -

CONICAL

CONICAL

. .

/

SURFACE

,..„,. ,. wt7"""1 Lhaseht as building '

r4

A _.,,... , Bldg. providii;

shielding '.

\ n

r=7 L slope ' --J

CONICAL SURFACE

- - ,,,,, •INNER HORIZONTAL / .,

SURFACE /

'

t

\ _.:..

Projected behisd

IlltMEA

41a-

--

HORIZONTAL SURFACE

, .

..-

providing shleleng

/ /

7/

CONICAL SURFACE

OW. ..,

WA41II

Bldg. providing shielding INNER

Projected behind the building - sone

height es building

SURFACE •

SectfimA-A

Approach Transitional

Inner horizontal

finer approach

Section B-B

[ sZTtT II —11rTrg 3(ii)

17Trff ,z141 : 3mturrur 35

7tF

Appendix F

Diagrams of Obstacle Limitations Surfaces, ILS Critical Areas and Shielding Benefits

C60)31:1! 1 ion haggle+ sulf•AstE

36 (PART if—Sec. 3(ii)1 THE GAZETTE OF INDIA : EXTRAORDINARY

rite t 2

Appendix F2

Balked landing Inner transitional

Balked landing

A L Inner transitional

u3,

Inner approach

Section A-A

Inner transitional 7 v. Inner horizontal

Balked landing/

Section B-B

Inner approach, inner transitional and balked landing obstacle limitation surfaces

[(O

f Ina

—II

OBSTACLE LIMITATION SURFACES Note.—The figure shows the obstacle limitation surfaces at an aerodrome with two runways, an instrument runway and a non-instrument runway. Both are also take-off runways.

Takeoff climb surface 15000m 3.4 Slope 2%

Inner horizontal suiting Instrument runways

4000m 3500m 34 1,2

1111111111/WO:Areerel'.

Transilinual surface

Slope 14,3% 3,4

'Olt 1,2 Appoach surface

Non-instrument runway 3000m 3,4 2500m 2 1600m 1

Code number

3 2 Take-on climb surface

15000m 3,4 2500m 2 1600m 1

8400m Horizontal-minors

38

THE GAZETTE OF INDIA : EXTRAORDINARY

IP I I—SEC. 3(ii)I

lerr7TIZ 7F 4

Appendix F4

[ (O

E ka

la—

II k

ik% ]

Critical Area of G.P. Runway

40

THE GAZETTE OF INDIA : EXTRAORDINARY [PART H—SEc. 3(ii)J

MINISTRY OF CIVIL AVIATION

NOTIFICATION

New Delhi, the 14th January, 2010

S.O. 84(E).—In exercise of the powers conferred by section 9-A of the Aircraft Act, 1934 and in supersession of the notification of the Government of India in the Ministry of Civil Aviation number S.O. 1589(E), dated the 30th June, 2008, the Central Government being of opinion that it is necessary and expedient so to do for the safety of aircraft operations hereby direct as under:

1. No building or structure shall be constructed or erected and no tree shall be planted on any land within the limits specified in Annexure I and II from Civil and Defence Aerodromes and Aeronautical communication stations listed in Annexure-IIIA, IIIB, IIIC, IIID and IIIE without obtaining 'No Objection Certificate'.

2. For the purpose of issuing of No Objection Certificate referred to in paragraph 1 (a) the Airports Authority of India shall be responsible for issuing the No Objection Certificate on behalf of Central Government in respect of all civil aerodromes in India including the State Government aerodromes and the Private aerodromes where civil commercial flights are operating as listed at Annexure IIIA; (b) for Defence aerodromes, defence authorities shall be responsible for issuing No Objection Certificate in accordance with this notification and subject to any other restriction or condition which such authorities deemed fit for issuing the 'No Objection Certificate'.

3. No building or structure higher than the height specified in Annexure I and II shall be constructed or erected and no tree which is likely to grow or ordinarily grows higher than the height specified in the said Annexure I and II shall be planted on any land within a radius of twenty kilometers from the aerodrome reference point.

4. In respect of Aerodromes which are required to be constructed or developed where the height of any existing building or structure or tree on any land within the limits specified in Annexure I and Annexure II, exceeds the height specified in this notification, the owner or the person having control of such building, structure or tree shall reduce the height thereof within a period of one month from the date of publication of notification in this regard so as not to exceed the specified height.

5. Where the owner or the person having control over the building or structure or tree fails to reduce the height within the period specified in para 4, the State Government authorities or any other concerned authority shall esponsible for taking action in respect of such building, structure or tree; and any building or structure including tower, installation or chimney that is constructed or erected or

[ 3TITT II — tguS 3(ii)

'WM it ,-1141 : 317:PITT4T 41

any tree that is grown in violation of the provisions contained in this notification shall be considered as illegal and the authorities referred to above shall be responsible for removal or reduction of height thereof.

6. In case of Government and Private civil aerodromes and airstrips specified in Annexure III B where, at present, civil schedule operations are not taking place or there is no possibility of such operations taking place for reasons including airspace restrictions, permanent structures or terrain penetrating the obstacle limitation surface, national security, etc., the provisions of this notification shall be applicable on the basis of the aerodrome reference code and operational usage of that aerodrome or strip.

7. Each Aerodrome Operator shall be responsible for preparing zoning maps in conformity with the provisions of this notification with digitized data in WGS84 Coordinates indicating all the latest features around the airport.

F. No. AV-20036 '66,2000-AA11

ALOK SINHA, Jt. Secy.

ANNEXURE-I

The Land area specified below shall be completely free from all obstacles as provided hereunder:- 1. The land comprising within the Runway strip of uniform width of 150 meters

on either side of centerline which extends to 60 meters beyond each extremity of Runway end along extended centerline of Runway for a Instrument runway code 3 and 4.

2. The land comprising within the Runway strip of uniform width of 75 meters on either side of centerline which extends to 66 meters beyond each extremity of Runway end along extended centerline of the Runway for instrument Runway code 1 and 2 for non-Instrument runway code 3 and 4.

3. The land comprising within the Runway strip of uniform width of 40 meters on either side of centerline which extends to 60 meters beyond each extremity of Runway end along extended centerline of the Runway for a non- Instrument runway code 2.

4. The land comprising within the Runway strip of uniform width of 30 meters on either side of centerline which extends to 30 meters beyond each extremity of Runway end along extended centerline of the Runway for a Instrument runway code 1.

5. The rectangular area of land enclosed within the approach funnel of the Runway within a maximum distance of 300 meters from the extremity of the Runway and 60 meters on either side of the extended Runway centerline for code 3 and 4 and 45 meters on either side of extended Runway centerline for code 1 and 2.

42

THE GAZETTE OF INDIA : EXTRAORDINARY IPARr II-St( 3(ii)J

6. In an aerodrome, where-

(a) Very High Frequency Omni Radio Range (VOR)/ Distance Measuring Equipments (DME)/Very High Frequency Direction Finder (VHF DF) facilities are available, land within the 300 meters radius of the facility;

(b) Localizer facilities are available, the area bounded by the following, namely:- (i) a line 300 meters in the direction of approach or nearest end of

the runway, whichever is greater from localizer antenna and perpendicular to the runway;

(ii) a line 60 meters from the centerline of localizer antenna on both side and parallel to the runway;

(iii) a line containing centre of localizer antennas and perpendicular to the runway; and

(iv) area within circle of 75 meters radius with centre at middle of the antenna system;

(c) GLIDE PATH facilities are available, the area bounded by the following, namely-

(i) a line 300 meters in the direction of approach from the glide path facility;

(ii) a line containing glide path antenna and perpendicular of runway;

(iii) near edge of the runway from the glide path; (iv) a line 30 meters in the directions away from the runway and parallel to it;

(d) Locators or Markers Beacons facilities are available, the land within a radius of 30 meters of the site of the markers and locator beacons;

(e) Air Surveillance Radar facilities are available, no structure will be permitted on the land above the level of 3 meters below the pedestal height up to the distance of 500 meters from Radar antenna;

(0 Air Routes Surveillance Radar facilities are available, no structure will be permitted on land above the level of 5 meters below the pedestal height up to the distance of 200 meters from Radar antenna;

(g) Secondary Surveillance Radar are available, the distance and the height restriction shall be the same as in respect of the Air Surveillance Radar or Air Routes Surveillance Radar, depending upon operational usage;

(h) Microwave Link facilities are available, on corridor of 30 meters on either side of the direct line of the azimuth and 10 meters below from the direct line or flight in the vertical plane;

[ ITTTT - (.9 u 3(ii)

ITTra' AFT ti ,314 : 317:111/717 43

(i) Ultra High Frequency (UHF) Link facilities are available, on a corridor of 30 meters on either side of the direct line of the azimuth and 10 meters below from the direct line of sight in the vertical plane;

(j) En-route Beacons facilities are available, land within a radius of 30 meters around the antenna;

(k) Remote Receiver facilities are available, land within a radius of 1525 meters of the site.

