AD 2 AERODROMES

WSSS —  SINGAPORE / SINGAPORE CHANGI INTL

WSSS AD 2.1 AERODROME LOCATION INDICATOR AND NAME

WSSS —  SINGAPORE / SINGAPORE CHANGI INTL

WSSS AD 2.2 AERODROME GEOGRAPHICAL AND ADMINISTRATIVE DATA

1 ARP coordinates and site at AD012133.16N 1035921.57E (Control Tower)
2Direction and distance from (city)061°, 17.2km from City Centre (The Fullerton, Singapore)
3Elevation/Reference temperature6.66 M (21.85ft) / 32.6 C
4Geoid Undulation (AD elevation position)10.29 M
5MAG VAR /Annual change0°26' E (2015) / negligible
6 AD Administration, address, telephone, telefax, AFS

RWY 02L/20R and RWY 02C/20C
CHANGI AIRPORT GROUP (SINGAPORE) PTE LTD
Singapore Changi Airport
P.O.Box 168, SINGAPORE 918141
Tel: (65)65956868 or (65)65423223
AFS: WSSSYAYX

7Types of traffic permittedIFR
8Remarks
  1. Scheduled closure periods for RWY 02L/20R and RWY 02C/20C: refer to WSSS AD 2-12.

  2. Not available to all non-scheduled civil aircraft types of 40-seater or below except in special circumstances. Aircraft larger than the above category shall not plan their arrival between 0900-1559UTC.

  3. Aircraft shall leave nose-in position (90 degrees) with the aid of aircraft tow tractors. Reverse thrust or variable pitch propellers shall not be used. Aircraft operators shall make suitable arrangements.

  4. PPR for aircraft not equipped with RTF.

  5. A subsonic jet aircraft, unless otherwise exempted, is not permitted to operate in Singapore unless it possesses a noise certificate stating that it meets the noise standards of ICAO Annex 16, Volume 1, Chapter 3, or equivalent. The noise certificate may also take the form of a suitable statement contained in another document approved by the State of Registry of the aircraft.

  6. Direct transit area: Overnight transit in Singapore City, TEL: (65)65956868 or (65)65423223

  7. RVR minima for CAT II ILS operations is limited to 350m due to runway and taxiway light spacing requirements on the airfield.

  8. Frangible poles are installed for the purpose of identifying 90m away from the centreline of RWY 02L/20R and RWY 02C/20C

WSSS AD 2.3 OPERATIONAL HOURS

Operational Hours
1Aerodrome Administration:
RWY 02L/20R and RWY 02C/20C
H24
2Customs and ImmigrationH24
3Health and SanitationH24
4AIS Briefing OfficeH24
5ATS Reporting OfficeH24
6MET Briefing OfficeH24
7Air Traffic ServicesH24

WSSS AD 2.4 HANDLING SERVICES AND FACILITIES

1Cargo Handling FacilitiesCargo terminals equipped with advanced storage stacker, material and pallet container handling systems, computerised cargo information, data and documentation systems.
Forklift (10 tonnes), Aircraft Main Deck Loaders (27 tonnes), trailers (e.g. 20-40 containers) on hire from hauliers.
2Fuel / Oil TypesJET A1(for jet aircraft),
Engine Oil - 2380, MJ02, 750, ET025.
Lubricating Oil - Aeroshell 390, 750.
Hydraulic Oil - Skydrol LD4, 500B4, 500B, Hyjet IV
3Fuelling Facilities / CapacityNo limitation. H24 service.
4Hangar space for visiting aircraftBy arrangement with SIA Engineering Company (SIAEC) or ST Aerospace Services Co. Maintenance hangars with multiple aircraft stands to accommodate up to A380 size aircraft.
5Repair facilities for visiting aircraftMajor and minor maintenance and repairs for commercial aircraft up to and including A380, subject to availability of specialised equipment/ spares/toolings.
6Remarks
  1. Marshalling Service: No pilot shall taxi an aircraft on its own into a gate/stand without the aid of a docking system or a marshaller.

  2. Oxygen And Related Servicing: Oxygen for all cabin and aircraft system. No CO2 recharging facilities.

WSSS AD 2.5 PASSENGER FACILITIES

1HotelsRooms available inside transit area, adjacent to airport terminal and in the city but advisable advance booking.
2RestaurantsAvailable in both transit and public areas.
3TransportationBuses, taxis and MRT train.
Car rental service is available from 0700-2300 hrs daily
4Medical FacilitiesAvbl H24 at Airport Clinic. Ambulance.
General Hospitals located at Simei (12km) and City (23km).
5Bank and Post OfficeAvailable at airport
6Tourist OfficeAvailable at airport
7RemarksInternet address : http://www.changiairport.com.sg
for airport and flight information, shops and restaurants, facilities and services, flight connections and tourist information.

WSSS AD 2.6 RESCUE AND FIRE FIGHTING SERVICES

1AD category for fire fightingCAT10 (No facilities for foaming of runways)
2Rescue equipmentAdequately provided as recommended by ICAO.
3Capability for removal of disabled aircraftFour 25-ton (Type G) and two 40-ton (Type F) pneumatic elevators, two 80-ton hydraulic recovery jacks, one set of tethering equipment and other accessory equipment. Capable of handling all wide-bodied aircraft. Provided by SIA at Tel:(65)65416329 or (65)65427116.
4RemarksAll Airport Emergency Service personnel are trained in rescue and fire-fighting as well as medical first-aid.

WSSS AD 2.7 SEASONAL AVAILABILITY - CLEARING

There is no requirement for clearing. The aerodrome is available throughout the year.

WSSS AD 2.8 APRONS, TAXIWAYS AND CHECK LOCATIONS/POSITIONS DATA

1Apron surface and strengthRWY 02L/20R
RWY 02C/20C
Surface:
Strength:
Concrete
PCN 85/R/B/W/U
2Taxiway width, surface and strengthRWY 02L/20R
RWY 02C/20C
Width:
45m (147ft) Taxiway V2;
35m (115ft) Taxiways NC3, EP and WP;
25m (82ft) Taxiway EP (from Taxilanes B1 and B3);
23m (75ft) Taxiway SA;
30m (100ft) All other Taxiways
Surface:Cement Concrete - Taxiways W1, W9, E1, E3, E11 and EP (between E10 and E11);
Bituminous Concrete - All other Taxiways
Strength:PCN 85/R/B/W/U - Taxiways W1, W9, E1, E3, E11 and EP (between E10 and E11);
PCN 72/F/B/W/U - All other Taxiways
3ACL location and elevationSee AD-2.WSSS-ADC-2/Chart (flip side) for coordinates and elevations of aircraft stands.
4INS checkpoints
5RemarksNIL

WSSS AD 2.9 SURFACE MOVEMENT GUIDANCE AND CONTROL SYSTEM AND MARKINGS

1Use of aircraft stand ID signs, TWY guidelines and visual docking/parking guidance system of aircraft stands.

Taxiing guidance signs at all intersections with TWY and RWY at all holding positions. Guidelines at apron. Nose-in guidance at aircraft stands. For information on Safegate Aircraft Docking Guidance System, Aircraft Parking Restrictions, Procedures for Start-up and Pushback of Aircraft, Pushback Procedures for Aircraft (Diagrams), Taxiing Guidance System at Singapore Changi Airport, refer to WSSS AD 2-9.

Aircraft stand manoeuvring guidance lights are provided at aircraft stands 1 to 17, 101 to 104 and aircraft stands at Terminal 3.

2RWY and TWY markings and LGT

RWY 02L/02C and RWY 20C

RWY LGT: refer to WSSS AD 2-14 to WSSS AD 2-15.

TWY LGT: Blue LGT on TWY curved edges, selected straight TWY edge sections and apron TWY edges only. Blue TWY edge markers along selected straight TWY edge sections. Red stop bar at TWY INT controllable on/off. Red stop bar LGT at TWY HLDG PSN entrances to RWY are controllable on/off and are supplemented with elevated RWY guard LGT at the sides.
Internally/externally lighted mandatory or information TWY signboards.
Yellow TWY centre line markings, supplemented by green centre line LGT with selective control along rapid exit TWY, taxi-routes to and from main RWY and aprons.

MARKING AIDS: THR, touchdown zone, centre line, side stripe, RWY designations, aiming point markings, TWY centre line, taxi holding positions - all taxiways, apron guide lines.
For positions of aircraft nosewheel in relation to stopbar and description of the Safegate Aircraft Docking Guidance System - refer to WSSS AD 2-9.

RWY 20R

RWY LGT: refer to WSSS AD 2-14 to WSSS AD 2-15.

TWY LGT: same as for RWY 02L/02C and RWY 20C.

MARKING AIDS: Pre-threshold centre-line, transverse stripe for displaced THR, RWY designations, THR, touchdown zone, aiming point marking, RWY centre-line and stripe marking aids.

3Stop bars: Stop bars where appropriate.
4Remarks: Nil
1 SAFEGATE AIRCRAFT DOCKING GUIDANCE SYSTEM - SAFEDOCK
1.1 INTRODUCTION
1.1.1 The Safegate Aircraft Docking Guidance System - SAFEDOCK is a fully automatic aircraft docking guidance system installed at the fixed gates in Terminals 1, 2 and 3 of Singapore Changi Airport. There are two types of ADGS in Singapore Changi Airport, Safedock Type 1 ADGS and Safedock Type 2 ADGS.
1.2 DESCRIPTION OF SYSTEM
1.2.1 The system is based on a laser scanning technique and it tracks both the lateral and longitudinal position of the aircraft. This 3D technique allows the system to identify the incoming aircraft and check it against the one selected by the operator to ensure that the pilot is provided with the correct stop indication for the aircraft.
1.2.2 The system is operated only in the Automatic Mode. When the system fails, the aircraft is to be marshalled into the stand manually.
1.2.3 Azimuth guidance, continuous closing rate information, aircraft type, etc., are shown to the pilot on a single display clearly visible for both pilot and co-pilots. Figure A shows the Display and Laser Scanning Unit mounted on the terminal in front of the aircraft stand.
LED DISPLAY AND LASER SCANNING UNIT

Safedock Type 1Safedock Type 2
Figure A
1.3 DOCKING PROCEDURES
Safedock
Type 1
Safedock
Type 2
1.3.1

Check that the correct aircraft type is displayed. The scrolling arrows indicate that the system is activated (see figure 1).


Figure 1:
System tracking for aircraft.
1.3.2

Follow the lead-in line

1.3.3

When the aircraft has been caught by the scanning unit, the scanning unit checks that the aircraft is the correct type and the display provides azimuth guidance information. When the solid yellow closing rate bar appears, the aircraft is being tracked by the system. (see figure 2).


Figure 2:
Aircraft tracked by the system.
1.3.4

Look for the flashing red arrow and solid yellow arrow which provide azimuth guidance information. The flashing red arrow shows which direction to steer, while the solid yellow arrow gives an indication of how far the aircraft is off the centreline (see figures 2 and 3).

1.3.5

When the aircraft is 15m from the stop position, closing rate information is given. “Distance to go” is indicated by turning off one row of LEDs (Laser Electronic Displays) for every half metre that the aircraft advances towards the stop position. From 15m to the stop position, a digital display will indicate the distance from the stop position for every 1m. At 3m from the stop position, the display will indicate the distance from the stop position for every 0.2m (see figures 3 and 4).


Figure 3
LED closing rate bar starts diminishing when the aircraft is 15m from stopbar at one row for every 0.5m that the aircraft moves forward.
1.3.6

When the correct stop position is reached, all of the LEDs for the closing rate bar will be off, the word “STOP” will appear in the display. For Safedock Type 1 ADGS, the word “STOP” will be displayed in red with red border. For Safedock Type 2 ADGS, the word “STOP” will be displayed in yellow and two red, rectangular fields will light in the azimuth guidance area of the display (see figure 5).


Figure 4
LED closing rate bar getting shorter as aircraft moves nearer to stopbar.
1.3.7

If the aircraft stops in the correct position, “OK” will be displayed after a few seconds (see figure 6).


Figure 5
Pilot to stop aircraft when “STOP” is displayed.

Figure 6
Informs the pilot that everything is in order and he can shutdown engine.
1.3.8

If the aircraft has gone past the correct stop position, the display will show “TOO FAR” (see figure 7).


Figure 7
Indicates that the aircraft has gone beyond the stopbar.
Pilot to check with ground engineer on the next move.
1.3.9

If some object is blocking the view towards the approaching aircraft or the detected aircraft is lost before 12m to the correct stop position, the system will show “WAIT” (see figure 8).

1.3.10

The aircraft must be identified at least 12m before the correct stop position. Otherwise, the display will show “WAIT”, “STOP” and “ID FAIL” (see figures 8, 9 and 10).


Figure 8
Pilot to hold aircraft and wait for other instructions from the display.
1.4 SAFETY MEASURES
Safedock
Type 1
Safedock
Tye 2
1.4.1

Pilot should not turn an aircraft into the parking stand if the docking system is not activated or on seeing a wrong aircraft type displayed on the system.


Figure 9
“STOP" may appear suddenly in the process of docking.
Pilot to stop immediately and wait for further instructions.
1.4.2

Pilot should not proceed beyond the passenger loading bridges unless the scrolling arrows (see figure 1) have been superseded by the solid yellow closing rate bar (see figure 2).

1.4.3

When using the docking system, pilots are to taxi into the aircraft stand at minimum speed. The system will display “SLOW” to inform the pilot if the aircraft's taxiing speed exceeded 1.2 m/s (see figure 11).


Figure 10
Indicates the system fails to identify the aircraft.
1.4.4

In bad weather conditions, the docking system may go into downgrade mode. The display will show the aircraft type and “SLOW” and the scrolling arrows are disabled (see figure 12). When the system has detected the aircraft, the solid yellow closing rate bar appears. Docking process is allowed to continue but pilots should exercise caution.


Figure 11
Informs the pilot that the aircraft travelling speed is too fast.
Pilot to slow down the speed. Similar for both Safedock Type 1 and Type 2
1.4.5

To avoid overshooting, pilots are advised to approach the stop position slowly and observe the closing rate information displayed. Pilots should stop the aircraft immediately when seeing the “STOP” or “WAIT” display, when given the stop sign by the aircraft marshaller or is unsure of the information displayed during the docking process.


Figure 12
The system goes into ‘downgrade’ mode due to bad weather conditions, pilot will be prompted to slow down. Docking process will continue when the aircraft is detected but pilot should exercise caution.
1.4.6

Pilot should stop the aircraft immediately if the display goes black during the docking process. The aircraft is to be marshalled into the stand manually.

