VOHS AD 2.1 AERODROME LOCATION INDICATOR AND NAME

VOHS - RAJIV GANDHI INTERNATIONAL AIRPORT , SHAMSHABAD

VOHS

AD 2.2

AERODROME GEOGRAPHICAL AND ADMINISTRATIVE DATA

1

Aerodrome reference point coordinates and its site

171426N 0782544E

North of PTB, ARP Elevation 1975 ft

2

Direction and distance of aerodrome reference point from the center of the city or town which the aerodrome serves

Bearing 210 DEG/20 KM from Husain Sagar

3

Aerodrome elevation and reference temperature

2030 FT / 39.0 DEG C

4

Magnetic variation, date of information and annual change

1.25 DEG W (2010) /0.01667 DEG E

5

Name of aerodrome operator, address, telephone, telefax, e-mail address, AFS address, website (if available)

GMR Hyderabad International Airport Ltd. Shamshabad, Ranga Reddy- Dist,

Telangana, PIN-500108,

Telephone:

(91) 40 67394129

Fax:

(91) 40 67395559

AFS:

----

Email:

ceo.ghial@gmrgroup.in

6

Types of traffic permitted (IFR/VFR)

IFR/VFR

7

Remarks

1. Air Traffic Services:

General Manager (ATM)

Airports Authority of India,

Shamshabad, Ranga Reddy- Dist, Telangana. PIN-500108

Tel: +91-40-2400830324005201;

Fax: +91-40-24008307

Email: gmatmhial@aai.aero

2. Vertivcal Datum : EGM08

All Coordinates are in WGS-84

3. AD Reference Code: 4F

VOHS

AD 2.3

OPERATIONAL HOURS

1

Aerodrome Operator

Mon to Fri: 0330-1230 UTC ( 0900-1800 IST )

Sat: 0330-0730 UTC ( 0900-1300 IST )

Sun & Holiday: Closed

2

Custom and immigration

H24

3

Health and sanitation

H24

4

AIS briefing office

H24

5

ATS reporting office (ARO)

H24

6

MET Briefing office

H24

7

Air Traffic Service

H24

8

Fuelling

H24

9

Handling

H24 Prior Arrangement

10

Security

H24

11

De-icing

NIL

12

Remarks

1. The approved hourly RWY traffic handling capacity is as follows:

For RWY 27L/09R:

MAX NR of ARR and DEP--42

MAX NR of ARR only --34

MAX NR of DEP only --31

2. For RWY 27R/09L when RWY 27L/09R is taken for schedule

maintenance:

(a) Case 1-

When RWY27L/09R is not available for taxiing purpose:

MAX NR of ARR and DEP --29

MAX NR of ARR only --18

MAX NR of DEP only --22

(b) Case 2-

When RWY 27L/09R is available for taxiing purpose between

taxiways A1 and A3 and between taxiways A8 and A10:

MAX NR of ARR and DEP --33

MAX NR of ARR only --22

MAX NR of DEP only --26

3. Airlines are required to share with airport Operator (GMR - RGIA,

Hyderabad) any reports of reportable incidents which occur on

the ground at RGI Airport or during the initial (take off) or final

(approach & landing) phases of flight to or from RGI Airport

VOHS

AD 2.4

HANDLING SERVICES AND FACILITIES

1

Cargo-handling facilities

By GMR Hyderabad Air Cargo ( A Division of GMR Air Cargo and

Aerospace Engineering Ltd.)

2

Fuel and Oil types

JET A1

3

Fuelling facilities and capacity

Hydrant and bowzer (12 Dispensers + 07 Refuellers)

4

De-icing facilities

NIL

5

Hangar space for visiting aircraft

NIL

6

Repair facilities for visiting aircraft

Available with AIESL & GMRATL with Hanger facility

7

Remarks

NIL

VOHS

AD 2.5

PASSENGER FACILITIES

1

Hotel(s) at or in the vicinity of aerodrome

Novotel Business Brand Hotel with 305 rooms at a distance of 2.75km from PTB and hotels in Hyderabad city.

2

Restaurant(s) at or in the vicinity of aerodrome

Level C: KFC, McDonalds, Coffee Hut, Food street (Multi cuisine Restaurant). Level D: Cafe Coffee Day, Subway, Karachi Bakery, McDonalds, Coffee Hut,

Hatti kapi

Level F: At visitors’ gallery- Coffee Hut, Forecourt : Coffee Café, Check In- Coffee club, Domestic SHA: Monsoon Bar, Barista coffee, Indian Paradise, KFC, Taste of India Domestic bus gates: Coffee club International SHA: Dosa Factory, Indian Paradise, Grab and Fly, Khao Gali, Coffee club

Level B & E: Canteen (for Employees of GMR & Airlines)

3

Transportation possibilities

Taxi (Prepaid & Metered) Bus services (TSRTC Town- Volvo, TSRTC

Pushpak), Free shuttle bus from Airport to PTC

4

Medical Facilities

24 hrs Medical and Dental facilities provided by Apollo Hospital Enterprises

Limited (One full-fledged medical centre housing minimum 17 beds), First Aid

counters at Level D, E and F.

5

Bank and post office at or in the vicinity of

aerodrome

Banks: Canara Bank at Level C and State Bank of India at Level F

ATM: Total 13 Nos. (Level C- 2, Level D- 6 & Level F- 5) Foreign exchange counters: Total 5 Nos. (Level F- 2,Level E- 1 & Level D- 2)

6

Tourist office

TSTDC (Telangana State Tourism Development Corporation at Level D)

7

Remarks

APTDC (Andhra Pradesh Tourism Development Corporation at Level D)

VOHS

AD 2.6

RESCUE AND FIRE FIGHTING SERVICES

1

Aerodrome category for fire fighting

Within ATS HR: CAT-9 (can be upgraded to CAT- 10 with 01 Hour prior notice)

2

Rescue equipment

Available as per Airport Services Manual Part1 for CAT- 9

3

Capability for removal of disabled aircraft

1. The critical aircraft for the airport is B744/B773.

2. Primary responsibility for removal of disabled aircraft rests with the concerned airline.

3. The airlines may contact ‘Aerodrome Coordinator for Disabled Aircraft Removal Operations’ for coordinating with the agencies having Disabled Aircraft Recovery Kit.

4. Contact Details of Aerodrome Coordinator for Disabled Aircraft Removal Operations:

Chief Operating Officer

Contact No : +91-40-66602100

Email : Resource.Planning@gmrgroup.in

4

Remarks

NIL

VOHS

AD 2.7

SEASONAL AVAILABILITY CLEARING

1

Type(s) of clearing equipment

NIL

2

Clearance priorities

NIL

3

Remarks

NIL

VOHS

AD 2.8

APRONS, TAXIWAYS AND CHECK LOCATIONS/POSITIONS DATA

1

Designation, surface and strength of aprons

Surface: Rigid

Strength: See AD 2.23

2

Designation, width, surface and strength of

taxiways

See AD 2.23

3

Location and elevation of altimeter checkpoints

Location All aircraft stands on the passenger terminal apron. Elevation ---

4

Location of VOR checkpoints

At Runway holding positions on TWYs A1, A2, A3 & A9.

5

Position of INS checkpoints

NIL

6

Remarks

Refer Aircraft Parking / Docking for Details

VOHS

AD 2.9

SURFACE MOVEMENT GUIDANCE AND CONTROL SYSTEM AND MARKINGS

1

Use of aircraft stand identification signs, taxiway guidelines and visual docking/parking guidance system at aircraft stands

Aircraft Stand ID signs: All stands are provided with stand identification sign and straight lead-in lines Taxiing guidance signage are provided at all intersections and straight sections as recommended by ICAO annex 14.

Air Bridges: 44 (Total ) -Stand No. 3, 4, 5, 6, 7, 8, 9, 13, 14, 42, 43, 44, 45, 46, 47, 48, 49, 50, 51, 52, 53, 54L, 54R, 55L, 55R, 56L, 56R , 57L, 57R, 58L, 58R, 59L, 59R, 60L, 60R, 61, 62, 63L, 63R, 64, 66, 67, 68 & 69.

Visual Docking Guidance Systems (VDGS/A-VDGS):56 (Total) From Stand no. 3, 4, 5, 6, 7, 8, 9, 13, 14, 39, 40, 41,42, 43, 44, 45, 46, 47, 48, 49, 50, 51, 52, 53, 54L, 54, 54R, 55L, 55, 55R, 56L, 56, 56R, 57L,57, 57R, 58L, 58, 58R, 59L, 59, 59R, 60L, 60, 60R, 61, 62, 63L, 63, 63R, 64, 65, 66, 67,

68 & 69.

For proper response from VDGS/A-VDGS pilots are advised not to exceed taxi speed of 4m per sec while docking

2

Runway and taxiway markings and lights

RWY Markings

RWY 09R/27L : Designation /THR / TDZ / CL / Aiming Point / Side strip

RWY 09L/27R: Designation / THR / TDZ / CL / Aiming Point / Side strip / Displaced THR

RWY Lights

RWY 09R: THR/ EDGE/ TDZ/ CL/ END AND CAT-II APP

RWY 027L: THR/ EDGE/ CL/ END AND CAT-I APP

RWY 09L: THR/ EDGE/ THR IDENT LGT/ END AND CAT-I APP

RWY 27R: THR/ EDGE/ THR IDENT LGT/ END AND CAT-I APP

TWY Marking

CL / EDGE / RHP / Enhanced TWY CL / Intermediate Holding PSN Markings. Enhanced taxiway centerline marking provided on taxiways A1, A2, A3, A8, A9, A10, B,B1,B2, B3, B4, B5 and B6 Mandatory instruction marking provided on Taxiways A1,A2,A3,A8,A9,A10,B1,B2, B3, B4,B5 and B6

TWY Lights

TWY A1, A2, A3, A8, A9, A10, RET L1, L2, L3, L4, R1, R2, R3, R4, B2, B3, B4, B5, E3, E4, TXL H1, J1, J2, J3, C, C1 with Inset CL LGT & Elevated Edge LGT (for EAST edge H1 & WEST Edge J3). TWY B (between B2 & B6) with inset CL LGT on straight portion and Elevated Edge LGT at junctions. TWY B (west of B6), B1, B2, B6, E, M, M1, K, K1, D, C, TXL H, H1, TXL K3 (North of TXL K3) with Elevated Edge LGT only. Additionally TWY Edge LGT AVBL for RWY 09L / 27R and portion RWY 09R-27L between TWY A1 to A3 and TWY A8 to A10 when used for Taxi Purpose.

3

Stop bars (if any)

Provided on TWY A1, A2, A3, A8, A9 & A10

Stop bar lights provided on TWY B2, B3, B4, B5 and B6 at RWY 09L/27R

HLDG PSN.