Explanation.- For the purpose of this Annexure,-

(a) "Runway Strip" means a defined area included the runway and stopway, if provided, intended:-

(i) to reduce the risk of damage to aircraft running off a runway; and (ii) to protect aircraft flying over it during take off or landing

operations;

(b) "Runway Code", means the Runway Code, in relation to the dimension of Runway strip, specified in column (1) of the Table below:

DIMENSION OF RUNWAY STRIP

Runway Code

Length (Meter)

Width Extending laterally on either side of Runway Centre Line (Meter)

Length beyond Runway End/ Stopway (Meter)

Width Exterlding laterally on either side of Runway Centre Line (Meter)

Length beyond Runway End/ Stopway (Meter)

(1) (2) (3) (4) (5) (6) 1. <800 75 60 30 30 2. 800<1200 75 60 40 60 3. 1200<1800 150 60 75 60 4. 1800 85

above 150 60 75 60

(c) "Approach funnel", in relation to-

(i) an Instrument runway code 3 and 4, means the area in the shape of an isosceles trapezium having the longer parallel side 4800 meters long (2400 meters on either side of the extended centerline o the runway) and smaller parallel side 300 meters long (150 meters on either side of the extended centerline of the runway), where the smaller and longer parallel sides are placed at a distance of 60 meters and 15060 meters respectively, from the end of the runway and at right angles to the extended centerline;

44

THE GAZETTE OF INDIA : EXTRAORDINARY !FART II--SEC. 3(ii)J

(ii) an Instrument runway (precision) code 1 and 2, means the area in the shape of an isosceles trapezium having the longer parallel side 4650 meters long 92325 meters on either side of the extended centerline of the runway) and smaller parallel side where the smaller and longer parallel sides are placed at a distance of 60 meters and 15060 meters respectively, from the end of the runway and at right angles to the extended centerline;

(iii) an Instrument runway (non precision) code 1 and 2, means the area in the shape of an isosceles trapezium having the longer parallel side 900 meters long (450 meters on either side of the extended centerline of the runway) and smaller parallel side 150meters long (75 meters on either side of the extended centerline of the runway) where the smaller and longer parallel sides are placed at a distance of 620 meters and 2560 meters respectively, from the end of the runway and at right angles to the extended centerline;

(iv) non-Instrument runway code 3 and 4, means the arc in the shape of an isosceles trapezium having the longer parallel side 750 meters long (375 meters on either side of the extended centerline of the runway) and smaller parallel side 150 meters long (75 meters on either side of the extended centerline of the runway) where the smaller and longer parallel sides are placed at a distance of 60 meters and 3060 meters respectively, from the end of the runway and at right angles to the extended centerline;

(v) an Instrument runway code 2, means the area in the shape of an isosceles trapezium having the longer parallel side 580 meters long 9290 meters on either side of the extended centerline of the runway) where the smaller and longer parallel sides are placed at a distance of 60 meters and 2560 meters respectively, from the end of the runway and at right angles to the extended centerline;

(vi) an Instrument runway code 1, means the area in the shape of an isosceles trapezium having the longer parallel side 320 meters long (160 meters on either side of the extended centerline of the runway) and smaller parallel side 60 meters long (30 meters on either side of the extended centerline of the runway) where the smaller and longer parallel sided are placed at a distance of 30 meters and 1660 meters respectively, from the end of the runway and at right angles to the extended centerline. The diagrams of Runway strip and approach funnel of Instrument runway code 1, 2, 3 and 4 and non-Instrument runway code 3 and 4 have been shown in the Appendix;

(d) "Instrument runway" means a runway served by visual aid and non-visual aids providing directional guidance adequate for a straight in approach and intended for the operation of aircraft using instrument approach procedures;

[ WITT 11--(gus 3(ii) 1 VTI-ff T,T tis3114 : 317711177

45

(i) Non-precision approach runway- An instrument runway served by visual aids and a non-visual aid providing at least directional guidance adequate for a straight-in approach,

(ii) Precision approach runway, category I- An instrument runway served by Instrument Landing System and/ or MLS and visual aids intended for operations with a decision height not lower than 60 meters and either a visibility not less than 800 meters or a runway visual range not less than 550 meters,

(iii) Precision approach runway, category II- An instrument runway served by Instrument Landing System and or MLS and visual aids intended for operations with a decision height lower than 60 meters but not lower than 30 meters and a runway visual range not less than 350 meters,

(iv) Precision approach runway, category III- An instrument runway served by Instrument Landing SysLem and/ or MLS to and along the surface of the runway and-

A- intended for operations with a decision height lower than 30 meters, or no decision height and a runway visual range not less than 200 meters, B-intended for operations with a decision height lower than 15 meters, or no decision height and a runway visual range less than 200 meters but not less than 50 meters, C- intended for operations with no decision height and no runway visual range limitations.

(e) "Non-Instrument runway" means a runway intended for operations of the aircraft using visual approach procedure;

(f) "Very High Frequency Omni Radio Range, Terminal Very High Frequency Omni Radio Range, and Doppler Very High Frequency Omni Radio Range" means the facilities operating in the Very High Frequency band of frequencies 112 to 118 MHz radiate signals whereby an aircraft with the help of an instrument in its cockpit when tuned to the ground equipment frequency automatically gets its direction with respect to the facility and helps an aircraft to navigate on a predetermined course or home to an airport served by the facility;

(g) "Instrument Landing System" means the facility which serves to help an aircraft to make a safe landing on the runway in conditions of poor visibility and comprises of the following component facilities, namely:-

(i) Localizer facility which radiates Very High Frequency signals which when picked up by an aircraft guide it onto the centerline of the runway in the horizontal lane and is normally situated about 305 meters from the runway end;

46 THE GAZETTE OF INDIA : EXTRAORDINARY IP ART II—Sec 3(01 (ii) Glide Path facility radiates Ultra High Frequency signals and is normally situated about 275 meters to 305 meters from the runway threshold and offset about 122 meters to 137 meters from the centerline of the runway and provides the glide angle information to a landing aircraft with the help of an instrument in the cockpit which when tuned to the glide path frequency indicates whether the aircraft is flying up or down or along the correct glide angle;

(iii) Outer Marker or Outer Locator facility operating on 75 MHz in the Very High Frequency band is normally installed along the extended centerline of the runway at a distance between 3.5 and 6 nautical miles (1 nautical mile = 1853 meters) and produces radiation pattern to indicate the landing aircraft, the pre-determined distance from the threshold along the Instrument Landing System glide path;

(h) "Radar" includes-

(i) Air Surveillance Radar which is a radar facility serving an aerodrome to scan the air traffic within 50 to 60 nautical miles of the aerodrome;

(ii) Air Routes Surveillance Radar or Secondary Surveillance Radar is a high power long-range radar covering a distance of 200 nautical miles approximately and it scans air traffic to a larger distance than Air Surveillance Radar;

(i)

Communication / Navigational facilities include T

(i) Microwave Link which is a radio facility whereby mostly intelligence/data is carried to the Air Traffic Control Display site;

(ii) Ultra High Frequency Link which is a radio relay facility operating in Ultra High Frequency Band;

(iii) Beacons which are radio transmitters operating in the Medium Frequency band from 200 to 400 KLHz radiating omni directionally in the horizontal plane and an aircraft equipped with a suitable cockpit instrument can get its location automatically with respect to this facility;

(iv) Remote Receivers which are radio receiving stations (HF Band) installed at remote site away from factory or industrial areas to avoid interference link man-made static, etc.

Note 1: Any equipment or installation required for air navigation purposes must be located-

[ ITTTT 3(ii)

ITTrd i t I vt 4 i : 37TriTrT9r 47

(a) on that portion of the strip within: i) 75 meters of the Runway centerline where the Runway code

is 3 or 4, ii) 45 meters of the Runway centerline where Runway code is 1

or 2; or

(b) on a runway end safety area, a taxiway strip or within the distances specified in Annex 14 of the guidelines of the International Civil Aviation Organisation; or

(c) on a clearway and which would endanger an aircraft in the air, and shall be frangible and mounted as low as possible.

Note 2: Any equipment or installation required for air navigation purposes which must be located on or near a strip of precision approach Runway category I, II or III of Instrument Landing System and which-

(a) is situated on that portion of the strip within the 77.5 meters of the Runway centerline where the code number is 4 and code letter is F;

(b) is situated within 240 meters from the end of the strip and within-

(i) 60 meters of the extended Runway centerline where Runway code is 3 or 4: or

(ii) 45 meters of the extended Runway centerline where Runway code is 1 or 2: or

(iii) penetrates the inner approach surface, the inner transitional surface or the balked landing surface,

and shall be frangible and mounted as low as possible.

NOTE 3. Location of Navigational Aids shall be determined as per the provisions of Annex-10 of the guidelines of International Civil Aviation Organisation.

15000M---

11 48 OM

/5000M----

15000M FOR PRE: 'SION

APP CODE. :12 2500M FOR NON Pal CISION

APP CODE 1a2

Appendix to Annexure I A 00

Rwy strip & approach funnel of instrument Rwy code 3&4

Rwy strip & approacl funnel of instrument Rwy code 1&2

4650' EJR PRECISION CODE 1&2

900M FC NON PRECISION

'P ( -ODE 132

Rwv strip & approach funnel of non instrument Rwy code 3&4

75 M 12 )M

• 3000M

TH

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IND

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XT

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OR

DIN

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[ I1TTT II —WaT 3(ii)

WTTR zET "fr471' : WITEITTuT 49

ANNEXURE-II

The height or permissible elevations shall be calculated based upon the Annex 14 obstacle limitation surfaces, the radio navigation aids based on Annex 10 and the operational requirements for minimum altitudes of various segments of published instrument approach procedures based on Document 8168, VOI II of International Civil Aviation Organisation.