2 AIRCRAFT PARKING RESTRICTIONS
2.1 TERMINAL 1 AIRCRAFT STANDS
Aircraft types that can be parked at stands (✈) are as follows:
StandsC1C11C13C15C16C17C18C19C20C22C23C24C25C26
A300
A310
A319
A320
A321
A332
A333
A342
A343
A345
A346
A359
A380
B707
B717
B727
B737
B747
B74S
B757
B762
B763
B772
B773
B773ER
B788
B789
BA146
DC10
DC9
F100
IL62
IL86
IL96
L101
MD11
MD80/82
MD83
MD88
2.2 TERMINAL 1 AIRCRAFT STANDS
Aircraft types that can be parked at stands (✈) are as follows:
StandsD30D32D34D35D36D37D38D40D41D42D42L &
D42R
D44D46D47D48D49
A300
A310
A319
A320
A321
A332
A333
A342
A343
A345
A346
A359
A380
B707
B717
B727
B737
B747
B74S
B757
B762
B763
B772
B773
B773ER
B788
B789
BA146
DC10
DC9
F100
IL62
IL86
IL96
L101
MD11
MD80
MD82
MD83
MD88
YK42
2.3 TERMINAL 2 AIRCRAFT STANDS
Aircraft types that can be parked at stands (✈) are as follows:
StandsE1E2E3E4E5E6E7E8E10E11E12E20E22E24E24LE24RE26E27E28
A300
A310
A319
A320
A321
A332
A333
A342
A343
A345
A346
A359
A380
B707
B727
B737
B747
B748
B74S
B757
B762
B763
B772
B772LR
B773
B773ER
B788
B789
DC10
DC9
F70
F100
IL62
IL86
IL96
L101
MD11
MD80
MD82
MD83
MD87
MD88
2.4 TERMINAL 2 AIRCRAFT STANDS
Aircraft types that can be parked at stands (✈) are as follows:
StandsF30F31F32F33F34F35F36F37F40F41F42F50F52F54F56F58F59F60
A300
A310
A319
A320
A332
A333
A342
A343
A345
A346
A359
A380
B707
B727
B737
B747
B748
B74S
B757
B762
B763
B772
B772LR
B773
B773ER
B788
B789
DC10
DC9
F70
L101
MD11
MD87
StandsF35LF35RF52LF52RF56LF56RF59LF59R
A319
A320
A321
B737
B737(100-500)
B737(600-900)
MD83
2.5 TERMINAL 3 AIRCRAFT STANDS
Aircraft types that can be parked at stands (✈) are as follows:
StandsA1A2A3A4A5A9A10A11A12A13A14A15A16A17A18A19A20A21
A300
A310
A319
A320
A321
A332
A333
A343
A345
A346
A359
A380
B737
B744
B788
B789
B757
B767
B772
B772LR
B773
B773ER
StandsB1B2B3B4B5B6B7B8B9B10
A300
A310
A319
A320
A321
A332
A333
A343
A345
A359
A346
A380
B707
B737
B744
B788
B789
B757
B767
B772
B773
B773ER
2.6 REMOTE STANDS
Aircraft types that can be parked at stands (✈) are as follows:
Stands103104200200L200R201202202L202R203205206207208209
A300, A310
A319, A320
A321
A330, A342
A343, A345
A359
A380
AT72
B707, B727
B737
B747, B74S, B788
B748
B757
B767, B772, B773
B773ER
B789
DC8
DC10
DHC7
F70
IL62
L101
MD11
MD83
Stands300301302303304305306307308309310400401402403404
A300, A310
A319, A320
A330, A342
A343, A345
A359
AT72
B707
B727
B737 (100-500)
B737 (600-900)
B747
B74S, B788
B757, B767
B772, B773
B773ER
B789
DC10
DC8
F70
L101
MD11
MD83
2.7 CARGO STANDS
Aircraft types that can be parked at stands (✈) are as follows:
Stands502503504505506507508509510 to
515
600511600L512600R513601514602515601602603604605611612
A300
A306
A310
A319
A320
A321
A330
A332
A333
A342
A343
A345
A346
A359
A380
AN24
B707
B727
B737
B744
B747
B748
B74S
B752
B753
B757
B762
B763
B764
B772
B772LR
B773
B773ER
B777F
B788
B789
DC8
DC10
IL62
IL86
L101
MD11
2.8 REMOTE STANDS
Aircraft types that can be parked at stands (✈) are as follows:
Stands1234567891011121314151617701702
AT72
ATR72-500
A318
A319
A320
A321
B733
B734
B735
B736
B737
B738
B739
DHC7
2.9 MARS STANDS

Aircraft types that can be parked at stands (✈) are as follows:

Stands101101L101R102102L102R516516L516R517517L517R
A300
A310
A319
A320
A321
A332
A333
A342
A343
A345
A346
A359
A388
AN124
B727
B737
B747
B748
B757
B762
B763
B764
B772
B772LR
B773
B773ER
B788
B789
DC10
L101
MD11
2.10 SOUTH APRON

Aircraft types that can be parked at stands (✈) are as follow:

Stands461462462L462R463463L463R
A306
A310
A318
A319
A320
A321
A332
A333
A342
A343
A345
A346
A359
A380
B733
B734
B735
B736
B737
B738
B739
B744
B752
B753
B762
B763
B764
B772
B773
B773ER
B788
B789
3 PROCEDURES FOR START-UP AND PUSHBACK OF AIRCRAFT
3.1 Ground crew must ensure that the area behind an aircraft is clear of vehicles, equipment and other obstructions before the start-up or pushback of aircraft commences.
3.2 When the pilot is ready for start-up and pushback, he shall seek confirmation from the ground crew that there is no hazard to his aircraft starting up. He shall then notify the Ground Movement Controller (Callsign: Singapore Ground) that he is ready for pushback. On being told by Singapore Ground that pushback is approved, he shall co-ordinate with the ground crew for the start-up and pushback of the aircraft.
3.3 The following table describes the procedures for the pushback of aircraft from the various aircraft stands. When it becomes necessary to vary a procedure to expedite aircraft movements, Singapore Ground will issue specific instructions to the pilot.
3.4 The lead-in lines are for aircraft nose-in guidance. For aircraft stands without dedicated pushback lines, ground crew may use the lead-in lines for pushback guidance.
APRON/ ACFT STANDSPUSHBACK PROCEDURESPHRASEOLOGY USED BY SINGAPORE GROUND

T3 WEST

A1

The aircraft shall be pushed back onto TWY V6 to face West such that the pushback line is always kept midway between the aircraft main gear until its nosewheel is at the “END OF PUSH (for A1 nose gear)” position. The aircraft shall then be towed forward along the pushback line until its nosewheel is at the “END OF TOW (for A1, A2, B1, B2)” position. The aircraft may breakaway from there. Engine start up is not permitted during standard pushback.

Standard pushback approved

Alternate Pushback

The aircraft (on idle thrust) shall be pushed back onto Taxilane V6 to face East, followed by TWY WA, such that the alternate pushback line is always kept midway between the aircraft main gear until the nose of the aircraft is behind the stopbar behind aircraft stand A3 or B2. The aircraft may breakaway from there. This alternate pushback procedure can only be exercised if the auxiliary power unit of aircraft is unserviceable.

Pushback approved, to face North (or South) on TWY WA

A2

The aircraft (on idle thrust) shall be pushed back onto TWY V6 to face West such that the pushback line is always kept midway between the aircraft main gear until its main gear is at the intersection of the pushback line and TWY V6 centreline and the nosewheel stops at the “END OF PUSH (A2, B2)” position. The aircraft shall then be towed forward along TWY V6 centreline until its nosewheel is at the “END OF TOW (for A1, A2, B1, B2)” position. The aircraft may breakaway from there.

Standard pushback approved

A3

The aircraft (on idle thrust) shall be pushed back onto TWY WA until its nosewheel is at the intersection of the aircraft stand lead-in line and TWY WA centreline. The aircraft may breakaway from there.

Pushback approved, to face North (or South).

A4

The aircraft (on idle thrust) shall be pushed back onto TWY WA to face North (or South) such that the pushback line is always kept midway between the aircraft main gear until its nosewheel is at TWY WA centreline. The aircraft may breakaway from there.

Pushback approved, to face North (or South).

A5, A9

The aircraft (on idle thrust) shall be pushed back:

  • onto TWY U2 to face North such that the pushback line is always kept midway between the aircraft main gear until the nose of the aircraft is behind the stopbar behind aircraft stand A11. The aircraft may breakaway from there.
OR

Pushback approved, to face North.

  • onto TWY WA to face South until the nose of the aircraft is behind the stopbar behind aircraft stand A4. The aircraft may breakaway from there.

Pushback approved, to face South.

A10

The aircraft (on idle thrust) shall be pushed back:

  • onto TWY U2 to face North until the nose of the aircraft is behind the stopbar behind aircraft stand A11. The aircraft may breakaway from there.
OR

Pushback approved, to face North.

  • onto TWY WA to face South until the nose of the aircraft is behind the stopbar behind aircraft stand A4. The aircraft may breakaway from there.

Pushback approved, to face South.

A11

The aircraft (on idle thrust) shall be pushed back:

  • onto TWY U2 to face North until the nose of the aircraft is at the intersection of the aircraft stand lead-in line and TWY U2 centreline. The aircraft shall then be towed forward until the nose of the aircraft is behind the stopbar behind aircraft stand A11. The aircraft may breakaway from there.
OR

Pushback approved, to face North.

  • onto TWY U2 to face South until the nose of the aircraft is at the intersection of the aircraft stand lead-in line and TWY U2 centreline. The aircraft shall then be towed forward until its nosewheel is behind the stopbar behind aircraft stand A12. The aircraft may breakaway from there.

Pushback approved, to face South.

A12

The aircraft (on idle thrust) shall be pushed back:

  • onto TWY U2 to face North until the nose of the aircraft is at the intersection of the aircraft stand lead-in line and TWY U2 centreline. The aircraft shall then be towed forward until its nosewheel is behind the stopbar behind aircraft stand 11. The aircraft may breakaway from there.
OR

Pushback approved, to face North.

  • onto TWY U2 to face South until its nosewheel is at the intersection of the aircraft stand lead-in line and TWY U2 centreline. The aircraft may breakaway from there.

Pushback approved, to face South.

A13, A14, A15

The aircraft (on idle thrust) shall be pushed back:

  • onto TWY WA to face North until the nose of the aircraft is behind the stopbar behind aircraft stand A16. The aircraft may breakaway from there.
OR

Pushback approved to face North.

  • onto TWY U2 to face South until the nose of the aircraft is behind the stopbar behind aircraft stand A12. The aircraft may breakaway from there.

Pushback approved to face South.

A16

The aircraft (on idle thrust) shall be pushed back onto TWY WA until its nosewheel is at the intersection of the aircraft stand lead-in line and TWY WA centreline. The aircraft may breakaway from there.

Pushback approved to face North (or South).

A17

Pushback facing West

The aircraft (on idle thrust) shall be pushed back onto TWY V8 to face West until its nosewheel is at the “END OF PUSH” position behind aircraft stand A17. The aircraft may breakaway from there.

Pushback approved, to face West.

Pushback facing South

The aircraft (on idle thrust) shall be pushed back onto TWY WA to face South until the nose of the aircraft is behind the stopbar behind aircraft stand A16. The aircraft may breakaway from there.

Pushback approved, to face South.

A18

The aircraft (on idle thrust) shall be pushed back onto TWY U4 to face West such that the pushback line is always kept midway between the aircraft main gear until its main gear is aligned with the centreline of TWY U4 and the nose of the aircraft is behind the stopbar behind aircraft stand A18. The aircraft may breakaway from there. Pushback to face East is not permitted.

Standard pushback approved

A19

The aircraft (on idle thrust) shall be pushed back onto TWY U4 to face West such that the pushback line is always kept midway between the aircraft main gear until its main gear is aligned with the centreline of TWY U4 and the nose of the aircraft is behind the stopbar behind the “END OF PUSH” line. The aircraft may breakaway from there. Pushback to face East is not permitted.

Standard pushback approved

A20

The aircraft (on idle thrust) shall be pushed back onto TWY U4 to face West such that the pushback line is always kept midway between the aircraft main gear until its main gear is aligned with the centreline of TWY U4 and the nose of the aircraft is behind the stopbar behind the “END OF PUSH (for A20 nose gear)” position. The aircraft may breakaway from there. Pushback to face East is not permitted.

Standard pushback approved

A21

The aircraft (on idle thrust) shall be pushed back onto Taxilane U4 to face East such that the pushback line is always kept midway between the aircraft main gear until its nosewheel is at the “END OF PUSH (for A21 nose gear)” position. The aircraft shall then be towed forward to face West until its nose is behind the stopbar behind aircraft stand A18. The aircraft may breakaway from there

Standard pushback approved

B1

The aircraft shall be pushed back onto TWY V6 to face West such that the pushback line is always kept midway between the aircraft main gear until its nosewheel is at the “END OF PUSH (for B1 nose gear)” position. The aircraft shall then be towed forward along the pushback line until its nosewheel is at the “END OF TOW (for A1, A2, B1, B2)” position. The aircraft may breakaway from there. Engine start up is not permitted during standard pushback.

Standard pushback approved

Alternate Pushback

The aircraft (on idle thrust) shall be pushed back onto Taxilane V6 to face East, followed by TWY WA, such that the alternate pushback line is always kept midway between the aircraft main gear until the nose of the aircraft is behind the stopbar behind aircraft stand A3 or B2. The aircraft may breakaway from there. This alternate pushback procedure can only be exercised if the auxiliary power unit of aircraft is unserviceable.

Pushback approved, to face North (or South) on TWY WA.

B2

The aircraft (on idle thrust) shall be pushed back onto TWY V6 to face West such that the pushback line is always kept midway between the aircraft main gear until its main gear is at the intersection of the pushback line and TWY V6 centreline and the nosewheel stops at the “END OF PUSH (A2, B2)” position. The aircraft shall then be towed forward along TWY V6 centreline until its nosewheel is at the “END OF TOW (for A1, A2, B1, B2)” position. The aircraft may breakaway from there.

Standard pushback approved

B3

The aircraft (on idle thrust) shall be pushed back onto TWY WA until its nosewheel is at the intersection of the aircraft stand lead-in line and TWY WA centreline. The aircraft may breakaway from there.

Pushback approved, to face North (or South).

B4

The aircraft (on idle thrust) shall be pushed back onto TWY WA to face North (or South) such that the pushback line is always kept midway between the aircraft main gear until its nosewheel is at TWY WA centreline. The aircraft may breakaway from there.

Pushback approved, to face North (or South).

B5, B6

The aircraft (on idle thrust) shall be pushed back:

  • onto TWY WA to face North until the nose of the aircraft is behind the stopbar behind aircraft stand B4. The aircraft may breakaway from there.
OR

Pushback approved, to face North.

  • onto TWY U1 to face South such that the pushback line is always kept midway between the aircraft main gear until the nose of the aircraft is behind the stopbar behind aircraft stand B7. The aircraft may breakaway from there.

Pushback approved, to face South.

B7

The aircraft (on idle thrust) shall be pushed back:

  • onto TWY U1 to face South until the nose of the aircraft is behind the stopbar behind aircraft stand B7. The aircraft may breakaway from there.
OR

Pushback approved, to face South.

  • onto TWY WA to face North until the nose of the aircraft is behind the stopbar behind aircraft stand B4. The aircraft may breakaway from there.

Pushback approved, to face North.

B8

The aircraft (on idle thrust) shall be pushed back:

  • onto TWY U1 to face South until its nosewheel is at the intersection of the aircraft stand lead-in line and TWY U1 centreline. The aircraft may breakaway from there.
OR

Pushback approved, to face South.

  • onto TWY U1 to face North until its nosewheel is at the intersection of the lead-in line and TWY U1 centreline. The aircraft shall then be towed forward until its nosewheel is at the intersection of the aircraft stand B9 lead-in line and TWY U1 centreline. The aircraft may breakaway from there.

Pushback approved, to face North.

B9, B10

The aircraft (on idle thrust) shall be pushed back onto TWY U1 until its nosewheel is at the intersection of the aircraft stand lead-in line and TWY U1 centreline. The aircraft may breakaway from there.

