SUPP 03 13 new - Copy

Transcription

SUPP 03 13 new - Copy
REPUBLIC OF INDONESIA
DIRECTORATE GENERAL OF CIVIL AVIATION
Phone/ Fax : 62 21 3507603
Telegraphic Address
AFS
: WRRRYNYX
DIRECTORATE OF AIR NAVIGATION
SUB DIRECTORATE MANAGEMENT OF
AERONAUTICAL INFORMATION
Jl. Medan Merdeka Barat No. 8 Gedung Karya Lt. 7
Jakarta 10110
or
P.O.Box 3109/JKT, Jakarta 10000
Email :[email protected],
[email protected]
Web : http://www.aimindonesia.info/
AIRAC
AIP
SUPPLEMENT
Nr : 03 / 13
30 MAY 13
THE OPERATION OF NEW AERODROME
KUALANAMU INTERNATIONAL AIRPORT- MEDAN
ASSOCIATED WITH THE ATS AIRSPACE AND FLIGHT PROCEDURES
1.
Introduction
New
aerodrome
Kualanamu
International
Airport
are
completely
constructed by phase I with runway number designation 05/23, this new
aerodrome is located 15 NM North East (NE) of Polonia Airport, those
contiguous airports are impacted each other to these airports operation.
When the new aerodrome Kualanamu be operated that Polonia airport is
not intended to close in hence that the flight procedures of Polonia Airport
are revised and be published under separate AIP Supplement publication.
2.
This AIRAC AIP Supplement is to supersede and cancel the AIC
number 04/08 dated 17 September 2008, the other AIC coming for
issuing information regarding another runway parallel development.
3.
The Operation Procedures and changes
3.1
As from 25 July 2013 at 00.01 UTC all incoming and outgoing
aircraft to Medan will use Kualanamu International Airport, in order
Directorate General of Civil Aviation, Indonesia
Publication Date : 30 MAY 13
Effective Date
: 25 JUL 13
AIRAC
AIP SUPPLEMENT 04/13
Page 2 of 3
to achieve safety and to maintain an orderly flow of air traffic,
Polonia Airport Medan shall not be used for schedule and
unschedule commercial and civil flight. Aircraft flight destination
Polonia-Medan which intend to remain over night at Polonia must
regulate the schedule and accord to the line of the Polonia Airport
operation function as an air force base.
3.2
The ATS airspace boundary for Medan Terminal Area (TMA) is not
changed,
and due to geographically Kualanamu International
Airport and Polonia airport are contiguous, Medan Control Zone
(CTR) is redefined and will be centered at “DES” VOR/DME with
radius 40 NM lateral limit from Surface (SFC) to FL120, Aerodrome
Traffic Zone (ATZ) boundaries of Kualanamu and Polonia airport are
not defined.
3.3
The ATS Routes segmentation which use “MDN” VOR/DME are not
changed and still used for En Route until any further realignment.
3.4
Kualanamu International Airport will take over the functions of AMS
Sub Centre of Polonia airport and will use the location indicator
WIMM as its AFTN address for receiving and sending messages,
the status of location Indicator of Polonia Airport will changed as a
tributary address by using WIMK.
a. Kualanamu International Airport with specified units address as
follows :
Aerodrome AIS Unit
: WIMMYOYW
Aerodrome Control Tower Unit
: WIMMZTZW
Approach Control Unit
: WIMMZAZW
Meteorological Station Unit
: WIMMYMYW
Directorate General of Civil Aviation, Indonesia
Publication Date : 30 MAY 13
Effective Date
: 25 JUL 13
AIRAC
AIP SUPPLEMENT 04/13
Page 3 of 3
b. Polonia Airport with specified units address as follows:
4.
Aerodrome AIS Unit
: WIMKYOYW
Aerodrome Control Tower Unit
: WIMKZTZW
Terminal Control Unit
: WIMKZLZW
Meteorological Station Unit
: WIMKYMYW
The new aerodrome data and Charts related to Aerodrome layout,
Ground Movement, Radar Minimum Altitude and Flight Procedures
are depicted on the attachments of this AIRAC AIP Supplement as
follows:
5.
-
Attachment A, Aerodrome Data (A1 to A36)
-
Attachment B, Aerodrome Chart;
-
Attachment C, Aircraft Parking / Docking Chart;
-
Attachment D1 to D4, Aerodrome Ground Movement Charts;
-
Attachment E1 & E2, SID RWY 05 & RWY 23;
-
Attachment F1 & F2, STAR RWY 05 & RWY 23;
-
Attachment G, Radar Minimum Altitude Chart – ICAO;
-
Attachment H1, IAP VOR/DME RWY 05;
-
Attachment H2, IAP VOR/DME RWY 23;
-
Attachment H3, IAP ILS RWY 05;
-
Attachment H4, IAP ILS RWY 23;
-
Attachment I, Fuel Dumping Procedure Chart;
Any changes to the information content on this AIRAC AIP
Supplement will be notified through NOTAM or superseded by other
AIP Supplement.
----- end ----Directorate General of Civil Aviation, Indonesia
Publication Date : 30 MAY 13
Effective Date
: 25 JUL 13
AIRAC
AIP SUPPLEMENT 03 / 13
Attachment “A1”
WIMM AD 2.1 AERODROME LOCATION INDICATOR AND NAME
WIMM – MEDAN / Kualanamu Internasional
WIMM AD 2.2 AERODROME GEOGRAPHICAL AND ADMINISTRATIVE DATA
ARP Coordinates and Site at AD……….…….
Direction and Distance From (City)…………..
Elevation / Reference Temperature………….
MAG VAR / Annual Change…………………..
AD Administration………………………………
Address………………………………………….
Telephone……………………………………….
Telefax…………………………………………...
Telex……………………………………………..
E-mail............................................................
AFTN…………………………………………….
Type of Traffic Permitted………………………
Type of rwy
Remarks…………………………………………
03˚ 38’ 32” N 098˚ 53’ 07” E
23,78 km North East From Medan City
23 ft / 32 º C
1º West
PT. Angkasa Pura II (Persero)
Kualanamu International Airport
Kec.Beringin, Lubuk Pakam Post Code
20552
(+62) 61 88880300
(+62) 61 88880301
Reserved
Reserved
WIMMYOYW
IFR and VFR
Instrument rwy cat.I
Website : Reserved
WIMM AD 2.3 OPERATIONAL HOURS
AD Administration………………………………
Custom and Immigration………………………
Health and Sanitation………………………….
AIS Briefing Office……………………………..
ATS Reporting Office…………………………..
MET Briefing Office…………………………….
ATS………………………………………………
Fuelling…………………………………………..
Handling…………………………………………
Security………………………………………….
De-Icing………………………………………….
Remarks…………………………………………
MON – FRI
: 01.00 – 10.00
H24
H24
H24
H24
H24
H24
H24
H24
H24
NA
NA
WIMM AD 2.4 HANDLING SERVICE AND FACILITIES
Cargo Handling Facilities……………………… Warehouse with advance storage, stacker
material, pallet container handling system
(PHCS), handling service are provided by:
- PT. Gapura Angkasa
- PT. Jasa Angkasa Semesta
- PT. NATS Nusantara
- PT.Jasa Karya Semesta
- PT. Dharma Bandar Mandala
- PT. Raya Utama Logistik
- PT. Prima Sakti Indo
- PT. Prathita Titian Nusantara
Directorate General of Civil Aviation
Publication Date : 30 MAY 13
Effective Date
: 25 JUL 13
AIRAC
AIP SUPPLEMENT 03 / 13
Attachment “A2”
- PT. Wawasan Berjaya
Fuel / Oil / Type………………………………… AVTUR 50/Jet A1 , AVGAS and Oil ASW
100,
Fuelling Facilities / Capacity…………………. Fuel Tank Capacity, Hydrant Pit,
.
Dispenser and Fuel Truck 72 million Liters
De-Icing Facilities………………………........... Not Available
Hangar Space for Visiting Aircraft.….……….. Not Available
Repair Facilities for Visiting Aircraft................ For minor repairing
Remarks………………………………………… All requests for ACFT marshalling should
be directed to the airlines or ground
handling agent except for non handling
agent flight service by AMC (Apron
Movement Control)
WIMM AD 2.5 PASSENGER FACILITIES
Hotels……………………………………………
Restaurant……………………………………....
Transportation…………………………............
Medical Facilities…………………….…………
Available in Medan City.
Available at the Airport.
Taxi, Bus, Train and Rent Car.
H 24 Airport Health Service, Patar Asih
Hospital (3 km).
Bank and Post Office……………….………… Available at the airport.
Tourist Office…………………………………… Available at the Airport
Remarks………………………………………… NIL
WIMM AD 2.6 RESCUE AND FIRE FIGHTING
AD Category for Fire Fighting…….................. Category IX
Rescue Equipment………………….…………. 4 units Foam Tender Type I,
1 unit Rapid Intervention Vehicle,
1 unit Command Car
3 units Ambulance.