1. Based on Annex 14 Obstacle Limitation surface as under:

1.1 Take-off climb surface - The dimensions of the take-off climb surface shall not be less than the dimensions specified in the table given below except that if a runway is meant for takeoff, a lesser length may be adopted for the takeoff climb surface where such lesser length would be consistent with procedural measures adopted to govern the outward flight of aeroplanes, namely:-

Table Dimensions and slopes of obstacle limitation surfaces

(RUNWAYS MEANT FOR TAKE-OFF)

Surface and dimensions*

(1)

Code Number 1

(2) 2

(3)

3or 4 2 (4)

TAKE-OFF CLIMB Length of inner edge 60 meters 80 meters 180 meters Distance from runway end

30 meters 60 meters 60 meters

Divergence (each side)

10% 10% 12.05%

Final width 380 meters 580 meters 1200meters 1800 meters **

Length 1600 meters 2500 meters 15000 meters Slope 5% 4% 2% * All dimensions are measured horizontally.

** 1800 meters when the intended track includes changes of heading greater than 15 degree for operations conducted in IMC, VMC by night.

1.2 Transitional Surface

1.2.1 The outer limit of the transitional surface is determined by its intersection with the plane containing inner horizontal surface and the slopes of transitional surfaces are as given below, namely:-

1.2.2 (i) Precision approach Runway 14.3% (1:7) (ii) Non precision

14.3% (1:7) for code 3 & 4 20% (1:5) for code 1 & 2

(iii) Non-Instrument runway

14.3% (1:7) for code 3 & 4. 20% (1:5) for code 1 & 2;

175 GI/10-7

50

THE GAZETTE OF INDIA : EXTRAORDINARY I PART II—Sec. 3(ii))

1.2.3 The slope of the transitional surface shall be measured in a vertical plane at right angles to the center line of the Runway;

1.2.4 The elevation of a point on a lower edge shall be- (a) along the side of approach surface, equal to the elevation approach

surface at the point; and (b) along the strip, equal to the elevation of nearest point of the center line

of the Runway or its extension;

1.3 Approach Surface

1.3.1 The approach surface shall be established for each Runway strip in the direction of intended landing of the aeroplanes and the limits and slopes are given in table below:

1.3.1.1. Instrument runway (divergence 15% on either side) Length of Inner edge - 150 meters for Code No. 1 and 2

300 meters for Code No. 3 and 4 Distance from Threshold

60 meters

Table

RUNWAY Precision approach Non-Precision Runway approach Runway

Code Length (meter) First Second First Second Horizontal No. Section Section Section Section Section

Length Length length Length (Meter) (Meter) (Meter) (meter) (Meter) Slope Slope Slope Slope

1 . <800 3000 12000** 2500 - - 2.5% 3% 3.33% -

. 800<1200 3000 12000** 2500 - - 2.5% 3.33% 3.33% - -

3. 1200<1800 3000 3600 3000 3600 8400** 2% 2.5% 2% 2.5%

4. 1800 and Above 3000 3600 3000 3600 8400** 2% 2.5% 2% 2.5%

*Total length of approach surface for code No. 3 and 4 (precision and non- precision shall be 15000 meters.

** Total length of approach surface for Precision approach Runway Code No. 1 and 2 shall be 15000 meters.

1.3.1.2. Non-Instrumental runway

Length of Inner edge - 80 meters for code No. 1 and 2 and 150 meters for Code No. 3 and 4

[ 17171 II -13117-4 3(ii)

(1117-4 t I srlti : angtirrri

51

Distance from Threshold - 60 meters

Table

RUNWAY DIVERGENCE 10% ON EITHER SIDE

Code No.

Code Length No. (Metre)

<800

Length (Meter) 1600

Section slope

5% 1. 2. 800<1200 2500 4% 3. 1200<1800 3000 3.33% 4. 1800 86 above 3000 2.5%

1.3.1.3.

1.3.1.4.

1.3.1.5.

Aerodrome where there are more than one runway with over-lapping approach areas and associated surface, most stringent of the two would be the applicable criteria.

for determining the approach, the physical extremities of the runway shall only be considered. In case of displaced threshold the permissible height shall be calculated based on approach surface and transitional surface with respect to the runway extremity or displaced threshold whichever is more restrictive. However in case the threshold has been displaced due to obstacles of permanent nature, which are not likely to be removed, the displaced threshold will be taken as reference point.

at Aerodromes, where the proposals for runway extension exist, the requisite surface shall be determined from the proposed extension as well as from the existing runway strip/ associated clearway, as applicable and the lower of the two elevations shall be permitted.

1.3.1.6. the elevation of the associated Runway extremity/ displaced threshold/ proposed extension of Runway shall be the datum for approach surface.

1.3.1.7. the slope of the approach surface shall be measured in a vertical plane containing the centerline of the runway.

1.4 Inner Horizontal Surface

1.4.1 Dimensions and permissible heights of Inner Horizontal Surface are given in the table below:

DIMENSIONS AND PERMISSIBLE HEIGHTS OF INNER HORIZONTAL SURFACE

RUNWAY INSTRUMENT NON-INSTRUMENT Code No.

Length (Meter)

Radius (Meter) 3500*

Height (Meter)

45

Radius (Meter) 2000*

Height (Meter)

45 1. <800


IP %RI II—SEc. 3(ii)i

2. 800<1200 3500* 45 2500* 45 3. 1200<1800 4000** 45 4000** 45 4. 1800 and above 4000** 45 4000** 45

*Radius shall be measured from the Aerodrome Reference Point.

** Radius shall be measured from the extremities of the Runway.

1.4.1.1. The reference datum for Inner-Horizontal Surface shall be the Aerodrome elevation as defined in clause (g) of the Explanation to this notification.

1.4.2. For Runway code 3 and 4, the Inner Horizontal Surface shall be a composite pattern, which consists of two circular areas centered at the two ends with a radius of 4000 meters These areas shall be joined tangentially to form an elliptical shape as shown in Appendix-A.

1.4.3. Where it is required to protect two or more widely spaced long runways, an even more complex pattern involving four or more circular areas are formed. These areas should be joined tangentially by straight lines and the Inner Horizontal Surface shall be defined by the external limits of the resulting pattern.

1.4.4. When two aerodromes are close to each other with overlapping circuits the Inner Horizontal Surface will be drawn as prescribed in para 1.4.2. The inner horizontal surface of these two aerodromes shall be joined tangentially to form one common Inner Horizontal Surface.

1.4.5. In case of common horizontal surface serving two aerodromes, the elevation of the Inner Horizontal Surface will be the lower of the two aerodromes.

1.5. Conical Surface

1.5.1. The conical surface shall be projected upwards and outwards from the periphery of the Inner Horizontal Surface. The slope 5% (1:20) of the conical surface shall be measured in a vertical plane perpendicular to the periphery of Inner Horizontal Surface. The outer limits and permissible heights of the conical surface are given in the table below:

Table OUTER LIMITS AND PERMISSBLE HEIGHTS OF CONICAL SURFACE

RUNWAY INSTRUMENT RUNWAY NON-INSTRUMENT RUNWAY

Code Length (Meter Precision Non- Horizontal Maximum No. Runway precision

Runway Distance of Conical

Height above

Surface beyond

Inner Horizontal

[ WIT 3(ii) ]

Wrd T,T ,(141i4A 317:TFUTTITT

53

Inner Horizontal Surface (Meter)

Surface (Meter)

1. <800 1200 60 1200 60 700 35 2. 800<1200 1200 60 1200 60 1100 35 3. 1200<1800 2000 100 1500 75 1500 75 4. 1800 & above 2000 100 2000 100 2000 100

The reference datum for Conical Surface shall be the aerodrome elevation as defined in this Annexure.

Note: Where a part of Inner Horizontal Surface and conical surface lies below the approach/ take - off climb surface, the permissible heights shall be the lowest of the applicable surfaces..

1.6 Outer Horizontal Surface

1.6.1. The Outer Horizontal Surface shall extend to 15000 meters from the Aerodrome Reference Point for Aerodrome with runway code 3 and 4.

1.6.2. In case of Aerodrome with Runway Code-2, the Outer Horizontal Surface shall extend to 14740 meters from Aerodrome Reference Point for Instrument runways and 13740 meters for Non-Instrument runways.

1.6.3. Where combined Outer Horizontal Surface is established for two Aerodromes, the Outer Horizontal Surface shall be centered on the Aerodrome Reference Point of the Aerodrome of higher category.

1.6.4. Outer Horizontal Surface for Aerodrome with runway code No. 1 shall not be established.

1.6.5. The Outer Horizontal Surface, would be defined such that the Conical Surface may continue to be extended at 5% slope to a point wherein the permissible maximum height of 300 meters (above aerodrome elevation) is reached and thereafter this surface is maintained upto 15 Kilometers from Aerodrome Reference Point. Construction (s) protruding above these surfaces shall normally not be permitted. Obstructions existing in the area should be marked or lighted.