Runway Guard Lights: At every runway holding position point, both sides of taxiway with a pair of elevated guard lights flashing alternate yellow facing the taxiways (A1, A2, A3, A8, A9, A10, B1, B2, B3,B4, B5 & B6)

4

Remarks

Surface Movement Guidance and Control radar has been provided

VOHS

AD 2.10

AERODROME OBSTACLES

In circling area and at AD

TOWERPOLE

171406171340.5N7N

07825180782656.1E

2258 2034 FT

LGTDNIL

Lightening Arrester on ATC TowerMET Antenna Pole

In circling area and at AD

OTHER

171339.8N

0782656.2E

2033 FT

NIL

Electrical Panel Top

In circling area and at AD

ANTENNANAVAID

171339.8N1N

07826550782457.0E7E

2052 2019 FT

NILLGTD

MET GP Antenna 09R Top

In circling area and at AD

ANTENNANAVAID

171340.7N8N

07826560782658.1E2E

2034 2072 FT

NILLGTD

Antenna

GP Antenna 27L Top

In circling area and at AD

BUILDING

171340.8N

0782657.9E

2033 FT

LGTD

GP HutHut 27L Top

In circling area and at AD

NAVAIDBUILDING

171340171339.8N2N

07826580782458.2E1E

2070 1981 FT

LGTD

GP 27 Hut 09R Top

In circling area and at AD

NAVAID

171340.8N

0782700.7E

2042 2043 FT

LGTD

GP Monitor Antenna Top27L Monitor

Antenna Top

In circling area and at AD

NAVAID

171349171339.6N1N

07827000782455.2E1E

2047 1991 FT

LGTD

GP 09R Monitor

Wind Sock Antenna Top

In circling area and at AD

BUILDINGTOWER

171337171405.8N7N

07824580782517.0E9E

1984 2258 FT

LGTD

Lightening Arrester

Obstacle Light on MET HutATC Tower

In circling area and at AD

OTHERBUILDING

171338171337.2N8N

07825000782457.2E9E

1992 1986 FT

LGTD

Obstacle Light on MET Instrument TopHut

In circling area and at AD

NAVAIDANTENNA

171339.1N2N

07824550782500.1E8E

1991 1976 FT

LGTD

GP Monitor Antenna TopRVR Antenna

In circling area and at AD

NAVAIDPOLE

171339171224.1N4N

07824570782617.7E4E

2018 2184 FT

LGTD

GP 09 Top

TS Electricity Pylon Mast

In circling area and at AD

BUILDINGPOLE

171339171224.1N5N

07824580782609.0E7E

1979 2189 FT

LGTD

GP Hut Top

TS Electricity Pylon Mast

In circling area and at AD

BUILDINGNAVAID

171339171349.2N6N

07825000782700.8E2E

1976 2047 FT

LGTD

RVR Windsock Top

In circling area and at AD

NAVAID

171347171348.9N0N

0782456.1E

1993 FT

LGTD

Wind Sock Windsock Top

VOHS

AD 2.11

METEOROLOGICAL INFORMATION PROVIDED

1

Name of the associated meteorological office

VOHS International (AMO)

2

Hours of service and, where applicable, the designation of the responsible meteorological office outside these hours

H24

3

Office responsible for preparation of TAFs and periods of validity and interval of issuance of the forecasts

AMO Shamshabad (VOHS)

09 HRS & 30

HRS

4

Availability of the trend forecast for the aerodrome and interval of issuance

Trend

H24. Half hourly

5

Information on how briefing and/or consultation is provided

Personal ConsultationH24. Briefing provided mainly OLBS,Partial self-briefing and Telephone to Forecaster.

6

Types of flight documentation supplied and language(s) used in flight documentation

Charts, abbreviated plain language text.

ENGLISH

7

Charts and other information displayed or available for briefing or consultation

SWH (National), SWM (National), SW International, Wind/Temp Charts (FL 050 to FL 530), SIGMET charts from OLBS

8

Supplementary equipment available for providing information on meteorological conditions, e.g. weather radar and receiver for satellite images;

TELE 040-24005219/24008233,FAX 040- 24008269

9

The air traffic services unit(s) provided with meteorological information

Shamshabad / Begumpet ATC and ACS

10

Additional information, e.g. concerning any limitation of service.

Integrated WX system RWY 09R/27L AVBL for OPR purpose. RVR INSTR RWY 09R/27L available.

VOHS

AD 2.12

RUNWAY PHYSICAL CHARACTERISTICS

09R

88.91 DEG

4260 x 60 M

77/F/B/W/T

THR:

171342.91N

0782446.11E

RWY END:

171344.89N

0782710.27E

27L

268.91 DEG

4260 x 60 M

77/F/B/W/T

THR:

171344.89N

0782710.27E

RWY END:

171342.91N

0782446.11E

09L

88.91 DEG

3707 x 45 M

77/F/B/W/T

THR:

171350.35N

0782454.80E

RWY END:

171352.08N

0782700.25E

27R

268.91 DEG

3707 x 45 M

77/F/B/W/T

THR:

171352.08N

0782700.25E

RWY END:

171350.35N

0782454.80E

THR: 19711970.0FT

TDZ: 1978.0FT

0.95%

NIL

NIL

4380 x 280 M

THR: 2026.0FT

TDZ: 20202026.0FT

0.95%

NIL

NIL

4380 x 280 M

THR: 1974.0FT

TDZ: 1984.0FT

0.92%

NIL

NIL

3827 x 280 M

THR: 2030.0FT

TDZ: 20162030.0FT

0.92%

NIL

NIL

3827 x 280 M

285M x 150M

Existing

1. RUNWAY PCN: First 150M both ends 88/R/C/W/T

2. Vertical datum: EGM08

3. 0.029% (Min) 0.95% (Max) from RWY09R towards RWY27L Transverse slope 1.50% (throughout)

285M x 150M

Existing

1. RUNWAY PCN: First 150M both ends 88/R/C/W/T

2. Vertical datum: EGM08

3. 0.029% (Min) 0.95% (Max) from RWY09R towards RWY27L Transverse slope 1.50% (throughout)

283M x 90M

Displacement 310 M

Existing

Instrument non- precision approach runway

0.084% (min) 0.918% (max) from RWY09L towards RWY27R transverse

slope1.5% (throughout)

250M x 90M

Displacement 343 M

Existing

Instrument non- precision approach runway

0.084% (min) 0.918% (max) from RWY09L towards RWY27R transverse

slope1.5% (throughout)

VOHS

AD 2.13

DECLARED DISTANCES

09R

4260

4260

4260

4260

27L

4260

4260

4260

4260

09L

3707

3707

3707

3707

The displaced portion of RWY 09L and 27R, shall not be available as part of TORA

27R

3707

3707

3707

3707

The displaced portion of RWY 09L and 27R, shall not be available as part of TORA

VOHS

AD 2.14

APPROACH AND RUNWAY LIGHTING

09R

CAT II

900 M

LIH

Green

PAPI

LEFT/3.00 DEG

MEHT

(73.82FT)

900 M

27L

CAT I

900 M

LIH

Green

PAPI

LEFT/3.00 DEG

MEHT

(73.82FT)

NIL

09L

CAT I

900 M

LIH

Green

PAPI

LEFT/3.00 DEG

MEHT

(73.82FT)

NIL

27R

CAT I

900 M

LIH

Green

PAPI

LEFT/3.00 DEG

MEHT

(73.82FT)

NIL

4260 M

15 M

LIH

White

4260 M

60 M

White

LIH

Red

NIL

1.Runway centerline lights variable white from the THR to the point 900 m

from the runway end; alternate red and variable white from 900 m to 300

m from the runway end; and red from 300 m to the runway end

2.Runway edge lights variable white, Last 600m yellow towards the landing

direction

4260 M

15 M

LIH

White

4260 M

60 M

White

LIH

Red

NIL

1.Runway centerline lights variable white from the THR to the point 900 m

from the runway end; alternate red and variable white from 900 m to 300

m from the runway end; and red from 300 m to the runway end.

2.Runway edge lights variable white, Last 600m yellow towards the landing

direction

NIL

3707 M

60 M

White

LIH

Red

NIL

1.Runway edge lights variable white, Last 600m yellow towards the landing

direction

2.Threshold identification light available (flashing white)

NIL

3707 M

60 M

White

LIH

Red

NIL

1.Runway edge lights variable white, Last 600m yellow towards the landing direction

2.Threshold identification light available (flashing white)

VOHS

AD 2.15

OTHER LIGHTING, SECONDARY POWER SUPPLY

1

Location, characteristics and hours of operation of aerodrome beacon/identification beacon (if any)

ABN

On top of ATC Tower, 24FPM, white and green, 400,000cd Switched on only during the operation of AD Ground LGTs.

IBN

NIL

2

Location and lighting (if any) of anemometer/landing direction indicator;

LDI

Illuminated, White light between Runways 09R/27L & 09L/27R, 145M north of Runway 09R-27L centreline & 80M south of Runway 09L-27R (171348.534N, 0782552.001E) Horizontal and Perpendicular segment are of 4M length with 11 lights each spaced equidistant. Each bulb is of 50W halogen with White lens.

Anemometer

1. For RWY 09R & 27L one each South of RWY near TDZ coordinates

a. Near RWY 09R : 171339.03 N 0782500.69 E

b. Near RWY 27L : 171340.08 N 0782656.04 E

2. For RWY 09L & 27R one each North of RWY near TDZ coordinates

a. Near RWY 09L : 171354.07 N 0782508.07 E

b. Near RWY 27R : 171355.82 N 0782647.08 E

3

Taxiway edge and taxiway centre line lights;

Edge

Elevated blue lights placed at 3m from taxiway edge. The lateral distance between lights are 60m on straight section and on curved portion varies on the radius of the curve.

Centre Line

Inset Bidirectional Green Light with the gap of 15 M & 30 M on Straight Sections. On Rapid Exit TWY The CL LGT are Unidirectional LGT Showing Green towards the Runway. TWY Edge LGT are Elevated Blue LGT installed at 3 M from the TWY Edge with the gap of 60 M on Straight

sections.

4

Secondary power supply including switch-over time;

DG power as standby, 15 sec switchover time. Critical circuits provided with UPS for zero percent switchover time (Threshold/End/Rwy center line/Edge lights)

5

Remarks

WDI: Two

(i) North of RWY 27L Beginning

(ii) North of RWY 09R Beginning.

Colours: Orange & white bands &illuminated.

VOHS

AD 2.16

HELICOPTER LANDING AREA

1

Geographical coordinates of the geometric centre of touchdown and lift-off (TLOF) or of each threshold of final approach and take-off (FATO) area

Not Established

2

TLOF and/or FATO area elevation:

Not Established

3

TLOF and FATO area dimensions to the nearest metre or foot, surface type, bearing strength and marking;

Not Established

4

True bearings of FATO;

Not Established

5

Declared distances available

Not Established

6

Approach and FATO lighting;

Not Established

7

Remarks

Not Established

VOHS

AD 2.17

AIR TRAFFIC SERVICE AIRSPACE

1

Airspace designation, geographical

coordinates and lateral limits

CTR: Area bounded by lines joining points 172410N 0783743E then along the clockwise arc of a circle of 15NM radius centred on 171426N 0782544E to 172708N 0781717E then along the clockwise arc of a circle of 10NM radius centred on 172712N 0782745E to point of origin.