Trainned Personel 96 persons
Capability For Removal of Disabled
Aircraft…………………………………….…….. 1 unit Salvage Equipment
Remarks………………………………………… Nil
WIMM AD 2.7 SEASONAL AVAILABILITY CLEARING
Type Of Clearing Equipment…………………. RWY Sweeper 2 units
Grass car mower 5 units
Rubber Deposit Removal 1 unit
Clearance…………………………………... …. 1) Runway
2) Taxiway
3) Apron
Remarks………………………………………… Nil
Directorate General of Civil Aviation
Publication Date : 30 MAY 13
Effective Date
: 25 JUL 13
AIRAC
AIP SUPPLEMENT 03 / 13
Attachment “A3”
WIMM AD 2.8 APRONS, TAXIWAYS AND CHECK LOCATION DATA
APRON SURFACE AND STRENGTH
APRON Victor
Surface
Strength
Dimension
= Concrete
= PCN 109 R/C/W/T
= 205 m x 216 m
APRON Whisky
Surface
Strength
Dimension
= Concrete
= PCN 109 R/C/W/T
= 166 m x 700 m
APRON Yankee
Surface
Strength
Dimension
= Concrete
= PCN 109 R/C/W/T
= 205 m x 216 m
TAXIWAY WIDTH, SURFACE, AND STRENGTH
TWY ALPHA (A) (Parallel)
Surface
Strength
Dimension
= Concrete
= PCN 109 R/C/W/T
= 3750 m x 30 m
TWY BRAVO (B) (Parallel)
Surface
Strength
Dimension
= Concrete
= PCN 109 R/C/W/T
= 2000 m x 30 m
TWY CHARLIE (C)
Surface
Strength
Dimension
= Concrete
= PCN 109 R/C/W/T
= 132,5 m x 36,25 m
TWY DELTA (D)
Surface
Strength
Dimension
= Concrete
= PCN 109 R/C/W/T
= 348,06 m x 30,40 m
TWY ECHO (E)
Surface
Strength
Dimension
= Concrete
= PCN 109 R/C/W/T
= 328,91 m x 30,41 m
TWY GOLF (G)
Surface
Strength
Dimension
= Concrete
= PCN 109 R/C/W/T
= 328,91 m x 30 m
Directorate General of Civil Aviation
Publication Date : 30 MAY 13
Effective Date
: 25 JUL 13
AIRAC
AIP SUPPLEMENT 03 / 13
Attachment “A4”
TWY HOTEL (H)
Surface
Strength
Dimension
= Concrete
= PCN 109 R/C/W/T
= 132,5 m x 41,25 m
TWY SIERRA (S)
Surface
Strength
Dimension
= Concrete
= PCN 109 R/C/W/T
= 937 m x 30 m
TWY TANGO (T)
Surface
Strength
Dimension
= Concrete
= PCN 109 R/C/W/T
= 465,71 m x 30 m
TWY A1
Surface
Strength
Dimension
= Concrete
= PCN 109 R/C/W/T
= 70 m x 30 m
TWY A2
Surface
Strength
Dimension
= Concrete
= PCN 109 R/C/W/T
= 70 m x 30 m
TWY A3
Surface
Strength
Dimension
= Concrete
= PCN 109 R/C/W/T
= 70 m x 30 m
TWY A4
Surface
Strength
Dimension
= Concrete
= PCN 109 R/C/W/T
= 70 m x 30 m
TWY A5
Surface
Strength
Dimension
= Concrete
= PCN 109 R/C/W/T
= 70 m x 30 m
TWY Apron Victor
Surface
Strength
Dimension
= Concrete
= PCN 109 R/C/W/T
= 220 m x 30 m
TWY Apron Whiskey
Surface
Strength
Dimension
= Concrete
= PCN 109 R/C/W/T
= 700 m x 30 m
Directorate General of Civil Aviation
Publication Date : 30 MAY 13
Effective Date
: 25 JUL 13
AIRAC
AIP SUPPLEMENT 03 / 13
Attachment “A5”
TWY Apron Yankee
Surface
Strength
Dimension
= Concrete
= PCN 109 R/C/W/T
= 220 m x 30 m
TWY Uniform (U)
Surface
Strength
Dimension
= Concrete
= PCN 109 R/C/W/T
= 198 m x 30 m
TWY Zulu (Z)
Surface
Strength
Dimension
= Concrete
= PCN 109 R/C/W/T
= 98 m x 30 m
ACL Location and Elevation………………….. NIL
DES VOR ………………….............................. 1.400 meter from TDZ rwy 05
Remarks………………………………………… NIL
WIMM AD 2.9 SURFACE MOVEMENT GUIDANCE AND CONTROL SYSTEM AND
MARKING
Use of Aircraft ID Sign, TWY Guide Lines and
Visual Docking / Parking Guidance System of
Aircraft Stands…………………………………….. Nose Wheel Guidelines at Apron
RWY and TWY Marking and LGT………………. RWY Marking :
RWY designation, THR, TDZ, Centerline,
Fixed distance marking, Side Stripe, Aiming
Point
RWY LGT :
THR, RWY end,
Centerline, RTIL,
RWY
edge,
RWY
TWY Marking :
Centerline, TWY holding position, Side Strip
TWY LIGHT :
Available
Stop Bars……………………………………….….. Available
Remarks………………………………………….… NIL
WIMM AD 2.10 AERODROME OBSTACLE
Reserved
Directorate General of Civil Aviation
Publication Date : 30 MAY 13
Effective Date
: 25 JUL 13
AIRAC
AIP SUPPLEMENT 03 / 13
Attachment “A6”
WIMM AD 2.11 METEOROLOGICAL INFORMATION PROVIDED
Associated Met Office……………………........ AD Meteorological, Climatology and
Geophysical Station Medan Kualanamu
Hours of Service / Met Office Outside Hours.. H 24
Office Responsible for TAF Preparation
Period of Validity……………………………….. AD Meteorological, Climatology and
Geophysical Station Medan Kualanamu
Trend Forecasts & Interval Issuance…….… TREND–every hours 0300-1500 of
issuance
Briefing / Consultation Provided……………… Personal consultation
Flight Documentation - Language Used…...... Chart – English
Charts and Other Information Available for
Briefing or Consultation……………………… Photo Satellite, and QAM
Supplementary Equipment Available for
Providing Information………………………….. Satellite, Weather Radar and AWOS
ATS Units Provided With Information…….….. TWR, APP and Aerodrome AIS Unit
Additional Information (Limitation of
Service etc.)…………………………………….. H 24
WIMM AD 2.12 RUNWAY PHYSICAL CHARACTERISTICS
1
2
Designations
RWY NR
True
BRG
05
045º
3
Dimension of
RWY
3750 x 60 m
23
225º
Directorate General of Civil Aviation
4
Strength
(PCN) and
Surface of
RWY and
SWY
71 F/B/W/T
Asphalt
Concrete
5
6
THR
Coordinates
THR
Elevation
and
Highest
Elevation
of TDZ of
Precision
APP RWY
03 37 33.24 N
098 51 30.96 E
23 ft
03 38 59.44 N
098 52 56.86 E
20 ft
Publication Date : 30 MAY 13
Effective Date
: 25 JUL 13
AIRAC
AIP SUPPLEMENT 03 / 13
Attachment “A7”
7
8
9
10
11
Slope of
RWY - NR
SWY
Dimension
CWY Dimension
Strip
Dimension
OFZ
Transverse
Slope
(1.5%)
60 x 60 m
300 x 300 m
Remarks
NIL
3990 x 300 m
60 x 60 m
12
RESA Dimension
180m x120m
(both of RWY)
300 x 300 m
Longitudinal
Slope
(0.023%)
NIL
WIMM AD 2.13 DECLARED DISTANCES
1
2
3
4
5
RWY
Designator
TORA
TODA
ASDA
LDA
05
3750 m
4050 m
3810 m
3750 m
23
3750 m
4050 m
3810 m
3750 m
WIMM AD 2.14 APPROACH AND RUNWAY LIGHTING
1
RWY
Designator
05
23
2
APCH LIGHT
Type LEN
PALS Cat.1
High Intensity
900 m
SQFL
PALS Cat.1
High Intensity
900 m
SQFL
Directorate General of Civil Aviation
3
THR LGT Color
WBAR
4
VASIS (MEHT)
PAPI
5
TDZ LGT LEN
Green
PAPI (3o)
NIL
Green
PAPI (3o)
NIL
Publication Date : 30 MAY 13
Effective Date
: 25 JUL 13
AIRAC
AIP SUPPLEMENT 03 / 13
Attachment “A8”
6
RWY
Centerline LGT
Length Spacing
Color
7
RWY Edge LGT
LEN Spacing
Color
8
RWY End LGT
Color WBAR
9
SWY
LGT
LEN (m) Color
10
Remarks
Red - Clear
Clear - Clear
Clear - Red
Yellow - Clear
Clear - Clear
Clear - Yellow
High Intensity
Comb.