1.6.6. In order to avoid abrupt vertical changes in surfaces, the surfaces beyond the conical surfaces will slope laterally at 1:7 from edges of the approach and take off surfaces between the permissible heights of 150 meters to 300 meters.

1.6.7. The datum for Outer Horizontal Surface shall be the aerodrome elevation as defined in this Annexure.

1.7. The Inner approach, inner transitional and balked landing surfaces (OFZ).

54

THE GAZETTE OF INDIA : EXTRAORDINARY [PART II—Sec. 3(ii)]

1.7.1 Obstacles free zone shall be established for precision approach Category II and III operations. The zone shall be kept free from fixed objects other than light weight frangible mounted aids to air navigation which must be:near the Runway to perform their functions, and from transient objects such as aircraft and vehicles when the Runway is being used for Category II or III operations.

1.7.2 The dimensions and slopes of the Obstacles free zone (Code 3 and 4) are given below:

Note: Obstacles free zone for Runway code No. 1 and 2 are not established.

1.7.2.1 The Inner approach surface Width

120 meters Distance from Threshold- 60 meters Length 900 meters Slope 2%

1.7.2.2 The inner transitional surface Slope 33.3%

1.7.2.3 Balked Landing surface Length of the Inner edge- 120 meters Distance from Threshold- 180 meters Divergence 10% Slope 3.33%

1.8. The No Objection Certificate needs to be obtained from the competent authority in all cases wherein the requested height of the structure etc. is more than 150 meters above the reference datum up to a distance of 20 Kilometers from the Reference point.

2. Based on Annex 10 (Navigational Aids)

2.1 Very High Frequency Omni Radio Range (VOR), Terminal Very High Frequency Omni Radio Range (TVOR), and Very High Frequency Omni Radio Range Distance Measuring Equipment (VOR DME)- An area beyond the radius of 300 meters from the facility no structure shall sustain vertical angle greater than 1.5 degree at the center of the Very High Frequency Omni Radio Range counterpoise from the horizontal plane passing through the counterpoise.

2.2 Stand alone Distance Measuring Equipment- Beyond 150 meters no steel towers, power lines, metal buildings shall protrude elevation angle of 3 degree measured from the base of Distance Measuring Equipment antenna.

[ WTI II -WM 3(ii) ]

ITTM : &MAIM:TT 55

2.3 Localizer

2.3.1. Beyond the area specified in Annexure I and within ± 10 degrees azimuth in front of antenna, an object should not sustain an angle of elevation more than 0.75 degrees at the centre of antenna array.

2.3.2. Beyond areas specified in Annexure I and within + 10 degrees to ± 35 degrees azimuth in front of antenna an object should not sustain an angle of elevation more than 2.4. Beyond the area specified in Annexure I and within ± 8 degrees azimuth in front of the glide path antenna, a building/ structure should not subtend an angle of elevation of more than 1.1 degree at antenna base.

2.5 Air Surveillance Radar:

Beyond 500 meters from particular Radar site the height of the permissible structures may be increased at the rate of 0.05 meter per meter, up to a point wherein the height of the permissible structure does not protrude above the line drawn from a point 10% below the minimum sector altitude at the farthest point (from Radar site) to the center of antenna pedestal, considering the Minimum Sector Altitude (MSA) in that particular sector. Beyond the above stated point no large object would be permitted to protrude above the line drawn from a point 10% below the minimum sector altitude at the farthest point (from Radar site) to the center of antenna pedestal depending on the Minimum Sector Altitude in that particular sector. Large object means the structure/s in isolation or collectively subtending azimuth angle of 0.4 degree or above at Radar antenna. In case of cluster of buildings wherein the gap between the two adjacent buildings subtends an azimuth angle of less than 0.4 degree on the antenna pedestal, the entire cluster should be considered as one object. Diagrammatic representation is at Appendix-B.

2.6 Air Route Surveillance Radar:

Beyond 200 meters from particular Radar site the height of the permissible structures may be increased at the rate of 0.05 meter per meter up to a point wherein the height of the permissible structure does not protrude above an angle of elevation of more than 0.5 degree at the antenna pedestal or an angle equal to antenna tilt angle set during last flight inspection whoever is higher. Beyond the above stated point, no large object would be permitted to protrude above the line drawn at an angle of 0.5 degree from antenna pedestal or an angle equal to antenna tilt angle set during last flight inspection whichever is higher. Large object means the structure subtending azimuth angle of 0.4 degree or above at Radar antenna. In case of cluster of buildings wherein the gap between the two adjacent buildings subtends an azimuth angle of less than 0.4 degree on the antenna pedestal, the entire cluster should be considered as one object. Diagrammatic representation is at Appendix-C.

2.7 Secondary Surveillance Radar


iPART II—Sec. 3001

Same as Air Surveillance Radar / Air Route Surveillance Radar depending on operational usage.

2.8 Advance Surface Movement Guidance and control system (ASMGCS) No structure should be built on the relevant area of the airport surface which blocks the line of sight between any of the sensors of the Advance Surface Movement Guidance and control system and the relevant operational area. In case there is operational or safety/ security requirement to add a structure on the airport surface which may obstruct the line of sight between Surface Movement Radar (SMR) antenna/ sensors, Airports Authority of India (AAI) would augment the system to meet the Advance Surface Movement Guidance and control system operational requirement.

2.9 Indian Land Uplink Station (INLUS)/Indian National Reference Station (INRES) of GPS Aided Geo Augmented Navigation (GAGAN) System No structure will be permitted to protrude the above the plane inclined at elevation angle of 2 degree from the horizontal surface drawn at the level of antenna of Indian Land Uplink Station and Indian National Reference Station of GPS Aided Geo Augmented Navigation system which is a part of Global Navigation Satellite System (GNSS).

2.10 Communication Navigation Surveillance (CNS) Simulation study In case any structure is required to be made within aerodrome surface in the operational interest which creates an obstruction from Communication Navigation Surveillance point of view, a simulation study could be carried out to study the impact of this structure on the performance of the relevant facility and in case the study confirms that the impact would not hamper the operability of the facility, such structure could be permitted within the aerodrome boundary.

3. Operational criteria based on Document 8168, Vol II

In order to achieve the lowest possible operating minima for aircraft operation, it is necessary to protect not only the Annex 14 Obstacle Limitation Surfaces but also to safeguard the Procedure for Air Navigation Service (PANS) Operations (OPS) (Document 8168) Surfaces. Considerations need to be given to the objects which penetrate the Procedure for Air Navigation Service Operations Surface, regardless whether or not they penetrate Annex 14 Obstacle Limitation Surfaces. Such obstacle may result in an operational penalty like higher Obstruction Clearance Altitude or Height (OCA/H) and introduction of longer approach segment. Therefore, while examining the cases for issue of No Objection Certificate from the considerations of Annex 14 and Annex 10 criteria as provided para 1 and 2 above, the operational criteria needs to be considered based on the provisions of Document 8168, Vol. II. It needs to be ensured that the minimum altitude of the following segment of published or the proposed instrument approach procedures are not infringed by the proposed construction either within the Obstruction Limit Surface (OLS) or outside of it.

(i) Minimum Sector Altitude (MSA) (ii) Minimum Holding Altitude (MHA)

[ VT71 II 3(ii)

W! 1 WI' : 317:TTUTTUT 57

(iii) Minimum Vectoring Altitude (MVA) (iv) Minimum Altitude of Initial and intermediate Segments (v) OCA/H (Straight-in and Circling) for all aircraft categories.

Note: 1. Instrument approach procedures of all the civil aerodromes in India have been published in the AIP India under the section Aerodrome. In the published procedures, the minimum altitudes of the various segments of instrument approach procedures have been specified.

2. The minimum obstacle clearance criteria are applied as per the provisions of International Civil Aviation Organization (ICAO) Document 8168 Vol. II. Normally, for minimum sector altitudes (applicable upto 30 NM from the facility on which procedure is designed), minimum vectoring altitudes, minimum holding altitudes and for the initial approach an obstacle clearance of 1000 feet is applied.

3. Final approach areas of Very High Frequency Omni Radio Range (VOR)/ Non Directional Beacon (NDB) have been illustrated in Appendix-D.

4. Shielding Benefit

Shielding principles as indicated below are employed with respect to natural terrain/ duly authorized existing obstacles which penetrate above the obstacle limitation surfaces described and as contained in this document, subject to aeronautical study, if considered necessary by the competent authority.

4.1 Aerodrome and Ground Aids (AGA) parameters

4.1.1 The following criteria shall be applied for the purpose of applying shielding benefits for the proposed building or structure with respect to existing natural terrain/building structures.

4.1.2 The principle of shielding will not be applied in the transitional surface area.

4.1.3 The principle of shielding shall be applied in the approach areas beyond 4000 meters of the inner edge of runway strip.

4.1.4 The principle of shielding shall be applied in the Inner Horizontal Surface (IHS) beyond radius of 3000 meters from the nearest runway strip.