2

Vertical limits

5500 FT AMSL

3

Airspace classification

D

4

Call sign and language(s) of the air

traffic services unit providing service;

Shamshabad TWR, English

5

Transition altitude

7000 FT

6

Hours of applicability

H24

7

Remarks

NIL

VOHS

AD 2.18

AIR TRAFFIC SERVICES COMMUNICATION FACILITIES

1

2

3

4

OTHER

Hyderabad Control/ Radar

120.950 MHZ

OTHER

Hyderabad Control/ Radar

128.350 MHZ

OTHER

Shamshabad Delivery

121.625 MHZ

TWR

Shamshabad TWR

118.200 MHZ

TWR

Shamshabad TWR

118.450 MHZ

ATIS

----

126.475 MHZ

ALRS

----

121.500 MHZ

RADAR

Hyderabad APP/Radar

120.250 MHZ

RADAR

Hyderabad APP/Radar

125.550 MHZ

SMC

Shamshabad GND

118.200 MHZ

SMC

Shamshabad GND

121.850 MHZ

5

6

7

H24

200 NM Coverage

H24

200 NM Coverage

H24

5 NM Coverage

H24

(ALTN Frequency) 25 NM coverage

H24

25 NM coverage

H24

75NM Coverage

H24

50 NM Coverage

H24

75NM Coverage

H24

75 NM Coverage

H24

ALTN Frequency 5 NM Coverage

H24

5 NM Coverage

VOHS

AD 2.19

RADIO NAVIGATION AND LANDING AIDS

1

2

3

4

LOC 09R

CAT II

IHBD

108.500 MHz

H24

LOC 27L

CAT I

ISAM

110.900 MHz

H24

LOC 09L

CAT I

IHYN

108.900 MHz

H24

GP 09R

IHBD

329.900 MHz

H24

GP 27L

ISAM

330.800 MHz

H24

GP 09L

329.300 MHz

H24

DME ILS 09R

IHBD

CH22X

H24

DME ILS 27L

ISAM

CH46X

H24

DME ILS 09L

IHYN

CH26X

H24

VOR/DME

HIA

113.800 MHz

CH85X

H24

Geographical

coordinates of the

position of the

transmitting

antenna

Elevation of

transmitting

antenna of

DME/

elevation of

GBAS

reference point

Service volume radius

from the GBAS

reference point

Remarks

5

6

7

8

171345.1N

0782725.3E

1. 25NM Coverage

2. ILS 09R (Freq 108.500 MHz) working within CAT-1 limit. LOC 09R is restricted to 300FT above RWY threshold due siting

171342.7N

0782431.3E

25 NM Coverage

171352.5N

0782726.4E

Localizer is restricted in 150 Hz Sector upto 30 degree.

171339.0N

0782457.7E

Glide angle 3.0 DEG

171340.7N

0782658.1E

10 NM coverage

171354.5N

0782506.0E

1. GP Coverage is restricted at 10NM above 2000 FT HAT (Height above threshold)

2. Glide Angle : 3.0 Deg.

171338.9N

0782457.7E

1990 FT

Vertical Datum: EGM-08

171340.7N

0782658.1E

2067 FT

1. 25 NM Coverage 2. Vertical Datum: EGM-08

171354.5N

0782506.0E

1994 FT

171346.7N

0782420.7E

2003 FT

(I) Gravity Model: EGM-08

(II) DME colocated with DVOR.

VOHS

AD 2.20

LOCAL AERODROME REGULATIONS

1. RWY 09L/27R available for day and night operations and is a dependent RWY i.e. at a time RWY 09L/27R or RWY

09R/27L can be used for landing or take-off.

2. ATC initiated continuous descent OPR (CDO) in vogue WI Hyderabad TMA, whenever feasible, DIST to touchdown and

CLR limit will be specified by ATC for continuous descent OPR. Pilots are required to REP fuel saving for the CDO after

LDG on 121.850 MHZ and send a detail debrief to email: vohs.ops@aai.aero

3. Runway Capacity Enhancement Measures:

3.1 Departure Procedure

3.1.1 Taxiing aircraft should maintain a minimum taxiing speed of not less than 15 knots on the straight portion of taxiways

and between 8-12 knots during turning manoeuvres during fair weather conditions.

3.1.2 ATC may alter the departure sequence of an aircraft, which is not adhering to the procedure enumerated in sub para

1.1 to optimize the runway utilization.

3.1.3 Pilots shall complete all mandatory pre-departure checks before entering the active runway for departure so that the

aircraft is in a position to take off immediately upon receipt of take-off clearance. Pilots not able to comply with this

requirement must notify SMC/TWR before reaching the holding point.

3.1.4 When the aircraft is issued with a line-up and take-off clearance at the taxi holding position it shall be in a position to

line up and initiate an immediate take-off in one continuous movement, if unable advise ATC.

3.1.5 When the aircraft is issued with a take-off clearance after lining up on the runway it shall commence take-off roll

immediately. If the Controller observes a delay in respect of the departing aircraft commencing its take off run after

issuance of take-off clearance, the take- off clearance shall be cancelled and the aircraft shall be advised to vacate the

runway immediately at the nearest taxiway to make way for the subsequent arrival or departure. Necessary entries in

this regard shall be recorded in the Log Book.

3.1.6 All departures requiring, or able intersection departure shall inform Shamshabad ground before requesting taxi.

3.2 Arrival Procedure

3.2.1 The speed control measures published in ENR 1.6 EAIP INDIA shall be followed by flight crew.

3.2.2 Pilots are reminded that rapid exit from the runway enables ATC to apply minimum spacing on final approach that will

achieve maximum runway utilisation and will minimise the occurrences of ‘go around’.

3.2.3 Aircraft are expected to vacate the runway via first available RET depending on aircraft performance in order to reduce

delays and maximise utilisation. Pilots not able to comply with this requirement/request should notify APP/TWR as

early as feasible.

3.2.4 All ATR category aircraft to vacate RWY preferably via RET (rapid exit TWY) L1 when RWY in use 09R and RET

(rapid exit TWY) R1 when RWY in use 27L.

3.2.5 All Code C aircraft to vacate RWY preferably via RET (rapid exit TWY) L2 when RWY in use 09R and RET (rapid exit

TWY) R2 when RWY in use 27L.

4. Operational Compatibility for Secondary Runway 09L-27R, and Speed Restriction at TWY K-K1:

4.1. Secondary Runway Operations

i. Secondary RWY 09L-27R is compatible for day and night operations to cater unavailaibility of Main RWY 09R-27L due

to any exigencyor scheduled/unscheduled maintenance works or other unforeseen events.

ii. SRY RWY 09L/27R shall be compatible for operations up to Code E aircraft.

iii. Arcraft operations shall be restricted to Secondary Runway (09L/27R) and would not be extended to Main Runway

(09R/27L) for taxiing purpose during the Night operations in case portion of RWY 09R-27L between TWY A1-A3 &

A8 -A10 not available. Markings for making 180 degree turn is provided abeam TWY A2-B1 and A9-A10 dispalced

portion area on SRY RWY 09L27R at the either end portions.

4.2 Following limitations/restrictions will remain in place while activation of secondary Runway.

i. No code F aircraft movement accepted during Secondary Runway operation.

ii. Taxiway B1 upto ATC control location (165 M from SRY RWY Centerline) shall be available for operation and MRO

movements shall be accommodated with prior coordination and approval of ATC, ASO and AOCC.

iii. In case of Isolation Bay (Stand No. 100) not available for parking during RWY 09L/27R operations due to operational/

technical difficulties in restoration of main RWY 09R/27L, as an alternate, portion of RWY 09R/27L between A1-A2 or

A8-A9 or Portion of TWY B1 beyond RHP shall be used for parking of Aircraft under contigency in coordination with

ATC, AOCC,ASG and other concerned department.

4.3. Description of AGL System during activation of Secondary Runway:

Sl.

No

AGL Circuits

Secondary Runway 09L-27R

Main Runway

09R-27L

Remarks

1

Runway Threshold lights

ON

OFF

-

2

Runway Edge lights

ON

OFF

-

3

Runway Centreline Lights

Not Applicable

OFF

4

Runway End lights

ON

OFF

-

5

Approach lights

ON

OFF

-

6

PAPI

ON

OFF

-

7

Beacon Wind cone

ON

-

-

8

Guard Lights

ON

OFF

-

9

TILS

ON

Not Applicable

-

10

Signage's

ON

OFF

-

11

Taxiway Edge and Centreline lights

(connecting to Secondary

Runway)

ON

(for taxiway B2, B3, B4,B5 & B6)

Optional

(for TWY A1 to

A10)

At the discretion of ATCO or on the request of pilot using portion of RWY 09R-27L between A1-A3 & A8-A10 for Departure or Arrival

Note:

i. The Secondary Runway (09L-27R) Edge lights and Taxiway Edge Lights are interlocked to preclude the possibility of

simultaneous operation of both form of lighting.

ii. TWY Edge lights is available for Aircraft guidance to use portion of Main Runway 09R-27L between TWY A1-A3 and

TWY A8-A9/10 for Aircraft requiring full length of Secondary Runway for Arrival or Departure.

iii. During daylight and optimum visibility condition ATC can switch off Secondary Runway 09L-27R AGL system except

guard lights and Threshold Identification lights.

4.4. Aircraft Taxing Speed Restriction at HOT SPOT- 5 & 6

(HOTSPOT-5: APRON SERVICE ROAD CROSSING TWY- K, TWY- K1 AND SERVICE ROAD CROSSING TWY B3)

TWY B3)

HOTSPOT-6: APRON SERVICE ROAD CROSSING TWY- M AND TWY- M1)

To mitigate the Hot-Spot - 5 (TWY K & TWY K1) & Hot-Spot -6 (TWY M & TWY M1), taxing speed restriction of

To mitigate the Hot-Spot - 5, taxing speed restriction of Max 7 knots is imposed on TWY K and TWY K1imposed. All the pilots are requested to adhere to the same.

5. AIRPORT COLLABORATIVE DECISION MAKING (A-CDM)

5.1 INTRODUCTION

5.1.1 Efficiency of Air Transport System is highly dependent on traffic predictability. A- CDM effectively enhances

predictability (this reduces buffer times for resource planning and flight times), overall efficiency and punctuality by linking

and sharing of accurate and timely information amongst Aircraft Operators, Airport Operator, ATC etc.

5.1.2 A-CDM is a Common Information Sharing Platform introduced to process timely and accurate information for quick

and precise decision making. A-CDM takes into consideration the ETAs of arriving aircraft, Target Off Block Times of

departures, Runway-in-use and the handling capacity of the runway and determines the arrival and departure sequence.

Based on the sequence and the parking position, it calculates the Target Take-Off Times & Target Start up Times of

departures and Target In-Block Times for arrivals.

5.2 TWO KEY PARAMETERS OF A-CDM: TOBT and TSAT

5.2.1 TARGET OFF-BLOCK TIME (TOBT)

5.2.1.1 Definition: The time that an Aircraft Operator estimates that an aircraft will be ready, all doors closed, boarding

bridge removed, push back vehicle available and ready to start up/push back immediately upon reception of clearance from

the SMC (GROUND). It is the real time target of ensuring readiness of an aircraft and therefore, more accurate than the

static departure time mentioned in the flight plan and hence, an ideal milestone to be used by all airport partners.

5.2.1.2 Communication of TOBT:

i. If no delay is expected, EOBT will be treated as TOBT. Action need not be performed by the Aircraft Operator in the

ACDM interface.

ii.For delay within 30 minutes of the EOBT, TOBT shall be updated in the ACDM interface by the aircraft operator.

Optionally, EOBT may be revised via AFTN through DLA/CHG message.

iii. For delay more than 30 minutes from the EOBT, EOBT shall be mandatorily revised through a DLA/CHG message.

(Option for changing TOBT will not be available in this case).

5.2.1.3 Accuracy: TOBTs must be updated to an accuracy of +/- 5 minutes.

5.2.2 TARGET START UP APPROVAL TIME (TSAT)

5.2.2.1 Definition: The time calculated by A-CDM application taking into account TOBT, CTOT and/or the traffic situation that an aircraft can expect to start-up/push back for departure.

Note: In case there is no congestion, ATC may allow the aircraft actual start up approval (ASAT) even before the TSAT.

5.2.2.2 Calculation of TSAT: TSAT is calculated automatically by A-CDM Application. The TSAT is calculated by taking into account TOBT, priority of aircraft, variable taxi times, and the runway capacity. Any revision of EOBT will trigger the A-CDM application to recalculate a new TSAT for that flight as well as to re-allocate earlier TSAT to next flight who meets the requisite conditions. TSAT is displayed in various ACDM interfaces in the following colour coded information.