Threshold
R/W End
NIL
NIL
Red - Clear
Clear - Clear
Clear - Red
Yellow - Clear
Clear - Clear
Clear - Yellow
High Intensity
Comb.
Threshold
R/W End
NIL
NIL
WIMM AD 2.15 OTHER LIGHTING, SECONDARY POWER SUPPLY
1.
ABN / lBN Location, Characteristic and Hours
Operation.
Rotating Beacon Light 24 flashes/
minutes on top of Tower.
2.
LDI Location and LGT
Anemometer Location and LGT
Available
3.
TWY Edge and Center Line LGT
Available
4.
Secondary Power Supply / Switch Over
Time
Genset: 1600 kVA : 2 units
2000 kVA : 5 units
UPS: 30 kVA : 2 sets
120 kVA : 5 sets
330 kVA : 2 sets
CCR: 4 kVA : 2 units
15 kVA : 7 units
25 kVA : 6 units
5.
Remarks
Directorate General of Civil Aviation
-
Wind Direction Indicator (WDI): 2
units on 150 m fm RWY 05 and
23
-
Flood Light 30 units
Publication Date : 30 MAY 13
Effective Date
: 25 JUL 13
AIRAC
AIP SUPPLEMENT 03 / 13
Attachment “A9”
WIMM AD 2.16 HELICOPTER LANDING AREA
1.
Coordinates TLOF THR FATO
NIL
2.
TLOF and / or FATO Elevation (m / ft)
NIL
3.
NIL
4.
TLOF and FATO Area Dimensions, Surface,
Strength, Marking
True Bearing and Magnetic Bearing Of FATO
5.
Declared Distance Available
NIL
6.
APP and FATO Lighting
NIL
7.
Remarks
NIL
NIL
WIMM AD 2.17 ATS AIRSPACE
1.
Designation and Lateral Limits
MEDAN CTR :
A circle with a radius of 40 NM centered at “DES”
VOR/DME
2.
Vertical Limits
SFC up to 12000 ft
3.
Airspace Classification
C
4.
Medan Director/English
5.
ATS Unit Call Sign/
Language(s)
Transition
6.
Remarks
NIL
Directorate General of Civil Aviation
11,000 ft / FL130
Publication Date : 30 MAY 13
Effective Date
: 25 JUL 13
AIRAC
AIP SUPPLEMENT 03 / 13
Attachment “A10”
WIMM AD 2.18 ATS COMMUNICATION FACILITIES
1
2
3
4
5
Service
Designator
Call sign
Frequency
Hours of
Operation
Remarks
APP
1
Medan Director
1
119.70 Mhz
120.65 MHz*
H-24
*Secondary
H-24
In the vicinity
of Aerodrome
2
TWR
Kualanamu Tower
118.6 Mhz
120.85 MHz*
Ground
Movement
Control
Kualanamu Ground
130.3 MHz
129.85 MHz*
FSS
Medan Info
(MWARA)
SSB
3416, 5631,
6595 kHz
H-24
H-24
Medan Info
(RDARA)
5631, 3416, 6595,
8957, 11305,
11366 kHz
H-24
Medan
4555, 5188, 5195,
6985, 8070 kHz
H24
ATIS
126.3 MHz
H24
Emergency
121.5 MHz
H24
Directorate General of Civil Aviation
Publication Date : 30 MAY 13
Effective Date
: 25 JUL 13
AIRAC
AIP SUPPLEMENT 03 / 13
Attachment “A11”
WIMM AD 2.19 RADIO NAVIGATION AND LANDING AIDS
1
2
3
Type of Aid
and Category
ID
Frequency
DVOR/DME
ILS/LLZ
RWY 05
DES
IDES
112.2
MHz/
CH-59X
4
Hours
of
Operat
ion
5
Site of Transmitting
Antenna Coordinates
H-24
03 37 01.59 N
098 50 59.68 E
H-24
CH-30X
H-24
110.9 MHz
H-24
ILS/DME
RWY 23
CH-46X
H-24
GP RWY 05
332.0 MHz
H-24
03 37 42.93 N
098 51 35.41 E
GP RWY 23
330.8 MHz
H-24
03 38 55.1 N
098 52 47.16 E
MM RWY 05
75 MHz
H-24
03 37 08.91 N
098 51 06.95 E
MM RWY 23
75 MHz
H-24
03 39 23.60 N
098 53 20.96 E
MSSR
(1030 &
1090)
MHz
H-24
03 37 29.18 N
098 52 51.39 E
ILS/LLZ
RWY 23
IDEL
7
Remarks
DVOR/DME
“DES” 0,7
NM fm THR
RWY 05
03 39 06.14 N
098 53 03.64 E
109.3 MHz
ILS/DME
RWY 05
6
Elevation
of DME
transmittin
g Antenna
03 37 26.32 N
098 51 24.28 E
ILS Category I
MM 1050 m
from THR
RWY 05/23
-
Directorate General of Civil Aviation
Publication Date : 30 MAY 13
Effective Date
: 25 JUL 13
AIRAC
AIP SUPPLEMENT 03 / 13
Attachment “A12”
WIMM AD 2.20 LOCAL TRAFFIC REGULATIONS
2.20.1
Airport regulation
2.20.1.1 Aerodrome Traffic Circuit Procedures
Rwy 05 Right Hand Circuit.
Rwy 23 Left Hand Circuit
2.20.1.2 Aircraft type indication
a) Confirm aircraft type displayed prior to turning into stand.
b) Discontinue docking when marshaller aircraft not on the
stand.
2.20.2 Aircraft Parking Stands and Coordinate.
Aircraft Type can be parked as follows :
No
Name of
Apron
Type of Aircraft
11
B.737 ER/NG
Longitude (E)
03 38 19.84 N
098 52 41.66 E
03 38 18.50 N
098 52 42.99 E
03 38 16.83 N
098 52 44.65 E
03 38 15.16 N
098 52 46.31 E
03 38 13.49 N
098 52 47.98 E
03 38 05.06 N
098 52 56.37 E
26
27
B.737 ER/NG
03 38 06.00 N
098 52 55.43 E
28
B.737 ER/NG
03 38 06.95 N
098 52 54.49 E
29
B.737 ER/NG
03 38 07.89 N
098 52 53.55 E
30
B.737 ER/NG
03 38 08.84 N
098 52 52.62 E
31
B.737 ER/NG
03 38 09.78 N
098 52 51.68 E
32
B.737 ER/NG
03 38 10.72 N
33
B.737 ER/NG
03 38 11.67 N
098 52 50.74 E
098 52 49.80 E
13
14
15
1
Latitude ( N )
B747/A330/
B737 ER
B747/A330/
B737 ER
B747/A330/
B737 ER
B747/A330/
B737 ER
B.737 ER/NG
12
W
(Whisky)
Coordinates
Aircraft
Stand
Number
Directorate General of Civil Aviation
Publication Date : 30 MAY 13
Effective Date
: 25 JUL 13
AIRAC
AIP SUPPLEMENT 03 / 13
V
(Victor)
2
3
Y
(Yankee)
Remark :
1.
2.
3.
Attachment “A13”
1
B.737 ER/NG
03 38 23.87 N
098 52 53.21 E
2
B.737 ER/NG
03 38 22.93 N
098 52 52.27 E
3
B.737 ER/NG
03 38 21.99 N
098 52 51.33 E
4
B.737 ER/NG
B.737 ER/NG
03 38 21.04 N
098 52 50.39 E
03 38 20.10 N
098 52 49 45 E
6
B.737 ER/NG
03 38 27.99 N
098 52 49.11 E
7
B.737 ER/NG
03 38 27.05 N
098 52 48.17 E
8
B.737 ER/NG
03 38 26.11 N
098 52 47.23 E
5
9
B.737 ER/NG
03 38 25.16 N
098 52 46.29 E
10
B.737 ER/NG
03 38 24.22 N
098 52 45.35 E
16
B.737 ER/NG
03 38 16.60 N
098 53 00.45 E
17
B.737 ER/NG
03 38 15.66 N
098 52 59.51 E
18
B.737 ER/NG
03 38 14.71 N
098 52 58.57 E
19
B.737 ER/NG
03 38 13.77 N
098 52 57.63 E
20
B.737 ER/NG
03 38 12.82 N
098 52 56.70 E
21
B.737 ER/NG
03 38 12.48 N
098 53 04.56 E
22
B.737 ER/NG
03 38 11.53 N
098 53 03.62 E
23
B.737 ER/NG
03 38 10.59 N
098 53 02.68 E
24
B.737 ER/NG
03 38 09.65 N
098 53 01.74 E
25
B.737 ER/NG
03 38 08.70 N
098 53 00.80 E
Aircraft Parking Stand number 12 – 15 aviobridge available for B747 and A330.
Aircraft Parking Stand number 26 – 33 aviobridge available for B737.
Distance security line apron taxiway : 42,5 M for code letter E.