4.1.5 The principle of shielding shall also be applied in conical and outer horizontal surfaces.

4.1.6 The shielding benefit is to be provided with respect to the authorized structures/natural terrain in a horizontal plane projected from the top of the each of the obstacle away from the runway and on a plane

GI/10-8

58 THE GAZETTE OF INDIA : EXTRAORDINARY f l'uo II—Si 3(ii)i

having negative slope of 10% towards the runway. In case of Inner Horizontal Surface the benefit of the negative slope shall be applicable upto 3000 meters from the nearest Runway end or the Aerodrome Reference Point as the case may be. In case of approach surface the benefit of negative slope shall be applicable upto 4000 meters from the nearest runway end. In case of Conical and Outer Horizontal surfaces, shielding benefit of negative slope shall be restricted to same surface.

4.1.7 The following guidelines are provided for determining the areas where the shielding benefit would be applicable:

4.1.7.1 Towards the runway (Negative slope)

(i) Draw a line from the highest point of the reference terrain/obstacle to the end of all runways for obstacles located within the Inner Horizontal Surface, Conical or the Outer Horizontal Surface.

(ii) The shielding benefit will cover the areas bound within the lines as in para 4.1.6 and para 4.1.7 (i).

(iii) In case of obstacle located within the approach surface of any runway, the negative shielding shall be applicable to that particular runway only. The area shall be drawn by joining the highest point of the reference terrain/ obstacle to the nearest runway end. The dimension of the area shall be same as the dimension of the obstacle.

4.1.7.2. Away from the runway (Horizontal plane)

(i) For obstacles located in the Inner Horizontal Surface, Conical and Outer Horizontal Surface, draw a line from the Aerodrome Reference Point to the centre of the obstacle.

(ii) Draw the projection from the extremities of the obstacle away from the runway parallel to the line drawn as per para 4.1.7.2 (i).

(iii) For obstacle located in the approach surface, draw a line from the nearest runway end to the centre of the obstacle.

(iv) Draw the projection of the obstacle away from the runway parallel to the line drawn as per para 4.1.7.2. (iii).

(v) The shielding benefit of horizontal plan shall be applicable to the obstacles located below the projection line drawn as per para 4.1.7.2 (ii and iv) as indicated in Appendix-E.

4.1.8. Tall and skeletal obstructions such as isolated towers, chimney, masts, electric pylons, telephone and power lines and poles will not provide any shielding.

4.1.9. While providing the shielding benefit it shall be ensured that the minimum altitude, of various segments of the published instrument approach procedures are not adversely affected.

[ WTI 3(ii)

VIM tiszimA : 3MTUrfur 59

4.2. Communication Navigation Surveillance (CNS) Parameters

For navigational Aids and Surveillance facilities shielding benefit could be provided to the structures in cases wherein such structures are in their shadow of highest existing authorized structure/terrain of permanent nature. Shadow for this purpose is defined as an area falling below a line drawn from the top and both the extremities of the existing authorized structure/terrain of permanent nature, to the facility and extrapolation of the same plane behind from the said obstacle.

5. Conduct of Aeronautical Study

The following guidelines are provided for conduct of aeronautical study:-

(ii) The request for aero—utical study shall be processed by Airports Authority of India on case to case basis.

(iii) Aeronautical study shall be undertaken by a predetermined and approved agency and as per guidelines.

(iv) Recommendations of aeronautical study after approval of the competent authority shall be considered by Airports Authority of India for issuing No Objection Certificate for the height sought.

6. Procedure for determining the maximum permissible heights:

6.1 The following steps shall be taken for calculating the maximum permissible heights for cases relating to the issue of No Objection Certificate for building/installations.

6.1.1 Annex 14 Criteria

(i) The site of the proposed buildings/installations shall be marked on the zoning map of the aerodrome, prepared by the aerodrome operator, where Annex 14 surfaces have been drawn.

(ii) If the location is within the approach/take off surface, the permissible applicable heights in the approach /take off climb surface, transitional surface, Inner Horizontal Surface/conical surface shall be calculated.

(iii) If the site is located outside the approach /take off climb surface, the height shall be determined as per the location applicable to the relevant surface (transitional, Inner Horizontal Surface, Conical or Outer Horizontal Surface.)

6.1.2. Annex 14 Criteria

Determine the distance of the proposed site from the each communication/navigational aid/surveillance facility separately and calculate the applicable heights based on the provisions as contained in para 2 of Annexure II.

60

THE GAZETTE OF INDIA : EXTRAORDINARY [PART II-SEC. 3001

6.1.3. The permissible height from the above two criterion shall be the lowest as applicable to the specific surface /individual communication /navigational aid/ surveillance facility.

6.2 Procedure for Air Navigation Service Operations (PANS OPS) Criteria

i) After having determined the permissible heights based on the Annex 14 Obstruction Limit Surface (OLS) criteria and Annex 10 criteria, it shall further be ensured that the Procedure for Air Navigation Service Operations (PANS OPS) Surfaces are not infringed and the minimum altitudes of the published/proposed segments of instrument approach procedures are fully protected. This has also been referred to at para 3.

ii) For the obstacles located even outside the limits of Annex 14 OLS, it shall be ensured that Procedure for Air Navigation Service Operations (PANS OPS) Surfaces of the published instrument approach procedures are not penetrated.

iii) For consideration of obstacle clearance in the final approach area for the proposed construction, the criteria of primary and secondary area shall be applicable.

iv) The limits of the Procedure for Air Navigation Service Operations (PANS OPS) Surfaces extend up to 30 NM from the facility [Very High Frequency Omni Radio Range (VOR) 86 Non Directional Beacon (NDB)] serving the aerodrome based on which procedure is designed. This is to ensure that the minimum sector altitudes and the minimum vectoring altitudes are not adversely affected by the proposed constructions.

6.3 The lowest height determined based on Annex 14, Annex 10 and Procedure for Air Navigation Service Operations (PANS OPS) shall be the 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 the purpose of this Annexure shall be as given hereunder and the diagrams in respect thereof shall be as given in Appendix-F-1 to F-5.

(a) Conical Surface — A surface sloping upwards and outwards from the periphery of the inner horizontal surface.

The limits of the conical surface shall comprise :

(i) a lower edge coincident with the periphery of the inner horizontal surface; and

(ii) an upper edge located at a specified height above the inner horizontal surface.

[ %MT II — tgus 3(ii)

VT17 tiA141 : arfritTrrat 61

The slope of the conical surface shall be measured in a vertical plane perpendicular to the periphery of the inner horizontal surface.

(b) Inner horizontal surface - A surface located in a horizontal plane above an aerodrome and its environs. The radius of outer limits of the inner horizontal surface shall be measured from a reference point or points established for such purpose.

(c) Inner approach surface - A rectangular portion of the approach surface immediately preceding the threshold. The limits of the inner approach surface shall comprise:

(i) a lower edge beginning at the intersection of the side of the approach surface with the inner horizontal surface and extending down the side of the approach surface with the inner edge of the approach surface and from there along the length of the strip parallel to the runway center line.

(ii) an upper edge located in the plane of the inner horizontal surface.

(d) Inner transitional surface - A surface similar to the transitional surface but closer to the runway. The limits of an inner transitional surface shall comprise:

(i) a lower edge beginning at the end of the inner approach surface and extending down the side of the inner approach surface to the inner edge of that surface, from there along the strip parallel to the runway centerline to the inner edge of the balked landing surface and from there up the side of the balked landing surface to the point where the side intersects the inner horizontal surface; and

(ii) an upper edge located in the plane of the inner horizontal surface.

(e) Balked landing surface - An inclined plane located at a specified distance after the threshold extending between the inner transitional surface. The limits of the balked landing surface shall comprise:

(i) an inner edge horizontal and perpendicular to the centre line of the runway and located at a specified distance after the threshold;

(ii) two sides originating at the ends of the inner edge and diverging uniformly at a specified rate from the vertical plane containing the centre line of the runway; and

(iii) an outer edge parallel to the inner edge and located in the plane of the inner horizontal surface.

(f) Take-off climb surface - The surface shall be established for a runway meant for take-off. The limits of the take-off climb surface shall comprise:

62

THE GAZETTE OF INDIA : EXTRAORDINARY [PART II—Sec. 3(01

(i) an inner edge horizontal and perpendicular to the centre line of the runway and located either at a 'specified distance beyond the end of the runway or at the end of the clear way when such is provided and its length exceeds the specified distance;

(ii) two sides originating at the ends of the inner edge o and diverging uniformly at a specified rate from the take-off to specified final width and continuing thereafter at that width for the remainder of the length of the take-off climb surface; and

(iii) an outer edge horizontal and perpendicular to the specified take-off track.

(g) Aerodrome elevation - The elevation of the highest point of the landing area.

(h) Aerodrome Reference Point - The designed geographical location of an Aerodrome.

(i) Threshold- The beginning of that portion of the runway usable for landing.

(j) Displaced Threshold- A threshold- not located at the extremity of a runway.

(k) Frangible Object - An object of low mast designed to break, distort or yield on impact so as to present the minimum hazard to aircraft.

(1) Obstacle- All fixed(whether temporary or permanent) and mobile objects, or parts thereof, that are located on an area intended for surface movement or aircraft or that extend above a defined surface (indicated in Annexure IV) intended to protect aircraft in-flight.

(m) Obstacle Free Zone (OFZ)- The airspace above the inner approach surface, inner transitional surfaces and balked landing surface and that portion of the strip bounded by these surfaces, which is not penetrated by any fixed obstacle other than low mast and frangible mounted one, required for air navigation purposes.

