VTSP  —  Phuket/ Phuket International Airport

VTSP  AD 2.1  AERODROME LOCATION INDICATOR AND NAME

VTSP  —  Phuket/ Phuket International Airport

VTSP  AD 2.2  AERODROME GEOGRAPHICAL AND ADMINISTRATIVE DATA

1

ARP coordinates and site at AD

080645N 0981833E

Centre of runway 660 M from THR RWY 09

2

Direction and distance from (city)

32 KM (NW)

3

Elevation/Reference temperature

25 M (82 FT) 33°C
4Geoid undulation at AD ELEV PSN

NIL

5

MAG VAR/Annual change

0° 29' W (2016) / 0° 1' E
6

AD Administration, address, telephone,
telefax, telex, AFS

Phuket International Airport
Airports of Thailand Public Company Limited (AOT)
222 Village No.6, Mai Khao Sub District, Thalang District

Phuket 83110, Thailand

Tel:  +667 632 7230-6

Fax:  +667 632 7478

AFS:  VTSPYDYX

7

Types of traffic permitted (IFR/VFR)

IFR/VFR

8

Remarks

Operator: Airports of Thailand Public Company Limited (AOT)

VTSP  AD 2.3  OPERATIONAL HOURS

1

Aerodrome Operator

H24

2

Customs 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

ATS

H24

8

Fuelling

H24

9

Handling

H24

10

Security

H24

11

De-icing

NIL

12

Remarks

AIS briefing office and ATS reporting office located at the 3rd floor in the domestic terminal building/the type of services via AFTN, internet

URL:  http://www.aerothai.co.th

VTSP  AD 2.4  HANDLING SERVICES AND FACILITIES

1

Cargo-handling facilities

Thai Airways International Public Co.,Ltd.

3 Folklift (5 T-1 Folklift, 3 T-2 Folklift) 2 Trucks.

Handling weight up to 200 T per day.

BAGS Ground Service Co.,Ltd.

2 Folklift (3 and 8 T), 1 Tractor (2.5 T), 1 Highlift.

1 Handling weight up to 35 T per day.

2

Fuel/oil types

JET A-1, AVGAS 100LL

3

Fuelling facilities/capacity

Refuel Jet A-1: Tank TTL 12,000,000 L

Jet A-1: 1 Refueller@ 22,000 L

1 Refueller@ 12,000 L

7 Hydrant dispensers

AVGAS 100LL: 1 Tank TTL 3,000 L

1 Trailer TTL 3,000 L

4

De-icing facilities

NIL

5

Hangar space for visiting aircraft

NIL

6

Repair facilities for visiting aircraft

NIL

7

Remarks

The Airport has provided ground handling agents as following:

  1. Thai Airways International Public Co.,Ltd. (TG)

    Ground Handling Services

    Email:  hktko@thaiairways.com, hktkk@thaiairways.com

    Tel:  +667 635 1218

    Fax:  +667 632 7246

    SITA:  hktkktg, hktkotg

    Operation Handling Inquiry

    Email:  hktkl@thaiairways.com, hktko@thaiairways.com

    Tel:  +667 635 1201, +667 635 1218

    Fax:  +667 632 7246

    SITA:  hktkltg, hktkktg, hktkotg

  2. BAGS Ground Services Co.,Ltd.

    Ground Handling Inquiry/Operation Handling Inquiry

    Email:  dutyhkt@bags-groundservices.com

    Tel:  +6661 178 9408

    Fax:  +667 632 7610

    SITA:  hktbsxh

  3. MJETS LIMITED. (Private Aircraft only)

    Ground Handling Inquiry

    Email:  ground@mjets.com

    Tel:  +667 635 1719

    Fax:  +667 632 7518

    Operation Handling Inquiry

    Email:  ground@mjets.com

    Tel:  +6685 484 8746

    Fax:  +662 034 5677

VTSP  AD 2.5  PASSENGER FACILITIES

1

Hotels

Adjacent to airport terminal and in the city
2

Restaurants

At Domestic terminal, level 3 and in the city

3

Transportation

Limousines, Airport bus, Taxis and Car rental service are available

At International and Domestic terminal arrival hall, level 1

4

Medical facilities

Medical clinic at the airport, located in the International terminal, level 1 and ambulance service is available 24H
5

Bank and Post Office

Bank: At the International and Domestic terminal

Post office: At the International terminal, level 1

6

Tourist Office

Office at the International terminal level 1

Tel:  +667 621 9878

Fax:  +667 632 7100

Office in the city

Tel:  +667 622 2177

Fax:  +667 635 4139

7

Remarks

URL:  http://www.airportthai.co.th/phuket

for airport and flight information

VTSP  AD 2.6  RESCUE AND FIRE FIGHTING SERVICES

1

AD category for fire fighting

Category 9

2

Rescue equipment

Facility of Category 9 is provided
3

Capability for removal of disabled aircraft

Available – Up to B747

4

Remarks

NIL

VTSP  AD 2.7  SEASONAL AVAILABILITY - CLEARING

1

Types of clearing equipment

NIL

2

Clearance priorities

NIL

3

Remarks

The aerodrome is available all seasons

VTSP  AD 2.8  APRONS, TAXIWAYS AND CHECK LOCATIONS/positions DATA

1Apron surface and strength

Surface: Concrete

Strength: PCN 78/R/C/X/T

2Taxiway width, surface and strength
  1. Taxiway A, B, E, F and G

    Width: 30 M

    Surface: Concrete

    Strength: PCN 78/R/C/X/T

  2. Taxiway C

    Width: 30 M

    Surface: Asphalt

    Strength: PCN 59/F/A/X/T

  3. Taxiway D

    Width: 23 M

    Surface: Asphalt

    Strength: PCN 59/F/A/X/T

  4. Taxiway P

    Width: 23 M

    Surface: Asphalt

    Strength: PCN 59/F/A/X/T

    Surface: Concrete

    Strength: PCN 78/R/C/X/T

  5. Taxilane T1

    Width from taxilane centre line to taxilane shouder: 13.42 M,

    Surface: Concrete, PCN 78/R/C/X/T

  6. Taxilane T2

    Width from taxilane centre line to taxilane shouder: 13.67 M.,

    Surface: Concrete, PCN 78/R/C/X/T

  7. Taxilane T3, T4, T5, T6, T7

    Surface: Concrete, PCN 78/R/C/X/T

3

Altimeter checkpoint location and elevation

Location: At Apron

Elevation: 5.18 M / 17 FT

4

VOR checkpoints

NIL

5

INS checkpoints

See AD2-VTSP-2-4 /Chart for coordinates of aircraft stand

6

Remarks

NIL

VTSP  AD 2.9  SURFACE MOVEMENT GUIDANCE AND CONTROL SYSTEM AND MARKINGS

1

Use of aircraft stand ID signs, TWY guide lines and visual docking/parking guidance system of aircraft stands

Taxiing guidance signs at all intersections with TWY and RWY

Nose-Wheel guide lines at apron.