VISUAL DOCKING PARKING AT AIRCRAFT STANDS
1.
2.
3.
4.
5.
Use of Aircraft ID sign, TWY guide lines and visual docking of Aircraft stands.
Taxiing guidance sign at all intersection with TWY and RWY at all holding
positions.
Guidance at apron nose-in.
Marking Aids THR touchdown zone, centerline, side stripe, TWY
destinations, TWY centerline, taxi holding positions all taxiways, apron guide
lines for position of aircraft parking.
Stop bars where appropriate.
Directorate General of Civil Aviation
Publication Date : 30 MAY 13
Effective Date
: 25 JUL 13
AIRAC
AIP SUPPLEMENT 03 / 13
Attachment “A14”
2.20.3 Procedure for Start-Up and Pushback of Aircraft
1. Ground crew must ensure that the area behind and Aircraft is clear
of vehicles, equipment and other obstruction before the start-up or
pushback of Aircraft commence.
2. When the pilot is ready for start-up and pushback. Pilot shall seek
confirmation from the ground crew and there is no hazard to this
Aircraft starting up. Pilot shall notify to Kualanamu Tower
Controller that pilot is ready for pushback. On being told by
Kualanamu
Tower that pushback is approved pilot shall
coordinate with the ground crew for the start-up and pushback of
the Aircraft.
3. The following table describes the procedure for the pushback of
Aircraft from the various parking bays. When it becomes
necessary to vary a procedure to expedite Aircraft movements.
Kualanamu Tower will issue specific instructions to the pilot.
4. Aircraft shall be pushed back refer to the aircraft pushback
procedure at the table below.
5. Ground movement procedures follow guidance line at own
discretion until holding point Charlie or Hotel.
APRON/
ACFT
STANDS
VICTOR/
1
PUSHBACK PROCEDURES
1) The aircraft (on idle thrust) shall be pushed back
facing North East till its nose wheel is at the
intersection of visual guidance aid.
PHRASEOLOGY
USED BY
KUALANAMU
GROUND
Pushback and pull
approved to face North
East
2) There shall be no simultaneous push back for aircraft
at aircraft stand 2,6,7
3) The aircraft may breakaway from here
OR
Pushback approved to
face South West
1) The aircraft (on idle thrust) shall be pushed back
facing South West till its nose wheel is at the
intersection of visual guidance aid.
2) There shall be no simultaneous push back for aircraft
at aircraft stand 2,6,7
3) The aircraft may breakaway from here
VICTOR/
2
1) The aircraft (on idle thrust) shall be pushed back
Pushback approved to
facing North East till its nose wheel is at the
face North East
intersection of visual guidance aid.
2) There shall be no simultaneous push back for aircraft
at aircraft stand 1,3,6,7,8
3) The aircraft may breakaway from here
Directorate General of Civil Aviation
Publication Date : 30 MAY 13
Effective Date
: 25 JUL 13
AIRAC
AIP SUPPLEMENT 03 / 13
Attachment “A15”
OR
VICTOR/
3
1) The aircraft (on idle thrust) shall be pushed back
facing South West till its nose wheel is at the
intersection of visual guidance aid.
2) There shall be no simultaneous push back for aircraft
at aircraft stand 1,3,6,7,8
3) The aircraft may breakaway from here
Pushback approved to
face South West
1) The aircraft (on idle thrust) shall be pushed back
facing North East till its nose wheel is at the
intersection of visual guidance aid.
2) There shall be no simultaneous push back for
aircraft at aircraft stand 2,4,7,8,9
3) The aircraft may breakaway from here
Pushback approved
to face North East
OR
1) The aircraft (on idle thrust) shall be pushed back
facing South West till its nose wheel is at the
intersection of visual guidance aid.
2) There shall be no simultaneous push back for
aircraft at aircraft stand 2,4,7,8,9
3) The aircraft may breakaway from here
VICTOR/
4
1)
2)
3)
OR
1)
2)
3)
The aircraft (on idle thrust) shall be pushed back
facing North East till its nose wheel is at the
intersection of visual guidance aid.
There shall be no simultaneous push back for
aircraft at aircraft stand 3,5,8,9,10
The aircraft may breakaway from here
The aircraft (on idle thrust) shall be pushed back
facing South West till its nose wheel is at the
intersection of visual guidance aid.
There shall be no simultaneous push back for
aircraft at aircraft stand 3,5,8,9,10
The aircraft may breakaway from here
Directorate General of Civil Aviation
Pushback approved
to face South West
Pushback approved
to face North East
Pushback approved
to face South West
Publication Date : 30 MAY 13
Effective Date
: 25 JUL 13
AIRAC
AIP SUPPLEMENT 03 / 13
VICTOR/
5
Attachment “A16”
1) The aircraft (on idle thrust) shall be pushed back
facing North West till its nose wheel is at the
intersection of visual guidance aid.
2) There shall be no simultaneous push back for aircraft
at aircraft stand 4,9,10,11,12,13
3) The aircraft may breakaway from here
Pushback approved to
face North West
OR
1)
2)
3)
The aircraft (on idle thrust) shall be pushed back
facing South Eest till its nose wheel is at the
intersection of visual guidance aid
There shall be no simultaneous push back for aircraft
at aircraft stand 4,9,10,11,12
The aircraft may breakaway from here
Pushback approved to
face South Eest
OR
1)
2)
3)
VICTOR/
6
The aircraft (on idle thrust) shall be pushed back
facing South West till its nose wheel is at the
intersection of visual guidance aid .
There shall be no simultaneous push back for aircraft
at aircraft stand 4,10,9.
The aircraft may breakaway from here
1) The aircraft (on idle thrust) shall be pushed back
facing North East till its nose wheel is at the
intersection of visual guidance aid .
2) There shall be no simultaneous push back for
aircraft at aircraft stand 1,2,7
3) The aircraft may breakaway from here
Pushback approved to
face South West
Pushback approved
to face North East
OR
1) The aircraft (on idle thrust) shall be pushed back
facing South West till its nose wheel is at the
intersection of visual guidance aid .
2) There shall be no simultaneous push back for
aircraft at aircraft stand 1,2,7
3) The aircraft may breakaway from here
Directorate General of Civil Aviation
Pushback approved
to face South West
Publication Date : 30 MAY 13
Effective Date
: 25 JUL 13
AIRAC
AIP SUPPLEMENT 03 / 13
VICTOR/
7
1) The aircraft (on idle thrust) shall be pushed
back facing North East till its nose wheel is at
the intersection of visual guidance aid .
2) There shall be no simultaneous push back for
aircraft at aircraft stand 1,2,3,6,8
3) The aircraft may breakaway from here
Attachment “A17”
Pushback approved to
face North East
OR
1) The aircraft (on idle thrust) shall be pushed
back facing South West till its nose wheel is at
the intersection of visual guidance aid .
2) There shall be no simultaneous push back for
aircraft at aircraft stand 1,2,3,6,8
3) The aircraft may breakaway from here
VICTOR/
8
1) The aircraft (on idle thrust) shall be pushed
back facing North East till its nose wheel is at
the intersection of visual guidance aid .
2) There shall be no simultaneous push back for
aircraft at aircraft stand 2,3,4,7,9
3) The aircraft may breakaway from here
Pushback approved to
face South West
Pushback approved to
face North East
OR
1) The aircraft (on idle thrust) shall be pushed
back facing South West till its nose wheel is at
the intersection of visual guidance aid .
2) There shall be no simultaneous push back for
aircraft at aircraft stand 2,3,4,7,9
3) The aircraft may breakaway from here
VICTOR/
9
1) The aircraft (on idle thrust) shall be pushed
back facing North East till its nose wheel is at
the intersection of visual guidance aid .
2) There shall be no simultaneous push back for
aircraft at aircraft stand 3,4,5,8,10
3) The aircraft may breakaway from here
Pushback approved to
face South West
Pushback and pull
approved to face North
East
OR
1) The aircraft (on idle thrust) shall be pushed
back facing South West till its nose wheel is at
the intersection of visual guidance aid .
2) There shall be no simultaneous push back for
aircraft at aircraft stand 3,4,5,8,10
3) The aircraft may breakaway from here
Directorate General of Civil Aviation
Pushback approved to
face South West
Publication Date : 30 MAY 13
Effective Date
: 25 JUL 13
AIRAC
AIP SUPPLEMENT 03 / 13
VICTOR/
10
1) The aircraft (on idle thrust) shall be pushed
back facing North West till its nose wheel is at
the intersection of the lead in line and the
taxiway W centreline .
2) There shall be no simultaneous push back for
aircraft at aircraft stand 4,5,9,11,12,13
3) The aircraft may breakaway from here
Attachment “A18”
Pushback approved to
face North West
OR
1) The aircraft (on idle thrust) shall be pushed
back facing South East till its nose wheel is at
the intersection of the lead in line and the
taxiway W centreline .