•Blue colour: TSAT -15 minutes up to TSAT -5 minutes

•Green colour: TSAT -5 minutes up to TSAT +5 minutes

•Red colour: After TSAT +5 minutes.

5.2.2.3 Generation of TSAT: TSAT is generated by ACDM interface at TOBT - 60 minutes.

5.2.2.4 Communication of TSAT: TSAT will be displayed in various A-CDM interfaces. The AO/GHA shall advise flight crew of TSAT, displayed in the A-CDM interface.

5.2.2.5 Priorities for generation of TSAT:

The following aircraft will be accorded priority by A-CDM application at the time of generating TSATs:

i.VVIP flights

ii.Ambulance aircraft

iii.Aircraft in relief missions

iv.Aircraft returning to stand after push back/taxiing out for any reason.

5.2.2.6 Airlines/GHAs are required to monitor the A-CDM interface regularly to get information on the revised TSAT if any, in respect of their aircraft. It may please be noted that the earlier allocated TSAT may get changed due to the following reasons:

i.Change of runway.

ii.Change in taxi times.

iii.Revised TOBT of the subject aircraft.

iv.Cancellation/ revision in TOBT of other aircraft in the departure sequence.

v.Priority handling.

vi.Unusual Occurrences, etc.

vii.Application of ATFM regulation or ATC restriction resulting in new CTOT or start up delay.

viii.Inclement Weather.

ix.Bird activity.*

x.Change of route (SID)*

* [Future provision]

5.2.2.7 Accuracy: The TSAT will remain valid for +/- 5 minutes.

5.3 Co-ordination with the Air Traffic Flow Management Unit (ATFMU) *

5.3.1 A fully automatic data exchange with the ATFMU is established. A-CDM system is receiving ELDT and CTOT from

C-ATFM.

5.3.2 The data sent from A-CDM to C-ATFM enables efficient CTOT calculations.

5.4 A-CDM Start-up/Push-back procedures

5.4.1 Pre-Departure Sequence: Pre-Departure sequence is the order, in which the ATC plans the aircraft to depart from their

Gate/Stands. It should not be confused with the Pre- Take-off sequence where ATC decides on the order in which the

aircraft at holding points of the runway will depart.

5.4.2 Start-Up and Push-Back Procedure:

i.The aircraft must be ready for Start-up/Push-back at TOBT. Any revisions in TOBT shall be updated by the aircraft

operator at the earliest.

ii. The Pilot will contact Clearance Delivery (CLD) and request for Pre-Departure Clearance between TSAT -15 minutes to

TSAT-5 minutes. (Blue Zone)

iii. Pilot shall contact SMC (GROUND) for Start-up/Push-back between TSAT-5 minutes and TSAT+ 5 minutes (Green

Zone), subject to change over from CLD.

Note: The system may prepone TSAT up to TOBT

iv. If by TSAT +5 minutes (Red Zone after TSAT+5 minutes), ATC has not received Start-up/Push-back request, the aircraft

will lose its position in sequence. In such case:

a. Aircraft Operator shall update the TOBT.

b. A revised TSAT will be issued because of resequencing done based on new TOBT.

v. ATC should normally be able to issue start-up/push-back at TSAT. Pilots will be informed by ATC if there is a delay.

vi. Taxi clearance shall be requested within 5 minutes of Start-up/Push-back approval time.

Note: If this has not occurred, SMC (GROUND) must be notified of the extent of delay. In such cases, aircraft may lose its

departure slot and a new TOBT may be required. Aircraft Operator shall be responsible to obtain new ADC number from

IAF-MLU.

vii. The Pre-Departure (Off- block) Sequence will be determined in accordance with Target Start up Approval Time (TSAT)

and NOT in accordance with the Start-up Request. Pre-Departure Sequence will not have any bearing on Actual Departure

sequence.

(Note: Actual Departure sequence may differ from pre-departure sequence in order to optimize the Runway and Airspace

utilization.)

5.5 INFORMATION DISSEMINATION TO A-CDM STAKEHOLDERS

Relevant information for stakeholders, available with A-CDM system, is disseminated through following means:

i. Access controlled application interface provided to representatives of Airline Operators, Ground Handlers and Airport Operator.

ii. Web interface that can be accessed over Internet.*

iii. Display boards on the airside at certain parking stands, in the viewable area of cockpit crew, where limited information is disseminated.*

* [Future provision]

5.6 TERMS AND ABBREVIATIONS

All Acronyms are time parameters which have a standard length of four characters and have been arranged as per aircraft

movement sequence.

[While developing the A-CDM procedures, the guidance material published by Euro control, ICAO and other Organizations

has been used].

S. No.

Acronyms

Definition

Explanation

6.1

ELDT

Estimated Landing Time

The estimated time that an aircraft will touchdown on the runway. (Equivalent to ATC ETA = Estimated Time of Arrival = landing).

6.2

ALDT

Actual Landing Time

The time that an aircraft lands on a runway. (Equivalent to ATC ATA = Actual Time of Arrival = Landing, ACARS = ON).

6.3

EXIT

Estimated Taxi-In Time

The estimated taxi time between landing and in- Block.

6.4

AXIT

Actual Taxi-In Time

AXIT = AIBT - ALDT

6.5

SIBT

Scheduled In- Block Time

The time that an aircraft is scheduled to arrive at its first parking position.

6.6

EIBT

Estimated In- Block Time

The estimated time that an aircraft will arrive in- blocks. (Equivalent to Aircraft Operator’s ETA = Estimated Time of Arrival).

6.7

AIBT

Actual In- Block Time

The time that an aircraft arrives in-blocks. (Equivalent to Aircraft Operator’s ATA = Actual Time of Arrival, ACARS = IN).

6.8

STTT

Scheduled Turnaround Time

STTT = SOBT - SIBT

6.9

ETTT

Estimated Turnaround Time

The time estimated by the AO/GH on the day of operation to turnaround a flight taking into account the operational constraints.

6.10

MTTT

Minimum Turnaround Time

The minimum turnaround time agreed with an AO/GH for a specified flight or aircraft type.

6.11

ATTT

Actual Turnaround Time

ATTT = AOBT - AIBT

6.12

ASRT

Actual Start Up Request Time

Time the pilot requests start up clearance.

6.13

TSAT

Target Start Up Approval Time

The time provided by ATC taking into account TOBT, CTOT* and/or the traffic situation that an Aircraft can expect start-up / push back approval. Note: The actual start up approval (ASAT) can be given in advance of TSAT.

6.14

ASAT

Actual Start Up Approval Time

Time that an aircraft receives its start-up approval.

6.15

SOBT

Scheduled Off- Block Time

The time that an aircraft is scheduled to depart from its parking position.

6.16

EOBT

Estimated Off- Block Time

The estimated time at which the aircraft will start movement associated with departure (ICAO).

6.17

TOBT

Target Off- Block Time

The time that an Aircraft Operator estimates that an aircraft will be ready, all doors closed, boarding bridge removed, push back vehicle available and ready to start up / push back immediately upon reception of clearance from the SMC (GROUND).

6.18

AOBT

Actual Off- Block Time

Time the aircraft pushes back / vacates the parking position. (Equivalent to Aircraft Operator’s ATD = Actual Time of Departure & ACARS = OUT)

6.19

ARDT

Actual Ready Time (for Movement)

When the aircraft is ready for start-up/push back or taxi immediately after clearance delivery, meeting the requirements set by the TOBT definition.

6.20

EXOT

Estimated Taxi-Out Time

The estimated taxi time between off-block and take off. This estimate includes any delay buffer time at the holding point prior to take off.

6.21

AXOT

Actual Taxi- Out Time

AXOT = ATOT - AOBT

6.22

ETOT

Estimated Take Off Time

The estimated take off time taking into account the EOBT plus EXOT.

6.23

CTOT

Calculated Take Off Time

A time calculated and issued by the appropriate Central Management unit, as a result of tactical slot allocation, at which a flight is expected to become airborne.

6.24

TTOT

Target Take Off Time

The Target Take Off Time taking into account the TOBT/TSAT plus the EXOT. Each TTOT on one runway is separated from other TTOT or TLDT to represent vortex and/or SID separation between Aircraft.

6.25

ATOT

Actual Take Off Time

The time that an aircraft takes off from the runway. (Equivalent to ATC ATD = Actual Time of Departure, ACARS = OFF).

VOHS

AD 2.21

NOISE ABATEMENT PROCEDURES

Consistent with safety of aircraft operations and in consideration of high intensity runway operations, pilots should minimise the use of reverse thrust after landing to reduce disturbance in areas adjacent to the aerodrome.

VOHS

AD 2.22

FLIGHT PROCEDURES

I. LOW VISIBILITY PROCEDURE:

1. Definitions and Abbreviations:

1 Low Visibility Procedures (LVP): Specific procedures applied at an aerodrome for the purpose of ensuring safe operations

during Categories II and III approaches and/or low visibility take-offs.

1.2 Low visibility take-off (LVTO). A term used in relation to flight operations referring to a take-off on a runway where the

RVR is less than 400 m.

1.3 Manoeuvring Area: That part of an aerodrome to be used for the take-off, landing and taxiing of aircraft, excluding

aprons.

1.4 Runway Visual Range: The range over which the pilot of an aircraft on the centerline of a runway can see the runway

surface markings or the lights delineating the runway or identifying its centreline.

1.5 Aerodrome Operating Minima: The limits of usability of an aerodrome for:

a. Take off, expressed in terms of runway visual range and / or visibility and, if necessary, cloud conditions;

b. Landing in 2D instrument approach operations, expressed in terms of visibility and/or runway visual range; minimum

descent altitude / height (MDA/H) and, if necessary, cloud conditions; and

c. Landing in 3D instrument approach operations, expressed in terms of visibility and/or runway visual range and

decision altitude/height (DA/H) appropriate to the type and/or category of the operation.

d. Aerodrome operating minima for Airports shall be established by the airline/aircraft operators on the OCA/OCH or

DA/DH and ALS facility published by AAI.

e. The adherence to the minima is the responsibility of pilot in command.

However, ATC is responsible to pass the latest meteorological information and status of aeronautical ground lights and other

related facilities at the airport to the pilot in command, including any significant changes

1.6 Safeguarding Procedures: Safeguarding Procedures are instructions for relevant airport departments and airside operators

to prepare ground services and facilities for low visibility operations, in order that when LVP are implemented all

Safeguarding procedures are complete and airport is configured for Low Visibility Take-offs.

1.7 Precision approach and landing operations: An instrument approach procedure based on navigation systems (ILS, MLS,

GLS and SBAS Cat I) designed for 3D instrument approach operations Type A or Baltitude/height (DA/H) appropriate to

the type and/or category of the operation.

1.8 ILS Category I (Cat I) Operations: A decision height not lower than 60 m (200 ft) and with either a visibility not less than

800 m or a runway visual range not less than 550 m.

1.9 Runway Visual Range: The range over which the pilot of an aircraft on the centreline of a runway can see the runway

surface markings or the lights delineating the runway or identifying its centreline.

1.10 Visibility: Visibility for aeronautical purposes is the greater of:

a. The greatest distance at which a black object of suitable dimensions, situated near the ground, can be seen and

recognized when observed against a bright background;

b. The greatest distance at which lights in the vicinity of 1 000 candelas can be seen and identified against an unlit

background.

Note 1: The two distances have different values in air of a given extinction coefficient, and the latter b) varies with the

background illumination. The former a) is represented by the meteorological optical range (MOR).

Note 2: The definition applies to the observations of visibility in local routine and special reports, to the observations of

prevailing and minimum visibility reported in METAR and SPECI and to the observations of ground visibility.