Pushback approved, to face North (or South).

MARS REMOTE

101, 101R

The aircraft (on idle thrust) shall be pushed back to face East until its nosewheel is at the “END OF PUSH” position. The aircraft shall then be towed forward until its nosewheel is at the “END OF TOW (EOT)” position on TWY L4 centreline. The aircraft may breakaway from there.

Standard pushback approved.

101L

The aircraft (on idle thrust) shall be pushed back onto TWY L4 centreline to face East. The aircraft shall then be towed forward along the centreline of TWY L4 until its nosewheel is at the “END OF TOW (EOT)” position. The aircraft may breakaway from there.

Standard pushback approved.

102, 102R, 102L

The aircraft (on idle thrust) shall be pushed back onto TWY L4 centreline to face East. The aircraft shall then be towed forward along the centreline of TWY L4 until the nose of the aircraft is behind the stopbar behind aircraft stand 102. The aircraft may breakaway from there.

Standard pushback approved.

EAST REMOTE

200, 201, 202, 203

The aircraft (on idle thrust) shall be pushed back onto TWY C6 to face North (or South).

Pushback approved, to face North (or South).

200L

The aircraft (on idle thrust) shall be pushed back:

  • onto Taxilane C6 centreline to face North until its nosewheel is on the end of push behind aircraft stand 200L. The aircraft may breakaway from there.
OR

Pushback approved, to face North.

  • onto Taxilane C6 centreline to face South.

Pushback approved, to face South.

200R, 202L 202R

The aircraft (on idle thrust) shall be pushed back onto Taxilane C6 centreline to face North (or South).

Pushback approved, to face North (or South).

SOUTH-EAST REMOTE

103, 104

The aircraft (on idle thrust) shall be pushed back onto Taxilane L4 centreline to face East until the nose of the aircraft is behind the stopbar behind aircraft stand 102. The aircraft may breakaway from there.

Standard pushback approved.

205, 206 207, 208

The aircraft (on idle thrust) shall be pushed back onto TWY C7 to face North (or South).

Pushback approved, to face North (or South).

209

The aircraft (on idle thrust) shall be pushed back to face North (or South) until its nosewheel is at the intersection of the lead-in line and TWY C7 centreline.

Pushback approved, to face North (or South).

NORTH REMOTE

300, 301, 302, 303, 304, 305, 306, 307, 308, 309, 310

The aircraft (on idle thrust) shall be pushed back:

  • facing West until its nosewheel is at the intersection of the lead-in line and taxiway NC2 centreline.
OR

Pushback approved, to face West.

  • facing East until its nosewheel is at the intersection of the lead-in line and taxiway NC2 centreline.

Pushback approved, to face East.

NORTH-EAST REMOTE

400, 401, 402 403, 404

The aircraft (on idle thrust) shall be pushed back to face North (or South) until its nosewheel is at the intersection of the lead-in line and TWY A6 centreline.

Pushback approved, to face North (or South).

WEST CARGO

502

The aircraft (on idle thrust) shall be pushed back to face North (or South). The aircraft may breakaway from here. There shall be no simultaneous pushback of aircraft unless with two aircraft stands separation.

Pushback approved, to face North (or South).

503, 504 505, 506

The aircraft (on idle thrust) shall be pushed back to face North (or South).

Pushback approved, to face North (or South).

507, 508, 509

The aircraft (on idle thrust) shall be pushed back to face North (or South). The aircraft may breakaway from there. There shall be no simultaneous pushback of aircraft unless with two aircraft stands separation.

Pushback approved, to face North (or South).

510

The aircraft (on idle thrust) shall be pushed back to face North (or South) until the nosewheel of the aircraft is at the intersection of the aircraft stand lead-in line and Taxiway WC centreline. The aircraft may breakaway from there. There shall be no simultaneous pushback of aircraft unless with two aircraft stands separation.

Pushback approved, to face North (or South).

511

The aircraft (on idle thrust) shall be pushed back
- onto Twy WC to face North until the nosewheel of the aircraft is at the intersection of the aircraft stand lead-in line and Taxiway WC centreline. The aircraft may breakaway from there.

OR

Pushback approved, to face North.

- onto TWY WC to face South until the nosewheel of the aircraft is at the intersection of the aircraft stand lead-in line and Taxiway WC centreline. The aircraft shall then be towed forward until the nosewheel is at the "EOT" position behind aircraft stand 510. The aircraft may breakaway from there.

Pushback approved, to face South.

512

The aircraft (on idle thrust) shall be pushed back
- onto Twy WC to face North until the nose of the aircraft is behind the stop bar behind aircraft stand 511. The aircraft may breakaway from there.

OR

Pushback approved, to face North.

- onto TWY WC to face South until the nosewheel of the aircraft is at the intersection of the aircraft stand lead-in line and Taxiway WC centreline. The aircraft shall then be towed forward until the nosewheel is at the "EOT" position behind aircraft stand 510. The aircraft may breakaway from there.

Pushback approved, to face South.

513

The aircraft (on idle thrust) shall be pushed back
- onto Twy WC to face North until the nosewheel of the aircraft is at the intersection of the aircraft stand lead-in line and Taxiway WC centreline. The aircraft may breakaway from there.

OR

Pushback approved, to face North.

- onto TWY WC to face South until the nose of the aircraft is behind the stop bar behind aircraft stand 515 on Taxilane WD. The aircraft may breakaway from there.

Pushback approved, to face South.

514

The aircraft (on idle thrust) shall be pushed back
- onto TWY WC to face North until the nose of the aircraft is behind the stop bar behind aircraft stand 513. The aircraft may breakaway from there.

OR

Pushback approved, to face North.

- onto TWY WC to face South until the nose of the aircraft is behind the stop bar behind aircraft stand 515 on Taxilane WD. The aircraft may breakaway from there.

Pushback approved, to face South.

515

The aircraft (on idle thrust) shall be pushed back onto Taxilane WD to face South until the nose of the aircraft is behind the stop bar. The aircraft may breakaway from there.

Standard pushback approved.

516, 517

The aircraft (on idle thrust) shall be pushed back onto Taxilane WD to face South until the nose of the aircraft is at the intersection of the aircraft stand lead-in line and Taxilane WD centreline. The aircraft shall then be towed forward until the nose of the aircraft is behind the stop bar behind aircraft stand 515. The aircraft may breakaway from there.

Standard pushback approved.

516L, 516R, 517L, 517R

The aircraft (on idle thrust) shall be pushed back to face South until its body is aligned with Taxilane WD centreline. The aircraft shall then be towed forward until the nose of the aircraft is behind the stop bar behind aircraft stand 515. The aircraft may breakaway from there.

Standard pushback approved..

EAST CARGO

600

The aircraft (on idle thrust) shall be pushed back onto Taxilane EA to face South until its nosewheel is at the intersection of the aircraft stand lead-in line and Taxilane EA centreline. The aircraft may breakaway from there.

Standard pushback approved

600L, 600R

The aircraft (on idle thrust) shall be pushed back onto Taxilane EA to face South until its nosewheel is at the intersection of the aircraft stand pushback line and Taxilane EA centreline. The aircraft may breakaway from there.

Standard pushback approved

601, 602

The aircraft (on idle thrust) shall be pushed back to face South until its nosewheel is at the intersection of the lead-in line and taxilane EA centreline.

Standard pushback approved

603

The aircraft (on idle thrust) shall be pushed back to face South until its nosewheel is at the intersection of the lead-in line and taxilane EA centreline. The aircraft shall then be towed forward along the centreline of taxilane EA till its nosewheel is on the “END OF TOW” marking behind aircraft stand 602.

Standard pushback approved

604

The aircraft (on idle thrust) shall be pushed back to face South until its nosewheel is at the position of “END OF PUSH”. The aircraft shall then be towed forward along the centreline of taxilane EA till its nosewheel is on the “END OF TOW” marking behind aircraft stand 602.

Standard pushback approved

605

The aircraft (on idle thrust) shall be pushed back to face West until its nosewheel of the aircraft is at the position of “EOP"on Taxilane EC. The aircraft shall then be towed forward along the centreline of taxilane EA till its nosewheel is on the “END OF TOW” marking behind aircraft stand 602. The aircraft may breakaway from there.

Standard pushback approved

611, 612

The aircraft shall be pushed back to face North until its nosewheel is at the “END OF PUSH” position. The aircraft shall then be towed forward along the centreline of taxilane EC and turn left onto the centreline of taxilane EA until its nosewheel is at the “END OF TOW” marking behind aircraft stand 602. The aircraft may breakaway from there. Engine start-up is not permitted during standard pushback.

Standard pushback approved

Alternate Pushback Procedure

The aircraft (on idle thrust) shall be pushed back to face North until its nosewheel is at the “END OF PUSH” position. Engine start-up is permitted only on the port engine. The aircraft shall then be towed forward along the centreline of taxilane EC and turn left onto the centreline of taxilane EA until its nosewheel is at the “END OF TOW” position (marking behind aircraft stand 602). The aircraft may breakaway from there. This alternate pushback procedure can only be exercised if the auxiliary power unit of the aircraft is unserviceable.

Alternate pushback approved

T1 WEST

C1, C20, C22, C23, C24, C25

The aircraft (on idle thrust) shall be pushed back onto TWY U1 to face North (or South).

Pushback approved, to face North (or South).

C26

The aircraft (on idle thrust) shall be pushed back:

  • onto TWY WA to face North. The aircraft may breakaway from there.
OR

Pushback approved, to face North.

  • onto TWY WA to face South until its nosewheel is at the intersection of the aircraft stand lead-in line and TWY WA centreline. The aircraft shall then be towed forward until its nosewheel is on the “END OF TOW’ position. This is marked as “EOT” on the ground. The aircraft may breakaway from there.

Pushback approved, to face South.

T1 CENTRAL

C11

The aircraft (on idle thrust) shall be pushed back such that the pushback line is always kept midway between the aircraft main gear until the nosewheel of aircraft is at the “EOP 21” position. The aircraft shall then be towed forward until its nosewheel is at the “EOT 22A” position.

Standard pushback approved

C13

The aircraft (on idle thrust) shall push back to face North such that the pushback line is always kept midway between the aircraft main gear until its nosewheel is at the “EOP 22” position. The aircraft shall be towed forward until its nosewheel is at the “EOT 22A” position.

Standard pushback approved

Alternate Pushback Procedure

The aircraft (on idle thrust) shall push back onto TWY N2 to face South followed by TWY N3 until the nose of the aircraft is behind the stopbar line behind aircraft stand D35. The aircraft may breakaway from there.

Pushback approved, onto TWY N3 to face South.

Alternate Pushback Procedure

The aircraft (on idle thrust) shall push back onto TWY N2 to face South followed by TWY N1 until the nose of the aircraft is behind the stopbar line behind aircraft stand C16. The aircraft may breakaway from there.

Pushback approved, onto TWY N1 to face South.

C15

The aircraft (on idle thrust) shall push back facing North until its nosewheel is at the intersection of the lead-in line and TWY N2 centreline.

Standard pushback approved

Alternate Pushback Procedure

The aircraft (on idle thrust) shall push back onto TWY N2 to face South followed by TWY N3 until the nose of the aircraft is behind the stopbar line behind aircraft stand D35. The aircraft may breakaway from there.

Pushback approved, onto TWY N3 to face South.

Alternate Pushback Procedure

The aircraft (on idle thrust) shall push back onto TWY N2 to face South followed by TWY N1 until the nose of the aircraft is behind the stopbar line behind aircraft stand C16. The aircraft may breakaway from there.

Pushback approved, onto TWY N1 to face South.

C16

The aircraft (on idle thrust) shall be pushed back to face North (or South) until its nosewheel is at the intersection of the lead-in line and TWY N1 centreline.

Pushback approved, to face North (or South).

Alternate Pushback Procedure

The aircraft (on idle thrust) shall be pushed back onto Taxilane N1 to face North until the nose of the aircraft is behind the stopbar line behind aircraft stand C15 on Taxilane N2. The aircraft may breakaway from there.

Pushback approved, to face North on Taxilane N2.

C17

The aircraft (on idle thrust) shall be pushed back to face North (or South) until its nosewheel is at the intersection of the lead-in line and TWY N1 centreline.

Pushback approved, to face North (or South).

Alternate Pushback Procedure

The aircraft (on idle thrust) shall be pushed back onto Taxilane N1 to face North until the nose of the aircraft is behind the stopbar line behind aircraft stand C15 on Taxilane N2. The aircraft may breakaway from there.

Pushback approved, to face North on Taxilane N2.

C18

The aircraft (on idle thrust) shall be pushed back to face North until its nosewheel is at the intersection of the lead-in line and TWY N1 centreline.

Standard pushback approved

Alternate Pushback Procedure

The aircraft (on idle thrust) shall be pushed back onto Taxilane N1 to face North until the nose of the aircraft is behind the stopbar line behind aircraft stand C15 on Taxilane N2. The aircraft may breakaway from there.

Pushback approved, to face North on Taxilane N2.

C19

The aircraft (on idle thrust) shall be pushed back to face North along TWY N1 until the “END OF PUSH” position.

Standard pushback approved

D30

The aircraft (on idle thrust) shall be pushed back such that the pushback line is always kept midway between the aircraft main gear until the nosewheel of the aircraft is at the “EOP 20” position. The aircraft shall then be towed forward until its nosewheel is at the “EOT” 22A” position.

Standard pushback approved

D32

The aircraft (on idle thrust) shall push back to face North such that the pushback line is always kept midway between the aircraft main gear until its nosewheel is at the “EOP 22” position. The aircraft shall then be towed forward until its nosewheel is at the “EOT 22A” position.

Standard pushback approved

Alternate Pushback Procedure

The aircraft (on idle thrust) shall push back onto TWY N2 to face South followed by TWY N3 until the nose of the aircraft is behind the stopbar line behind aircraft stand D35. The aircraft may breakaway from there.

Pushback approved, onto TWY N3 to face South.

Alternate Pushback Procedure

The aircraft (on idle thrust) shall push back onto TWY N2 to face South followed by TWY N1 until the nose of the aircraft is behind the stopbar line behind aircraft stand C16. The aircraft may breakaway from there.

Pushback approved, onto TWY N1 to face South.

D34

The aircraft (on idle thrust) shall push back to face North until its nosewheel is at the intersection of the lead-in line and TWY N2 centreline.

Standard pushback approved

Alternate Pushback Procedure

The aircraft (on idle thrust) shall push back onto TWY N2 to face South followed by TWY N3 until the nose of the aircraft is behind the stopbar line behind aircraft stand D35. The aircraft may breakaway from there.

Pushback approved, onto TWY N3 to face South.

Alternate Pushback Procedure

The aircraft (on idle thrust) shall push back onto TWY N2 to face South followed by TWY N1 until the nose of the aircraft is behind the stopbar line behind aircraft stand C16. The aircraft may breakaway from there.

Pushback approved, onto TWY N1 to face South.

D35, D36

The aircraft (on idle thrust) shall be pushed back to face North (or South) until its nosewheel is at the intersection of the lead-in line and TWY N3 centreline.

Pushback approved, to face North (or South).

Alternate Pushback Procedure

The aircraft (on idle thrust) shall be pushed back onto Taxilane N3 to face North until the nose of the aircraft is behind the stopbar line behind aircraft stand D34 on Taxilane N2. The aircraft may breakaway from there.

Pushback approved, to face North on Taxilane N2.