2) There shall be no simultaneous push back for
aircraft at aircraft stand 4,5,9,11
3) The aircraft may breakaway from here
Pushback approved to
face South East
OR
1) The aircraft (on idle thrust) shall be pushed
back facing South west till its nose wheel is at
the intersection of visual guidance aid .
2) There shall be no simultaneous push back for
aircraft at aircraft stand 4,6,9,11,12,13 (except
for 12,13 approved a/c type medium).
3) The aircraft may breakaway from here
YANKEE/
16
1) The aircraft (on idle thrust) shall be pushed
back facing North East till its nose wheel is at
the intersection of visual guidance aid.
2) There shall be no simultaneous push back for
aircraft at aircraft stand 17,21,22
3) The aircraft may breakaway from here
Pushback approved to
face South West
Pushback approved to
face North East
OR
1) The aircraft (on idle thrust) shall be pushed
back facing South West till its nose wheel is at
the intersection of visual guidance aid.
2) There shall be no simultaneous push back for
aircraft at aircraft stand 17,21,22
3) The aircraft may breakaway from here
Directorate General of Civil Aviation
Pushback approved to
face South West
Publication Date : 30 MAY 13
Effective Date
: 25 JUL 13
AIRAC
AIP SUPPLEMENT 03 / 13
YANKEE/
17
1) The aircraft (on idle thrust) shall be pushed
back facing North East till its nose wheel is at
the intersection of visual guidance aid.
2) There shall be no simultaneous push back for
aircraft at aircraft stand 16,18,21,22,23
3) The aircraft may breakaway from here
Attachment “A19”
Pushback approved to
face North East
OR
1) The aircraft (on idle thrust) shall be pushed
back facing South West till its nose wheel is at
the intersection of visual guidance aid.
2) There shall be no simultaneous push back for
aircraft at aircraft stand 16,18,21,22,23
3) The aircraft may breakaway from here
YANKEE/
18
1) The aircraft (on idle thrust) shall be pushed
back facing North East till its nose wheel is at
the intersection of visual guidance aid.
2) There shall be no simultaneous push back for
aircraft at aircraft stand 17,19,22,23,24
3) The aircraft may breakaway from here
Pushback approved to
face South West
Pushback approved to
face North East
OR
1) The aircraft (on idle thrust) shall be pushed
back facing South West till its nose wheel is at
the intersection of visual guidance aid.
2) There shall be no simultaneous push back for
aircraft at aircraft stand 17,19,22,23,24
3) The aircraft may breakaway from here
YANKEE/
19
1) The aircraft (on idle thrust) shall be pushed back
facing North East till its nose wheel is at the
intersection of visual guidance aid.
2) There shall be no simultaneous push back for
aircraft at aircraft stand 18,20,23,24,25
3) The aircraft may breakaway from here
Pushback approved to
face South West”
Pushback and pull
approved to face North
East
OR
1) The aircraft (on idle thrust) shall be pushed back
facing South West till its nose wheel is at the
intersection of visual guidance aid.
2) There shall be no simultaneous push back for
aircraft at aircraft stand 18,20,23,24,25
3) The aircraft may breakaway from here
Directorate General of Civil Aviation
Pushback approved to
face South West
Publication Date : 30 MAY 13
Effective Date
: 25 JUL 13
AIRAC
AIP SUPPLEMENT 03 / 13
YANKEE/
20
1)
Attachment “A20”
The aircraft (on idle thrust) shall be pushed back
facing North West till its nose wheel is at the
intersection of the lead in line and the taxiway W
centreline .
There shall be no simultaneous push back for
aircraft at aircraft stand 25,26,27,28
The aircraft may breakaway from here
Pushback approved to
face North West
1) The aircraft (on idle thrust) shall be pushed back
facing South East till its nose wheel is at the
intersection of the lead in line and the taxiway W
centreline .
2) There shall be no simultaneous push back for
aircraft at aircraft stand 25,26,28,29. (27
approved if push back face north west).
3) The aircraft may breakaway from here
Pushback approved to
face South East
2)
3)
OR
OR
1) The aircraft (on idle thrust) shall be pushed back
facing South West till its nose wheel is at the
intersection of visual guidance aid .
2) There shall be no simultaneous push back for
aircraft at aircraft stand 19, 24,25 (18 &23 if push
back heading, south west.
3) The aircraft may breakaway from here.
Directorate General of Civil Aviation
Pushback approved to
face South West
Publication Date : 30 MAY 13
Effective Date
: 25 JUL 13
AIRAC
AIP SUPPLEMENT 03 / 13
YANKEE/
21
1)
2)
3)
The aircraft (on idle thrust) shall be pushed back
facing North East till its nose wheel is at the
intersection of visual guidance aid.
There shall be no simultaneous push back for
aircraft at aircraft stand 16,17,22
The aircraft may breakaway from here
Attachment “A21”
Pushback approved to
face North East
OR
1)
2)
3)
1)
YANKEE/
22
2)
3)
The aircraft (on idle thrust) shall be pushed back
facing South West till its nose wheel is at the
intersection of visual guidance aid.
There shall be no simultaneous push back of
aircraft at stand 16,17,22
The aircraft may breakaway from here
The aircraft (on idle thrust) shall be pushed back
facing North East till its nose wheel is at the
intersection of visual guidance aid.
There shall be no simultaneous push back for
aircraft at aircraft stand 16,17,18,21,23,
The aircraft may breakaway from here
Pushback approved to
face South West
Pushback approved to
face North East
OR
1)
2)
3)
1)
YANKEE/
23
2)
3)
The aircraft (on idle thrust) shall be pushed back
facing South West till its nose wheel is at the
intersection of visual guidance aid.
There shall be no simultaneous push back for
aircraft at aircraft stand 16,17,18,21,23
The aircraft may breakaway from here
The aircraft (on idle thrust) shall be pushed back
facing North East till its nose wheel is at the
intersection of visual guidance aid.
There shall be no simultaneous push back for
aircraft at aircraft stand 17,18,19,22,24
The aircraft may breakaway from here
OR
1) The aircraft (on idle thrust) shall be pushed back
facing South West till its nose wheel is at the
intersection of visual guidance aid.
2)
3)
Pushback approved to
face South West”
Pushback approved to
face North East
Pushback approved to
face South West”
There shall be no simultaneous push back for
aircraft at aircraft stand 17,18,19,22,24
The aircraft may breakaway from here
Directorate General of Civil Aviation
Publication Date : 30 MAY 13
Effective Date
: 25 JUL 13
AIRAC
AIP SUPPLEMENT 03 / 13
YANKEE/
24
1) The aircraft (on idle thrust) shall be pushed
back facing North East till its nose wheel is at
the intersection of visual guidance aid.
2) There shall be no simultaneous push back for
aircraft at aircraft stand 18,19,20,23,25
3) The aircraft may breakaway from here
Attachment “A22”
Pushback and pull
approved to face North
East
OR
1) The aircraft (on idle thrust) shall be pushed
back facing South West till its nose wheel is at
the intersection of the lead in line and the
taxiway Y centreline .
2) There shall be no simultaneous push back for
aircraft at aircraft stand 18,19,20,23,25
3) The aircraft may breakaway from here
YANKEE/
25
1.
2.
3.
The aircraft (on idle thrust) shall be pushed
back facing North West till its nose wheel is at
the intersection of visual guidance aid .
There shall be no simultaneous push back for
aircraft at aircraft stand 20,26,27,28
The aircraft may breakaway from here
Pushback approved to
face South West
Pushback approved to
face North West
OR
1) The aircraft (on idle thrust) shall be pushed
back facing South East till its nose wheel is at
the intersection of visual guidance aid .
2) There shall be no simultaneous push back for
aircraft at aircraft stand 20,26,28,29. (27
approved if push back face north west).
3) The aircraft may breakaway from here
Pushback approved to
face South East
OR
1) The aircraft (on idle thrust) shall be pushed
back facing South West till its nose wheel is at
the intersection of visual guidance aid .
2) There shall be no simultaneous push back for
aircraft at aircraft stand 19, 20, 24
3) The aircraft may breakaway from here.
Directorate General of Civil Aviation
Pushback approved to
face South West
Publication Date : 30 MAY 13
Effective Date
: 25 JUL 13
AIRAC
AIP SUPPLEMENT 03 / 13
WHISKEY/
11
Attachment “A23”
MEDIUM
1) The aircraft (on idle thrust) shall be pushed
back facing North West till its nose wheel is at
the intersection of visual guidance aid .
2) There shall be no simultaneous push back for
aircraft at aircraft stand 5,10,12,13 (exception :
at stand 14 is medium aircraft and allowed to
push back simultaneously face north west)
3) The aircraft may breakaway from here
Pushback approved to
face North West
OR (MEDIUM)
1) The aircraft (on idle thrust) shall be pushed
back facing South West till its nose wheel is at
the intersection of visual guidance aid .