Solid Nose-Wheel guide lines at aircraft stands.

Nose-in guidance at aircraft stands.

Visual Docking System (VDGS)

Apron A at stand number 7-16 (not included MARS stands)

Apron B at stand number 1-6

Apron C at stand number 31-40 (included MARS stands)

2

RWY and TWY markings and LGT

RWY marking: RWY Designation, THR, TDZ, Centre line, Aiming Point and Side Strip

RWY LGT: THR, RWY Edge and RWY End lights

TWY marking: Centre line, Edge and RWY Holding Position and Intermediate Holding Position

TWY LGT: TWY Edge lights

3

Stop bars

Stop bars TWY A, B and G available.

4

Remarks

If VDGS is out of service, marshaller shall guide the aircraft to the parking position. No pilot shall taxi an aircraft on its own into the bays without the aid of docking system or a marshaller.

VTSP  AD 2.10  AERODROME OBSTACLES

In approach/TKOF areas

In circling areas and at AD

Remarks

123

RWY/Area affected

Obstacle type

Elevation

Markings/LGT

Coordinates

Obstacle type

Elevation

Markings/LGT

Coordinates

abcab

TKOF RWY 09/ APCH RWY 27

Mountain

HGT 138 M.MSL

See Aerodrome Obstacle Chart Type A, B

Transitional Surface

-Mountain 141 M.MSL

Inner Horizontal Surface

-Mountains 130, 268 and 210 M.MSL (North)

-Mountains 141, 120, 139 and 225 M.MSL (South)

Conical Surface

- Mountains 295 and 335 M.MSL

See Aerodrome Obstacle Chart Type B

NIL

VTSP  AD 2.11  METEOROLOGICAL INFORMATION PROVIDED

1

Associated MET Office

- Southern Meteorological Center (West Coast)

222 Moo.6, Mai Khao Sub District, Thalang District
Phuket

Tel: +667 632 8147

Tel: +667 632 7346

Fax: +667 632 8147

Email: s48565@metnet.tmd.go.th

- Aeronautical Radio of Thailand Ltd.

Location: at the 3rd floor in the Domestic Terminal Building

2

Hours of service

MET Office outside hours

H24

3

Office responsible for TAF preparation

Periods of validity

Supply TAF from Southern Meteorological center (West Coast)

Issue TAF on standard time 00, 06, 12, 18 UTC

4

Trend forecast

Interval of issuance

Supply TAF from Southern (West Coast) Regional MET center.

Issue TAF on standard time 00, 06, 12, 18 UTC

Issue METAR every haft an hour

Observe SPECI off standard time

Issue Trend Type Landing Forecast

5

Briefing/consultation provided

Yes
6

Flight documentation

Language(s) used

English

7

Charts and other information available for
briefing or consultation

Daily Weather Forecast

Upper wind levels 850, 700, 500, 300, 200 hpa. SIG.WX.Chart

SIG.WX.Chart

8

Supplementary equipment available for
providing information

AWOS, Radar

9

ATS units provided with information

ATS Workstation

10

Additional information (limitation of service, etc.)

IP system

VTSP  AD 2.12  RUNWAY PHYSICAL CHARACTERISTICS

Designations

RWY NR

TRUE BRG

Dimensions of RWY(M)

Strength (PCN) and surface of RWY and SWY

THR coordinates

RWY end coordinates

THR geoid undulation

THR elevation and highest elevation of TDZ of precision APP RWY
123456
09

085°

085° (MAG)

3000x45

PCN 59/F/A/X/T

Concrete and asphalt

080643.05N 0981811.90E
THR 5.792 M/19 FT
27

265°

265° (MAG)

3000x45

PCN 59/F/A/X/T

Concrete and asphalt

080652.23N 0981949.46E
THR 24.94 M/81.8 FT
Slope of RWY-SWY

SWY dimensions (M)

CWY dimensions (M)Strip dimensions (M)OFZRemarks
789101112
+0.12% +0.01%+1.0%+0.70%
(500M 1000M 2500M 3000M)
60x45

NIL

3240x150

NIL

NIL

-0.70% -1.0% -0.01% -0.12%
(500M 2000M 2500M 3000M)
60x45

NIL

3240x150

NIL

NIL

VTSP  AD 2.13  DECLARED DISTANCES

RWY Designator

TORA

(M)

TODA

(M)

ASDA

(M)

LDA

(M)

Remarks

123456
09 3000 3000 3060 3000

NIL

27 3000 3000 3060 3000

NIL

VTSP  AD 2.14  APPROACH AND RUNWAY LIGHTING

RWY Designator

APCH LGT

type

LEN INTST

THR LGT

colour

WBAR

VASIS

(MEHT)

PAPI

TDZ, LGT

LEN

RWY Centre Line LGT

Length, spacing,

colour,

INTST

RWY edge LGT

LEN, spacing,

colour

INTST

RWY End LGT

colour

WBAR

SWY LGT

LEN (M)

colour

Remarks

12345678910
09

RTIL

Green

PAPI

Both

64.07 FT

NIL

NIL

3000 M, 60 M

White

FM 2400 M - 3000 M

Yellow

LIH

Red

NIL

NIL

27

SALS

(7 BAR)

420 M

LIH

Green

PAPI

Both

3.2°

64.96 FT

NIL

NIL

3000 M, 60 M

White

FM 2400 M - 3000 M

Yellow

LIH

Red

NIL

NIL

VTSP  AD 2.15  OTHER LIGHTING, SECONDARY POWER SUPPLY

1

ABN/IBN location, characteristics and hours of operation

ABN: On the top of control tower FLG W G EV 4 sec. / IBN: NIL,

H24

2

LDI location and LGT

Anemometer location and LGT

WDI

: 1 Wind Direction Indicator near left PAPI 09

: 1 Wind Direction Indicator 350 M. left side FM THR 27,

100 M FM RCL, illuminated

Anemometer: See AD Ground Movement Chart

3

TWY edge and centre line lighting

EDGE: All TWY

CENTRE LINE: NIL

4

Secondary power supply/switch-over time

Secondary power supply to all lighting at RWY 27/09
Switch over time : 0 sec.(UPS)
5