D37

The aircraft (on idle thrust) shall be pushed back to face North until its nosewheel is at the intersection of the lead-in line and TWY N3 centreline.

Standard pushback approved

Alternate Pushback Procedure

The aircraft (on idle thrust) shall be pushed back onto Taxilane N3 to face North until the nose of the aircraft is behind the stopbar line behind aircraft stand D34 on Taxilane N2. The aircraft may breakaway from there.

Pushback approved, to face North on Taxilane N2.

D38

The aircraft (on idle thrust) shall be pushed back to face North along TWY N3 until the “END OF PUSH” position.

Standard pushback approved

T1 EAST

D40, D41, D42, D44, D46, D47, D48, D49

The aircraft (on idle thrust) shall be pushed back to face North (or South) until its nosewheel is at the intersection of the lead- in line and TWY A6 centreline.

Pushback approved, to face North (or South).

D42

The aircraft (on idle thrust) shall be pushed back onto Taxilane A6 to face North (or South) until its nosewheel is at the intersection of the aircraft stand lead-in line and Taxilane A6 centreline. The aircraft may breakaway from there.

Pushback approved, to face North (or South) on Taxilane A6.

D42L, D42R

The aircraft (on idle thrust) shall be pushed back following the pushback line onto Taxilane A6 to face North (or South) until its nosewheel is at the intersection of the aircraft stand pushback line and Taxilane A6 centreline. The aircraft may breakaway from there.

Pushback approved, to face North (or South) on Taxilane A6.

T2 CENTRAL

E1

The aircraft (on idle thrust) shall be pushed back such that the pushback line is always kept midway between the aircraft main gear until its nosewheel is at Stopbar 12. This is marked as “END OF PUSH” on the ground. The aircraft shall then be towed forward to Stopbar 9. This is marked as “END OF TOW” on the ground.

Standard pushback approved

E2

The aircraft (on idle thrust) shall be pushed back until its nosewheel is at the intersection of the lead-in line and TWY B2 centreline. The aircraft shall then be towed forward to Stopbar 9. This is marked as “END OF TOW” on the ground.

Standard pushback approved

E3

The aircraft (on idle thrust) shall be pushed back until its nosewheel is at Stopbar 9. This is marked as “END OF TOW” on the ground.

Standard pushback approved

E4

The aircraft (on idle thrust) shall be pushed back:

  • until its nosewheel is at the “END OF PUSH” 8 position
OR

Standard pushback approved

  • onto TWY B1 until its nosewheel is at the “END OF PUSH” 13A position
OR

Pushback approved, to pushback onto TWY B1

  • onto TWY B3 until its nosewheel is at the “END OF PUSH” 7A position.

Pushback approved, to pushback onto TWY B3.

E5, E6

The aircraft (on idle thrust) shall be pushed back until its nosewheel is at the intersection of the lead-in line and TWY B1 centreline. The aircraft shall then be towed forward to Stopbar 13. This is marked as “END OF TOW” on the ground.

Standard pushback approved

E7

The aircraft (on idle thrust) shall be pushed back until its nosewheel is at Stopbar 13. This is marked as “END OF TOW” on the ground.

Standard pushback approved

F30

The aircraft (on idle thrust) shall be pushed back such that the pushback line is always kept midway between the aircraft main gear until its nosewheel is at Stopbar 11. This is marked as “END OF PUSH” on the ground. The aircraft shall then be towed forward to Stopbar 9. This is marked as “END OF TOW” on the ground.

Standard pushback approved

F31

The aircraft (on idle thrust) shall be pushed back until its nosewheel is at Stopbar 10. This is marked as “END OF PUSH” on the ground. The aircraft shall then be towed forward to Stopbar 9. This is marked as “END OF TOW” on the ground.

Standard pushback approved

F32

The aircraft (on idle thrust) shall be pushed back until its nosewheel is at Stopbar 9. This is marked as “END OF TOW” on the ground.

Standard pushback approved

F33

The aircraft (on idle thrust) shall be pushed back:

  • until its nosewheel is at “END OF PUSH” 8 position.
OR

Standard pushback approved

  • onto TWY B1 until its nosewheel is at the “END OF PUSH” 13A position.

OR

Pushback approved, to pushback onto TWY B1

  • onto TWY B3 until its nosewheel is at the “END OF PUSH” 7A position.

Pushback approved, to pushback onto TWY B3.

F34, F35

The aircraft (on idle thrust) shall be pushed back until its nosewheel is at the intersection of the lead-in line and TWY B3 centreline. The aircraft shall then be towed forward to Stopbar 7. This is marked as “END OF TOW” on the ground.

Standard pushback approved

F35

The aircraft (on idle thrust) shall be pushed back onto Taxilane B3 to face south until its nosewheel is at the intersection of the aircraft stand lead-in line and Taxilane B3 centreline. The aircraft may breakaway from there.

Standard pushback approved

F35L

The aircraft (on idle thrust) shall be pushed back following the pushback line onto Taxilane B3 to face south until the nose of the aircraft is behind the stopbar behind aircraft stand F35. The aircraft may breakaway from there.

Standard pushback approved

F35R

The aircraft (on idle thrust) shall be pushed back following the pushback line onto Taxilane B3 to face south until its nosewheel is at the intersection of the aircraft stand pushback line and Taxilane B3 centreline. The aircraft may breakaway from there.

Standard pushback approved

F36

The aircraft (on idle thrust) shall be pushed back until its nosewheel is at Stopbar 7. This is marked as “END OF TOW” on the ground.

Standard pushback approved

T2 NORTH
E8

The aircraft (on idle thrust) shall be pushed back until its nosewheel is at Stopbar 14. This is marked as “END OF PUSH” on the ground. The aircraft shall then be towed forward to Stopbar 15. This is marked as “END OF TOW” on the ground.

Standard pushback approved

E10

The aircraft (on idle thrust) shall be pushed back with the main gear mid-point following the pushback line until its nosewheel is at position EOP 19.

Standard pushback approved

E11

Main pushback procedure (for all aircraft wingspan)

The aircraft (on idle thrust) shall be pushed back with the main gear mid-point following the main gear pushback line onto TWY A6 centreline. The aircraft shall then be towed forward to Stopbar 16 on TWY A5. This is marked as “END OF TOW” on the ground.

Standard pushback approved

Alternate pushback procedure (for aircraft with wingspan of less than 65m)

The aircraft (on idle thrust) shall be pushed back with the main gear mid-point following the main gear pushback line until its body is aligned with TWY A6 centreline.

Pushback approved, to pusback onto TWY A6.

Alternate pushback procedure (for aircraft with wingspan of more than 65m)

The aircraft (on idle thrust) shall be pushed back with the main gear mid-point following the main gear pushback line until its nosewheel is at the ‘EOP 19A’ position behind aircraft stand E24. The aircraft shall then be towed forward to ‘EOT 18B’ behind aircraft stand E26.

Pushback approved, to pushback onto TWY A6.

E12

The aircraft (on idle thrust) shall be pushed back:

  • until its nosewheel is at the intersection of the lead-in line and TWY A5 centreline. The aircraft shall then be towed forward to Stopbar 16. This is marked as “END OF TOW” on the ground.

OR

Standard pushback approved

  • onto TWY A6 until its nosewheel is at the intersection of TWY A5 and A6 centrelines.

Pushback approved, to pusback onto TWY A6.

E20

The aircraft (on idle thrust) shall be pushed back with the main gear mid-point following the main gear pushback line until its nosewheel is at Stopbar 17. The aircraft shall then be towed forward to “END OF TOW” Stopbar 18A. Aircraft may breakaway from there.

Standard pushback approved

E22

The aircraft (on idle thrust) shall be pushed back with the main gear mid-point following the main gear pushback line until its nosewheel is at Stopbar 19. This is marked as “END OF PUSH” on the ground. The aircraft shall then be towed forward to Stopbar 18. This is marked as “END OF TOW” on the ground.

Standard pushback approved

E24

The aircraft (on idle thrust) shall be pushed back facing North until its body is aligned with TWY A6 centreline. Aircraft may breakaway from there.

Standard pushback approved

E24L, E24R

The aircraft (on idle thrust) shall be pushed back facing North until its body is aligned with TWY A6 centreline. Aircraft may breakaway from there.

Standard pushback approved

E26

The aircraft (on idle thrust) shall be pushed back to face North until its body is aligned with TWY A6 centreline.

Standard pushback approved

E27, E28

The aircraft (on idle thrust) shall be pushed back to face North (or South) until its body is aligned with TWY A6 centreline.

Pushback approved, to face North (or South).

T2 SOUTH
F37

The aircraft (on idle thrust) shall be pushed back:

  • with the main gear following the main gear pushback line, until its nosewheel is behind aircraft stand F42. The aircraft shall then be towed forward to Stopbar 4. This is marked as “EOT 4” on the ground.

OR

Standard pushback approved

  • with the main gear following the main gear pushback line, until its nosewheel is on the “END OF PUSH (EOP)” Stopbar 5 on TWY C1.

Pushback approved, to face East on TWY C1.

F40, F52

The aircraft (on idle thrust) shall be pushed back until its nosewheel is at Stopbar 2. This is marked as “END OF PUSH” on the ground. The aircraft shall then be towed forward to Stopbar 3. This is marked as “END OF TOW” on the ground.

Standard pushback approved

F41

The aircraft (on idle thrust) shall be pushed back:

  • until its nosewheel is at the intersection of the lead-in line and the TWY C2 centreline. The aircraft shall then be towed forward to Stopbar 4. This is marked as “EOT 4” on the ground.

OR

Standard pushback approved

  • onto TWY C6 until its nosewheel is at the intersection of TWY C2 and TWY C6 centreline.

Pushback approved, to pushback onto TWY C6.

F42

Main pushback procedure (for all aircraft wingspan)

The aircraft (on idle thrust) shall be pushed back until its nosewheel is at the intersection of the lead-in line and the TWY C2 centreline. The aircraft shall then be towed forward to Stopbar 4. This is marked as “EOT 4” on the ground.

Standard pushback approved

Alternate pushback procedure (for aircraft with wingspan of less than 65m)

The aircraft (on idle thrust) shall be pushed onto TWY C6 until its nosewheel is at the intersection of TWY C2 and TWY C6 centreline.

Pushback approved, to pushback onto TWY C6.

Alternate pushback procedure (for aircraft with wingspan of more than 65m)

The aircraft (on idle thrust) shall be pushed back until its nosewheel is at the ‘EOP 4A’ position. The aircraft shall then be towed forward with its nosewheel following the towed forward line until its nosewheel is on the ‘EOT 4B’ position, behind aircraft stand F59.

Pushback approved, to pushback onto TWY C6.

F50

The aircraft (on idle thrust) shall be pushed back with the main gear following the main gear pushback line, facing south until its nosewheel is on the “END OF PUSH” Stopbar 1 marking painted on the ground behind aircraft stand F50. The aircraft shall then be towed forward with the nosewheel following the tow-forward line until its nosewheel is on the “END OF TOW” Stopbar 3 marking painted on the ground behind aircraft stand F52.

Standard pushback approved

F52L

The aircraft (on idle thrust) shall be pushed back to face south until its nosewheel is at the intersection of the aircraft pushback line and taxilane C6.

Standard pushback approved

F52R

The aircraft (on idle thrust) shall be pushed back to face south until its nosewheel is at the intersection of the aircraft pushback line and taxilane C6. The aircraft shall then be towed forward until its nosewheel is on the “END OF TOW” position.

Standard pushback approved

F54

The aircraft (on idle thrust) shall be pushed back until its nosewheel is at a point on TWY C6 in line with the mid-point of aircraft stands F52 and F54. It shall breakaway from this position.

Standard pushback approved

F56

The aircraft (on idle thrust) shall be pushed back to face South until its nosewheel is at the intersection of the aircraft pushback line and taxilane C6.The aircraft shall then be towed forward until its nosewheel is abeam aircraft stand F56.

Standard pushback approved

F56L, F56R56R

The aircraft (on idle thrust) shall be pushed back to face South until its nosewheel is at the intersection of the aircraft pushback line and taxilane C6.The aircraft shall then be towed forward until its nosewheel is abeam aircraft stand F56.

Standard pushback approved

F58

The aircraft (on idle thrust) shall be pushed back to face North (or South), on TWY C6 centreline.

Pushback approved, to face North (or South).

F59

The aircraft (on idle thrust) shall be pushed back to face North on TWY C6 centreline until its nosewheel is abeam aircraft stand F60.

OR

Pushback approved, to face North.

The aircraft (on idle thrust) shall be pushed back to face South on TWY C6.

Pushback approved, to face South.

F59L, F59R

The aircraft (on idle thrust) shall be pushed back to face North on taxilane C6 centreline until its nosewheel is abeam aircraft stand F60.

OR

Pushback approved, to face North.

The aircraft (on idle thrust) shall be pushed back to face South on taxilane C6 centreline.

Pushback approved, to face South.

F60

The aircraft (on idle thrust) shall be pushed back to face North (or South), on TWY C6 centreline.

Pushback approved, to face North (or South).

1, 2

The aircraft (on idle thrust) shall be pushed back:

  • to face West onto TWY L7 until its nosewheel is at the stopbar marked “END OF PUSH” behind aircraft stand 2. The aircraft may breakaway from there. Simultaneous pushback is not permitted for aircraft stands 1, 2 and 3.

Pushback approved, to face West.

OR
  • onto TWY L5 to face North until its nosewheel is behind the stopbar behind aircraft stand 3. The aircraft may breakaway from there. Simultaneous pushback is not permitted for aircraft stands 1, 2 and 3.
    Pushback from aircraft stands 1 and 2 to face South is not permitted.

Pushback approved, to face North.

3, 4, 5, 6, 7, 8, 9, 10

The aircraft (on idle thrust) shall be pushed back onto TWY L5 to face North or South until its nosewheel is at the intersection of the aircraft stand lead-in line and the centreline of TWY L5. The aircraft may breakaway from there. There shall be no simultaneous pushback of aircraft unless there is at least one aircraft stand separation. Simultaneous pushback is not permitted for aircraft stands 1, 2 and 3.

Pushback approved, to face North or South.

11, 12, 13

The aircraft (on idle thrust) shall be pushed back onto TWY L5 to face North or South until its nosewheel is at the “END OF PUSH (EOP)” position and the centreline of TWY L5. The aircraft may breakaway from there. There shall be no simultaneous pushback of aircraft unless there is at least one aircraft stand separation.

Pushback approved, to face North or South.

14

The aircraft (on idle thrust) shall be pushed back onto TWY L5 to face North until its nosewheel is at the “END OF PUSH (EOP)” position and the centreline of TWY L5. The aircraft may breakaway from there. There shall be no simultaneous pushback of aircraft unless there is at least one aircraft stand separation.

Pushback approved, to face North.

15, 16, 701, 702

The aircraft (on idle thrust) shall be pushed back onto TWY L5 centreline to face North. The aircraft shall then be towed forward until its nosewheel is at the position between aircraft stands 12 and 13. The aircraft may breakaway from there.

Pushback approved, to face North.

17

The aircraft (on idle thrust) shall be pushed back to face West until its nosewheel is at the “END OF PUSH (EOP)” position. The aircraft shall then be towed forward onto TWY L5 to face North until its nosewheel is at the position between aircraft stands 12 and 13. The aircraft may breakaway from there.

Standard pushback approved.