2) There shall be no simultaneous push back for
aircraft at aircraft stand 5,10,12,13 (exception :
at stand 14 is medium aircraft and allowed to
push back simultaneously face south west)
3) The aircraft may breakaway from here
Pushback and pull
approved to face South
West
HEAVY (Only One Direction)
1) The aircraft (on idle thrust) shall be pushed
back facing North West till its nose wheel is at
the intersection of visual guidance aid .
2) There shall be no simultaneous push back for
aircraft at aircraft stand 5,10,11,13,14
3) The aircraft may breakaway from here for
heavy
Pushback approved to
face North West
OR (HEAVY)
1) The aircraft (on idle thrust) shall be pushed
back facing South East till its nose wheel is at
the intersection of visual guidance aid .
2) There shall be no simultaneous push back for
aircraft at aircraft stand 5,10,11,13,14
(exception : at stand 13 or 14 is allowed to
pushed back simultaneously face north west or
at stand 14 is medium aircraft and allowed to
pushback simultaneously face south east)
3) The aircraft may breakaway from here for
heavy
Directorate General of Civil Aviation
Pushback approved to
face North West
Publication Date : 30 MAY 13
Effective Date
: 25 JUL 13
AIRAC
AIP SUPPLEMENT 03 / 13
WHISKEY/
12
WHISKEY/
13
Attachment “A24”
(MEDIUM)
1) The aircraft (on idle thrust) shall be pushed
back facing North West till its nose wheel is at
the intersection of visual guidance aid .
2) There shall be no simultaneous push back for
aircraft at aircraft stand 5,10,11,13,14
(exception : at stand 14 is medium aircraft and
allowed to pushback simultaneously face north
west )
3) The aircraft may breakaway from here
OR
1) The aircraft (on idle thrust) shall be pushed
back facing South East till its nose wheel is at
the intersection of visual guidance aid .
2) There shall be no simultaneous push back for
aircraft at aircraft stand 5,10,11,13,14
(exception : at stand 13 or 14 is allowed to
pushed back simultaneously face north west
3) The aircraft may breakaway from here
Pushback approved to
face North West
HEAVY
Pushback approved to
face North West
1)
2)
3)
Pushback approved to
face South East
The aircraft (on idle thrust) shall be pushed
back facing North West till its nose wheel is at
the intersection of the lead in line and the
taxiway W centerline.
There shall be no simultaneous push back for
aircraft at aircraft stand 5,10,11,12,14,15
(exception : aircraft at stand 12 is allowed to
pushed back simultaneously face south east)
The aircraft may breakaway from here
OR (HEAVY)
1) The aircraft (on idle thrust) shall be pushed
back facing South East till its nose wheel is at
the intersection of visual guidance aid .
2) There shall be no simultaneous push back for
aircraft at aircraft stand 5,10,11,12,14,15
(exception : aircraft at stand 14 or 15 is allowed
to pushed back simultaneously face north west)
3) The aircraft may breakaway from here
Directorate General of Civil Aviation
Pushback approved to
face South East
Publication Date : 30 MAY 13
Effective Date
: 25 JUL 13
AIRAC
AIP SUPPLEMENT 03 / 13
WHISKEY/
13
Attachment “A25”
MEDIUM
1) The aircraft (on idle thrust) shall be pushed back
facing North West till its nose wheel is at the
intersection of visual guidance aid .
2) There shall be no simultaneous push back for
aircraft at aircraft stand 5,10,11,12,14,15
(exception : aircraft at stand 15 is medium
aircraft and allowed to push back simultaneously
face north west or at stand 12 is allowed to
pushed back simultaneously face south east)
3) The aircraft may breakaway from here
Pushback approved to
face North West
OR (MEDIUM)
WHISKEY/
14
1) The aircraft (on idle thrust) shall be pushed back
facing South East till its nose wheel is at the
intersection of visual guidance aid .
2) There shall be no simultaneous push back for
aircraft at aircraft stand 5,10,11,12,14,15 (exception
: at stand 15 is medium aircraft and allowed to push
back simultaneously face south east or aircraft at
stand 14 or 15 is allowed to pushed back
simultaneously face north west)
3) The aircraft may breakaway from here
HEAVY
1) The aircraft (on idle thrust) shall be pushed back
facing South East till its nose wheel is at the
intersection of visual guidance aid .
2) There shall be no simultaneous push back for
aircraft at aircraft stand,11,12,13,15,33 (exception :
at stand 12 or 13 is allowed to pushed back
simultaneously face south east)
3) The aircraft may breakaway from here
Pushback approved to
face South East
Pushback approved to
face South East
OR
1) The aircraft (on idle thrust) shall be pushed back
facing South East till its nose wheel is at the
intersection of visual guidance aid .
2) There shall be no simultaneous push back for
aircraft at aircraft stand 5,10,11,12,13,15
3) The aircraft may breakaway from here
MEDIUM
1) The aircraft (on idle thrust) shall be pushed back
facing North West till its nose wheel is at the
intersection of visual guidance aid .
Directorate General of Civil Aviation
Pushback approved to
face North West
Publication Date : 30 MAY 13
Effective Date
: 25 JUL 13
AIRAC
AIP SUPPLEMENT 03 / 13
WHISKEY/
14
Attachment “A26”
2) There shall be no simultaneous push back for
aircraft at aircraft stand 12,13,15
(exception : at stand 12 is medium aircraft and
allowed to push back simultaneously face north
west or at stand 12 is allowed to pushed back
simultaneously face south east )
3) The aircraft may breakaway from here
OR (MEDIUM)
Pushback approved to
face South East
1) The aircraft (on idle thrust) shall be pushed back
facing South East till its nose wheel is at the
intersection of the lead in line and the taxiway W
centerline
2) There shall be no simultaneous push back for
aircraft at aircraft stand 13,15
3) The aircraft may breakaway from here
WHISKEY/
15
HEAVY
1)
The aircraft (on idle thrust) shall be pushed
back facing North West till its nose wheel is at
the intersection of visual guidance aid .
2)
There shall be no simultaneous push back for
aircraft at aircraft stand 13,14,33,32
3)
(exception : at stand 12 is allowed to pushed
back simultaneously face south east )
4)
The aircraft may breakaway from here
Pushback approved to
face North West
OR (HEAVY)
1)
2)
3)
The aircraft (on idle thrust) shall be pushed
back facing South East till its nose wheel is at
the intersection of visual guidance aid .
There shall be no simultaneous push back for
aircraft at aircraft stand 13,14,33,32
The aircraft may breakaway from here
Pushback approved to
face South East
OR (MEDIUM)
1)
2)
3)
The aircraft (on idle thrust) shall be pushed
back facing North West till its nose wheel is at
the intersection of visual guidance aid
There shall be no simultaneous push back for
aircraft at aircraft stand 13,14,33, (exception :
: at stand 13 is medium aircraft and allowed
to push back simultaneously face north west
or at stand 13 is allowed to pushed back
simultaneously face south east )
The aircraft may breakaway from here
Directorate General of Civil Aviation
Pushback approved to
face North West
Publication Date : 30 MAY 13
Effective Date
: 25 JUL 13
AIRAC
AIP SUPPLEMENT 03 / 13
WHISKEY/
15
OR (MEDIUM)
WHISKEY/
26
1)
Attachment “A27”
1)
The aircraft (on idle thrust) shall be pushed
back facing South East till its nose wheel is at
the intersection of the lead in line and the
taxiway W centerline.
2)
There shall be no simultaneous push back for
aircraft at aircraft stand 13,14,33, (exception :
at stand 13 is medium aircraft and allowed to
push back simultaneously face south east)
The aircraft may breakaway from here
2)
3)
The aircraft (on idle thrust) shall be pushed
back facing South East till its nose wheel is at
the intersection of visual guidance aid .
There shall be no simultaneous push back for
aircraft at aircraft stand 20,25,27,28,29
The aircraft may breakaway from here
Pushback approved to
face South East
Pushback approved to
face South East
OR
1)
2)
3)
WHISKEY/
27
1)
2)
3)
The aircraft (on idle thrust) shall be pushed
back facing South West till its nose wheel is at
the intersection of the lead in line and the
taxiway Y centreline .
There shall be no simultaneous push back for
aircraft at aircraft stand 19, 20, 24, 25, 27, 28,
29
The aircraft may breakaway from here
The aircraft (on idle thrust) shall be pushed back
facing North West till its nose wheel is at the
intersection of visual guidance aid .
There shall be no simultaneous push back for
aircraft at aircraft stand 26,28,29.
(ex : 29 heading south east)
The aircraft may breakaway from here
Pushback approved to
face South West
Pushback approved to
face North West
OR
1)
2)
3)
The aircraft (on idle thrust) shall be pushed back
facing South East till its nose wheel is at the
intersection of visual guidance aid .
There shall be no simultaneous push back for
aircraft at aircraft stand 20,25,26,28,29
(exception : aircraft at stand 26 is allowed to
pushed back simultaneously face north west)
The aircraft may breakaway from here
Pushback approved to
face South East
OR
1)
The aircraft (on idle thrust) shall be pushed back
facing South West till its nose wheel is at the
Directorate General of Civil Aviation
Publication Date : 30 MAY 13
Effective Date
: 25 JUL 13
AIRAC
AIP SUPPLEMENT 03 / 13
2)
3)
WHISKEY/
28
Attachment “A28”
intersection of the lead in line and the taxiway Y
centreline .