Remarks

NIL

VTSP  AD 2.16  HELICOPTER LANDING AREA

1

Coordinates TLOF or THR of FATO

Geoid undulation

NIL

2

TLOF and/or FATO elevation M/FT

NIL

3

TLOF and FATO area dimensions, surface, strength, marking

NIL

4

True BRG of FATO

NIL

5

Declared distance available

NIL

6

APP and FATO lighting

NIL

7

Remarks

Parking on Apron C

VTSP  AD 2.17  ATS AIRSPACE

1

Designation and lateral limits

A circle of 5 NM radius centre on 0806.7N 09818.6E

2

Vertical limits

2000 FT/AGL
3

Airspace classification

C
4

ATS unit call sign

Language(s)

Phuket Tower

English, Thai

5

Transition altitude

11000 FT
6

Remarks

NIL

VTSP  AD 2.18  ATS COMMUNICATION FACILITIES

Service designation

Call sign

Frequency

Hours of operation

Remarks

12345
APP

Phuket Approach

124.7 MHZ

284.0 MHZ

H24

*Emergency Freq.

**ON RDL 130, 170 AND 210 AT DIST 15 NM ALT 2 500 FT ARE BLIND SPOT

TWR

Phuket Tower

118.1 MHZ

*121.5 MHZ

**236.6 MHZ

**243.0 MHZ

H24
GND

Phuket Ground

121.9 MHZ

H24
ATIS Phuket Intl Airport

128.0 MHZ

H24

VTSP  AD 2.19  RADIO NAVIGATION AND LANDING AIDS

Type of aid,

MAG VAR

CAT of ILS/MLS

(For VOR/ILS/MLS, give declination)

ID

Frequency

Hours of operation

Position of transmitting antenna coordinates

Elevation of DME transmitting antenna

Remarks

1234567
DVOR/DME PUT

116.9 MHZ

CH 116X

H24
080654.83N 0981822.69E
16.72 M

DVOR/DME restriction due to mountainous terrain surround station coverage check does not provide adequate signal 40 NM at required altitudes in various area as follows:

  1. Radial 360º-030º altitude should not below 5 500 FT

  2. Radial 031º-170º altitude should not below 9 000 FT

  3. Radial 171º-220º altitude should not below 7 000 FT

  4. Radial 221º-359º altitude should not below 3 000 FT

ILS CAT I

LOC/DME

RWY 27

IPKT

109.9 MHZ

CH 36X

H24
080647.72N 0981819.73E
 
  1. ILS with non-standard localizer alignment, coverage over a sector of 35° either side of course, no back course and voice feature, the antenna array is located 245 M from end of RWY 27 120 M from runway centre line.

  2. Front course 266 Mag. Width 4.4°.

  3. Glide Path angle 3.2°

  4. Middle Marker (MM without compass locator) distance 804 M from approach end of RWY 27

  5. DME co-located with localizer

  6. Glide slope unusable starting at the middle marker (2.0 DME) to RWY THR. Glide slope shall not be used when DME out of service.

  7. Altitude will be restricted due to terrain at 4 DME not below 900 FT. Both DVOR and DME unusable beyond 40 NM in the following areas

    1. from 000°-130° below 5000 FT.

    2. from 130°-180° below 7000 FT.

    3. from 180°-230° below 5000 FT.

    4. from 230°-360° below 3500 FT.

GP  333.8 MHZH24
080648.27N 0981942.21E
 
MM  75 MHZH24
080655.43N 0982015.73E
 

VTSP  AD 2.20  LOCAL AERODROME REGULATIONS

1.  SURFACE MOVEMENT PROCEDURE
1.1 Ground Movement

The supplementary of surface movement procedures has been established at Phuket International Airport as follows:

1.1.1 Manoeuvring on movement area :
  1. Area of apron D and Almost of the area between apron A to apron C is the blind spot area, when ATC instruction is issued, aircraft are to manoeuvre by pilot discretion.

  2. Special manoeuvring procedure at Phuket Aerodrome on TWY P, When visibility below 3,000 M., due to minimum distance between RWY centre line is 150 M. aircraft code letter C, D and E that taxiing on TWY P shall be instructed to hold, under the following conditions :

    1. Before departing aircraft code C,D, and E enters the runway for take-off or

    2. Before arriving aircraft code C, D and E crossing 4 NM final for landing.

  3. Taxiing on TWY P in connection with TWY E due to the minimum separation distance between TWY centre line and objects is 39.5 M wide body aircraft to taxi with extreme caution.

2.  USE OF RUNWAY

To achieve the highest possible rate/hour for departure and arrival at Phuket International Airport, the runway occupancy times shall be reduced to a minimum. Therefore, the follow procedures are introduced;

2.1 Departing aircraft
  1. Commensurate with safety and standard operating procedure, when in receipt of a line up clearance, pilots should ensure that they are able to taxi into the correct hold and line up position on the runway as soon as the preceding aircraft has commenced its take-off roll.

  2. Cockpit checks should be completed before line up, any further checks requiring completion whilst on the runway shall be kept to a minimum. Pilots should ensure that they are able to commence the take-off roll immediately after a take-off clearance is issued.

  3. Pilots unable to comply with these procedures shall inform ATC prior to passing the runway holding position.

2.2 Arriving aircraft

Pilots are reminded that runway occupancy time should be kept to the minimum on the landing runway enables ATC to apply minimum spacing on Final Approach that will achieve maximum runway utilization as well as minimize the occurrence of go-arounds.