1. 11 The abbreviations used in this document have the following meanings:

AAI : Airports Authority of India

AOCC : Airport Operation Coordination Centre

ARFF : Airport Rescue and Fire Fighting Services

ASMGCS : Advanced Surface Movement Guidance and Control System

ATC : Air Traffic Control

ATIS : Automatic Terminal Information Service

ATM : Air Traffic Management

GHIAL : GMR Hyderabad International Airport Limited

CFT : Crash Fire Tender

DATIS : Datalink Automatic Terminal Information Service

DG : Diesel Generating Set

GP : Glide Path

ILS : Instrument Landing System

ITH : Intermediate Taxi Holding Position

LOC : Localizer

LSA : Localizer Sensitive Area

LVP : Low Visibility Procedure

LVTO : Low Visibility Take-off Procedure

MET: Meteorology

R/T: Radio Telephony

RGIA: Rajiv Gandhi International Airport

RWY: Runway

RVR: Runway Visual Range

SMC: Surface Movement Control

SP: Safeguarding Procedures

SSO : Shift Supervisory Officer

TDZ : Touchdown Zone

TWR SUP: Tower Supervisor

TWY: Taxiway

WSO : Watch Supervisory Officer

UPS : Uninterruptible Power Supply

2. Introduction:

The Low Visibility Procedure (LVP) incorporates safeguarding measures and defines operational restrictions to ensure safe Airside Operations taking into account the available Aerodrome facilities.

2.1 General:

2.1.1 Rajiv Gandhi International Airport, Shamshabad is equipped with CAT 1 ILS system for RWY 09R & RWY 27L.

2.1.2 ASMGCS is operational. Also, RWY and TWY centreline lights are available which can be used during LVP.

2.1.3 The following equipment shall be serviceable to the required standard to support LVP operations:

a. Aeronautical ground lighting System consisting of Runway (RWY) edge lights, RWY centreline lights, RWY end lights,

Taxiway (TWY) edge lights, Stop bar lights, Approach lights.

b. The critical lighting system RWY edge, RWY centre line and RWY end lights are supported by UPS for zero switch over

time.

c. Real time RVR reporting System (available for both RWYs). In case RVR equipment is unserviceable, manual RVR will

be made available.

d. Switchover time for standby power for ILS and Aeronautical ground lighting system excluding critical lighting system

mentioned in para 2.1.3 (b) is a maximum of 15 seconds.

2.2 Reporting RVR:

a. There are three RVR transmissometer located at Touch-down Zone (TDZ) and End Point Zone (END)and MID for

RWY 09R-27L. Also Two RVR transmissometer located at Touch-down Zone (TDZ), End Point Zone (END) for

RWY 09L-27R. The reference RVRvalue for the implementation and cancellation of LVP shall be the lower

of the TDZ & END RVR

b. When reporting RVR to pilots the TDZ RVR shall always be intimated for the concerned Landing RWY

2.3 Safeguarding Procedures (SP):

a. Positioning of 1 CFT each at the two predetermined positions (in front of main fire station and in front of satellite fire

station on fire access road);

b. Stopping of all works on the manoeuvring area and the associated strip area as well as removal of all men and mobile

equipment from the said area;c. Implementation of secondary power supply change over time NIL second for RWY Edge,

Centreline and End lights (Both circuit) as these lighting system are supported by UPS in RVR conditions less than 750M.

c. The appropriate Aeronautical ground lights must have been inspected during the hour preceding implementation of LVP,

and thereafter once every two-hour period. These lighting inspections should be accorded priority and, if necessary,

aircraft operations may have to be delayed.e. The Duty Manager AOCC in consultation with Air Side operation shall give

confirmation that SP is completed to WSO through SMC. This information may be passed on land line or on SMC

frequency.

d. When any required facility defined in Para 2.1.3 (a) of above facilities for LVP of Rajiv Gandhi International Airport,

Shamshabad becomes unserviceable during periods of LVP, TWR/SMC shall advise the aircraft and accordingly LVP

operations shall be suspended and information to this effect shall be included in ATIS broadcast.

Note: Runway Edge Lights are served by two dependent interleaved circuits. In case one circuit becomes unserviceable,

the Runway Lights System will not meet the stipulated specification for any operation (Precision, Non-Precision

and Non -Instrument). Hence, WSO shall take suitable action to inform all concerned regarding suspension of

operations till required facilities are available.

e. The triggers for various activities defined in the LVP procedures are based on RVR/Visibility Data. These triggers are

passed to AOCC/ARFF by SMC on telephone to initiate the SP.

2.4 Aeronautical Ground Lighting System

a. The Precision Approach CAT II lighting is installed for RWY 09R and Precision Approach CAT I lighting system

for RWY 27L, RWY 09L and RWY 27R at RGI Airport, Shamshabad for enhanced visual guidance for pilots.

b. All AGL critical circuits RWY edge, RWY centre line and RWY end lights are supported by UPS for zero switch over

time with 30 mins of power backup.

c. In case of power failure during low visibility UPS will take over without interruption (seamless transition) without

impacting any AGL facility.

d. In case of commercial powers supply is not restored even after 30 min, the DG shall takeover automatically from UPS.

e. When LVP is in force the Aeronautical Ground Lighting shall comply with the following minimum serviceability

requirement:

f. The Electrical Power Supply Systems for AGL are so designed that the time interval between failure of the primary source

of power and the complete restoration of the services for visual aids associated CAT I operations, shall be in accordance

with maximum switch-over times in Table 8-1 of Para 8 of DGCA CAR, Section 4 Series B Part I

g. All AGL critical circuits RWY edge, RWY centre line and RWY end lights are supported by UPS for zero switch over

time with 30 minutes of power backup.

h. Stop Bars: Stop bars have been provided as follows

i. On taxiway A1, A2, A3 at holding position for Runway 27L

ii. On taxiway A8, A9, A10 at holding position for Runway 09R

i. No entry bar: No entry bar lights are installed at RET L1, L2, L3, L4 & R1, R2, R3, R4

j. Taxiway centreline lights provided at Taxiways B3, B4, B5, B6, A1, A2, A3, L1, L2, L3, L4, R1, R2 R3, R4, A8, A9, A10,

C, C1, E3 and E4.

k. During LVP procedures in force the Aeronautical Ground Lighting shall comply with the following minimum

serviceability requirement in the below table:

Aeronautical Ground Lighting Facility

Un-serviceability

Restrictions

Approach Lights

More than 15% of all lights are unserviceablet

Suspend CAT-I Operations

Any two consecutive lights or more are unserviceable

Runway Edge lights

Any two consecutive lights or more are unserviceable

Suspend CAT I Operations

Any one of the two circuits serving the power supply

goes unserviceable

Runway centre line lights

More than 15% of all lights are unserviceable

Suspend CAT I Operations

Any two consecutive lights or more are unserviceable

Runway End lights

More than 25% of all Lights

Suspend CAT-I Operations

Two adjacent lamps

Standby Generators

Any of the generators is unserviceable

Suspend CAT I Operations

2.5 Selection of Runway in Use:

a. As both RWY 27L and RWY 09R are equipped with RVR instrument and RVR data is available to working controllers,

Tower shall determine Runway in Use depending on prevailing wind conditions during LVP.

b. In case of non-availability of Real time RVR, Manual RVR shall be obtained for the selected runway in use, prior to each

departure.

c. In case one of the RVR instrument is unserviceable, preference may be given to the RWY for which instrument RVR data

is available during NIL wind condition.

3. Implementation of Safeguarding Procedures (SP):

3.1 Safeguarding Procedures shall be initiated:

a. The RVR is less than 1200m or visibility is forecast to deteriorate to 750m or less; and/or

b. The cloud ceiling is 400ft and forecast to fall to 200ft or less.

3.2 WSO will inform AOCC for co-coordinating with all the concerned agencies for implementation of Low Visibility

Take-off Procedures.

3.3 When Met reported visibility reduces to 2500 Meters:

a. Surface Movement Control in consultation with Aerodrome Control Tower shall inform ARFF and AOCC as per

visibility /Weather standby criteria.

b. AOCC/Air Side Operation shall stop all work and withdraw all personnel working on the Runway strip and the

manoeuvring area and inform SMC.

c. Vehicles equipped with VEGA transponder only will be allowed on the manoeuvring area.

d. SMC shall inform ARFF/AOCC whenever visibility improves above 2500 Meters to enable ARFF/ AOCC/Air Side

Operation to resume normal operations.

3.4 When visibility reduces to 1500 Meters:

a. SMC shall inform AOCC/Air Side Operation when visibility reduces to 1500 Meters.

b. AOCC/Air Side Operation shall coordinate with Duty Manager, Technical Services to ensure that UPS and DG set are

performing normally.

c. AOCC/Air Side Operation shall ensure that Aeronautical light inspection is initiated and report status of Aeronautical

lighting system on completion of the inspection to SMC. SMC shall permit the Aeronautical Light Inspection and accord

priority for the same.

d. Met department shall provide instrument RVR data for R 27L and R 09R to the ATC. In case of unserviceability of the

RVR instrument, the same shall be intimated to ATC and manual RVR shall be provided. For this purpose, Air Side

Operation shall provide Leader vehicle, whenever required and inform Security Operations Control Centre (SOCC) to give

priority to the Met team to avoid any delay because of security checks near entry gate.

e. Aircraft RFFS ARFF shall position 1 one CFT each at the two predetermined position after obtaining permission from SMC on RTFR/T when

when visibility reduced to 1000M 1000m or RVR less than 1200M1200m (.)

3.5 When RVR reduces to 750 Meters:

a. SMC shall inform WSO/Tower Supervisor/AOCC whenever RVR reduces to 750 Meters;

b. AOCC/Air Side Operation shall ensure that the towing of aircraft is done under escort of Leader vehicles and inform ATC

of any deviation

c. SMC and AOCC/Air Side Operation shall not permit any ground run that needs to be performed on the manoeuvring area

except idle power run on the stands;

d. AOCC/Air Side Operation and SMC shall ensure that “Follow Me” services are provided to pilots on request;

e. AOCC Manager shall inform all users of the Apron of the imposition/withdrawal of low visibility procedures;

f. SMC shall inform AOCC whenever RVR improves above 750 meters;

g. AOCC/Air Side Operation shall confirm completion of safe guarding procedures to Aerodrome Control Tower.

4. Low Visibility procedure for Departures:

The low visibility procedure for departures shall be implemented when RVR reduces below 750 Meters and/or the cloud ceiling is less than 200ft.

Note: Though LVP is implemented when RVR is less than 750 m, ILS CAT I operations will continue till TDZ RVR is not

less than 550 m.

a. The safe guarding procedure shall be completed prior to commencement of Low Visibility Procedure Operations.

b. SMC shall inform WSO/ Tower Supervisor/ Duty Manager AOCC/Air Side Operation whenever RVR reduces below 750

Meters who in turn shall inform Duty Manager, Technical Services to check the UPS and DG serviceability and inform

DM ASO.

c. When SMC gets the information from AOCC about the UPS and DG serviceability report, SMC shall inform WSO/

Tower Supervisor/ Duty Manager AOCC/Air Side operations to start LVP operations.

d. Commercial power supply with UPS back up shall be the primary source when LVP becomes operational

e. In case of power failure during low visibility, UPS will take over without interruption (seamless transition) without

impacting any AGL facility.

f. In case of commercial powers supply is not restored even after 30 min, the DG shall takeover automatically from UPS.

g. The number of the vehicles shall be restricted to bare minimum and records of all operating on the manoeuvring area

shall be maintained by AOCC. These records can be in the form of electronic records or audio records.

h. SMC & AOCC/Air Side Operation shall permit towing of only one aircraft at a time on the Apron under escort of Leader

vehicles.

i. The following may be included in DATIS “LOW VISIBILITY PROCEDURES IN FORCE”

j. TWR shall permit departures only from the beginning of the Runway in use.

k. SMC shall inform WSO/Tower Supervisor/ AOCC/Air Side Operation whenever RVR improves above 750 Meters. Duty

Manager, AOCC/Air Side Operation shall inform Duty Manager, Technical Services when RVR improves above 750

Meters and trend forecast suggests upward improvement to enable transfer of power supply from DG set to Main power.

l. If instrument RVR is unserviceable during the above period, manual RVR readings shall be obtained by Meteorological

Personnel prior to each departure. For this purpose, Air Side Operation shall provide necessary vehicle whenever required

and inform Security Operations Control Centre (SOCC) to give priority to the Met team to avoid any delay because of

security checks near entry gate.