SOUTH APRON
461

The aircraft (on idle thrust) shall be pushed back onto taxiway S1 to face west until its nosewheel is at EOP position. The aircraft may breakaway from there. There shall be no simultaneous aircraft pushback from aircraft stands 462, 462L, 462R, 463, 463L and 463R.

Pushback approved, to face west

462

The aircraft (on idle thrust) shall be pushed back onto taxiway S1 to face west until its nosewheel is at the intersection of the aircraft stand pushback line and taxiway S1 centreline. The aircraft may breakaway from there. There shall be no simultaneous aircraft pushback from aircraft stands 461, 462L, 462R, 463, 463L and 463R.

Pushback approved, to face west

462L

The aircraft (on idle thrust) shall be pushed back onto taxiway S1 to face west until its nosewheel is at the intersection of the aircraft stand pushback line and taxiway S1 centreline. The aircraft may breakaway from there. There shall be no simultaneous aircraft pushback from aircraft stands 461, 462, 462R, 463, 463L and 463R.

Pushback approved, to face west

462R

The aircraft (on idle thrust) shall be pushed back onto taxiway S1 to face west until its nosewheel is at the intersection of the aircraft stand pushback line and taxiway S1 centreline. The aircraft may breakaway from there. There shall be no simultaneous aircraft pushback from aircraft stands 461, 462, 462L, 463, 463L and 463R.

Pushback approved, to face west

463

The aircraft (on idle thrust) shall be pushed back onto taxiway S1 to face west until its nosewheel is at the intersection of the aircraft stand pushback line and taxiway S1 centreline. The aircraft may breakaway from there. There shall be no simultaneous aircraft pushback from aircraft stands 461, 462, 462L, 462R, 463L and 463R.

Pushback approved, to face west

463L

The aircraft (on idle thrust) shall be pushed back onto taxiway S1 to face west until its nosewheel is at the intersection of the aircraft stand pushback line and taxiway S1 centreline. The aircraft may breakaway from there. There shall be no simultaneous aircraft pushback from aircraft stands 461, 462, 462L, 462R, 463 and 463R.

Pushback approved, to face west

463R

The aircraft (on idle thrust) shall be pushed back onto taxiway S1 to face west until the nose of the aircraft is behind the stop bar behind aircraft stand 463L. The aircraft may breakaway from there. There shall be no simultaneous aircraft pushback from aircraft stands 461, 462, 462L, 462R, 463 and 463L.

Pushback approved, to face west



4 ADVANCED MULTILATERATION SYSTEM
4.1 INTRODUCTION
4.1.1 The Multilateration System is a new surveillance system which is able to detect and identify all Mode S equipped aircraft and vehicles moving on the airport surface even during bad weather conditions such as heavy rain. It will integrate with the current radar-based ground surveillance system as part of the Advanced-Surface Movement Guidance and Control System (A-SMGCS) at Singapore Changi Airport. This will enhance the efficiency and safety at the airport.
4.2 CARRIAGE OF MODE-S SSR TRANSPONDER
4.2.1 Carriage and operation of Mode-S transponder is required for all civil aircraft operating at Singapore Changi Airport. The Mode-S transponder shall comply, at least, to the requirements of Level 2 as prescribed in ICAO Annex 10 Volume IV (Amendment 77 or later) Standards and Recommended Practices.
4.3 MULTILATERATION SYSTEM OUTLINE
4.3.1 The Multilateration System uses multiple receivers to pick up “squitters” transmitted by aircraft or vehicle Mode S transponders. It calculates the position of an aircraft or a vehicle by comparing the time its “squitter” arrives at each receiver.
4.3.2 The System will derive the identity of an aircraft by selectively interrogating its transponder to receive its assigned Mode A code or extracting its aircraft identification [that is, the ICAO callsign used in flight and inserted in the Flight Management System (FMS) or the Transponder Control Panel], if available, from its squitter. For transponder equipped vehicles, the system will derive their respective identities from the unique Mode S addresses contained in their squitters.
4.4 AIRCRAFT REQUIREMENTS
4.4.1 The Multilateration System is essentially passive. It relies on aircraft transponders squittering at all times when moving on the airfield. At present, some aircraft checklist procedures instruct pilots to turn off the transponder shortly after leaving the runway on arrival and, not to switch it on until reaching the runway holding point for departure. This is in line with the requirement that Mode A/C transponders should not transmit on the ground, which does not apply to Mode S transmissions.
4.4.2 For the Multilateration System to work effectively, all aircraft Mode S transponders need to transmit Mode S squitters at all times when moving on the airfield, starting immediately prior to pushback, and for arrival aircraft until they are stationary at the aircraft stands. The Mode S transponders should not respond to All-Call interrogations, but should respond to addressed interrogations.
4.5 PROCEDURES/ACTIONS REQUIRED BY PILOTS
4.5.1 The Multilateration System needs to receive squitters and to acquire the Mode A code of a Mode S equipped aircraft at all times when it is on the ground. This is to enable detection and identification of the aircraft (from its Mode A code or ICAO callsign) as soon as it pushes back. Hence, the following actions from pilots are required.
4.5.2 Pre-Pushback / Taxi
  1. Pilots will be required to enter an assigned Mode A code at start-up. This code will be either a discrete or non-discrete code (a conspicuity code, e.g. 1000).

  2. Pilots shall ensure that the aircraft transponder is operating (that is, XPNDR or the equivalent according to specific installation, AUTO if available, not OFF or STBY) and the assigned Mode A code is selected prior to the request for pushback or taxi, whichever is earlier.

  3. Whenever the aircraft is capable of reporting aircraft identification, the aircraft identification must also be entered prior to the request for pushback or taxi, whichever is earlier, through the FMS or the Transponder Control Panel. Flight crew must use the 3-letter ICAO designator of the operator, followed by flight identification number (for example, BAW123, SIA002).

4.5.3 After Landing
  1. Pilots shall ensure that the aircraft transponder is operating (that is, XPNDR or the equivalent according to specific installation, AUTO if available, not OFF or STBY) after landing, and continuously until the aircraft is stationary at the aircraft stand.

  2. Pilots shall ensure that the assigned Mode A code is not changed until the aircraft is stationary at the aircraft stand. (The system requires it for identification of the aircraft).

5 AIRFIELD GROUND LIGHTING CONTROL AND MONITORING SYSTEM (AGLCMS) AND MARKINGS
5.1 INTRODUCTION
5.1.1 The taxiing guidance system at Singapore Changi Airport consists of stop bars and selectable segments of green taxiway centreline lights. The system is designed to provide pilots with visual guidance while taxiing during night operations and during periods of low visibility. It is controlled by the Ground Movement Controller (GMC) at Changi Control Tower using the Airfield Ground Lighting Control and Monitoring System (AGLCMS).
5.2 ROUTE SELECTION AND PRIORITY
5.2.1 When a taxiing route is selected on the AGLCMS, corresponding segments of taxiway centreline lights on the manoeuvring area are switched on automatically. When two or more routes are selected, the system will give priority to the first route and activate red stopbar lights across conflicting routes, as necessary. A segment of the centreline lights of the conflicting routes that cut across the first route will also be suppressed. The GMC has the option of over-riding the taxiing route priority by selecting or deselecting the appropriate stopbar lights.
5.2.2 All taxiing guidance lights on taxiways leading to the runways terminate at the runway holding positions where, by default, red stopbar lights remain on unless deselected by the runway controller. When deselected, these stopbar lights will re-activate automatically after 50 seconds. Pilots shall not cross any lighted red stopbar lights.
5.2.3 Pilots shall enter / cross the runway or taxiway only when both the following conditions are met:
The crew have
  1. received positive ATC clearance to enter / cross the runway or taxiway, and
  2. observed that the red stop-bar lights are turned off.
5.3 INFORMATION AND MANDATORY SIGNS/MARKINGS
5.3.1 When following the directional guidance provided by the green taxiway centreline lights and red stop bar lights, pilots are advised to also navigate their taxi route with reference to information and mandatory signs/markings provided at the airport so as to maintain situational awareness of their whereabouts at all times.
5.4 TAXI INSTRUCTIONS USING THE GREEN TAXIWAY CENTRELINE LIGHTS
5.4.1 ATC will use the phraseology “Taxi on the greens .....” when issuing a clearance to pilots to taxi along the directional guidance provided by the green taxiway centreline lights.

WSSS AD 2.10 AERODROME OBSTACLES

IN APPROACH / TKOF AREASIN CIRCLING AREA AND AT AD
RWY/Area affectedOBST type, ELEV,
Markings/LGT
CoordinatesOBST type, ELEV,
Markings/LGT
Coordinates
12312
a)RWY 20R APCH
RWY 02L TKOF
Mast HGT ranging fm 98ft AMSL and above.Shipping channel aprx1290m from THR RWY 20R.a)Surface wind direction sleevesLOC at each end of RWY adjacent to GP hut
b)RWY 20C APCH
RWY 02C TKOF
Mast HGT ranging fm 98ft AMSL and above.Shipping channel aprx 2630m from THR RWY 20C.b)PAR hutBesides RWY 02L/20R, opposite the PTB
c)RWY 02L/20R APCH
RWY 02L/20R TKOF
RWY 02C/20C APCH
RWY 02C/20C TKOF
ILS LLZ co-located with LLZ antennas.Within the RWY strip.c)Frangible PAR reflectorsLocated at ends of RWY 02L/20R
d)RWY 20R APCHTwo antennae, HGT 72ft AMSL, marked and LGTD012311N 1035928Ed)GP huts co-located with GP antennasWithin the RWY strip
e)RWY 20R APCHAntenna, HGT 88ft AMSL, marked and LGTD012315N 1035931Ee)Antenna, HGT 82ft AMSL, marked and LGTD012036N 1035819E
f)RWY 02L APCHAntenna, HGT 82ft AMSL, marked and LGTD012051N 1035827Ef)Antenna, HGT 85ft AMSL, marked and LGTD012039N 1035821E
g)RWY 02L APCHPole, HGT 128ft AMSL, marked and LGTD011859N 1035748Eg)Antenna, HGT 78ft AMSL, marked and LGTD012042N 1035823E
h)RWY 02L APCHPole, HGT 160ft AMSL, marked and LGTD012058N 1035814Eh)Antenna, HGT 82ft AMSL, marked and LGTD012053N 1035827E
i)RWY 02L APCHPole, HGT 131ft AMSL, marked and LGTD012038N 1035848Ei)Antenna, HGT 78ft AMSL, marked and LGTD012049N 1035826E
j)RWY 20L APCHShipping channelAprx1600m from THR RWY 20L.j)Frangible poles, HGT 9ft AMSLInstalled APRX 200m from centre of RET to identify 58m away from TWY WP CL towards RWY 02L/20R
Obstacles in the APCH/TKOF areas, circling area and at the aerodrome are shown on the AOC, IAC and VAC.

WSSS AD 2.11 METEOROLOGICAL INFORMATION PROVIDED

1Associated MET OfficeSingapore Changi (WSSS)
2Hours of serviceH24
3Office responsible for TAF preparation
Periods of validity
Singapore Changi (WSSS)
12, 30
4Type of landing forecast, Interval of issuanceTREND
5Briefing/consultation providedP
6Flight documentation, Language usedCharts or Tabular forms, English
7Charts and other information available for briefing or consultationS, U, P
8Supplementary equipment available for providing informationHRPT: High Resolution Picture Transmission
APT: Automatic Picture Transmission
MDWR: MET Doppler Weather Radar
MAINT: Second WED of every month BTN 0200-0900 ALTN period: THU following the second WED.
9ATS units provided with informationSingapore ACC, Singapore RCC
10Additional informationTel: 65422837 (MET Office)

WSSS AD 2.12 RUNWAY PHYSICAL CHARACTERISTICS

Designations RWY NRTRUE BRGDimensions of RWYStrength (PCN) and surface of RWY and SWYTHR coordinates
(THR Geoid Undulation)
THR elevation and highest elevation of TDZ of precision APCH RWY
123456
02L

023.02°

4000 M x 60 M
72/F/B/W/U

Bituminous concrete

012056.26N 1035838.83E
(10.29 M)
6.66 M

6.23 M
20R(Threshold displaced by 740m southwards)

203.02°

4000 M x 60 M
72/F/B/W/U

Bituminous concrete

012233.95N 1035920.06E
(10.29 M)
4.01 M

4.31 M
02C

023.03°

4000 M x 60 M
72/F/B/W/U

Bituminous concrete

011943.51N 1035905.86E
(10.28 M)
4.32 M

4.52 M
20C

203.03°

4000 M x 60 M
72/F/B/W/U

Bituminous concrete

012143.37N 1035956.46E
(10.28 M)
4.58 M

4.56 M
Slope of RWY-SWY Transverse / LongitudinalSWY
Dimensions (m)
CWY
Dimensions (m)
STRIP
dimensions (m)
OFZRemarks
789101112
RWY 02L
0.76 / 0.24%
60 X 60270 X 1504240 X 300YesScheduled closure of runways
(see below)
RWY 20R
1.45 / 0.25%
60 X 60270 X 1504240 X 300
RWY 02C
1.50 / 0.03%
60 X 6060 X 1504240 X 300
RWY 20C
1.38 / 0.07%
60 X 6060 X 1504240 X 300
Remarks (continued from above)
Scheduled Closure of RWY 02L/20R

1a)

BTN 1630-2200 on every MON and THU of the month (preventive maintenance work).
In the event of an emergency, RWY will be re-opened within 30 minutes.

1b)

BTN 0225-0240 0630-0635 1000-1005 2300-2305 daily (inspection).
In the event of an emergency, RWY will be re-opened within 5 minutes.

Scheduled Closure of RWY 02C/20C

2a)

BTN 1630-2200 on every first, second and fourth WED of the month (preventive maintenance work).
In the event of an emergency, RWY will be re-opened within 30 minutes.

2b)

BTN 0300-0315 0650-0655 1020-1025 2320-2325 daily (inspection).
In the event of emergency, RWY will be re-opened within 5 minutes.