3.  START-UP PROCEDURE
3.1 When Flight Formalities have been completed, Pilot of all aircraft, other than VFR domestic flight, shall contact Phuket Delivery Control on frequency 118.55 MHZ 5 minutes before start up engine for request ATC Clearance, as appropriate information, of the following :
  1. Aircraft call sign

  2. Type of aircraft and category, if HEAVY

  3. Parking stand number / Location

  4. Identified of the latest ATIS received

  5. Destination

  6. Proposed flight level, if it is different from the filed flight plan

3.2 After received ATC Clearance, Pilot shall read back the following information :
  1. Call sign

  2. Destination

  3. SID and route

  4. Level

  5. Transponder Code, and

  6. Any restriction

3.3 Pilot shall contact Phuket Ground Control on frequency 121.9 MHZ for push back and start-up, after ATC Clearance has been received.
3.4 Unless other ATC restriction is imposed, the aircraft must be push back within 5 minutes from the time ATC clearance is received otherwise the ATC clearance will be cancelled. Additionally, in order to provide a more flexible ground traffic movement, all domestic departures shall no longer be required to push back within 5 minutes after clearance received.
3.5  If ATC clearance includes a departure time restriction in order to establish longitudinal separation, pilots shall maintain listening watch on Phuket ground in readiness for push back and are to call Phuket Ground in the appropriate time with the departure time restriction. Pilots who fail to comply with these requirements or amended departure time restriction will result in cancellation of ATC clearance.
3.6 When the weather condition below VMC, all of VFR operations on and in the vicinity of the Phuket aerodrome shall be suspended by Phuket Tower or Phuket Approach, if the pilot request SVFR, shall contact Phuket Delivery Control for SVFR clearance.
3.7 Communication failure procedure: If unable to contact Phuket Delivery Control, Pilot of all aircraft shall contact Phuket Ground Control on frequency 121.9 MHZ for request ATC clearance.
3.8 All aircraft shall start-up and push back with minimum power.
3.9 Pilot are reminded they shall start-up only one engine with minimum power (on idle power) when parking at aircraft stand or during push back. The other engines shall be allowed to start-up when push back procedure is complete (tow bar has been disconnected) and aircraft is aligned with the taxilane.
3.10 In case the pilot needs to start-up engine more than minimum power (such as Cross-Bleed Start Up), an approval must be received from ATC before push back. Pilots shall start-up engine more than minimum power within the taxilane only, a delay may result in requesting for such operation.
3.11 In case the pilot needs to test engine after repairing or replace new engines to the aircraft. Testing shall be conduct during the hours of 2300-1400 UTC at stand No.99 on taxiway A, heading of the aircraft to east.
3.12 For the purpose of noise and carbon emission reduction on the apron area, any aircraft that is designated to park at the stand served with passenger loading bridges shall utilize the fixed ground power supply(400HZ) and fixed pre-conditioned air supply provides by the airport if airport if serviceable.
  1. Fixed ground power supply(400HZ)-Operators are recommended to reduce electric load immediately after parking. May be used but not more than 5 minutes after the aircraft has parked. If fixed ground power supply is out of service, mobile GPU may be used.

  2. Fixed Pre-Conditioned Air (PCA) supply-Operators are recommended to turn off the cabin air re-circulation system to prevent outside air mixing with PC-Air. If fixed PCA is out of service, mobile ACU may be used.

  3. In the event of an aircraft needs to run an APU, it could be done only when park on the remote parking stands which are far from the concourse buildings.

4.  PUSH BACK PROCEDURE

APRON A

4.1 Push back (Face to North or Face to South) procedures for an aircraft parking at stand number 7 through 16 will be advised by ATC.
Aircraft stand Taxi outPush Back Instruction
10 and 11T3 Aircraft shall be pushed back face to north then further to the tow-bar release on marking (6) behind aircraft stand number 12L.
10 and 11T5Aircraft shall be pushed back face to south then further to the tow-bar release on marking (3) behind aircraft stand number 9.
15T2Aircraft shall be pushed back face to north then towed forward and the tow-bar released behind aircraft stand number 14.
15T7Aircraft shall be pushed back face to south then further to the tow-bar release on marking (7) behind aircraft stand number 15.
16T7Aircraft shall be pushed back face to south then further to the tow-bar release on marking (7) behind aircraft stand number 15.

APRON B

4.2 Push back (Face to East or Face to West) procedures for an aircraft parking at stand number 1 through 6 will be advised by ATC.

Apron D

4.3 Push back (Face to North or Face to South) procedures for an aircraft parking at stand number 31 through 40 will be advised by ATC.
Aircraft standTaxi outPush Back Instruction
33L, 33, 34L, 34, 34R and 35 T5Aircraft shall pushed back face to south then further to the tow-bar release on marking (1) behind aircraft stand number 33R.
34L, 34, 34R and 35 T4Aircraft shall pushed back face to north then further to the tow-bar release on marking (4) behind aircraft stand number 36.
39T1Aircraft shall pushed back face to north towed forward and the tow-bar released behind aircraft stand number 38.
39T7Aircraft shall pushed back face to south then further to the tow-bar release on marking (5) behind aircraft stand number 39.
40T7Aircraft shall pushed back face to south then further to the tow-bar release on marking (5) behind aircraft stand number 39.
4.4 Due to aircraft congestion, self-manoeuvring is not permitted at any parking stand, all aircraft must use tow-bar for push back procedure.
5.  PARKING PROCEDURE
5.1  Apron A: Use Taxilane T1, T2, T3, T4, T5, T6 and T7 to enter or exit aircraft stand number 7 – 16 as advised by ATC.
5.2  Apron B: Use Taxiway P to enter or exit aircraft stand number 1 – 6 as advised by ATC.
5.3  Apron C: Use Taxiway C, D or P to enter or exit aircraft stand number 21 – 28 as advised by ATC.
5.4 Apron D: Use Taxilane T1, T2, T3, T4, T5, T6 and T7 to enter or exit aircraft stand number 31-40 as advised by ATC.
5.5 The area between aircraft stands safety line belonging to aircraft stands number 1 through 6, 7 through 16 and 31 through 40 can be used as a temporary parking (during aircraft being in service only) for vehicles and ground service equipment.
6.  PROCEDURES FOR PRIVATE JET TAKING OFF AND LANDING AT PHUKET INTERNATIONAL AIRPORT
6.1 Procedures for private jet aircraft wishing to stay overnight
6.1.1 Aircraft owner/operator or PIC shall prepare the information as following:
  1. Passengers information (First name, last name, position, and overnight parking purposed);

  2. Aircraft nationality and registration marks;

  3. Aircraft type, weight, and height of aircraft;

  4. Date and time of arrival and departure;

  5. Route of Flight;

  6. Owner of the aircraft.

6.1.2 Aircraft owner/operator or PIC shall inform the airport authority at least three (3) workdays before the arrival aircraft
6.1.3 All private jet aircraft which has the permission grated by the authority concerned to take off and land at Phuket International Airport, shall have Ground Handling Agent.
6.1.4 The aircraft shall be pushed back by using the tow-bar only. If the aircraft does not have such equipment, it will not be allowed to self-maneuver.
6.1.5  The Private jet aircraft that is granted to operate at Phuket International Airport shall commence the flight in accordance with the approved time slot by the Slot Coordination Committee. If the flight is delay or arrive early, it should not more than 2 hours. In addition, when there is a change in the approved time slots, the aircraft shall notify the airport before flight commencement.
6.1.6 For further information, contact the following

Unit : Airside Operation Department, Phuket International Airport

Tel : +667 635 1887

Fax : +667 635 2347

E-mail : vtsp.privatejet@airportthai.co.th

7.  180 DEGREES TURN ON THE RUNWAY

To prevent runway pavement damage which may result in the closure of the aerodrome if such damage is severe, aircraft code letter C or higher are not allowed to make 180 degree turn on the runway. The turn shall be made on the runway turn pad located near the threshold of runway 27. Any breach done by the aircraft operator shall be recorded and reported to The Civil Aviation Authority Of Thailand / The Headquarter of that operator and shall be liable for the compensation caused by such violation.