(n) Runway - A defined rectangular area on a land aerodrome prepared for the landing and take off aircraft.

(o) Runway End Safety Area (RESA) - An area symmetrical about the extended runway centerline and adjacent to the end of the strip primarily intended to reduce the risk of damage to an aeroplane undershooting or overrunning the runway.

(p) Runway Strip - A defined area included the runway and stop-way, if provided, intended: -

To reduce the risk of damage to aircraft running off a runway; and To protect aircraft flying over it during take off or landing operations.

[ 1TM II —13Pig 3(ii)

1-1T17 t1 ,314 : 311TaTFUT 63

DIMENSION OF RUNWAY STRIP

Code No.

Length (Meter)

Width Extending laterally on

Length beyond Runway

Width Extending laterally on

Length beyond Runway

either side End/ either side of End/ of Runway Stopway Runway Stopway Centre Line (Meter) Centre Line (Meter) (Meter) (Meter)

1. <800 75 60 30 30 2. 800<1200 75 60 40 60 3. 1200<1800 150 60 75 60 4. 1800 and 150 60 75 60

above

(q) Clearway - A defined rectangular area on the ground or water under the control of the appropriate authority selected or prepared as a suitable area over which an aeroplane may make a portion of its initial climb to specified height.

(r) Stopway - A defined rectangular area on the ground at the end of take off run available prepared as a suitable area in which an aircraft can be stopped in case of an abandoned take-off.

(s) Take-off Runway - A runway intended to take-off only.

(t) Obstacle Clearance Altitude/Height (OCA/H) - The lowest altitude or the lowest height above the elevation of the relevant runway threshold or the aerodrome elevation as applicable used in establishing compliance with appropriate clearance criteria.

(u) Declared Distances:- (i) Take Off Run Available (TORA):- The length of the runway declared

available and suitable for the ground run of an aeroplane taking off.

(ii) Take Off Distance Available (TODA):- The length of take-off run available plus the length of clearway, if provided

(iii) Accelerate Stop Distance Available (ASDA):- The length of take-off run available plus the length of stopway, if provided.

(iv) Landing Distance Available (LDA):- The length of the runway declared available and suitable for the ground run of an aeroplane landing.

(v) Critical Area- Critical area is an area of defined dimensions about the localizer and glide path antenna where vehicles including aircraft are excluded during Instrument Landing System (ILS) operations. The critical area is protected because the presence of vehicles and/or aircraft inside its boundary will cause unacceptable discrepancies to the Instrument Landing System (ILS) signal in space.

64 THE GAZETTE OF INDIA : EXTRAORDINARY iPART II-SEC. 3(ii)11

ANNEXURE-III-A LIST OF AAI OPERATIONAL AERODROMES

S, NO.

AIRPORT STATE COORD. LAT /

LONG. (IN DEGREES)

ELEV. (IN MTRS.)

RUNWAY ORIENTA

TION

DIMENSION (IN MTRS.)

OWNER

1 AGARTALA TRIPURA 235326N 1403 18/36 2286X45 AM 911421E

2 AGATTI LAKSHWADEEP 104926N 4 04/22 1204 x 30 AAI ISLANDS (U.T.) 0721037E

3 AHEMDABAD GUJARAT 230414.4N 57.44 05/23 3505 x 45 AAI (SVBPI AIRPORT) 0723737.3E

4 AKOLA MAHARASHTRA 204152N 305 10/28 1219 x 45 AAI 0770332E

5 AMRITSAR (RAJA SANSI)

PUNJAB 314216N 074481 IE 229. 5

16/34 3289 x 45 AAI

6 AURANGABAD MAHARASHTRA 195152N 582 09/27 2286 x 45 AAI (CHIKAL THANA) 0752351E

7 BARAPANI MEGHALAYA 254210N 887 04/22 1829 x 45 AAI 'SHILLONG 0915152E

8 BELGAUM KMLNATAKA 155 I27N 759 08/26 1830 x 45 AM (SAMBRA) 0743707E

9 BHAVNAGAR GUJARAT 214513N 0721128E

13 07/25 1920 x 45 AAI

10 BHOPAL MADHYA 523 12/30 2045 x 45 (RAJA BHOJ

AIRPORT) PRADESH

231711N 0772017.4E

AAI

11 BHUBNESHWAR ORISSA 201448N 44.5 i4/32 2243 x 45 (BIJU PATNAIK 0854906E 05/23 1381 x 45 AAI

AIRPORT) 12 CHENNAI TAMIL NADU 215941.7N 15.84 07/25 3658 X 45 AAI

0801031.8E 12/30 2032 X 45 13 COIMBATORE

(PEELAMEDU) TAMIL NADU I10149N

0770230E 404

05/23 2290 x 45

AAI

14 COOCH BEHAR WEST BENGAL 261949N 41.5 04/22 1069 x 30 AAI 0892815E

15 CUDDAPAH ANDRA 1431N 131 11/29 1098 x 18 AAI PRADESH 07847E

16 DELHI 227 10/28 3810 x 45 DIAL DELHI IGI 283407.42N

AIRPORT (PALAM) 0770643.69E 09/27 11/29

2813 x 45 4280 x 60

IV

17 DEHRADUN UTTARAKHAND 301I25N 550 08/26 2140 x 45 AAI (JOLLYGRANT) 0781054E

18 DIBRUGARH ASSAM 27285I.7N 110 05/23 1829 x 45 IAF (MOHANBARI) 0950104.9E

19 NAGALAND 255258N 144 12/30 2290 x 45 AAI DIMAPUR

0934628E 20 GUWAHATI (LGBI ASSAM 2606 I 7.8N 49.21 02/20 2743 x 45 AAI

AIRPORT) 0913507.7E

21 GAYA BIHAR 24445IN 110 10/28 2286 x 45 AAI 0845641E

22 HUBLI KARNATAKA I52139N 659 08/26 1674 x 30 AAI 0750508E

23 HYDERABAD ANDRA 172709N 531 09/27 3103 x 45 AAI (BEGUMPET) PRADESH 0782750E

24 IMPHAL MANIPUR 244549N 774.2 04/22 2746 x 45 AAI (TULIHAL) 0935411E

[ WTI H-131:1T 3(ii)

t14141 : 3TRIRTMT

65

25 INDORE DEVI AHILYABAI

HOLKAR AIRPORT

MADHYA PRADESH

224321.9N 0754823.4E

560.8 07/25 2750 x 45 AAI

26 JABALPUR MADHYA PRADESH

231058N 0800343E

495 06/24 1988 x 45 AAI

27 JAIPUR (SANGANER)

RAJASTHAN 264926N 0754812E

385 09/27 2797 x 45 AAI

28 JHARSUGUDA ORISSA 215451N 0840303E

228 06/24 1882x45 AAI

29 MUMBAI(JUHU) MAHARASHTRA 190548N 2.74 16/34 727 x 45 AAI 0725004E 08/26 1143 x 30

30 KESHOD GUJARAT 211852N 51 05/23 1372 x 45 AAI 701610E

31 KANDLA GUJARAT 230642N 29 05/23 1524 x 30 AAI 0700605E

32 GAGGAL HIMACHAL 320954N 759.6 15/33 1372 x 45 AAI (KANGRA) PRADESH 0761542E

33 KANPUR (CIVIL) UTTAR 262625N 125 10/28 1082 x 45 AAI PRADESH 0802153E

34 KHAJURAHO MADHYA 244910N 217.4 01/19 1829 x 45 AAI PRADESH 0795512E

35 CALICUT KERALA 110817N 104 10/28 2860 x 45 AAI (KOZHIKODE) 0755701E

36 KOLHAPUR MAHARASHTRA 163955N 606.5 07/25 1372 x 45 AAI 0741729E

37 KOLKATA -WEST BENGAL 223911.0N 5 OIR/19L 3627 x 46 AAI (NSCBI AIRPORT) 0882657.25 OIL/19R 2399 x 46

38 KULLU-MANALI HIMACHAL 315237N 1088.8 16/34 1128 x 30 AAI (BHUNTAR) PRADESH 0770919E

39 NORTH ASSAM 271726N

100 04/22 2286 x 45 AAI LAKHIMPUR (LILABARI)

0940549E -

40 LUCKNOW UTTAR 264543N 122 09/27 2742 x 45 AAI (AMOUSI) PRADESH 0805301E

41 LUDHIANA PUNJAB 305120N 254 12/30 1463 x 30 AAI 0755706E

42 MADURAI TAMIL NADU 095001N 136 09/27 1826 x 45 AAI 0780522E

43 MANGALORE KARNATAKA 125743N 102.6 09/27 1625 x 45 AAI (BAJPE) 0745323.9E 06/24 2450 x 45

44 MUMBAI (CSI MAHARASHTRA 190527N 8 09/27 3489 x 45 MIAL AIRPORT) 0725200E 14/32 2925 x 45 JV

45 KARNATAKA 121345N 716 05/23 1348 x 45 AAI MYSORE 0763930E 09/27 1740x30

46 NAGPUR MAHARASHTRA 210528N 308.45 14/32 3200 x 45 MIHAN (SONEGAON) 0790259E 09/27 1957 x 45 JV

47 PANTNAGAR UTTARAKHAND 290156N 0792827E

233 10/28 1097 x 38.4 AAI

48 BIHAR 253537N 51.18 07/25 1954 x 45 AAI PATNA 0850531E

49 PORBANDAR GUJARAT 213859N 5.18 09/27 1372 x 45 AAI 0693932E

50 CHATTISGARH 211049N 313 06/24 1955 x 45 AAI RAIPUR (MANA) 0814425E

51 RAJ AHMUNDARY ANDHRA 170630N 45 05/23 1750 x 45 AAI PRADESH 0814916E

52 RAJKOT GUJARAT • 221834N 133.4 05/23 1846 x 45 AAI

0704645E

53 RANCHI JHARKHAND 231851N 646 13/31 2713 x 45 AAI (BIRSA MUNDA 0851915E

AIRPORT)