WSSS AD 2.13 DECLARED DISTANCES

RWY DesignatorIntersection DeparturesTORA
(m)
TODA
(m)
ASDA
(m)
LDA
(m)
Remarks
1234567
20RNot applicable
4000
4270
4060
3260
Thr displaced by 740m southwards
W2
3850
4120
3910
Not applicable
W3
3050
3320
3110
Not applicable
W4
2600
2870
2660
Not applicable
W5
2150
2420
2210
Not applicable
02LNot applicable
4000
4270
4060
4000
Nil
W8
3850
4120
3910
Not applicable
W7
3050
3320
3110
Not applicable
W6
2600
2870
2660
Not applicable
20CNot applicable
4000
4060
4060
4000
Nil
E2
3850
3910
3910
Not applicable
E3
3425
3485
3485
Not applicable
E4
2750
2810
2810
Not applicable
E5
2250
2310
2310
Not applicable
02CNot applicable
4000
4060
4060
4000
Nil
E10
3850
3910
3910
Not applicable
E9
3345
3405
3405
Not applicable
E8
3205
3265
3265
Not applicable
E7
2555
2615
2615
Not applicable
E6
2105
2165
2165
Not applicable

Note: Intersection departures are allowed subject to the following:

  1. initiated by pilot and approved by ATC, traffic permitting.
  2. ATC is able to keep aircraft visual at all times

WSSS AD 2.14 APPROACH AND RUNWAY LIGHTING

RWYApch Lgt
Type, Len Intensity
Thr Lgt colour
WBAR
PAPI
(MEHT)
TDZ
Lgt
Len
RWY
Centreline
Lgt Len,
spacing,
colour,
INTST
RWY Edge
Lgt, Len,
spacing,
colour,
INTST
RWY
End Lgt
colour
SWY
Lgt
colour
123456789
02LCAT II
High Intensity consisting of extended centreline and Red row barrettes, 2 crossbars, 2 approach beacons and sequenced flashing lights.
Green supplemented by green wing bar and 2 thr ident lights.PAPI 003° loc either side of rwy, 422m behind rwy thr, 2 White lgt and 2 Red lgt (20.6m), 3 White lgt and 1 Red lgt (23.1m), 4 White lgt (25.6m). Acft with eye-to-wheel hgt greater than 8m are adz to fly with 2 White and 2 Red lgt visible so as to achieve sufficient wheel clearance.WhiteInset High Intensity centreline lights as flw: From thr to 900m fm rwy end: White, 300m to 900m fm rwy end: Altn Red/ White, 300m to rwy end: Red.Bi-directional raised White/Amber edge lights.RedElevated Red
20RCAT I
High Intensity distance coded centreline lgts showing variable White and crossbars at 150m, 300m, 450m, 600m and 750m.
Green supplemented by green wing bar and 2 thr ident lights.PAPI 003° located either side of rwy, 410m fm thr. 2 White lgt and 2 Red lgt (20.0m), 3 white lgt and 1 Red lgt (22.6m), 4 White lgt (25.0m). Acft with eye-to-wheel hgt greater than 8m are adz to fly with 2 White and 2 Red lgt visible so as to achieve sufficient wheel clearance.NilInset High Intensity centreline lights as flw: From thr to 900m fm rwy end: White, 300m to 900m fm rwy end: Altn Red/ White, 300m to rwy end: Red.Red rwy edge lgts in the direction of Rwy 20R before the displaced thr. Bi-directional raised White/Amber edge lights after the displaced thr.RedElevated Red
02CCAT I
High Intensity consisting of centreline barrettes showing variable white, 1 crossbar, 2 approach beacons and sequenced flashing lights.
Green supplemented by green wing bar and 2 thr ident lights.PAPI 003° located either side of rwy, 418m fm thr. 2 White lgt and 2 Red lgt (20.4m), 3 White lgt and 1 Red lgt (23.1m), 4 White lgt (25.5m). Acft with eye-to-wheel hgt greater than 8m are adz to fly with 2 White and 2 Red lgt visible so as to achieve sufficient wheel clearance.NilInset High Intensity centreline lights as flw: From thr to 900m fm rwy end: White, 300m to 900m fm rwy end: Altn red/ white, 300m to rwy end: Red.Bi-directional raised White/Amber edge lights.RedElevated Red
20CCAT II
High Intensity consisting of extended centreline and red row barrettes, 2 crossbars, 2 approach beacons and sequenced flashing lights.
Green supplemented by green wing-bar and 2 THR ident lights.PAPI 003° located left side of RWY, 418m fm THR. 2 White lgt and 2 Red lgt (19.8m), 3 White lgt and 1 Red lgt (23.7m), 4 White lgt (26.2m). Acft with eye-to-wheel hgt greater than 8m are adz to fly with 2 White and 2 Red lgt visible so as to achieve sufficient wheel clearance.WhiteInset High Intensity centreline lights as flw: From THR to 900m fm RWY end: White, 300m to 900m fm RWY end: Altn Red/White, 300m to RWY end: Red.Bi-directional raised White/Amber edge lights.RedElevated Red

WSSS AD 2.15 OTHER LIGHTING, SECONDARY POWER SUPPLY

1ABN/IBN location, characteristics and hours of operation

ABN: 012209.22N 1035858.47E (western side of RWY 02L/20R)
ALTN FLG W G EV 2.3 SEC, OPR hours HN + IMC
IBN: 012301.28N 1035959.52E (top of building N of SIA hangar) FLG G ‘CH’ EV 7 SEC, OPR hours HN + IMC

2LDI location and LGT
Anemometer location and LGT

Pressure tube anemometer and wind vane situated 345m west of middle of RWY 02L/20R. Cup anemometers and wind vanes at ends and middle of both runways. Windsocks at ends of both runways. Transmissometers at both ends and in the middle of both runways

3TWY Edge and Centreline Lighting

RWY 02L/20R and RWY 02C/20C: Blue lights on TWY curved edges and apron TWY edges and Green centreline lights on all TWY.

4Secondary power supply/switch-over time

Automatic standby generator power supply AVBL for airfield lighting with switchover time of 1 second during Category II low visibility operations.

5Remarks

Vehicles painted yellow or displaying chequered red/white or orange/white flag at highest point of vehicle

WSSS AD 2.16 HELICOPTER LANDING AREA

Refer to ENR 3.4

WSSS AD 2.17 ATS AIRSPACE

1Designation and Lateral
Limits
CHANGI CTR
013300N 1040149E 013042N 1040654E 012542N 1040448E thence along Kuala Lumpur/Singapore FIR bdry to 012000N 1041218E 010018N 1035524E 011100N 1035134E 013300N 1040149E
2Vertical LimitsSFC to 3,000ft ALT
3Airspace ClassificationC
4ATS Unit Callsign
Language(s)
Singapore Tower
English
5Transition Altitude11000 FT (3,350m)
6RemarksA helicopter shall not be operated within the Changi CTR unless prior permission has been obtained from the Director-General of Civil Aviation, CAAS. Email to caas_ats_ansp@caas.gov.sg

WSSS AD 2.18 ATS COMMUNICATION FACILITIES

Service
Designation
Call signFrequency
(P-Pri, S-Sec)
Hours of
operation
Remarks
ACCSingapore
Radar
P123.7 MHz
S127.3 MHz
H24for ATS Routes B469, G219, G334, R208, L625, L629, L635, L642, L644, M751, M753, M758, M761, M763, M771, N884, N891 and N892.
133.8 MHz0000-1430
P133.25 MHz
S135.8 MHz
H24for ATS Routes A457, A464, A576, B466, R325 (all northbound) and R469.
P134.2 MHz
S133.35 MHz
for ATS Routes , G580, L644, M646 and M767
P134.4 MHz
S128.1 MHz
255.4 MHz
for ATS Routes A464, A576, G579 (all southbound), B470, L644, N875 and in area in the immediate vicinity of Singapore.
124.05 MHz0000-1530Flow control service provided for ARR/DEP ACFT
MAINT Period: Monthly - EV third SAT 1601-2359
Singapore
Radio
6556 kHz
11297 kHz
H24SEA 1, Emission: A3AJ. SSB suppressed carrier, SATCOM service available
5655 kHz
8942 kHz
11396 kHz
SEA 2, Emission: A3AJ. SSB suppressed carrier, SATCOM service available
6556 kHzSEA 3, Emission: A3AJ. SSB suppressed carrier, SATCOM service available
APPSingapore
Approach
P120.3 MHz
S124.6 MHz
H24TAR - Intermediate approach to Singapore Changi AP and other airports in Singapore. DEP from all airports in Singapore.
Singapore
Arrival
119.3 MHzTAR - Intermediate and final approach to Singapore Changi Airport.
ASR I MAINT Period: Monthly, EV first SAT 1601-2359
ASR II MAINT Period: Monthly, EV fourth SAT 1601-2359
TWRSingapore
Tower
118.6 MHzH24
0000-1600
for TKOF/LDG.
for ACFT OPR on RWY 02L/20R
118.25 MHz0000-1600for ACFT OPR on RWY 02C/20C
Singapore
Ground
124.3 MHz1600-0000
0000-1600
for start-up / push-back / taxiing of all aircraft
for ground movement of aircraft west of Terminal 3
121.725 MHz0000-1700
2100-0000
for ground movement of aircraft east of Terminal 2
121.85 MHz0000-1800
2300-0000
for ground movement of aircraft north of Terminal 1
129.95 MHzH24for ground emergency
Singapore
Delivery
121.65 MHzH24for Pre-flight check/ATC clearance
Changi Tower / Changi Apron121.9 MHzH24for vehicular movements on taxiways and runways. Towing of all aircraft and requests for engine runs on apron and taxiways, excluding runways, will be regulated by Changi Apron.
D-ATISSingapore
Changi Airport
Information
128.6 MHzH24Data Link Service available. AP IDENT WSSS
Messages comply with ARINC 623 Standards.
Updating of data: H+00 to H+10 and H+30 to H+40

WSSS AD 2.19 RADIO NAVIGATION AND LANDING AIDS

Type of aid and VariationIdentFrequencyOPR HrPosition of Transmitting Antenna CoordinatesDME Transmitting Antenna Elevation / Remarks
123456 & 7
SINJON
DVOR/DME
SJ113.5 MHz
CH82X
H24011319.28N 1035120.08E201° MAG 14.5km from THR RWY 02 (Paya Lebar). Antenna HGT: 194ft AMSL.
Coverage 200NM.
EM: F1.
Maintenance period:
Third Thursday of every month between 0200-0600
TEKONG
DVOR/DME
VTK116.5 MHz
CH112X
H24012455.36N 1040120.17E023° MAG 6.4km from THR RWY 20C (Singapore Changi).
Antenna HGT: 150ft AMSL.
Coverage 200NM. EM: F1
Maintenance Period:
Third Friday of every month between 0200-0600
RWY 20C
ILS LLZ
ICC109.7MHzH24011932.48N 1035901.20ELocated 368m (1207ft) from THR RWY 02C, along RWY centreline.
Course width 3.38°. EM: A0/A2.
Maintenance Period:
May - October
Second Friday of every month between 1600-2300
November - April
Second Friday of every month between 0200-0900
RWY 20C
ILS GP
-333.2MHzH24012131.73N 1035955.72ELocated 338m (1109ft) from THR RWY 20C on left side of RWY, 120m (394ft) from RWY centreline.
GP angle 3°.
HGT of ILS reference datum: 17m (56ft)
EM: A0/A2
RWY 20C
ILS DME
ICCCH34XH24012131.73N 1035955.72EDME co-located with GP.
EM: P9
RWY 20C
ILS MM
-75MHzH24012211.94N 1040008.52ELocated 957m (3140ft) from THR RWY 20C along extended centreline of RWY. No back beam.
RWY 02C
ILS LLZ
ICE108.3MHzH24012154.41N 1040001.08ELocated 368m (1207ft) from THR RWY 20C, along RWY centreline.
Course width 3.38°. EM: A0/A2.
Maintenance Period:
May - October
Second Friday of every month between 0200-0900
November - April
Second Saturday of every month between 0200-0900
RWY 02C
ILS GP
-334.1MHzH24011952.11N 1035913.68ELocated 338m (1109ft) from THR RWY 02C on left side of RWY, 120m (394ft) from RWY centreline.
GP angle 3°.
HGT of ILS reference datum: 18m (58ft)
EM: A0/A2
RWY 02C
ILS DME
ICECH20XH24011952.11N 1035913.68EDME co-located with GP.
EM: P9
RWY 02C
ILS MM
-75MHzH24011915.04N 1035853.83ELocated 945m (3100ft) from THR RWY 02C along extended centreline of RWY. No back beam.
RWY 20R
ILS LLZ
ICH108.9MHzH24012045.23N 1035834.17ELocated 368m (1207ft) from THR RWY 02L, along centreline of the RWY.
Course width 3.38°. EM: A0/A2.
Maintenance Period:
May - October
First Saturday of every month between 0200-0900
November - April
First Friday of every month between 0200-0900
RWY 20R
ILS GP
-329.3MHzH24012225.54N 1035912.29ELocated 330m (1083ft) from displaced THR RWY 20R on right side of the RWY, 120m (394ft) from RWY centreline.
GP angle 3° .
HGT of ILS REF datum: 17m (56ft)
EM: A0/A2
RWY 20R
ILS DME
ICHCH26XH24012225.54N 1035912.29EDME co-located with GP. Rwy 20R ILS DME not available beyond 15 degrees west of RWY 20R centreline below 2500ft.
EM: P9
RWY 20R
ILS MM
-75MHzH24012307.50N 1035934.23ELocated 1122m (3681ft) from displaced THR RWY 20R, along centreline of the RWY.
RWY 02L
ILS LLZ
ICW110.9MHzH24012307.03N 1035934.03ELocated 1105m (3625ft) from displaced THR RWY 20R, along centreline of RWY.
Course width 2.81° EM:A0/A2
Maintenance Period:
May - October
First Friday of every month between 0200-0900
November - April
First Saturday of every month between 0200-0900
RWY 02L
ILS GP
-330.8MHzH24012108.34N 1035838.94ELocated 343m (1125ft) from THR RWY 02L on left side of RWY, 143m (469ft) from RWY centreline.
GP angle 3°
HGT of ILS Reference datum: 18m (58ft)
EM:A0/A2
RWY 02L
ILS DME
ICWCH46XH24012108.34N 1035838.94EDME co-located with GP
EM:P9
RWY 02L
ILS MM
-75MHzH24012027.53N 1035826.70ELocated 957m (3140ft) from THR RWY 02L along extended centreline of RWY. No back beam.

WSSS AD 2.20 LOCAL TRAFFIC REGULATIONS

1 DESIGNATION OF PAYA LEBAR AIRPORT AS AN ALTERNATE AERODROME FOR SINGAPORE CHANGI AIRPORT
 
Please refer to pages WSAP AD 2-5 to WSAP AD 2-7 for details.
2 WRONG APPROACHES AND LANDINGS OF AIRCRAFT BOUND FOR SINGAPORE CHANGI AND PAYA LEBAR AIRPORTS
2.1 INTRODUCTION
2.1.1 The attention of all pilots is drawn to the existence of Paya Lebar Airport close to Singapore Changi Airport. The runway at Singapore Changi Airport is orientated in the same true bearing as the runway at Paya Lebar Airport i.e. 023°/203°. Due to the close proximity of these two runways, pilots are cautioned against mistaking Paya Lebar Airport for the runway of Singapore Changi Airport and thus making an inadvertent visual landing or approach to land at Paya Lebar.
2.1.2 Erroneous approaches or landings usually occurred during the hours of darkness. In almost every instance, the weather prevailing at the time of the incident was generally good or fair.
2.1.3 There is intensive local flying at Paya Lebar and Seletar during the day and night. Thus, the risk of collision is very great if a wrong approach is made to any of the above two airports. Likewise, wrong approaches into Singapore Changi Airport can also be disastrous.
2.2 POINTS TO BEAR IN MIND WHEN APPROACHING SINGAPORE CHANGI AIRPORT OR PAYA LEBAR
2.2.1 The following points are highlighted to serve as a guide to assist pilots in making a correct approach into Singapore Changi Airport or Paya Lebar Airport and should be remembered and followed:
  1. The runways at Singapore Changi Airport and Paya Lebar Airport are identically aligned on 02/ 20. Therefore exercise extreme vigilance when leaving NYLON or SAMKO Holding Areas inbound and maintain correct tracks to the respective runways as listed below.

  2. Adhere strictly to IFR procedures even in VMC which calls for a procedure turn over NYLON Holding Area or SAMKO Holding Area as prescribed.