8.  SAFEGATE DOCKING SYSTEM – IN SYSTEM AT PHUKET INTERNATIONAL AIRPORT
8.1 INTRODUCTIONS
8.1.1 The SAFEGATE Docking System – in system is install at aircraft identification no. 1, 2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 14, 15, 16 and 31, 32L, 32, 32R, 33L, 33, 33R, 34L, 34, 34R, 35, 36, 37, 38, 39 and 40
8.1.2 The system enables the pilots seated on the left of the cockpit to position his aircraft on the correct stand centre line and stop position
8.2 PILOT OPERATING INSTRUCTION
8.2.1 Safety procedure
  1. General warning

    The DGS system has a built-in error detection program to inform the aircraft pilot of impending dangers during the docking procedure. If the pilot is unsure of the information, being shown on the DGS display unit, he must immediate stop the aircraft and obtain further information for clearance.

  2. Item to check before entering the stand area

    Warning : The pilot shall not enter the stand area, unless the docking system first is showing the vertical running arrows. The pilot must not proceed beyond the bridge, unless these arrows have been superseded by the closing rate bar.

    Warning : The pilot shall not enter the stand area, unless the aircraft type displayed is equal to the approaching aircraft/ The Correctness of other information, such as ‘door 2’, shall also be checked.

  3. The SBU message

    The message STOP SBU means that docking has been interrupted and has to be resumed only by manual guidance. Do not try to resume docking without manual guidance.


START-OF-DOCKING

The system is started by pressing one of the aircraft type buttons on the operator panel. When the button has been pressed, WAIT will be displayed.


CAPTURE

The floating arrows indicate that the system is activated and in capture mode, searching for an approaching aircraft. It shall be checked that the correct aircraft type is displayed. The lead-in line shall be followed. The pilot must not proceed beyond the bridge, unless the arrows have been superseded by closing rate bar.


TRACKING

When the aircraft has been caught by the laser, the floating arrow is replaced by the yellow centre line indicator. A flashing red arrow indicates the direction to turn. The vertical yellow arrow shows position in relation to the centre line. This indicator gives correct position and azimuth guidance.


CLOSING RATE.

Display of digital countdown will start when the aircraft is 20 M from stop position.When the aircraft is less than 12 M from the stop position, the closing rate is indicated by turning off one row of the centre line symbol per 0.5 M, covered by the aircraft. Thus, when the last row is turned off, 0.5 M remains to stop.


ALIGNED TO CENTRE.

The aircraft is 8 M from the stop position. The absence of any direction arrow indicates an aircraft on the centre line.


SLOW DOWN.

If the aircraft is approaching faster than the accepted speed, the system will show SLOW DOWN as a warning to the pilot.


AZIMUTH GUIDANCE.

The aircraft is 4 M from the stop-position. The yellow arrow indicates an aircraft to the right of the centre line, and the red flashing arrow indicates the direction to turn.


STOP POSITION REACHED.

When the correct stop-position is reached, the display will show STOP and red lights will be lit.

DOCKING COMPLETE.

When the aircraft has parked, OK will be displayed.


CHOCKS ON.

CHOCK ON will be displayed, when the ground staff has put the chocks in front of the nose wheel and pressed the “Chocks On” button on the operator panel.


OVERSHOOT.

If the aircraft overshoot the stop-position, TOO FAR will be displayed.


BAD WEATHER CONDITION.

During heavy fog, rain or snow, the visibility for the docking system can be reduced. When the system is activated and in capture mode, the display will deactivate the floating arrows and show DOWN GRADE. This message will be superseded by the closing rate bar, as soon as the System detects the approaching aircraft. The pilot must not proceed beyond the bridge, unless the DOWN GRADE text has been superseded by the closing rate bar


AIRCRAFT VERIFICATION FAILURE.

During entry into the stand, the aircraft geometry is being checked. If, for any reason, aircraft verification is not made 40 FT before the stop-position, the display will first show WAIT and make a second verification check. If this fails STOP and ID FAIL will be displayed. The text will be alternating on the upper two rows of the display. The pilot must not proceed beyond the bridge without manual guidance, unless the WAIT message has been superseded by the closing rate bar.


GATE BLOCKED.

If an object is found blocking the view from the DGS to the planned stop position for the aircraft, the docking procedure will be halted with a GATE BLOCK message. The docking procedure will resume as soon as the blocking object has been removed. The pilot must not proceed beyond the bridge without manual guidance, unless the WAIT message has been superseded by the closing rate bar.


VIEW BLOCKED.

If the view towards the approaching aircraft is hindered for instance by dirt on the window, the DGS will report a view block condition. Once the system is able to see the aircraft through the dirt, the message will be replaced with a closing rate display. The pilot must not proceed beyond the bridge without manual guidance, unless the WAIT message has been superseded by the closing rate bar.


SBU-STOP

Any unrecoverable error during the docking procedure will generate an SBU condition. The display will show red stop bar and the text STOP SBU. A manual backup procedure must be used for docking guidance.


EMERGENCY STOP

When the emergency stop button is pressed, STOP is displayed.


ERROR

If a system error occurs, the message ERROR is display with an error code. The code is used for maintenance purposes and explained else where.


SYSTEM BREAKDOWN

In case of a severe system failure, the display will go black, except for a red stop indicator. A manual backup procedure must be used for docking guidance.


POWER FAILURE

In case of a power failure, the display will be completely black. A manual backup procedure must be used for docking guidance.

9.  General Information

The supplementary of general information has been established at Phuket International Airport as follows :-

9.1  APRON A and B
  1. Type of apron : Remote parking and contact gate parking

  2. Aircraft can be parked for overnight parking and layover.

  3. Nose-in parking system

  4. Visual Docking Guidance System-VDGS is provided at stand 1-6 for apron B and stand 7-16 for apron A. If VDGS is out of service, a marshaller shall guide the aircraft to the parking position.