175 GI/10-9

66


[PART II-SEC. 3(ii)]

54 SALEM TAMIL NADU 114647N 300 04/22 1829 x 45 AAI 0780355E

55 SHIMLA HIMACHAL 310454N 1540 14/32 1189 x 23 AM (JUBBARHATTI) PRADESH 0770407E

56 SHOLAPUR MAHARASHTRA 173735N 481 15/33 1365 x 45 AAI 0755606E

57 SURAT GUJARAT 210647N 6 04/22 2250 x 45 AAI 0724435E

58 TIRUPATHI ANDHRA 133759N 106.75 08/26 2286 x 45 AAI PRADESH 0793230E

59 TIRUCHIRAPALLI TAMIL NADU I04557N 85 09/27 1864 x 45 AAI (TRICHY) 0784253E

60 THIRUVANANTHA KERALA 082847N 4 14/32 3398 x 45 AAI

-PURAM 0765511E 10/28 1224 x 45

61 TUTICORIN TAMIL NADU 084317N 25.6 10/28 1350 x 30 AAI (TOOTHKUDI) 0780140E

62 UDAIPUR RAJASTHAN 243702N 509 08/26 2281 x 45 AAI (MAHARANA 0735343E

PRATAP AIRPORT) 63 VADODARA GUJARAT 221946N 37 04/22 2469 x 45 AAI

0731310E 64 VARANASI U.P. 252703N 80 09/27 2206 x 45 AAI

(BABATPUR) 0825138E 65 VIJAYAWADA ANDHRA 163135N 21 08/26 1745 x 45 AAI

PRADESH 0804754E

STATE GOVERNMENT OWNED OPERATIONAL AIRPORTS

S. NO.

AIRPORT STATE COORD. LAT / LONG. (IN DEGREES)

ELEV. (IN MTRS.)

RUNWAY ORIENTA

TION

DIMENSIO N (IN

MTRS.)

OWNER

1 AIZAWL (LENGPUI) MIZORAM 235016.88N 0923736.38E

418 17/35 2500x45 SG

2 DIU UNION TERRITORY

204247N 0705514E

4.9

_

05/23 13/31

1826 x 45 1069x25

U.T.

PRIVATE AIRPORTS

S. NO.


ELEV. (IN MTRS.)

RUNWAY ORIENTA

TION.

DIMENSIO N (IN

MTRS.)

OWNER

I COCHIN INTERNATIONAL AIRPORT LTD( CIAL)

KERALA 1009I4N 0762425E

7.68 09/27 3400 x 45 PVT

2 HYDERABAD ANDHRA 171426N 617 09/27 4260x60 PVT INTERNATIONAL PRADESH 0782544E JV AIRPORT(HIAL) SHAMSABAD

3 BENGALURU KARNATAKA 131155.92N 914.68 09/27 4000x45 PVT INTERNATIONAL 774219.70E JV AIRPORT (BIAL) DEVANI IALLI

4 PUTTAPARTHY

ANDHRA PRADESH

1409N 07748E

475 09/27 2237x45 PVT

5 VIDYANAGAR KARNATAKA 151019N 502 13/31 1600 x 30 PVT 0763837E

6 MUNDRA GUJARAT 225003N 5.18 ' 05/23 1700x30 PVT 0694552E

7 JAMSHEDPUR JHARKHAND 2249N 141.7 08/26 1220 x 45 PVT. 08610E

[ Tim 3(ii)

%TIM ffiT t 1 ,r1 41 : 3MTUTTET1

67

ANNEXURE-IIIB LIST OF AERODROMES CONTROLLED BY AAI

S. NO.


ELEV. (IN MTRS.)

RUNWAY ORIENTA

TION

DIMENSIO N (IN

MTRS.)

OWNER

1 AIZAWL (TURIAL) MIZORAM 234443N 334 01/19 1190x27 AAI 0924822E

2 ASANSOL WEST BENGAL 2340N 98 10/28 1826 x 45 AAI 08701E

3 BALURGHAT WEST BENGAL 251547N 24 09/27 1097x30 AAI 0884754E

4 BEHALA WEST BENGAL 223022N 3 18/36 861 x 30 AAI 0881748E

5 BILASPUR CHATTISGARH 220000N 274 06/24 1448X45 AAI 0820400E 17/35 1455X45

6 CHAKULIA JHARKHAND 222736N 129 17/35 2221X45 AAI 0864237E

7 DEESA GUJARAT 241604N 145 06/24 1008 x 30 AAI (PALANPUR) 0721218E

8 ANDHRA 1550N 142 04/23 915X30 AAI DONAKONDA

PRADESH 7930E

9 GONDIA MAHARASHTRA 2131N 08020E

311.16 05/23 1966 x 45 AAI

10 JHANSI UTTAR 244 15/33 1295 x 45 AAI PRADESH

2529N 07834E

(UNDER ARMY)

11 JHARSUGUDA ORISSA 2155N 228 06/24 1890X45 AAI 08403E

12 JOGBANI BIHAR 2618N 59 09/27 1525X152 AAI 8718E

13 KAILASHAHAR TRIPURA 241828N 24 03/21 900X30 AAI 920033E

14 KAMALPUR TRIPURA 240754N 39 01/19 1372 x 30 AAI 0914851E

15 KHANDWA MADHYA 215125N 329 10/28 890X30 AAI PRADESH 761959E

16 KHOWAI TRIPURA 240342N 29 18/36 915X30 AM 913627E

17 KISHANGARH RAJASTHAN 2636N 480 03/21 1219 x 30 AAI 07449E

18 KOTA RAJASTHAN 250935N 273 08/26 1220 x 38 AAI 0755056E

19 LALITPUR MADHYA 244258N 367 10/28 1890 x 45 AAI PRADESH 0782503E

20 MALDA WEST BENGAL 250040N 24 11/29 1099X30 AAI 880750E

21 MUZZAFARPUR BIHAR 260701N 53 11/29 1219 x 30 AAI

0851854E

22 ANDRA 1711N 552 14/32 914 x 23 AAI NADIRGUL PRADESH 07833E

23 MADHYA 243915N 424 17/35 1538X18 AAI PANNA PRADESH 810546E

24 ARUNACHAL 2806N 157 17/35 1006X18 AAI PASSIGHAT PRADESH 9523E

25 PONDICHERRY PONDICHERRY 1 15759N 43 07/25 1222 x 30 AAI 0794843E

26 RAXAUL BIHAR 2658N 79 10/28 1097X30 AAI

8450E

27 RUPSI ASSAM 2608N 40 05/23 1829X45 AM 8945E

28 DELHI DELHI 283504N 212 . 12/30 1180 x 45 AAI

(SAFDARJUNG) 0771229E

68


[PART II—Sec. 3(11)]

29 SATNA MADHYA

PRADESH 243345N 0805116E

319 11/29 1062X30 AAI

30 VELLORE TAMIL NADU 125424N 0790406E

233 07/25 793 x 150 AAI

31 WARANGAL ANDHRA PRADESH

175452N 0793608E

284 09/27 1859 x 45

AAI

ANNEXURE - IIIC

LIST OF DEFENCE AERODROMES S. NO.


ELEV. (IN MTRS.)

RUNWAY ORIENTA

TION

DIMENSION (IN MTRS.)