  3. Make full use of all available navigational and landing aids available and positively identify every aid used.

  4. Switch to the correct ILS localizer frequency at Singapore Changi Airport under all conditions.

2.3 AERODROME CHARACTERISTICS OF SINGAPORE CHANGI AND PAYA LEBAR AIRPORTS
2.3.1 Tabulated below are details of aerodrome characteristics of Singapore Changi Airport and Paya Lebar Airport which indicate the similarities and significant differences for ease of identification by pilots operating into these two airports.
Aeronautical
Service
PAYA LEBAR
Airport
SINGAPORE CHANGI
Airport
Significant
Differences and Remarks
Magnetic heading of RWY02/2002L/20R
02C/20C
Exercise caution due to similar RWY alignment
Approach LightsRWY 02
Modified Calvert High INTST with centreline and 3 crossbars. High INTST white LGT with brilliancy control and sequenced flashing lights.
RWY 02L
Precision APCH LGT CAT II. Extended centreline with red side row barettes, 2 crossbars, 2 APCH beacons and sequenced flashing lights.
RWY 20
Modified Calvert High INTST with centreline and 3 crossbars. High INTST white LGT with brilliancy control and sequenced flashing lights.
RWY 20R
Precision APCH LGT CAT I. Centreline barettes flashing white, 2 APCH beacons and sequenced flashing lights. (refer to chart
AD-2-WSSS-ADC-2)
ILSRWY 20 - NilRWY 20R
IDENT ICH
No back beam
LLZ 108.9 MHz
GP 329.3 MHz
RWY 02 - NilRWY 02L
IDENT ICW
No back beam
LLZ 110.9 MHz
GP 330.8 MHz
IBNFlashing R ‘PL’
HN and IMC
Flashing G ‘CH’
HN and IMC
ABNNilALTN Flashing W G every 2.3 SEC

WSSS AD 2.21 NOISE ABATEMENT PROCEDURES

1.1 To alleviate the problem of noise, all aircraft on AWY G579 between SINJON (SJ) and JAYBEE (JB) shall operate at/above 5,000ft.
1.2 The Standard Instrument Departure routes for aircraft departing on RWY 20R/20C are for the purpose of noise abatement in addition to being used for air traffic control.
1.3 Departures on RWY 20R are restricted between 1600-2200UTC. This restriction is not applicable when RWY 20C/02C is unavailable because of maintenance works or for other reasons.
1.4 Unless it is necessary for operational or safety reasons, when using engine reverse, arrivals on RWY 02L/20R between 1600-2200UTC may not exceed idle reverse thrust.

WSSS AD 2.22 FLIGHT AND GROUND PROCEDURES

1 LOW VISIBILITY PROCEDURES (LVP) FOR CATEGORY II ILS OPERATIONS
1.1 Introduction
1.1.1 Category II ILS approaches will be made available at Singapore Changi Airport to authorised flights during prolonged periods of low visibility, except during thunderstorms. RVR minima for CAT II ILS operations is limited to 350m due to runway and taxiway light spacing requirements on the airfield.
1.2 Authorisation for Category II ILS Approaches
1.2.1 Operators who wish to conduct Category II ILS operations at Singapore Changi Airport must have obtained operational approval from the relevant State of Operator and be authorised by the Civil Aviation Authority of Singapore.
1.3 Category II ILS Runways
1.3.1 At Singapore Changi Airport, Category II ILS approaches are available only on RWY 02L and RWY 20C, which are also equipped with precision approach Category II lighting system. When required, pilots making Category II ILS approaches to Singapore Changi Airport should refer to the procedures in the Instrument Approach Charts AD-2-WSSS-IAC-1 to AD-2-WSSS-IAC-11 and the Precision Approach Terrain Charts for RWY 02L and RWY 20C at AD-2-WSSS-PATC-1 and AD-2-WSSS-PATC-2 respectively.
1.4 Initiation of Category II ILS Operations
1.4.1 Preparations will be made to implement LVP for Category II ILS operations at Singapore Changi Airport during prolonged period of low visibility, except during thunderstorms, when the RVR drops below 800 metres.
1.4.2 Availability of the Category II ILS approaches will be made known through NOTAM and ATIS broadcasts as well as air traffic control radio communications.
1.4.3 During LVP operations, aircraft will not be cleared for Category II ILS approach if any of the ILS or approach/runway lights fall below Category II requirements. Aircraft will not be cleared for landing if the Touchdown Zone RVR is unserviceable.
1.5 ILS Sensitive Areas
1.5.1 Upon landing, pilots shall report to Changi Tower once the aircraft has cleared the runway and has passed the ILS sensitive areas demarcated by alternate yellow and green lights along the centrelines of Rapid Exit Taxiways and Cross Taxiways.
1.6 Termination of LVP for Category II ILS Operations
1.6.1 LVP for Category II ILS operations will be terminated when RVR has improved above 800 metres. Termination of LVP for Category II ILS operations will be made known through NOTAM and ATIS broadcasts as well as air traffic control radio communications.
1.7 Operations of flights Not Authorised for Category II ILS
Operations
1.7.1 During Category II ILS operations, if the RVR is 550 metres or above, flights not authorised for Category II ILS operations may continue to make approaches and land. Airlines planning to operate flights not authorised for Category II ILS operations into Changi shall monitor the METAR to ascertain the RVR values when launching their flights and be prepared to divert if the RVR is below 550 metres.
2 RUNWAY UTILISATION
2.1 Runway-in-use
2.1.1 The runway-in-use (Departure/Arrival) is selected by Aerodrome Control as the optimum for general purposes and to maximise runway utilisation. If the assigned runway is unsuitable for a particular operation, the pilot can obtain permission from ATC to use another runway but should anticipate delay.
2.2 Departures
2.2.1 Pilots should arrange their taxi such that they are ready to depart without delay on reaching the runway holding point. As standard ICAO wake turbulence separation is being applied, pilots are to advise ATC early if more time is needed for the aircraft to be ready for departure. When informed, ATC will be able to make changes in the departure sequence, if necessary, to minimise delays to other succeeding departures.
2.2.2 Pilots should complete cockpit checks prior to line-up for departure and keep any checks on the runway to a minimum.
2.2.3 Conditional line-up clearance may be used by ATC to facilitate an expeditious flow of traffic. On receipt of line-up clearance, pilots should taxi into position promptly without delay. Unless given instructions to line-up and wait, pilots should be ready and prepared to depart without stopping. On receipt of take-off clearance, pilots to commence take-off roll without delay.
2.3 Clearance for Immediate Take-Off
2.3.1 A pilot receiving the ATC instruction ‘cleared for immediate take-off’ is required to act as follows:
  1. if waiting clear of the runway, taxi immediately on to it and begin take-off run immediately without stopping the aircraft;
  2. if already lined-up on the runway, take-off without delay;
  3. if unable to comply with the instruction, inform ATC immediately.
2.4 Arrivals - Minimum Runway Occupancy Time (ROT)
2.4.1 Arriving aircraft upon landing are reminded that it is imperative to vacate the runway as quickly as practicable to enable ATC to apply minimum spacing on final approach and minimise the occurrence of “go-arounds”.
2.4.2 To achieve minimum ROT and reduce missed approaches due to occupied runway, pilots should vacate the runway via the first available exit taxiway corresponding to operational requirements, or as instructed by ATC. If an exit taxiway other than the first available exit taxiway is required, pilots shall advise the Tower Controller on first contact.
2.4.3 To enhance planning, pilots can make reference to the Landing Exit Distance (LED), the distance from threshold to the furthest edge of the exit taxiway:
RWYExit Taxiway (LED in metres)Remarks
20RW6*(1655), W7*(2123) and W8 (3061)

Note 1: Recommended exit taxiways are bold and underlined.

Note 2: * Indicates Rapid Exit Taxiway (RET) and maximum design ground speed for the exit taxiway is 50kts.

20CE6*(1948), E7*(2391) and E8 (3152)
02LW5*(1966), W4*(2491) and W3* (2876)
02CE5*(2055), E4*(2565) and E3* (3267)
2.4.4 Pilots can expect initial taxi instructions from the Runway Controller before clearing the exit taxiway. Aircraft vacating the runway-in-use should not stop on the exit taxiway until the entire aircraft has passed the runway holding point.
2.4.5 BTN 0830-1030 daily estimated delays of about 15 minutes can be expected for arrivals into Singapore Changi Airport.
2.5 Land after Procedures
2.5.1 Normally, only one aircraft is permitted to land or take-off on the runway-in-use at any one time. However, when the traffic sequence is two successive landing aircraft, the second aircraft may be allowed to land before the first aircraft has cleared the runway-in-use provided:
  1. the runway is long enough;
  2. during daylight hours;
  3. the second aircraft will be able to see the first aircraft clearly and continuously until it is clear of the runway;
  4. the second aircraft has been warned.
2.5.2 ATC will provide this warning in the landing clearance as shown in para 2.7.
2.5.3 Responsibility for ensuring adequate separation between the two aircraft rests with the pilot of the second aircraft.
2.6 Special Landing Procedures
2.6.1 Special landing procedures may be in force at Singapore Changi Airport in conditions shown as follows:
  1. When the runway-in-use is temporarily occupied by other traffic, landing clearance may be issued to an arriving aircraft provided that at the time the aircraft crosses the threshold of the runway-in- use the following separation distances will exist:
    1. Landing following landing - The preceding landing aircraft will be clear of the runway-in-use or will be at least 2,500m from the threshold of the runway-in-use.
    2. Landing following departure - The departing aircraft will be airborne and at least 2,500m from the threshold of the runway-in-use, or if not airborne, will be at least 2,500m from the threshold of the runway-in-use.
2.6.2 These procedures will be used only under the following conditions:
  1. during daylight hours;
  2. visibility of at least 5km;
  3. cloud ceiling of 1,500ft in the departure/missed approach area;
  4. ATC is satisfied that the pilot of the next arriving aircraft will be able to observe continuously the relevant traffic;
  5. no unfavourable surface wind conditions (including significant tailwind, windshear, turbulence, etc);
  6. when the runway is dry and free of all precipitants such that there is no evidence that the braking action may be adversely affected.
2.7 Phraseology
2.7.1 When issuing a landing clearance following the application of these procedures, ATC will issue the second aircraft with the following instructions:

.... (call sign) .... after the landing / departing .... (Aircraft Type) Runway .....(Designator) cleared to land.

3 AIRPORT COLLABORATIVE DECISION MAKING (A-CDM) MODE OF OPERATIONS
3.1 A-CDM aims to optimise airport operations by having an efficient turnaround process and improving the predictability of operational events. It also helps to improve gate management, flight punctuality, reduce apron taxiway and holding point congestion which is beneficial to all airport partners. A-CDM involves sharing of accurate and timely operational information amongst airport partners through different airport systems and improving work processes by implementing a set of operational procedures.
3.2 The A-CDM procedures apply to all scheduled flights departing Singapore Changi Airport except for VVIP, CASEVAC, SAR and aircraft on special tasks. ATC shall have full discretion in conduct of such operations.
3.3 Definition of commonly used terms in A-CDM
  1. Target Off Block Time (TOBT) – The time an aircraft operator (AO) or ground handling agent (GHA) estimates that an aircraft will be ready, all doors closed, boarding bridge removed, pushback vehicle available and ready to start-up / pushback immediately upon receipt of clearance from ATC.
  2. Target Start Up Approval Time (TSAT) – The time provided by ATC that an aircraft can expect start-up / push back approval.
  3. Calculated Take Off Time (CTOT) – A time calculated as a result of tactical slot allocation, at which a flight is expected to become airborne.
4 A-CDM PRE-DEPARTURE PROCEDURES
4.1 Singapore Changi Airport’s A-CDM portal will automatically calculate a system TOBT for each departure flight taking into account the estimated or actual in-block time (EIBT / AIBT), minimum turnaround time (MTT) and scheduled time of departure (STD)
4.2 If the calculated TOBT (EIBT / AIBT + MTT) is earlier than STD, the system will take the STD as TOBT.
4.3 If the calculated TOBT (EIBT / AIBT + MTT) is later than STD, the amount of turnaround delay that system predicts is equal to TOBT – STD.
4.4 AO are required to assess the system generated TOBT at 40 minutes prior to departure and update it if the prediction of departure readiness is different. Thereafter, TOBT needs to be monitored and updated constantly if it is expected to differ by 5 minutes or more until the flight commences pushback. AO can consider delegating the responsibility of TOBT submission to their ground handling agent (GHA) subject to prior internal arrangements between AO and GHA.
4.5 TOBT shall be updated through the following systems:
  1. Airport Operations Centre System (AOCS) A-CDM web based portal; or
  2. Gate Message Input Display (GMID) at boarding rooms;

4.6 AO/GHA is encouraged to update TOBT through ONLY one of the above systems in order to avoid any chance of a miscommunication.
4.7 TOBT information is available through the following channels:
  1. AOCS A-CDM portal;
  2. GMID;
  3. Aircraft Docking Guidance System (ADGS) at contact stands;
  4. Radio communication with GHA or AO.

4.8 The Pre-Departure Sequencer (PDS) will calculate the TSAT automatically by taking into account factors such as TOBT, calculated take-off time (CTOT), variable taxi times (VTT), wake turbulence category, departure separation, etc. A pre-departure sequence is determined from the calculated TSATs, thus the accuracy of TOBT is vital to an optimal TSAT.
4.9 Flights with an invalid or expired TOBT will be instructed by ATC to update TOBT when requesting for clearance. For non-compliant flights, delays can be expected. AO or GHA are strongly encouraged to update TOBT as soon as any expected delay to the aircraft readiness for pushback is made available to avoid unnecessary hold-ups.
4.10 TSAT information is available through the following channels:
  1. AOCS A-CDM portal;
  2. GMID;
  3. ADGS at contact stands;
  4. Radio communication with GHA or AO;
  5. ATC - Upon issuance of ATC clearance (for flights parked at aircraft stands without ADGS).

5 A-CDM START-UP PROCEDURES
5.1 Pilot shall ensure aircraft is ready for pushback at TOBT.
5.2 Pilot to maintain communication with the AO / GHA as they are responsible for updating the TOBT. Notify the AO / GHA to update the TOBT if it is expected to differ by 5 minutes or more.
5.3 Pilot to contact Ground Movement Planner (Clearance Delivery) and request for ATC clearance within 5 minutes of TOBT using the following phraseology:

- Callsign
- Destination
- Proposed flight level and alternate level, if any
- Parking position

  1. Pilot shall only request for ATC clearance provided aircraft is ready to pushback at TOBT. Any updates to TOBT after receipt of ATC clearance will result in cancellation of clearance issued as the ATC clearance validity is based on the initial TOBT.

5.4 ATC will advise the pilot whether the proposed flight level or other alternate flight level is available and an ATC clearance will be issued accordingly. If pre-departure coordination with an adjacent unit or centre is required, the pilot will be instructed to standby.
5.5 ATC will update TSAT changes if any, during issuance of ATC clearances. Note that TSAT displayed on ADGS may not be final and can be revised due to en-route clearance restrictions, ground congestion or flow measures.
5.6 Pilot shall request for pushback from Ground Movement Control within 5 minutes of TSAT after obtaining ATC clearance, or as directed by ATC.
  1. ATC may swap pushback sequence based on real-time readiness of aircrafts to maximise apron and runway capacity and reduce the overall delay to traffic as and when required.
  2. At the end of pushback, the departing aircraft must have all engines started and be ready to taxi immediately, unless otherwise instructed by ATC.

Note: The first aircraft to taxi may not necessarily be the first aircraft to take-off as distances between aircraft stands and the departure runway vary.