  5. Visual Docking Guidance System-VDGS is not provided for MARS stand (12L,12R,14L,14R), a marshaller shall guide the aircraft to the parking position.

  6. Refuel JET A-1 and AVGAS by trailer and hydrant system.

9.2  APRON C
  1. Type of apron : Remote parking

  2. Visual Docking Guidance System-VDGS is not provided

  3. Refuel JET A-1 and AVGAS by trailer.

9.3 APRON D
  1. Type of apron : Remote parking

  2. Aircraft can be parked for overnight parking and layover.

  3. Nose – in parking system

  4. Visual Docking Guidance System-VDGS is provided at each stand (included MARS stands). If VDGS is out of service, a marshaller shall guide the aircraft to the parking position.

  5. Refuel JET A-1 and AVGAS by trailer and hydrant system.

9.4 Aircraft stand taxilane
  1. Taxilane T1 is the parallel to Taxilane T2. (Taxilane T1 located behind aircraft stand NO.31-40 and Taxilane T2 located behind aircraft stand NO.7-16)

  2. The distance between centre lines of T1 and T2 is 80 M.

  3. The distance between centre line of Taxilane T1 and aircraft tail limit line is 47.50 M.

  4. The distance between centre line of Taxilane T2 and aircraft tail limit line is 47.40 M.

  5. Taxilane T3, T4, T5, T6 and T7 connected with Taxilane T1 and T2 can accommodate aircraft code letter E and below

9.5 Ground services are provided by aircraft operating agency, for non-agency aircraft are persuaded to contact THAI INTER traffic on VHF 131.5 MHZ or BAGS on VHF 131.35 MHZ 15 minutes prior to arrival or notify by Flight Plan.

VTSP  AD 2.21  NOISE ABATEMENT PROCEDURES

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VTSP  AD 2.22  FLIGHT PROCEDURES

1.  REVISED IMPLEMENTATION OF THE CONTINUOUS DESCENT OPERATIONS (CDO) FOR ARRIVALS INTO PHUKET INTERNATIONAL AIRPORT
1.1 INTRODUCTION
1.1.1 As part of AEROTHAI’s ongoing efforts to improve operational efficiency and air traffic management, Continuous Descent Operations (CDO) will commence from 1700 UTC on 12 October 2017 with trial period from 1700 UTC on 11 September 2017 until 1659 UTC on 12 October 2017. CDO is an operation, enabled by airspace design, procedure design and ATC facilitation, in which an aircraft continuously descends, to the greatest possible extent, by employing minimum engine thrust, ideally in a low drag configuration, prior to Final Approach Fix / Final Approach Point.
1.1.2 Vertical profile of CDO aims to improve flight stability (minimal level-off), increase terrain safety, ensure environmental friendly procedures by reducing aircraft noise, fuel consumption and emissions, enhanced flight punctuality and predictability, as well as other economic benefits for flights into Phuket International Airport.
1.2 CONDITION OF USE
1.2.1  Conditions for Conducting a CDO
1.2.1.1 CDO application can be either under surveillance or Procedural environment.
1.2.1.2 CDO can be requested by pilot or initiated by ATC. Pilot should request CDO at least 5 minutes prior to reaching Top of Descent (TOD) for any type of approach.

Note: 1.There is limited benefit if CDO clearance is received at altitude lower than 10,000 FT.

Note: 2.In case of CDO procedure being impractical due to an emergency, weather condition, traffic situation or any other reasons, an alternate instruction will be issued by ATC, or requested by pilot.

1.2.2 Application of Other ATC Procedures
1.2.2.1 When conducting CDO, standard ATC procedures continue to apply. ATC may issue clearance to an intermediate approach level while facilitating a CDO profile.
1.2.2.2 In doing so, ATC shall endeavour to issue further descent clearance prior to the CDO flight reaching the last assigned altitude so as to prevent aircraft from levelling off.
1.2.3 Change of Runway-In-Use
1.2.3.1 In case of change on Runway-in-Use prior to aircraft reaching Final Approach Fix / Final Approach point, i.e. from RWY 27 to RWY 09 CDO procedure shall be cancelled.
1.2.3.2 Pilot should then re-plan arrival route to the revised landing runway and inform ATC if the flight would still be able to meet all required speed/altitude restrictions.
1.2.4 Aircraft Type

CDO procedure is applicable for FMS capable aircraft.

1.2.5 Arrival Routes

CDO procedure is in place for all aircraft on G458 inbound to Phuket International Airport via STAR SAVSA1D.

1.2.6 Operations Time

CDO is available 24 hours.

1.2.7 Available Runway

CDO procedure is available for RWY 27

1.2.8 Types of Approach
1.2.8.1 ILS or LLZ RWY 27
1.2.8.2 RNAV (GNSS) RWY 27
1.2.8.3 VOR Z RWY 27
1.2.9 Speed

When traffic permits, aircraft will operate at an optimum speed calculated by FMS, depending on aircraft type. The following speed guidance should be applicable in case of high traffic volume.

Flight StatusSpeed Range
Above 10 000 FT.250 – 320 IAS
Below 10 000 FT.220 – 250 IAS
Final Segment (up to 4 NM)160 – 180 IAS
1.2.10 Minimum Flight Altitude
1.2.10.1 Outside Phuket TMA, aircraft shall comply with altitude constraints of the CDO procedure.
1.2.10.2 Inside Phuket TMA, during CDO, minimum safety altitudes are identical to those within Instrument Approach Procedures required or minimum radar vector altitude.
1.3 CDO PROCEDURE
1.3.1 Before aircraft reaching TOD (approximately 150 NM from the airport), either pilot or ATC can initiate CDO using phraseologies described in paragraph 1.4.
1.3.2 When all requirements for CDO are met and situation permits, CDO will commence.
1.3.3 Pilot shall operate aircraft FMS to plan optimal descent profile and report CDO execution commencing descent.
1.3.4 Aircraft should descend continuously on normal arrival route to Phuket TMA.
1.3.5 Longitudinal separation required will be at least 3 minutes or 8 NM on final approach segment between CDO traffic.
1.3.6 Operations without Vectoring
1.3.6.1 ILS or LLZ, RNAV (GNSS) and VOR Z RWY27 Instrument Approach Procedure
  1. Aircraft Arriving on G458

    1. Aircraft Arriving on G458, reaching SAVSA altitude not higher than 10,000 FT., then follow on SAVSA1D to BARON altitude not lower than 3,000 FT. then connect to IF for ILS or LLZ, RNAV (GNSS) or VOR Z RWY 27 approach procedure as published in AIP Thailand.