4.1 RVR reduces below 200 Meters:

a. All operations will be stopped.

b. An aircraft may be allowed to depart below 200 metres, if within its minima.

c. Tower Controller shall make log entry of such aircraft and relevant signal to be sent to all concerned as per internal

procedure.

4.2 RVR improves above 200 Meters:

a. SMC shall inform AOCC/Air Side Operation whenever RVR improves above 200 Meters.

b. The respective agencies follow the procedures mentioned in para 4 and para 3 respectively as visibility improves.

5. Summary of actions by various Units.

5.1 Actions by Air Traffic control (ATC)

a. Surface Movement Control in consultation with Aerodrome Control Tower shall inform ARFF and AOCC as per

visibility/Weather standby criteria.

b. SMC shall inform WSO/Tower Supervisor/AOCC whenever RVR reduces to 750 Meters;

c. SMC shall inform WSO/ Tower Supervisor/ Duty Manager AOCC/Air Side Operation whenever RVR reduces below 750

Meters who in turn shall inform Duty Manager, Technical Services Services to check the UPS and DG serviceability and

inform DM ASO.

d. When SMC gets the information from AOCC about the UPS and DG serviceability report, SMC shall inform WSO/ Tower

Supervisor/ Duty Manager AOCC/Air Side operations to start LVP operations.

e. The following may be included in DATIS “Low Visibility Procedures in force”.

f. TWR shall permit departures only from the beginning of the Runway in use.

g. SMC shall inform WSO/Tower Supervisor/ AOCC/Air Side Operation whenever RVR improves above 750 Meters. Duty

Manager, AOCC/Air Side Operation shall inform Duty Manager, Technical Services when RVR improves above 750

Meters and trend forecast suggests upward improvement to enable transfer of power supply from DG set to Main power.

5.2 Actions by Airside operations (AOCC)

a. AOCC/Air Side Operation shall stop all work and withdraw all personnel working on the Runway strip and the

manoeuvring area and inform SMC.

b. AOCC/Air Side Operation shall coordinate with Duty Manager, Technical Services to ensure that UPS and DG set are

performing normally.

c. AOCC/Air Side Operation shall ensure that Aeronautical light inspection is initiated and report status of Aeronautical

lighting system on completion of the inspection to SMC. SMC shall permit the Aeronautical Light Inspection and accord

priority for the same.

d. Vehicles equipped with VEGA transponder only will be allowed on the manoeuvring area.

e. AOCC/Air Side Operation shall confirm completion of safe guarding procedures to Aerodrome Control Tower.

f. AOCC/Air Side Operation shall ensure that the towing of aircraft is done under escort of Leader vehicles and inform ATC

of any deviation;

g. AOCC/Air Side Operation and SMC shall ensure that “Follow Me” services are provided to pilots on request;

h. AOCC Manager shall inform all users of the Apron of the imposition/withdrawal of low visibility procedures;

i. The number of the vehicles shall be restricted to bare minimum and records of all operating on the manoeuvring area shall

be maintained by AOCC. These records can be in the form of electronic records or audio records.

j. If instrument RVR is unserviceable during the above period, manual RVR readings shall be obtained by Meteorological

Personnel prior to each departure. For this purpose, Air Side Operation shall provide necessary vehicle whenever required

and inform Security Operations Control Centre (SOCC) to give priority to the Met team to avoid any delay because of

security checks near entry gate.

6. Actions by other Agencies (Airlines, Refuelling companies, catering agencies, etc.)

a. All agencies operating in the operational area shall ensure that only those vehicles that are absolutely essential for aircraft

operations operate in the operational area. The drivers of these vehicles should keep a look out for taxiing aircraft and other

vehicles to prevent accidents

b. All the vehicles must have their Vega/obstruction lights “ON” during Low Visibility Procedures operations.

c. Follow all instructions/sign boards provided for vehicular movement area/service roads.

7. Termination of Low Visibility Procedures:

a. When metrological condition improves to 750M or more, cloud ceiling is 200 feet or Higher and trend is for improvement,

WSO/Tower Supervisor would terminate operations of LVP. He may obtain advice from Duty Met. Officer regarding

improvement in weather conditions for the purpose of termination of LVP operations.

b. The WSO/Tower Supervisor will intimate AOCC/Air Side Operation regarding the termination of LVP operations.

c. On cancelling LVP, Aerodrome Control shall include it in the subsequent two ATIS broadcasts that “LOW VISIBILITY

PROCEDURES ARE CANCELLED”.

d. If SP are implemented and LVP are not subsequently initiated and meteorological conditions improve and the visibility

/RVR is more than 1200m and/or the cloud ceiling is 400ft or higher and both are forecast to remain above the required SP

criteria, WSO may cancel SP.

8. Applicability

LVTO is applicable to Airport Operator, ATS provider, and to those airline operators having specific DGCA approval as per Civil Aviation Requirements issued by DGCA India under Section 8, Series ‘C’, Part I. Pilots are required to report their approved take off minima (in metres) to ATC on Ground Frequency (121.85 MHz).

II. TRANSPONDER OPERATING PROCEDURES ON GROUND

1. Introduction:

Advanced Surface Movement Guidance and Control System (A-SMGCS) using Mode-S Multi-lateration has been commissioned Airport. The Aircraft Transponder Operating Procedures, particularly in the movement area of the airport(s), where A-SMGCS has been commissioned, is as given below:

2. DEPARTURE

i. At the Gate/Stand:

Select STBY

Enter the discrete SSR code received from Clearance Delivery/Surface Movement Control. Enter the three letter ICAO

designator followed by the flight identification number (e.g. AIC748) through the FMS or the Transponder control panel,

depending on the avionics.

ii. On requesting Pushback/Taxi (whichever is earlier):

Select Transponder or equivalent and AUTO if available

This action will enable the aircraft ID, used as the Call sign by ATC, to be displayed on the surveillance display of ATC.

ATC can verify the data and use it for necessary identification.

iii. When Lining up:

Select TCAS

Select TCAS only after receiving the clearance to line up, to ensure that the performance of systems based on SSR

frequencies (including airborne TCAS units, SSR and A-SMGCS) is not compromised.

3. ARRIVAL

a. When on the Runway:

Keep TCAS selected

b. After vacating the Runway:

Select Transponder or equivalent and AUTO if available

There is a need that the Transponder remains able to exchange data with the A-SMGCS system. However to ensure that the performance of systems based on SSR frequencies (including airborne TCAS Unit, SSR & A-SMGCS) is not compromised, TCAS shall be deselected when vacating the Runway.

4. Parked on Stand:

Select STBY

The Transponder will not reply to interrogation. The discrete SSR Code given to that particular flight can now be recycled for other flights.

Note: When on ground the aircraft must squawk Mode C, in order to provide the altitude information to the surveillance

system, and thereby prevent

a. Clutter on Terminal Approach Radar Display (and )

b. False automatic detection of departure for aircraft still on ground.

III Following measures measures are being implemented for reducing RTF congestion and enhancing Operational efficiency

a. Departing aircraft passing 1000ft to change over to HYD APP (freq 120.25Mhz)unless otherwise specified by ATC tower

b. Departing aircraft on first contact with approach shall Transmit only the callsign, altitude passing and assigned SID in all other cases of first contact with an approach unit, aircraft shall transmit only it's callsign.

c. ACARS equipped aircraft to obtain pre departure clearance through datalink whenever clearance delivery is active.

d. Aircraft shall comply with speed control whenever imposed by ATC.

e. Aircraft to vacate RWY via rapid exit TWY as assigned by tower on final approach or inform inability to ATC.

f. Arriving aircraft on vacating RWY to contact ground on freq 121.85 Mhz unless specifically instructed by tower.

h. Arriving aircraft on reaching the allotted stand need not contact ATC for informing the same.

i. Arriving and departing aircraft to minimize RWY occupancy time for enhancing RWY capacity.

j. Aircraft not to demand time to touch down and direct routings. ATC whenever practicable issue the same

VOHS

AD 2.23

ADDITIONAL INFORMATION

I. PARKING STANDS

Stand No.

PCN/

Surface

Co-ordinates

Remarks

3

66/R/B/W/T

Rigid

171408.82N

0782555.24E

Deep Pushback on to taxilane K3 up to Nose wheel stop position marking

and pull forward on taxilane K2 facing North East abeam stand 5 and then

engine startup approved. For Towing guidance white dashed line provided.

Suitability: Code C

Elevation (m): 607.000

4

66/R/B/W/T

Rigid

171408.94N

0782556.71E

Pushback on TXL K2 facing East, pull abeam stand 4 and then engine

start-up approved. Pushback guidance line provided with white dashed line.

Suitability: Code C

Elevation (m): 607.000

5

66/R/B/W/T

Rigid

171409.58N42N

0782558.48E

Pushback on TXL K2 facing North East, pull abeam stand 5 and then

engine start-up approved.

Suitability: Code C

Elevation (m): 607.000

6

66/R/B/W/T

Rigid

171410171409.15N96N

0782559.72E

Pushback on TXL K2 facing North East, pull abeam stand 6 and then engine start-up approved.

Suitability: Code C

Elevation (m): 607.000

7

66/R/B/W/T

Rigid

171410.71N54N

0782600.96E

Pushback on TXL K2 facing North East, pull abeam stand 7 and then engine start-up approved.

Suitability: Code C

Elevation (m): 607.000

8

66/R/B/W/T

Rigid

171411.13N

0782602.48E

Pushback on TXL K2 facing East, pull abeam stand 8 and then engine start-up approved.

Suitability: Code C

Elevation (m): 607.000

9

66/R/B/W/T

Rigid

171411.15N

0782603.96E

Pushback on TXL K2 facing East, pull abeam stand 9 and then engine start-up approved.

Suitability: Code C

Elevation (m): 607.000

10

66/R/B/W/T

Rigid

171411.28N11N

0782605.43E

Pushback on TXL K2 facing East, pull abeam stand 10 and then engine start-up approved.

Suitability: Code C

Elevation (m): 607.000700

11

66/R/B/W/T

Rigid

171411.30N13N

0782606.91E

Pushback on TXL K2 facing East, pull abeam stand 11 and then engine start-up approved.

Suitability: Code C

Elevation (m): 607.000800

12

66/R/B/W/T

Rigid

171411.32N15N

0782608.28E

Pushback on TXL K2 facing East, pull abeam stand 12 and then engine start-up approved.

Suitability: Code C

Elevation (m): 607.000900

13

66/R/B/W/T

Rigid

171409.63N

0782607.63E47E

Pushback on TXL K1 facing North / South, abeam stand 14 then engine start-up approved.

Suitability: Code C

Elevation (m): 607.000800

14

66/R/B/W/T

Rigid

171408.21N

0782607.66E50E

Pushback on TXL K1 facing North / South, pull abeam stand 14 then engine start-up approved.