There shall be no simultaneous push back for
aircraft at aircraft stand 19,20,24,25,28,26,29,
The aircraft may breakaway from here
Pushback approved to
face South West
1) The aircraft (on idle thrust) shall be pushed back
facing North West till its nose wheel is at the
intersection of visual guidance aid .
2) There shall be no simultaneous push back for
aircraft at aircraft stand 20,25,27,29 (exception :
aircraft at stand 29 is allowed to pushed back
simultaneously face south east)
3) The aircraft may breakaway from here
Pushback approved to
face North West
OR
1) The aircraft (on idle thrust) shall be pushed back
facing South East till its nose wheel is at the
intersection of visual guidance aid .
2) There shall be no simultaneous push back for
aircraft at aircraft stand 29,27 (exception : aircraft
at stand 27 is allowed to pushed back
simultaneously face north west)
3) The aircraft may breakaway from here
Pushback approved to
face South East
OR
WHISKEY/
29
1) The aircraft (on idle thrust) shall be pushed back
facing South West till its nose wheel is at the
intersection of the lead in line and the taxiway Y
centreline .
2) There shall be no simultaneous push back for
aircraft at aircraft stand 26, 27, 29
The aircraft may breakaway from here
1) The aircraft (on idle thrust) shall be pushed back
facing North West till its nose wheel is at the
intersection of visual guidance aid .
2) There shall be no simultaneous push back for
aircraft at aircraft stand 28,30 (exception :
aircraft at stand 30 is allowed to pushed back
simultaneously face south east)
3) The aircraft may breakaway from here
OR
The aircraft (on idle thrust) shall be pushed back
facing South East till its nose wheel is at the
intersection of visual guidance aid .
1) There shall be no simultaneous push back for
aircraft at aircraft stand 28,30 (exception :
aircraft at stand 28 is allowed to pushed back
simultaneously face North West)
Directorate General of Civil Aviation
Pushback approved to
face South West
Pushback approved to
face North West
Pushback approved to
face South East
Publication Date : 30 MAY 13
Effective Date
: 25 JUL 13
AIRAC
AIP SUPPLEMENT 03 / 13
WHISKEY/
29
Attachment “A29”
2) The aircraft may breakaway from here
OR
1) The aircraft (on idle thrust) shall be pushed back
facing South West till its nose wheel is at the
intersection of the lead in line and the taxiway Y
centreline .
2) There shall be no simultaneous push back for
aircraft at aircraft stand 27, 28, 30
3) The aircraft may breakaway from here
WHISKEY/
30
1) The aircraft (on idle thrust) shall be pushed back
facing North West till its nose wheel is at the
intersection of visual guidance aid .
2) There shall be no simultaneous push back for
aircraft at aircraft stand 29,31
3) The aircraft may breakaway from here.
OR
1) The aircraft (on idle thrust) shall be pushed back
facing South East till its nose wheel is at the
intersection of visual guidance aid .
2) There shall be no simultaneous push back for
aircraft at aircraft stand 26,29,31
3) The aircraft may breakaway from here
WHISKEY/
31
1) The aircraft (on idle thrust) shall be pushed back
facing North West till its nose wheel is at the
intersection of visual guidance aid .
2) There shall be no simultaneous push back for
aircraft at aircraft stand 30,32
3) The aircraft may breakaway from here
OR
1) The aircraft (on idle thrust) shall be pushed back
facing South East till its nose wheel is at the
intersection of visual guidance aid .
2) There shall be no simultaneous push back for
aircraft at aircraft stand 30,32.
3) The aircraft may breakaway from here
WHISKEY/
32
1) The aircraft (on idle thrust) shall be pushed back
facing North West till its nose wheel is at the
intersection of visual guidance aid .
2) There shall be no simultaneous push back for
aircraft at aircraft stand 15,31,33 (exception :
aircraft at stand 15 is allowed to push back
simultaneously for medium).
Directorate General of Civil Aviation
Pushback approved to
face South West
Pushback approved to
face North West
Pushback approved to
face South East
Pushback approved to
face North West”
Pushback approved to
face South East ”
Pushback approved to
face North West
Publication Date : 30 MAY 13
Effective Date
: 25 JUL 13
AIRAC
AIP SUPPLEMENT 03 / 13
WHISKEY/
32
Attachment “A30”
3) The aircraft may breakaway from here
OR
1) The aircraft (on idle thrust) shall be pushed back
facing South East till its nose wheel is at the
intersection of visual guidance aid .
2) There shall be no simultaneous push back for
aircraft at aircraft stand 15,31,33 (exception :
aircraft at stand 15 is allowed to push back
simultaneously face south east)
3) The aircraft may breakaway from here
WHISKEY/
33
1) The aircraft (on idle thrust) shall be pushed back
facing North West till its nose wheel is at the
intersection of visual guidance aid .
2) There shall be no simultaneous push back for
aircraft at aircraft stand 14,15, 32 (exception :
aircraft at stand 14 is medium aircraft )
3) The aircraft may breakaway from here
Pushback approved to
face South East
Pushback approved to
face North West
OR
1) The aircraft (on idle thrust) shall be pushed back
facing South East till its nose wheel is at the
intersection of visual guidance aid .
2) There shall be no simultaneous push back for
aircraft at aircraft stand 14,15,32 (exception : at
stand 15 is medium aircraft and allowed to push
back simultaneously face south east)
3) The aircraft may breakaway from here
Pushback approved to
face South East
2.20.4 Taxiing To and From Stands.
See Aerodrome Ground Movement Procedure Charts.
2.20.5 Parking Area for Small Aircraft
Reserved
2.20.6 Parking Area for Helicopter
Reserved
2.20.7 Apron - Taxiing During Winter Conditions
Reserved
Directorate General of Civil Aviation
Publication Date : 30 MAY 13
Effective Date
: 25 JUL 13
AIRAC
AIP SUPPLEMENT 03 / 13
Attachment “A31”
2.20.8 Taxiing – Limitations
1) Pilot operating aircraft with code letter E shall take note that
judgemental oversteering may be required when manoeuvering
round taxiway turns.
2)
Pilot operating aircraft with code letter E are advised to apply
minimum thrust when turning from apron W to apron V or apron
Y.
2.20.9 School and Training Flights –Technical Test Flights – Use of Runways
Reserved
2.20.10
Helicopter Traffic – Limitation
Reserved
2.20.11
Removal of Disable Aircraft From Runways
Reserved
WIMM AD 2.21 NOISE ABATEMENT PROCEDURES
Reserved
WIMM AD 2.22 FLIGHT PROCEDURES
2.22.1
RESPONSIBILITY of ATS
2.22.1.1
Kualanamu Aerodrome Control Tower (TWR) is responsible
for providing of Air Traffic Control Service to all controlled
flight within Kualanamu ATZ.
2.22.1.2
Medan Approach Control Unit (APP) is responsible for
providing of Air Traffic Control Service to all controlled flight
within Medan CTR.
Directorate General of Civil Aviation
Publication Date : 30 MAY 13
Effective Date
: 25 JUL 13
AIRAC
AIP SUPPLEMENT 03 / 13
2.22.2
2.22.3
Attachment “A32”
ALTIMETER SETTING PROCEDURES
2.22.2.1
This ICAO altimeter setting procedures shall be used by all
aircraft operating within
Kualanamu ATZ and Medan CTR,
QNH provided in milibars and inches available on request.
2.22.2.2
Transition Altitude 11,000 feet transition level FL130.
COMMUNICATION PROCEDURES
All aircraft within Medan CTR shall be equipped with radio capable of
conducting and maintaining two way communication.
2.22.3.1
COMMUNICATION FAILURE PROCEDURES
2.22.3.1.1 In the event of failure of two-way communications while
operating on the radar frequency, the pilot shall change to any
other alternative ATC frequencies and request instructions.
2.22.3.1.2 If able to receive but not transmit, the pilot shall remain on the
frequency on which he has been communicating and comply
with instructions issued by the radar controller designed to
establish that the aircraft is receiving. If this is established,
further instructions appropriate to the circumstances will be
issued.
2.22.3.1.3 If unable to make contact on the alternative frequencies, the
pilot shall comply with the standard radio failure procedures
as specified below.