    2. The pilot may request permission to fly directly to Intermediate Fix (IF); however, this would be an ATC’s jurisdiction whether the request can be approved, depending on traffic conditions. In this case, the pilot shall fly directly to (IF), and will be advised by ATC, after (IF) follow the ILS or LLZ, RNAV (GNSS) or VOR Z RWY 27 approach procedure as published in AIP Thailand.

1.3.7 Operations under Vectoring
1.3.7.1 Pilot should receive CDO clearance at altitude not lower than 10,000 FT.
1.3.7.2 ATC shall provide vectoring guidance and track mile estimate to pilot.
1.3.8 Radio Communications Failure
1.3.8.1 In the event of radio communication failure, CDO flight will be terminated immediately
1.3.8.2 Pilot is to apply radio failure procedures stated in AIP Thailand ENR 1.6-6 paragraph 6.
1.4 PHRASEOLOGY
1.4.1 The following phraseology does not phrases and regular radio telephony procedure words contain in Doc 4444 and Doc 9432, but it enables clear and concise communications between pilot and controller to maintain safety of CDO arrivals
1.4.2 ATC-initiated CDO

“(aircraft call sign), (ATC unit), CDO AVAILABLE, DO YOU ACCEPT?”

1.4.3 Pilots response to ATC-initiated CDO
1.4.3.1 “(aircraft call sign), ACCEPT CDO”
1.4.3.2 “(aircraft call sign), NEGATIVE CDO”
1.4.4 Pilot-requested CDO

“(ATC Unit), (aircraft call sign), REQUEST CDO (type of approach) APPROACH”

1.4.5 Approval CDO by Bangkok Area Control Centre

“(aircraft call sign), CDO (type of approach) APPROVED DESCEND TO (level or altitude), QNH (number) SAVSA1D ARRIVAL”

1.4.6 Denial CDO by Bangkok Area Control Centre
1.4.6.1 “(aircraft call sign), UNABLE TO APPROVED, DUE TO (reason)”
1.4.6.2 “(aircraft call sign), EXPECT CDO FROM PHUKET APPROACH
1.4.7  CDO Cleared or Approved by Phuket Approach Control Unit
1.4.7.1 “(aircraft call sign), CDO DESCEND VIA STAR TO (level), QNH (number) INFORMATION…. CURRENT EXPECT (Type of approach) APPROACH RWY (Number)”
1.4.7.2 “(aircraft call sign), DESCEND TO (level), QNH (number), CDO (type of approach) APPROVED”
1.4.8 When vectoring for CDO

“(aircraft call sign), FLY HEADING (three digits); TURN LEFT (or RIGHT) HEADING (three digits) VECTORING FOR CDO, POSITION (number) MILES FROM TOUCHDOWN”

1.4.9 CDO Cancellation
1.4.9.1 “(aircraft call sign), CANCEL CDO DUE TO (reason), STOP DESCEND (level or altitude), QNH (number)”
1.4.9.2 “(aircraft call sign), CDO TERMINATED DUE TO (reason)”
1.4.10 Resuming CDO

“(aircraft call sign), RESUME CDO DIRECT (point), DESCEND TO (level or altitude), QNH (number), CLEAR (type of approach) APPROACH RWY27

1.4.11 Pilot report leaving assigned level

“(aircraft call sign), CDO LEAVING (level)”

1.4.12 Warning of aircraft below CDO Profile

“(aircraft call sign), BELOW CDO PROFILE, ALTITUDE SHOULD BE (altitude) OR ABOVE”

1.5 INFORMATION/TRAINING
1.5.1 Each airline must ensure that, for each type of aircraft, pilots are aware of CDO performance requirements.
1.5.2 Airlines are expected to define strategy to be adopted to drag-generating parts extension to stabilize aircraft in landing configuration at an altitude in compliance with flight safety, taking into account glide path at 3.2° in Final Approach.

VTSP  AD 2.23  ADDITIONAL INFORMATION

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VTSP  AD 2.24  CHARTS RELATED TO AN AERODROME

Chart name

Page

Aerodrome Chart - ICAO

AD 2-VTSP-2-1

Aircraft Parking/Docking Chart - ICAO

AD 2-VTSP-2-3

Aircraft Parking/Docking Chart - ICAO (Verso)

AD 2-VTSP-2-4

Aerodrome Ground Movement Chart - ICAO

AD 2-VTSP-2-5

Aerodrome Obstacle Chart - ICAO - Type A - RWY 09/27

AD 2-VTSP-3-1

Aerodrome Obstacle Chart - ICAO - Type B - RWY 09/27

AD 2-VTSP-3-3

Standard Departure Chart - Instrument (SID) - ICAO - RWY 09/27

AD 2-VTSP-6-1

Standard Departure Chart - Instrument (SID) - ICAO - RWY 09/27 (Tabular description 1)

AD 2-VTSP-6-2

Standard Departure Chart - Instrument (SID) - ICAO - RWY 09/27 (Tabular description 2)

AD 2-VTSP-6-3

Standard Departure Chart - Instrument (SID) - ICAO - RNAV RWY 09 - ANPUB1A EMRIT1A EPGOT1A IGEVI1A ONETI1A REBED1A SATVA1A SAVSA1A SUSID1A UBNEN1A UPSAB1A

AD 2-VTSP-6-5

Standard Departure Chart - Instrument (SID) - ICAO - RNAV RWY 09 - ANPUB1A EMRIT1A EPGOT1A IGEVI1A ONETI1A REBED1A SATVA1A SAVSA1A SUSID1A UBNEN1A UPSAB1A (Tabular description 1)

AD 2-VTSP-6-6

Standard Departure Chart - Instrument (SID) - ICAO - RNAV RWY 09 - ANPUB1A EMRIT1A EPGOT1A IGEVI1A ONETI1A REBED1A SATVA1A SAVSA1A SUSID1A UBNEN1A UPSAB1A (Tabular description 2)

AD 2-VTSP-6-7

Standard Departure Chart - Instrument (SID) - ICAO - RNAV RWY 09 - ANPUB1A EMRIT1A EPGOT1A IGEVI1A ONETI1A REBED1A SATVA1A SAVSA1A SUSID1A UBNEN1A UPSAB1A (Waypoint list table)