Suitability: Code C

Elevation (m): 607.000900

15

71/R/B/W/T

Rigid

171409.27 62 N

0782618.3 E

Pushback facing East or West on TWY D, Pull abeam stand 15 and then engine startup approved

Suitability: Code C

Elevation: 610.000 M

16

71/R/B/W/T

Rigid

171409.29N63N

0782619.68E

Pushback facing East or West on TWY D, Pull abeam stand 16 and then engine startup approved

Suitability: Code C

Elevation: 610.470 M

17

71/R/B/W/T

Rigid

171409.31N65N

0782621.05E

Pushback facing East or West on TWY D, Pull abeam stand 17 and then engine startup approved

Suitability: Code C

Elevation: 610.860 M

18

71/R/B/W/T

Rigid

171409.33N67N

782622.42E

Pushback facing East or West on TWY D, Pull abeam stand 18 and then engine startup approved

Suitability: Code C

Elevation: 611.270 M

19

71/R/B/W/T

Rigid

171409.22 70 N

0782624.52 E

Pushback facing East or West on TWY D, Pull abeam stand 19 and then engine startup approved

Suitability: Code C and Q 400

Elevation: 611.960 M

20

71/R/B/W/T

Rigid

171409.24 N

0782625.62 E

Pushback facing East or West on TWY D, Pull abeam stand 20 and then engine startup approved

Suitability: Code C and Q 400

Elevation: 612.320 M

21

71/R/B/W/T

Rigid

171409.26 N

0782626.99 E

Pushback facing East or West on TWY D, Pull abeam stand 21 and then engine startup approved

Suitability: Code C and Q 400

Elevation: 612.760 M

22

71/R/B/W/T

Rigid

171409.28 N

0782628.48 76 E

Pushback facing East or West on TWY D, Pull abeam stand 22 and then engine startup approved

Suitability: Code C and Q 400

Elevation: 613.230 M

23

71/R/B/W/T

Rigid

171409.30 N

0782630.16 E

Pushback facing East or West on TWY D, Pull abeam stand 23 and then engine startup approved

Suitability: Code C and Q 400

Elevation: 613.640 M

24

71/R/B/W/T

Rigid

171409.31 N

0782631.53 E

Pushback facing East or West on TWY D, Pull abeam stand 24 and then engine startup approved

Suitability: Code C and Q 400

Elevation: 614.000 M

25

71/R/B/W/T

Rigid

171409.33 N

0782632.90 E

Pushback facing East or West on TWY D, Pull abeam stand 25 and then engine startup approved

Suitability: Code C and Q 400

Elevation: 614.450 M

26A

71/R/B/W/T

Rigid

171410.38 N

0782634.39 E

Pushback facing North or South on TWY H, Pull abeam stand 26A and then engine start-up approved

Suitability: Code B

Elevation: 614.510 M

26B

71/R/B/W/T

Rigid

171409.35 N

0782634.50 E

Pushback facing North or South on TWY H, Pull abeam stand 26B and then engine start-up approved

Suitability: Code B

Elevation: 614.84 900 M

27A

71/R/B/W/T

Rigid

171408.05 N

0782634.52 E

Pushback facing North or South on TWY H, Pull abeam stand 27A and then engine start-up approved

Suitability: Code B

Elevation: 614.790 800 M

27B

71/R/B/W/T

Rigid

171407.03 N

0782634.54 E

Pushback facing North or South on TWY H, Pull abeam stand 27B and then engine start-up approved

Suitability: Code B

Elevation: 614.540 M

28

71/R/B/W/T

Rigid

171408.03 N

0782632.92 E

Pushback facing East or West on TWY C, Pull abeam stand 28 and then engine startup approved

Suitability: Code C and Q 400

Elevation (m): 614.420 M

29

71/R/B/W/T

Rigid

171408.01 N

0782631.54 E

Pushback facing East or West on TWY C, Pull abeam stand 29 and then engine startup approved

Suitability: Code C and Q 400

Elevation (m): 614.000

30

71/R/B/W/T

Rigid

171408.00 N

0782630.18 E

Pushback facing East or West on TWY C, Pull abeam stand 30 and then engine startup approved

Suitability: Code C and Q 400

Elevation: 613.650 M

31

71/R/B/W/T

Rigid

171407.98 N

0782628.80 E

Pushback facing East or West on TWY C, Pull abeam stand 31 and then engine startup approved

Suitability: Code C and Q 400

Elevation: 613.310 M

32

71/R/B/W/T

Rigid

171407.96 N

0782627.01 E

Pushback facing East or West on TWY C, Pull abeam stand 32 and then engine startup approved

Suitability: Code C and Q 400

Elevation: 612.750 M

33

71/R/B/W/T

Rigid

171407.94 N

0782625.64 E

Pushback facing East or West on TWY C, Pull abeam stand 33 and then engine startup approved

Suitability: Code C and Q 400

Elevation: 612.350 M

34

71/R/B/W/T

Rigid

171407.92 47 N

0782624.27 E

Pushback facing East or West on TWY C, Pull abeam stand 34 and then engine startup approved

Suitability: Code C and Q 400

Elevation (m): 611.100800

35

71/R/B/W/T

Rigid

171407.79N45N

782622.44E

Pushback facing East or West on TWY C, Pull abeam stand 35 and then engine startup approved Suitability: Code C

Elevation: 611.240 M

36

71/R/B/W/T

Rigid

171407.77N43N

782621.07E

Pushback facing East or West on TWY C, Pull abeam stand 36 and then engine startup approved Suitability: Code C

Elevation: 610.890 M

37

71/R/B/W/T

Rigid

171407.75N41N

782619.70E

Pushback facing East or West on TWY C, Pull abeam stand 37 and then engine startup approved Suitability: Code C

Elevation: 610.460 M

38

71/R/B/W/T

Rigid

171407.73N39N

782618.33E

Pushback facing East or West on TWY C, Pull abeam stand 38 and then engine startup approved Suitability: Code C

Elevation: 610.430 M

39

71/R/B/W/T

Rigid

171405.65N

0782607.84E69E

Pushback on TXL K1 facing North or South, pull abeam stand 39 then engine start-up approved. Suitability: Code C

Elevation: 607.760 M

40

88/R/C/W/T

Rigid

171403.77N 0782608.63E

Pushback facing East or West on TWY E1, Pull abeam stand 40 and then engine startup approved Suitability: Code C

Elevation: 607.760 M

41

88/R/C/W/T

Rigid

171403.75N 0782607.16E

Pushback facing East or West on TWY E1, Pull abeam stand 41 and then engine startup approved Suitability: Code C

Elevation: 607.660 M

42

88/R/C/W/T

Rigid

171403.73N 0782605.68E

Pushback facing East or West on TWY E1, Pull abeam stand 42 and then engine startup approved Suitability: Code C

Elevation: 607.540 M

43

88/R/C/W/T

Rigid

171403.71N 0782604.21E

Pushback facing East or West on TWY E1, Pull abeam stand 43 and then engine startup approve Suitability: Code C

Elevation: 607.430 M

44

88/R/C/W/T

Rigid

171403.69N 0782602.74E

Pushback facing East or West on TWY E1, Pull abeam stand 44 and then engine startup approved Suitability: Code C

Elevation: 607.360 M

45

88/R/C/W/T

Rigid

171403.67N 0782601.27E

Pushback facing East or West on TWY E1, Pull abeam stand 45 and then engine startup approved Suitability: Code C

Elevation: 607.340 M

46

88/R/C/W/T

Rigid

171403.65N 0782559.80E

Pushback facing East or West on TWY E1, Pull abeam stand 46 and then engine startup approved Suitability: Code C

Elevation: 607.400 M

47

88/R/C/W/T

Rigid

171403.68N 0782558.32E

Pushback facing East or West on TWY E1, Pull abeam stand 47 and then engine startup approved Suitability: Code C

Elevation: 607.390 M

48

88/R/C/W/T

Rigid

171403.61N 0782556.85E

Pushback facing East or West on TWY E1, Pull abeam stand 48 and then engine startup approved Suitability: Code C

Elevation: 607.340 M

49

88/R/C/W/T

Rigid

171403.58N 0782555.38E

Pushback facing East or West on TWY E1, Pull abeam stand 49 and then engine startup approved Suitability: Code C

Elevation: 607.390 M

50

88/R/C/W/T

Rigid

171403.55N 0782553.92E

Pushback facing East or West on TWY E, Pull abeam stand 50 and then engine startup approved Suitability: Code C

Elevation: 607.350 M

51

88/R/C/W/T

Rigid

171403.53N 0782552.45E

Pushback facing East or West on TWY E, Pull abeam stand 51 and then engine startup approved Suitability: Code C

Elevation: 607.370 M

52

88/R/C/W/T

Rigid

171403.96N 0782550.80E

Pushback facing East or West on TWY E, Pull abeam stand 52 and then engine startup approved Suitability: Code C

Elevation: 607.500 M

53

88/R/C/W/T

Rigid

171403.34N 0782549.19E

Pushback facing East or West on TWY E, Pull abeam stand 53 and then engine startup approved Suitability: Code C

Elevation: 607.310 M

54

88/R/C/W/T

Rigid

171404.05N 0782546.91E

Pushback facing East or West on TWY E, Pull abeam stand 54 and then engine startup approved. MARS aircraft parking system, when ACFT parked on stand 54, stand 54L and 54R not available.

Suitability: Code E

Elevation: 607.490 M

54 L

88/R/C/W/T

Rigid

171403.29N 0782546.43E

Pushback facing East or West on TWY E, Pull abeam stand 54L and then engine startup approved. MARS aircraft parking system, when ACFT parked on stand 54L, stand 54 not available.

Suitability: Code C

Elevation: 607.370 M

54 R

88/R/C/W/T

Rigid

171404.24N 0782547.79E

Pushback facing East or West on TWY E, Pull abeam stand 54R and then engine startup approved. MARS aircraft parking system, when ACFT parked on stand 54R, stand 54 not available. Suitability: Code C

Elevation: 607.490 M

55

88/R/C/W/T

Rigid

171404.01N 0782544.20E

Pushback facing East or West on TWY E, Pull abeam stand 55 and then engine startup approved. MARS aircraft parking system, when ACFT parked on stand 55, stand 55L and 55R not available. Suitability: Code F

Elevation: 607.480 M

55 L

88/R/C/W/T

Rigid

171403.24N 0782543.47E

Pushback facing East or West on TWY E, Pull abeam stand 55L and then engine startup approved. MARS aircraft parking system, when ACFT parked on stand 55L, stand 55 not available. Suitability: Code C

Elevation: 607.330 M

55 R

88/R/C/W/T

Rigid

171404.37N 0782544.82E

Pushback facing East or West on TWY E, Pull abeam stand 55R and then engine startup approved. MARS aircraft parking system, when ACFT parked on stand 55R, stand 55 not available. Suitability: Code C

Elevation: 607.670 M

56

88/R/C/W/T

Rigid

171403.95N 0782541.23E

Pushback facing East or West on TWY E, Pull abeam stand 56 and then engine startup approved. MARS aircraft parking system, when ACFT parked on stand 56, stand 56L and 56R not available. Suitability: Code F

Elevation: 606607.860 600 M

56 L

88/R/C/W/T

Rigid

171403.19N 0782540.49E

Pushback facing East or West on TWY E, Pull abeam stand 56L and then engine startup approved. MARS aircraft parking system, when ACFT parked on stand 56L, stand 56 not available. Suitability: Code C

Elevation: 605607.890 300 M

56 R

88/R/C/W/T

Rigid

171404.33N 0782541.86E

Pushback facing East or West on TWY E, Pull abeam stand 56R and then engine startup approved. MARS aircraft parking system, when ACFT parked on stand 56R, stand 56 not available. Suitability: Code C

Elevation: 607.610 M

57

88/R/C/W/T

Rigid

171403.91N 0782538.34E

Pushback facing East or West on TWY E, Pull abeam stand 57 and then engine startup approved. MARS aircraft parking system, when ACFT parked on stand 57, stand 57L and 57R not available.