OWNER

1 AGRA UTTAR 270932N 167.7 05/23 2744X45 IAF PRADESH 775730E

2 ALLAHABAD UTTAR 252626N 97.2 12/30 2477X45 IAF PRADESH 814409E

3 ALONG ARUNACHAL 281035N 250 05/23 914 x 45 IAF PRADESH 0944824E

4 BAGDOGRA WEST BENGAL 264108N 126 18/36 2744 x 45 IAF (SILIGURI) 0881948E

5 BENGLURU (HAL) KARNATAKA 125703N 888 09/27 3306 x 45 HAL 0773957E

6 BHUJ GUJARAT 231713N 78 05/23 2515 x 45 IAF (RUDRAMATA) 0694015E

7 BIKANER (NAL) RAJASTHAN 280418N 215 05/23 2746 x 45 IAF 0731225E

8 CHANDIGARH UNION 3040N 314 11/29 2744 x 45 IAF TERRITORY 07647E

9 DAPARIJO ARUNACHAL 2800N 244 07/25 1001 x 27 IAF PRADESH 09411E

10 GOA (DABOLIM) GOA 152247.41N 46 08/26 3430 x 45 NAVY 0734940.05E

11 GORAKHPUR UTTAR 264429N 78 11/29 2744 x 45 IAF PRADESH 0832709E

12 GWALIOR MADHYA 261730N 188 06/24 2744 x 45 IAF PRADESH 0781341E

13 JAISALMER RAJASTHAN 2653N 236 04/22 2744 x 45 IAF 07052E

14 JAMMU J & K 234132N 291 18/36 2042 x 45 IAF/CE 0745024E

15 JODHPUR RAJASTHAN 26125N 217 05/23 2743 x 45 IAF 0730308E

16 JORHAT ASSAM 2644N 91 04/22 2652 x 45 IAF 09411E

17 KANPUR UTTAR 2624N 124 09/27 2744 x 45 IAF (CHAKERI) PRADESH 08025E

18 LEH J & K 3408N 3256 07/25 2922 x 45 IAF 07733E

19 OZAR (NASIK) MAHARASHTRA 2007N 598 09/27 3000 x 45 IAF 07355E -

20 PATHANKOT PUNJAB 321402N 312 01/19 2744 x 45 IAF 0753802E

21 PORT BLAIR ANDAMAN I138549N 5 04/22 3414 x 45 INDIAN (VEER SAVARKAR ISLAND 0924406E NAVY AIRPORT)

22 PUNE MAHARASHTRA 183458N 592 IAF (LOHEGAON) 0735513E

10/28 2535 x 45

23 SILCHAR ASSAM 245448N 103 06/24 1785 x 45 IAF (KHUMBIGRAM) 092585IE

24 SRINAGAR J & K 3359N 1656.5 13/31 3658 x 45 IAF 07447E

25 TEZPUR ASSAM 2643N 70 05/23 2744 x 45 IAF 09247E

26 VISHAKAPATNAM ANDHRA 174316N 3 05/23 1829 x 45 NAVY PRADESH 0831329E 10/28 3048 x 45

[ s7T1T II —"WM 3(ii) 'WM TT 7771TX : 3TfITIITTuT

69

Annexure III D

Stand alone Aeronautical Communication Stations

S. No.

Station Name of the Facility

Coordinates Coord N (WGS

84) Coord E (WGS -

84) 1. Aligarh CVOR/DME(HP) 27 49' 45.5" 78 10' 42"

2 Behrampur MSSR 19 26'00" 84 52' 08"

3 Bellary DVOR/DME(HP) 15 09'54.4" 76 52' 50"

4 Bikaner-Lunka 1 DVOR/DME(HP) 28 33' 09.84" 77 47' 15.61"

5 Bikaner - Lunka 2

DVOR/DME(HP) 28 11' 20.422"

74 06' 41.267"

6 Chillarki CVOR/DME(HP) 28 20' 51.2" 76 39' 20.2"

7 Gulbarga DVOR/DME(HP) 17 18' 48.8" 76 48' 11"

8 Jalalabad CVOR/DME(HP) 27 41' 39.6" 79 42' 44.7"

9 Jharsuguda NDB 2153' 47.6" 84 02' 19.5"

10 Kanchipuram DVOR/DME(HP) 12 47' 1 5.1" 79 42' 44.7"

11 Katihar NDB 25. 34'1.7" 8733' 20.6"

12 Keshod NDB 21 18' 53" 7016' 10"

13 Khammam NDB 17 15' 45" 80 08' 15"

14 Kishanganj NDB 26 06' 45" 87 56' 30.3"

15 Pratap' garh DVOR/DME(HP) 24 02' 13.65" 74 44' 38.16"

16 Rajamundri NDB 17 06' 31" 81 49' 18"

17 Sakras CVOR/DME(HP) 27 50' 54.4" 77 00' 29.6"

18 Sampla CVOR/DME(HP) 28 49' 11.1" 76 49' 9.6"

19 Sikndrabad CVOR/DME(HP) 28 23' 36.2" 77 42' 29.2"

20 Songarh NDB 21 10' 2.5' 73 33' 57.4"

21 Tuticorin NDB 08 43' 32.2" 78 01' 32.5"

22 Vikarabad NDB 17 20' 3.8" 77 53' 55.5"

!T.} E

QV

C)

1.r)

' ft 17. /

04-11

-.,11 E i

P -.7 i

70 THE GAZETTE OF INDIA : EXTRAORDINARY (PART II—SEC. 3(ii)]

Annexure HI E

List of aerodromes for which Government has given "in-principle" approval

for setting up of aerodromes

S.

No. Name

State/ Union

Territory

Location Elevati-

on

Meters

(feet)

R/w

Directi-

ons

Dimen-

sions

Meters

(feet)

Latitude (North) LongitudA (East)

1. Dabra Madhya

Pradesh 25°49'42.8"N 078° '1.7"E ' 240 R09/27 3000x45

2. Navi

Mumbai Maharashtra 18°59' 33"N 073°04' 18"E 5.00 R08/26 3700x60

3. Pakyong Sikkim 27°13' 58.2691N 088°35' 18.7927 E 1321.27 R02/20 1700x30

4. Durgapur West Bengal 23°37' 27.7" N 087°14' 32.5"E 85 R16/34 3315x45

OUTER CONICAL OUTER TRANSITIONAL

OUTER HORIZANTAL SURFACE

° From Rwy extremity

°° From Rwy strip

OM

[ %TM II — tgus 3(d) ]

1-1Trd : 311:11VITUT

71

Appendix A -2

Line Drawn from

Antenna pedestal;

to 10 % below

MSA at 25 NM

Slo e= 05m/mtr

Beyond Point A all obstructions having azimuth width less than o.4 degree on RADAR Antenna can be permitted above this line Subjected to other conditions in para 2.5 and restrictions from AGA & PAN-OPS

H - 3

- ►

500 M

72 THE GAZETTE OF INDIA : EXTRAORDINARY I PART I i-SEC. 3(ii)I

Appendix B

Fig 1 Criteria for height restriction with respect to ASR

Beyond Point A all obstructions having azimuth width less than o.4 degree ON RADAR Antenna can be permitted above this line subjected to other conditions in para 2.6 and restrictions from AGA & PAN-OPS

Angle Tilt angle of the antenna or 0.5 degree whichever is higher

SI4e=0.Qm/mtr

[ 1717 3(ii) 17117 tiszuma : 311:1TITRTT

73

Appendix C

200 M

H

H - 5

Fig 2 Criteria for height restriction with respect to ARSR

175 GI/10-10

Appendix D

•

VOR or ND8 facility

7.8°,NOR-113.3°MDB 1

I 3.7km (2.014M)/VOR Nominal Muhl: path —

4.6km (2.5NM)/NDB

TH

E G

AZ

ET

TE

OF

IND

I A : E

XT

RA

OR

DIN

AR

Y

— FINAL

POACH A REA r'A "=',N f'=") - KLA N'):!1

1(n )E

"V

A I

Runway I

[ %MT 3(n) ] 1;1Tff : 3114TETMIT 75

Appendix E

Runways 4000M Bldg. providing shielding

CONICAL SURFACE CONICAL SURFACE

C • NICAL SURFACE

1LLUST DATION OF SHIELDING BENEFITS

1, . CONICAL SURFACE

WIM•41.1l: 674 Wan • samo

sa bu:kft

INNER HORIZONTAL SURFACE

/rejenta Irthind th

height as lat. .

Projected behind the building-same

height as building

Bldg. prowling shielding

Bldg. providing shielding INNER HORIZONTAL

SURFACE

Inner approach St ip

Inner horizontal

1—Conical –

4—B

Approach

1111 Inner horizontal

Approach Transitional •.

inner horizontal

Inner approach

Section B-B

76 THE GAZETTE OF INDIA : EXTRAORDINARY P n R i I I—Sec. 3(ii)j

Appendix F-1

Diagrams of Obstacle Limitations Surfaces, ILS Critical Areas and Shielding

Benefits

SectrctArA

ObsInde limnitaco staketS

[ WTI II —rous 3(11) ]

'WM TiT thrl 41 : 3114171MT

77

Appendix P -2

Inner approach Balked landing

Inner transitional

Balked Inner transitional

landing

Section A-A

Inner transitional Inner horizontal

Balked landing

Section B-B

Inner approach, inner transitional and balked landing obstacle limitation surfaces

101.1)

E .3

3S—

ii 1/

1Vd

1

OBSTACLE LIMITATION SURFACES Note.—The figure shows the obstacle limitation surfaces at an aerodrome with two runways, an instrument runway and a non-instrument runway. Both are also take-off runways.

Take -oll climb surface 15000m 3.4 Slope 2%

Inner horizontal sof lac Instrument runways

4000m 3500m 34 1,2

1114•1111/.. wr

- T7:..isurlat c;

Slope 143% 3,4

Take-oll climb surface

15000m 3,4

2500m 2 1600m 1

Slops 2% 4% 5%

Approach seduce Non-inseurnent runway

3 000 m 3,4 2500 m 2 1 600 m I

Code number 4 3 2

tr-n rk

Critical Area of LLZ

Runway

12(

300m or near end of the Rwy whichever Is the greater.

[ (!

!)£ 9r

1E

-II lat

I

Aft

80


(PART II—Sec. 3(ii)

Appendix F-5

Printed by the Manager, Government of India Press, Ring Road, Mayapuri, New Delhi-110064

and Published by the Controller of Publications, Delhi-110054.

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