2.22.3.2
TOTAL RADIO COMMUNICATION FAILURE PROCEDURES
2.22.3.2.1 If total radio communication failure occurs in VMC during
daylight hours, the pilot shall continue to fly in VMC and land
at the most suitable aerodrome. If it occurs in VMC during the
hours of darkness (between sunset and sunrise) action shall
be taken in accordance below:
 If total radio communication failure occurs in IMC, ATC
action is based on the assumption that the aircraft will
continue to its destination and if unable to land, will
proceed to its nominated alternate. Separation standards
will be increased and airspace reserved accordingly. (see
Directorate General of Civil Aviation
Publication Date : 30 MAY 13
Effective Date
: 25 JUL 13
AIRAC
AIP SUPPLEMENT 03 / 13
Attachment “A33”
Appendices ‘A’ and ‘B’). SEE DOC.4444 PANS ATM
AMANDEMENT 4 15 NOP THN 2012

In IMC, or if unable to maintain VFR, the pilot shall either
leave or avoid controlled airspace and areas of dense
traffic and establish VFR operation or, alternatively, shall:
a) Proceed according to the current flight plan, at the
last assigned flight level, to the clearance limit
and thereafter at the flight plan level.
b) Arrive at the destination as close as possible to ETA.
c) Commence descent as close as possible to EAT (or
ETA if no EAT has been acknowledged).
d) If unable to land within 30 minutes of the time descent
should have started (i.e. EAT or ETA if no EAT has
been acknowledged), proceed to cross fix Holding
Area at 4000ft then via R461 at FL170 if Kuala
Lumpur is the nominated alternate or via W12 at FL
210 if Pekanbaru is the nominated alternate or via
G468 at FL 150 if Penang is the nominated alternate
or via N563 at FL 230 if Singapore is the nominated
alternate otherwise proceed at the planned flight level
to other nominated alternate.
Note:
1) Aircraft are to follow the established radio failure
procedures as laid down by the respective airports.
2) During this 30 minutes period ATC will reserve the
airspace at the aircraft’s flight level and below. At the
expiry of this period with the concurrence of other
users normal operations will resume.
2.22.3.2.2 In all cases, the pilot shall contact ATC as soon as possible
after landing.
2.22.4
RADIO FAILURE - TRANSPONDER - EQUIPPED AIRCRAFT
2.22.4.1 Aircraft equipped with transponder shall set transponder to Mode A/C
Code 7600.
Directorate General of Civil Aviation
Publication Date : 30 MAY 13
Effective Date
: 25 JUL 13
AIRAC
AIP SUPPLEMENT 03 / 13
Attachment “A34”
2.22.4.2 Partial Radio Failure
a) Aircraft Unable to Receive
Pilots shall adopt the complete RTF failure procedures specified in
para 2.22.4 above.
b) Aircraft Able to Receive
Following verification that aircraft is able to receive ground
transmissions, ATC will
continue to issue instructions and/or
clearance to pilots. Such instructions and clearances will be repeated.
2.22.5
IDENTIFICATION OF RUNWAY-IN-USE
ATC will switch on the appropriate approach lights and the ILS serving the
runway-in-use to assist the pilot in its identification. If the approach lights
for the runway-in-use are sighted but the ILS frequencies not received, the
pilot shall assume that the ILS is inoperative and shall proceed to land on
the runway on which the approach lights have been sighted.
2.22.6
TOTAL RADIO COMMUNICATION FAILURE - SPECIAL PROCEDURES
– KUALANAMU AIRPORT – DEPARTURES ( MEDIUM AND HEAVY
AIRCRAFT )
2.22.6.1 When an aircraft which has been cleared by ATC to an
intermediate level experiences total radio communication failure
immediately after departure from Kualanamu Airport and it is
deemed unsafe for it to continue to its destination, the pilot will
set the aircraft transponder to Mode A/C Code 7600 and adhere
to the procedures below.
2.22.6.2 When radio communication failure occurs immediately after the
aircraft has departed on RWY 05/23, the pilot shall proceed
according to the following procedures
a)
Directorate General of Civil Aviation
RUNWAY 05
1.
Proceed to BONAR Holding Area , climb to the last
assigned altitude. At BONAR, climb/descend to
maintain 7,000ft ;
2.
Hold at BONAR for 4 minutes. Leave BONAR and
proceed to AMASE holding area for dumping fuel
,maintaining 7.000 ft .
3.
After fuel dumping, proceed to DES VOR maintain
7,000ft. At D17 DES VOR FOLLOW ARC TO
BONAR descend for an instrument approach on
RWY 05. Identify the runway-in-use in accordance
with para 2.22.7
4.
ATC action is based on the assumption that the
aircraft will take a minimum of 10 min to dump fuel.
An aircraft therefore should not leave earlier than
Publication Date : 30 MAY 13
Effective Date
: 25 JUL 13
AIRAC
AIP SUPPLEMENT 03 / 13
Attachment “A35”
10 min after arrival at AMASE Holding Area even if
fuel dump is completed at a shorter time or if
dumping is not necessary or possible unless
circumstances require an immediate return.
b)
RUNWAY 23
1.
2.
3.
4.
2.22.7
2.22.8
Proceed to NAGAH holding point , climb to the last
assigned altitude. At NAGAH, climb/descend to
maintain 7,000ft;
Hold at NAGAH for 4 minutes. Leave NAGAH
proceed to AMASE holding area for dumping fuel
maintaining 7.000 ft.
After fuel dumping, proceed to DES VOR. AT D20
DES VOR FOLLOW ARC TO NAGAH Holding
Area maintain 7,000ft. At NAGAH descend for an
instrument approach on RWY 23. Identify the
runway-in-use in accordance with para 2.22.7
ATC action is based on the assumption that the
aircraft will take a minimum of 10 min to dump fuel.
An aircraft therefore should not leave earlier than
10 min after arrival at AMASE Holding Area even if
fuel dump is completed at a shorter time or if
dumping is not necessary or possible unless
circumstances require an immediate return.
TOTAL RADIO COMMUNICATION FAILURE - SPECIAL PROCEDURES
– KUALANAMU AIRPORT – DEPARTURES ( LIGHT AIRCRAFT)
2.22.7.1
Aircraft experiencing radio failure are to descend on the Left
Downwind RWY 23/Right Downwind RWY 05 of the runway
to 600 ft and rock the aircraft when passing abeam the
Control Tower.
2.22.9.2
Unless the pilot unmistakably sees a green light from the
Tower, he is not to assume that he is cleared to land but is to
carry out the same procedure again.
FUEL DUMPING PROCEDURE
AMASE Holding Area at Radial 360 distance 40 Nm from “DES” VOR,
Procedure Holding: Right Hand Circuit With One Minute Leg Alt.6000
feet and Speed 220 knots, entry heading 180.
Directorate General of Civil Aviation
Publication Date : 30 MAY 13
Effective Date
: 25 JUL 13
AIRAC
AIP SUPPLEMENT 03 / 13
Attachment “A36”
Entry to Area:
1)
2)
Pilot inform to ATC (Tower/APP/ACC) If he needed to fuel
dumping/burning .
ATC will inform Pilot the direction of amase Holding Point and
instruct the altitude to joint the pattern.
Exit from Area:
1)
2)
Pilot inform to ATC if the fuel dumping/burning was finished and
request to return to land at Kualanamu International Airport.
ATC will inform rwy in used to the pilot and instruct the altitude to
joint traffic circuit KUALANAMU.
WIMM AD 2.23 ADDITIONAL INFORMATION
Reserved
WIMM AD 2.24 CHARTS RELATED TO THE AERODROME
-
WIMM AD 2.24-1, AERODROME CHART- ICAO, dated 25 JUL 13;
-
WIMM AD 2.24-2, AIRCRAFT PARKING/DOCKING CHART, dated 25 JUL 13;
-
WIMM AD 2.24-3, AERODROME GROUND MOVEMENT CHARTS, dated 25 JUL 13;
-
WIMM AD 2.24-7A, STANDARD DEPARTURE CHART – INSTRUMENT (SID)-ICAO RWY 05,
dated 25 JUL 13;
-
WIMM AD 2.24-7B, STANDARD DEPARTURE CHART – INSTRUMENT (SID)-ICAO RWY 23,
dated 25 JUL 13;
-
WIMM AD 2.24-9A, STANDARD ARRIVAL CHART – INSTRUMENT (STAR)-ICAO RWY 05,
dated 25 JUL 13;
-
WIMM AD 2.24-9B, STANDARD ARRIVAL CHART – INSTRUMENT (STAR)-ICAO RWY 23,
dated 25 JUL 13;
-
WIMM AD 2.24-10, RADAR MINIMUM ALTITUDE CHART-ICAO, dated 25 JUL 13
-
WIMM AD 2.24-11A, IAC – ICAO VOR/DME RWY 05, dated 25 JUL 13;
-
WIMM AD 2.24-11B, IAC – ICAO VOR/DME RWY 23, dated 25 JUL 13;
-
WIMM AD 2.24-11C, IAC – ICAO ILS RWY 05, dated 25 JUL 13;
-
WIMM AD 2.24-11D, IAC – ICAO ILS RWY 23, dated 25 JUL 13;
-
WIMM AD 2.24-12, FUEL DUMPING PROCEDURE CHART, dated 25 JUL 13.
Directorate General of Civil Aviation
Publication Date : 30 MAY 13
Effective Date
: 25 JUL 13