Suitability: Code E

Elevation: 607.510 M

57 L

88/R/C/W/T

Rigid

171403.15N 0782537.64E

Pushback facing East or West on TWY E, Pull abeam stand 57L and then engine startup approved. MARS aircraft parking system, when ACFT parked on stand 57L, stand 57 not available. Suitability: Code C

Elevation: 607.270 M

57 R

88/R/C/W/T

Rigid

171404.13N 0782539.00E

Pushback facing East or West on TWY E, Pull abeam stand 57R and then engine startup approved. MARS aircraft parking system, when ACFT parked on stand 57R stand 57 not available. Suitability: Code C

Elevation: 607.540 M

58

88/R/C/W/T

Rigid

171403.87N 0782535.49E

Pushback facing East or West on TWY E, Pull abeam stand 58 and then engine startup approved. MARS aircraft parking system, when ACFT parked on stand 58, stand 58L and 58R not available.

Suitability: Code E

Elevation: 607.530 M

58 L

88/R/C/W/T

Rigid

171403.11N 0782534.79E

Pushback facing East or West on TWY E, Pull abeam stand 58L and then engine startup approved. MARS aircraft parking system, when ACFT parked on stand 58L stand 58 not available. Suitability: Code C

Elevation: 607.270 M

58 R

88/R/C/W/T

Rigid

171404171403.06N 14N 0782536.15E

Pushback facing East or West on TWY E, Pull abeam stand 58R and then engine startup approved. MARS aircraft parking system, when ACFT parked on stand 58R stand 58 not available. Suitability: Code C

Elevation: 607.540 M

59

88/R/C/W/T

Rigid

171403.89 N

782532.62 E

Pushback facing East or West on TWY E, Pull abeam stand 59 and then engine startup approved MARS aircraft parking system, when stand 59R or 59L occupied stand 59 not available.

Suitability: Code E

Elevation: 607.400 M

59R

88/R/C/W/T

Rigid

171403.94N 26N 0782533.28E

Pushback facing East or West on TWY E, Pull abeam stand 59R and then engine startup approved. MARS aircraft parking system, when stand 59 occupied stand 59R & 59L not available

Suitability: Code C

Elevation: 607.350 M

59L

88/R/C/W/T

Rigid

171403.11 20 N

782531.87 E

Push back facing East or West and pull abeam stand 59L and then engine startup approved.MARS aircraft parking system, when stand 59 occupied stand 59R & 59L not available.

Suitability: Code C

Elevation: 607.340 M

60

133/R/B/W/T

Rigid

171403.85 N

782529.78 E

Pushback facing East or West on TWY E, Pull abeam stand 60 and then engine startup approved. MARS aircraft parking system,when stand 60R or 60L occupied stand 60 not available.

Suitability: Code E

Elevation: 607.200 M

60R

133/R/B/W/T

Rigid

171403.90 18 N

782530.44 E

Pushback facing East or West on TWY E, Pull abeam stand 60R and then engine startup approved. MARS aircraft parking system, when stand 60 occupied stand 60R & 60L not available.

Suitability: Code C

Elevation: 607.000 M

60L

133/R/B/W/T

Rigid

171403.07 16 N

782529.03 E

Pushback facing East or West on TWY E, Pull abeam stand 60L and then engine startup approved. MARS aircraft parking system, when stand 60L occupied stand 60 not available.

Suitability: Code C

Elevation: 606.860 M

61

133/R/B/W/T

Rigid

171403.65N

0782527.87E

Push back deep facing East on TWY E and pull forward till stand 60L or deep pushback facing West till stand 60L or pushback facing south on to TWY M till TDP and then engine startup approved.

Suitability: Code E

Elevation: 606.630 M

62

133/R/B/W/T

Rigid

171404.36N

0782526.16E27E

Pushback deep straight up to TWY M1 till the push back limit line and then pull forward on TWY M, facing south till TDP south of stand 62 and then engine startup approved.

Suitability: Code C

Elevation: 606.460 M

63

133/R/B/W/T

Rigid

171406.76N

0782527.23E

Pushback facing south on TWY M and pull

forward abeam stand 63 and then engine startup

approved.

Suitability: Code E

Elevation: 606607.231 100 M

63L

133/R/B/W/T

Rigid

171407.60N

0782526.02E19E

Pushback facing south on TWY M and pull

forward abeam stand 63L and then engine startup

approved.

Suitability: Code C

Elevation: 605.898 M

63R

133/R/B/W/T

Rigid

171406.29N

07825270782526.13E17E

Pushback facing south on TWY M and pull

forward abeam stand 63R and then engine startup

approved.

Suitability: Code C

Elevation: 606.720 M

64

133/R/B/W/T

Rigid

171409.89N

0782527.13E

Pushback facing South on TWY M and pull

forward abeam Stand 64 and then engine startup

approved.

Suitability: Code E

Elevation: 606607.248 000 M

65

133/R/B/W/T

Rigid

171411.90N

07825250782526.92E09E

Pushback facing South on TWY M and pull

forward abeam Stand 64 and then engine start up

approved.

Suitability: Code C

Elevation: 606607.353 100 M

66

66/R/B/W/T

Rigid

171411.95N60N

0782528.96E

Pushback facing Northwest on TWY M2 and pull

forward abeam Stand 66 and then engine startup

approved.

Suitability: Code C

Elevation: 606.100 900 M

67

66/R/B/W/T

Rigid

171411.29N08N

0782530.22E

Pushback facing Northwest on TWY M2 and pull

abeam Stand 67 and then engine startup approved.

Suitability: Code C

Elevation: 606.124 900 M

68

66/R/B/W/T

Rigid

171410.76N55N

0782531.48E

Pushback facing Northwest on TWY M2 and pull

abeam Stand 67 and then engine startup approved.

Suitability: Code C

Elevation: 606.128 900 M

69

66/R/B/W/T

Rigid

171409.87N65N

0782532.82E

Pushback facing Northwest on TWY M2 and pull

abeam Stand 67 and then engine startup approved.

Suitability: Code C

Elevation: 606.205 M

70

71/R/B/W/T

Concrete

171402.41N

0782618.31E

Push back facing North or South and pull/push abeam stand 71 and then engine startup approved.

Suitability: Code C

Elevation: 610.510 M

71

71/R/B/W/T

Concrete

171400.98N

0782618.33E

Push back facing North or South and pull/push abeam stand 71 and then engine startup approved.

Suitability: Code C

Elevation: 610.370 M

72

71/R/B/W/T

Concrete

171359.55N

0782618.35E

Push back facing North or South and pull/push abeam stand 71 and then engine startup approved.

Suitability: Code C

Elevation: 610.160 M

73

71/R/B/W/T

Concrete

171359.57N

0782619.84E

Push back facing North or South and pull/push abeam stand 74 and then engine startup approved.

Suitability: Code C

Elevation: 610.490 M

74

71/R/B/W/T

Concrete

171401.00N

0782619.82E

Push back facing North or South and pull/push abeam stand 74 and then engine startup approved.

Suitability: Code C

Elevation: 610.860 M

75

71/R/B/W/T

Concrete

171402.43N

0782619.80E

Push back facing North or South and pull/push abeam stand 74 and then engine startup approved.

Suitability: Code C

Elevation: 610.980 M

76

71/R/B/W/T

Concrete

171402.49N

0782624.43E

Push back facing North or South and pull/push abeam stand 77 and then engine startup approved.

Suitability: Code C

Elevation: 612.370 M

77

71/R/B/W/T

Concrete

171401.06N

0782624.45E

Push back facing North or South and pull/push abeam stand 77 and then engine startup approved.

Suitability: Code C

Elevation: 612.190 M

78

71/R/B/W/T

Concrete

171359.63N

0782624.47E

Push back facing North or South and pull/push abeam stand 77 and then engine startup approved.

Suitability: Code C

Elevation: 611.900 M

79

71/R/B/W/T

Concrete

171359.68N

0782628.63E

Push back facing North or South and pull/push abeam stand 80 and then engine startup approved.

Suitability: Code C

Elevation: 613.000 M

80

71/R/B/W/T

Concrete

171401.11N

0782628.61E

Push back facing North or South and pull/push abeam stand 80 and then engine startup approved.

Suitability: Code C

Elevation: 613.400 M

81

71/R/B/W/T

Concrete

171402.54N

0782628.59E

Push back facing North or South and pull/push abeam stand 80 and then engine startup approved.

Suitability: Code C

Elevation: 613.600 M

82

71/R/B/W/T

Concrete

171402.60N

0782633.23E

Push back facing North or South and pull/push abeam stand 83 and then engine startup approved.

Suitability: Code C

Elevation: 614.940 M

83

71/R/B/W/T

Concrete

171401.17N

0782633.25E

Push back facing North or South and pull/push abeam stand 83 and then engine startup approved.

Suitability: Code C

Elevation: 614.810 M

84

71/R/B/W/T

Concrete

171359.74N

0782633.27E

Push back facing North or South and pull/push abeam stand 83 then engine startup approved.

Suitability: Code C

Elevation: 614.450 M

85

71/R/B/W/T

Concrete

171359.76N

0782634.76E

Push back facing North or South and pull/push abeam stand 86 and then engine startup approved.

Suitability: Code C

Elevation: 614.860 M

86

71/R/B/W/T

Concrete

171401.09N

0782634.74E

Push back facing North or South and pull/push abeam stand 86 and then engine startup approved.

Suitability: Code C

Elevation: 615.120 M

87

71/R/B/W/T

Concrete

171402.63N

0782634.72E

Push back facing North or South and pull/push abeam stand 86 then engine startup approved.

Suitability: Code C

Elevation: 615.240 M

100

60/R/C/W/T

Rigid

171356.51N 0782701.43E

Isolation stand

200

114/R/B/W/T

Rigid

171403.23N

0782514.56E

When ACFT parked on stand 200, stand 201 not available.

Suitability: Code C

Elevation: 602.000 M

201

114/R/B/W/T

Rigid

171403.57N

0782513.76E

When ACFT parked on stand 201, stand 200 & 202 not available.

Suitability: Code F

Elevation: 602.100 M

202

114/R/B/W/T

Rigid

171403.37N19N

0782512.97E

When ACFT parked on stand 202, stand 201 not available.

Suitability: Code C

Elevation: 602.000 M

203

114/R/B/W/T

Rigid

171403.19N01N

0782511.49E

When ACFT parked on stand 203, stand 203L not available.

Suitability: Code C

Elevation: 601.900 M

203L

114/R/B/W/T

Rigid

171403.53N

0782510.54E

When ACFT parked on stand 203L, stand 204 & 203 not available.

Suitability: Code F

Elevation: 602.100 M

204

114/R/B/W/T

Rigid

171403.17N

0782509.86E

When ACFT parked on stand 204, stand 203L not available.

Suitability: Code C

Elevation: 602.000 M

NP 7

77/F/B/W/T

Asphalt

171359.85 N 0782610.55 E

Aircraft Compatibility: Code “C” and Q 400

Power in Power out type stand.

Elevation: 608.300 M

NP 8

77/F/B/W/T

Asphalt

171359.80 N 0782606.93 E

Aircraft Compatibility: Code “C” and Q 400

Power in Power out type stand.

Elevation: 607.800 M

NP 9

77/F/B/W/T

Asphalt