AD 2-VTSP-6-8

Standard Departure Chart - Instrument (SID) - ICAO - RNAV RWY 27 - ANPUB1B EMRIT1B EPGOT1B IGEVI1B ONETI1B REBED1B SATVA1B SAVSA1B SUSID1B UBNEN1B UPSAB1B

AD 2-VTSP-6-9

Standard Departure Chart - Instrument (SID) - ICAO - RNAV RWY 27 - ANPUB1B EMRIT1B EPGOT1B IGEVI1B ONETI1B REBED1B SATVA1B SAVSA1B SUSID1B UBNEN1B UPSAB1B (Tabular description 1)

AD 2-VTSP-6-10

Standard Departure Chart - Instrument (SID) - ICAO - RNAV RWY 27 - ANPUB1B EMRIT1B EPGOT1B IGEVI1B ONETI1B REBED1B SATVA1B SAVSA1B SUSID1B UBNEN1B UPSAB1B (Tabular description 2)

AD 2-VTSP-6-11

Standard Departure Chart - Instrument (SID) - ICAO - RNAV RWY 27 - ANPUB1B EMRIT1B EPGOT1B IGEVI1B ONETI1B REBED1B SATVA1B SAVSA1B SUSID1B UBNEN1B UPSAB1B (Waypoint list table)

AD 2-VTSP-6-12

Standard Arrival Chart - Instrument (STAR) - ICAO - RNAV RWY 09 - ANPUB1C EMRIT1C EPGOT1C IGEVI1C MONBU1C ONETI1C SATVA1C SAVSA1C SUSID1C UBNEN1C UPSAB1C URGAD1C

AD 2-VTSP-7-1

Standard Arrival Chart - Instrument (STAR) - ICAO - RNAV RWY 09 - ANPUB1C EMRIT1C EPGOT1C IGEVI1C MONBU1C ONETI1C SATVA1C SAVSA1C SUSID1C UBNEN1C UPSAB1C URGAD1C (Tabular description 1)

AD 2-VTSP-7-2

Standard Arrival Chart - Instrument (STAR) - ICAO - RNAV RWY 09 - ANPUB1C EMRIT1C EPGOT1C IGEVI1C MONBU1C ONETI1C SATVA1C SAVSA1C SUSID1C UBNEN1C UPSAB1C URGAD1C (Tabular description 2)

AD 2-VTSP-7-3

Standard Arrival Chart - Instrument (STAR) - ICAO - RNAV RWY 09 - ANPUB1C EMRIT1C EPGOT1C IGEVI1C MONBU1C ONETI1C SATVA1C SAVSA1C SUSID1C UBNEN1C UPSAB1C URGAD1C (Tabular description 3)

AD 2-VTSP-7-4

Standard Arrival Chart - Instrument (STAR) - ICAO - RNAV RWY 09 - ANPUB1C EMRIT1C EPGOT1C IGEVI1C MONBU1C ONETI1C SATVA1C SAVSA1C SUSID1C UBNEN1C UPSAB1C URGAD1C (Waypoint list table)

AD 2-VTSP-7-5

Standard Arrival Chart - Instrument (STAR) - ICAO - RNAV RWY 27 - ANPUB1D EMRIT1D EPGOT1D IGEVI1D MONBU1D ONETI1D SATVA1D SAVSA1D SUSID1D UBNEN1D UPSAB1D URGAD1D

AD 2-VTSP-7-7

Standard Arrival Chart - Instrument (STAR) - ICAO - RNAV RWY 27 - ANPUB1D EMRIT1D EPGOT1D IGEVI1D MONBU1D ONETI1D SATVA1D SAVSA1D SUSID1D UBNEN1D UPSAB1D URGAD1D (Tabular description 1)

AD 2-VTSP-7-8

Standard Arrival Chart - Instrument (STAR) - ICAO - RNAV RWY 27 - ANPUB1D EMRIT1D EPGOT1D IGEVI1D MONBU1D ONETI1D SATVA1D SAVSA1D SUSID1D UBNEN1D UPSAB1D URGAD1D (Tabular description 2)

AD 2-VTSP-7-9

Standard Arrival Chart - Instrument (STAR) - ICAO - RNAV RWY 27 - ANPUB1D EMRIT1D EPGOT1D IGEVI1D MONBU1D ONETI1D SATVA1D SAVSA1D SUSID1D UBNEN1D UPSAB1D URGAD1D (Tabular description 3)

AD 2-VTSP-7-10

Standard Arrival Chart - Instrument (STAR) - ICAO - RNAV RWY 27 - ANPUB1D EMRIT1D EPGOT1D IGEVI1D MONBU1D ONETI1D SATVA1D SAVSA1D SUSID1D UBNEN1D UPSAB1D URGAD1D (Waypoint list table)

AD 2-VTSP-7-11

Instrument Approach Chart - ICAO - VOR y RWY 09

AD 2-VTSP-8-1

Instrument Approach Chart - ICAO - VOR y RWY 27

AD 2-VTSP-8-3

Instrument Approach Chart - ICAO - VOR z RWY 09

AD 2-VTSP-8-5

Instrument Approach Chart - ICAO - VOR z RWY 27

AD 2-VTSP-8-7

Instrument Approach Chart - ICAO - ILS or LLZ RWY 27

AD 2-VTSP-8-9

Instrument Approach Chart - ICAO - RNAV (GNSS) z RWY 09

AD 2-VTSP-8-11

Instrument Approach Chart - ICAO - RNAV (GNSS) z RWY 09 (Tabular description)

AD 2-VTSP-8-12

Instrument Approach Chart - ICAO - RNAV (GNSS) z RWY 27

AD 2-VTSP-8-13

Instrument Approach Chart - ICAO - RNAV (GNSS) z RWY 27 (Tabular description)

AD 2-VTSP-8-14

Instrument Approach Chart - ICAO - RNAV (RNP) y RWY 09

AD 2-VTSP-8-15

Instrument Approach Chart - ICAO - RNAV (RNP) y RWY 09 (Tabular description)

AD 2-VTSP-8-16

Instrument Approach Chart - ICAO - RNAV (RNP) y RWY 09 (Waypoint list table)

AD 2-VTSP-8-18

Instrument Approach Chart - ICAO - RNAV (RNP) y RWY 27

AD 2-VTSP-8-19

Instrument Approach Chart - ICAO - RNAV (RNP) y RWY 27 (Tabular description)

AD 2-VTSP-8-20

Instrument Approach Chart - ICAO - RNAV (RNP) y RWY 27 (Waypoint list table)

AD 2-VTSP-8-21