5.7 A flight issued with gate hold (TSAT>TOBT) but chooses to commence pushback before the assigned time will be allowed to do so subject to traffic. However, the flight should not expect an earlier departure time as the planned pre-departure sequence will be maintained.
5.8 If a flight is unable to pushback by TSAT + 5 minutes due to the aircraft being unready, ATC clearance and TSAT will be cancelled. Pilot must notify the AO / GHA to update the TOBT for a new TSAT before requesting for a new ATC clearance. This also applies to aircraft returning back to blocks after pushback.
  1. ATC will inform the aircraft when a clearance is cancelled using the phraseology; “(Callsign of aircraft) your ATC clearance and TSAT is cancelled (reason). Update TOBT before requesting for new clearance”.
  2. Flight may also have its ATC clearance cancelled if it develops a technical problem after pushback and is unable to taxi for prolonged duration.

5.9 Non-compliance of initial TSAT may result in an aircraft losing its existing position in the pre- departure sequence. Delay can be expected as a result of re-sequencing based on new TOBT input.
5.10 If delay in pushback is due to ground traffic movement or ATC clearance restrictions, the ATC clearance and TSAT will remain valid even if it exceeds TSAT + 5 minutes. TOBT need not be updated for such situations.
5.11 In the event that A-CDM mode of operations need to be cancelled due to any reason, the termination will be communicated to relevant parties through email by the airport operator and a NOTAM will be issued by ATC. Pilot shall follow the non-CDM procedures detailed in para 12.
6 A-CDM INFORMATION VIA AIRCRAFT DOCKING GUIDANCE SYSTEM (ADGS)
6.1 All contact stands in Singapore Changi Airport will have ADGS. The fundamental operation and usage of ADGS still remain the same for flight crew. Additional information which includes TOBT, TSAT and TOBT count-down timer will be displayed in local times as part of the improvements to support A-CDM operations.

Aircraft Docking Guidance System (ADGS)
DescriptionDisplay on ADGS

Aircraft arrival to stand

  • No change in existing functionality and display


40 minutes prior to TOBT

  • ADGS will display TOBT submitted by AO / GHA and a count down timer (2 digits) to TOBT in minutes

  • As ADGS can only display up to 7 characters per line, the displayed message will be scrolling.

  • Timings displayed will be in Local Time (LT)

  • TOBT timings will change instantly if there is an update done by AO / GHA


25 minutes prior to TOBT

  • ADGS will display TSAT derived by PDS

  • AS ADGS can only display up to 7 characters per line, the displayed message will be scrolling.

  • TSAT timings may change as the PDS is continuously optimising push back times based on real time traffic conditions


Aircraft departure from stand

  • ADGS will display the actual off-block time (AOBT)

  • As ADGS can only display up to 7 characters per line, the displayed message will be scrolling

  • TOBT, TSAT and TOBT countdown timer will be removed

  • AOBT display will be removed 3 minutes after AOBT


7 CONTACT AND INFORMATION
7.1 Please contact the airport operator, Changi Airport Group (CAG), at a-cdm@changiairport.com for application of AOCS A-CDM and GMID account or if you have any queries.
7.2 Aircraft operators may also contact their ground handling agent directly on queries regarding TOBT submission.
8 ASSIGNMENT OF FLIGHT LEVELS TO AIRCRAFT DEPARTING FROM SINGAPORE CHANGI AIRPORT
8.1 Assignment of flight levels to departing aircraft is made on a best-planned-best-served basis (with reference to TOBT for ATC clearance request detailed in para 5.3). Aircraft will normally be assigned the level requested unless an alternate level is offered after coordination with the adjacent ATC centres.
8.2 Departing flights from Singapore requesting FL280 or FL320 on L759, M770, N571, N571/N877 or P628 will be cleared as follows:
  1. Aircraft departing Singapore will be cleared to FL280;
  2. Succeeding aircraft on the same route will be cleared to FL280 with 10min longitudinal separation provided there is no closing speed with the preceding aircraft;
  3. Additional longitudinal separation as appropriate shall be imposed by ATC when the succeeding aircraft is faster than the preceding aircraft on the same route;
  4. The first aircraft from either Singapore or Kuala Lumpur to be over GUNIP on N571 or N571/N877, the Kuala Lumpur/Bangkok FIR boundary on M770 or L759 and VPL on P628 can expect its requested flight level

9 DELAY IN PUSHBACK AND/OR TAXIING DUE TO OTHER AIRCRAFT
9.1 Delays may be expected for the second aircraft to pushback and to taxi when two or more aircraft are parked either adjacent to one another or close together. However, it will retain its ATC clearance even if the 5 minutes grace period allowed for under para 5.8 is exceeded.

Note: The TSAT may not be able to predict delays arising from apron congestion as traffic movement on ground is dynamic and situations may change on a real time basis depending on aircraft readiness. ATC will facilitate pushback as soon as possible when traffic permits.

10 DELAY IN TAKE-OFF DUE TO RESTRICTIONS IN THE ATC CLEARANCE
10.1  The ATC clearance may require an aircraft to arrive at a reporting point at a specified time and level or to depart a number of minutes behind a preceding traffic to establish the appropriate longitudinal separation. Such delay will not deprive a departing aircraft of its ATC clearance even though the 5 minutes grace period allowed for under para 5.8 is exceeded.
11 DELAY DUE TO OVERFLIGHTS
11.1 These are flights operating through Singapore FIR without landing at Singapore Changi Airport. Depending on their positions, a departing aircraft requesting the same level may have to accept an alternate level or may have to delay its departure in order to establish the prescribed separation.
12 NON-CDM MODE OF OPERATIONS
12.1 The non-CDM procedures is applicable for non-scheduled flights departing Changi Airport or when TOBT and TSAT references used in A-CDM mode of operations become unavailable due to system issues or maintenance.
12.2 If TOBT cannot be submitted or it is unavailable through different channels stated in para 4.5,
  1. Pilots shall notify ATC when the aircraft is ready to pushback within 5 minutes.
  2. ATC will advise the pilot whether the proposed flight level or other alternate flight level is available and an ATC clearance will be issued accordingly. If pre-departure coordination with an adjacent unit or centre is required, the pilot will be instructed to standby.
  3. Once flight level is accepted by the pilot and an ATC clearance issued, the aircraft must be pushed back within 5 minutes from the time the ATC clearance is accepted unless other ATC restrictions are imposed. The ATC clearance will be cancelled on expiry of the 5 minutes grace period. This also applies to situations when aircraft return to blocks after pushback or develop technical issues and is unable to continue taxi.
  4. Pilots who are ready to depart following the cancellation of an ATC clearance will adopt the procedures as if it is the first time they are ready to depart.

12.3 If TSAT is unavailable through different means stated in para 4.10,
  1. AO and GHA shall continue to submit TOBT and pilots shall request for ATC clearance 5 minutes within TOBT stated in para 5.3
  2. ATC will revert to the gate hold procedures stated in para 13 and issue estimated pushback times accordingly.
13 GATE HOLD PROCEDURES FOR DEPARTING AIRCRAFT (DURING NON-CDM MODE OF OPERATIONS)
13.1 Whenever there are about five to seven departing aircraft at the runway holding point, subsequent pushback of departures will be regulated such that the Ground Movement Planner (GMP) on VHF frequency 121.65MHz will start to issue pilots with Expected Pushback Time (EPT) as TSAT used in A-CDM operations is not available. The determination of EPT will take into account an aircraft's parking stand as well as taxi time to the runway-in-use holding point.
13.2 When an EPT is issued, pilots will be instructed to either remain on GMP frequency or to monitor Singapore Ground Control (frequencies 124.3MHz, 121.725MHz or 121.85MHz). It should be noted that when instructed to monitor the Singapore Ground frequencies, pilots shall not establish contact with the Singapore Ground Control, rather, pilots shall maintain listening watch on the assigned Singapore Ground Control frequency and wait for pushback instruction. This is to prevent unnecessary frequency congestion.
13.3 A flight issued with an EPT but chooses to commence pushback before the assigned time will be allowed to do so subject to traffic. However, the flight should not expect an earlier departure time as the planned pre-departure sequence will be maintained.
13.4 In a situation when a departing aircraft is occupying a gate that has been assigned to an arriving aircraft, the departing aircraft will be instructed by GMP to contact Singapore Ground for pushback for the purpose of better gate utilisation.
13.5 To maximise runway utilisation, departure sequence will be planned on the basis of increasing runway throughput so as to enhance overall efficiency.
PROCEDURES FOR PUSH BACK AND ASSIGNMENT OF FLIGHT LEVELS TO AIRCRAFT DEPARTING FROM SINGAPORE CHANGI AIRPORT
Aircraft departing Singapore Changi Airport shall adhere to the procedures for push back and assignment of flight levels.
Assignment of flight levels to departing aircraft is made on a first-come-first-served basis. Aircraft will normally be assigned the level requested unless an alternate level is offered after coordination with the adjacent ATC centres.
Departing flights from Singapore requesting FL280 or FL320 on L759, M770, N571, N571/N877 or P628 will be cleared as follows:
  1. aircraft departing Singapore will be cleared to FL280;
  2. succeeding aircraft on the same route will be cleared to FL280 with 10 min longitudinal separation provided there is no closing speed with the preceding aircraft;
  3. additional longitudinal separation as appropriate shall be provided by ATC for the faster aircraft following a slower aircraft on the same route;
  4. the first aircraft from either Singapore or Kuala Lumpur to be over GUNIP on N571 or N571/N877, the Kuala Lumpur/Bangkok FIR boundary on M770 or L759 and VPL on P628 can expect its requested flight level.
To avoid confusion, pilots shall use the correct phraseology as detailed in para 3.5 when ready for push back.
The pilot shall notify ATC when the aircraft is ready to push back within 5 min using the following phraseology:

- callsign
- destination
- proposed flight level and alternate level, if any
- parking position

On receipt of the “ready to push back” call, ATC will advise the pilot whether the proposed flight level or other alternate flight level is available and an ATC clearance will be issued accordingly. If pre-departure coordination with an adjacent unit or centre is required, the pilot will be instructed to standby.
Once the flight level is accepted by the pilot and an ATC clearance issued, the aircraft must be pushed back within 5 minutes from the time the ATC clearance is accepted unless other ATC restrictions are imposed. The ATC clearance will be cancelled on expiry of the 5 minutes grace period.
At the end of the push back, the departing aircraft must have all engines started and be ready to taxi immediately, unless otherwise instructed by ATC.

Note: The first aircraft to taxi may not necessarily be the first aircraft to take-off as distances between aircraft stands and the departure runway vary.

GATE HOLD PROCEDURES FOR DEPARTING AIRCRAFT
Whenever there are about five to seven departing aircraft at the RWY holding point, subsequent push-backs of departures will be regulated such that the Ground Movement Planner (GMP) on VHF frequency 121.65MHz will start to issue pilots with Expected Push back Time (EPT). The determination of EPT will take into account an aircraft’s parking stand as well as taxi time to the RWY-in-use holding point.
When an EPT is issued, pilots will be instructed to either remain on GMP frequency or to monitor Singapore Ground Control (frequencies 124.3MHz, 121.725MHz or 121.85MHz). It should be noted that when instructed to monitor Singapore Ground frequencies, pilots shall not establish contact with the Singapore Ground Control, rather, pilots shall maintain a listening watch on the assigned Singapore Ground Control frequency and wait for push back instruction. This is to prevent unnecessary frequency congestion.
A flight issued with an EPT but chooses to commence push back before the assigned time will be allowed to do so. However, the flight should not expect an earlier departure time as the planned departure sequences will be maintained.
In a situation when a departing aircraft is occupying a gate that has been assigned to an arriving aircraft, the departing aircraft will be instructed by the GMP to contact Singapore Ground for push back for the purpose of better gate utilization.
To maximize runway utilization, departure sequence will be planned on the basis of increasing runway throughput so as to enhance overall efficiency.
DELAY IN PUSH BACK AND/OR TAXIING DUE TO OTHER AIRCRAFT
Delays may be expected for the second aircraft to push back and to taxi when two or more aircraft are parked either adjacent to one another or close together. However, it will retain its ATC clearance even if the 5 minutes grace period allowed for under para 3.7 is exceeded.
DELAY IN TAKE-OFF DUE TO RESTRICTIONS IN THE ATC CLEARANCE
The ATC clearance may require an aircraft to arrive at a reporting point at a specified time and level or to depart a number of minutes behind a preceding traffic to establish longitudinal separation. Such a delay will not deprive a departing aircraft of its ATC clearance even though the 5 minutes grace period would have been exceeded.
DELAY DUE TO OVERFLIGHTS
These are flights operating through Singapore FIR without landing at Singapore Changi Airport. Depending on their positions, a departing aircraft requesting the same level may have to accept an alternate level or may have to delay its departure in order to establish the prescribed separation.
FLIGHTS EXEMPTED
The above procedures are not applicable to VIP, CASEVAC, SAR and other special tasks aircraft. ATC shall have full discretion in the conduct of such operations.
CANCELLATION OF ATC CLEARANCE / OBTAINING A FRESH CLEARANCE
A departing aircraft may have its ATC clearance cancelled under the following circumstances:
  1. on expiry of the 5 minutes grace period under para 3.7, it is still unable to push back; or
  2. after pushing back, the pilot advises that it is returning to blocks; or
  3. it develops a technical problem and is unable to continue taxiing.
ATC will inform the aircraft when a clearance is cancelled using the phraseology;
“(Callsign of aircraft) your ATC clearance is cancelled (reason)”
Pilots who are ready to depart following the cancellation of an ATC clearance will adopt the normal procedures as if it is the first time they are ready to depart.
14 GROUND MOVEMENT PLANNER ON VHF 121.65MHz
14.1 The frequency shall be used for aircraft pre-flight checks and ATC clearances. Pilot-in-command to make his initial call from the parked position on this frequency.

15 GROUND MOVEMENT CONTROL ON VHF 124.3MHz, 121.85MHz AND 121.725MHz
15.1 This frequency shall be used for aircraft start-up/push-back clearance.
15.2 Unless otherwise instructed by ATC, the pilot-in-command shall prior to starting engines listen out on the Ground Movement Control frequency on 124.3MHz, 121.85MHz or 121.725MHz.
15.3 The pilot-in-command shall:
  1. Request and obtain taxi instructions prior to taxiing;

    Note: ATC clearance, including the assigned SSR code will normally be issued prior to push back. Pilot shall squawk the SSR code immediately when airborne.

  2. Change from Ground Movement Control frequency to the Runway Control frequency when instructed (118.6MHz or 118.25MHz). It should be noted that when instructed to monitor Singapore Tower frequencies, pilots shall not establish contact with Singapore Tower; rather, pilots shall maintain a listening watch on the assigned Singapore Tower frequency and wait for instruction. This is to prevent unnecessary frequency congestion.
15.4 Departing aircraft will be instructed when to change from 118.6MHz or 118.25MHz to Singapore Departure frequency 120.3MHz.
15.5 In the case of the aircraft having landed, the pilot-in-command shall change from 118.6MHz or 118.25MHz to 124.3MHz, 121.85MHz or 121.725MHz immediately upon instructed by ATC after clearing the runway. He shall maintain watch on 124.3MHz, 121.85MHz or 121.725MHz for taxiing and parking instructions until he arrives at his aircraft stand.
16 TAXIING
16.1 Taxi clearance given by Ground Movement Control will relate to movement on the manoeuvring area, but excluding the marshalling area.
16.2 Aircraft taxiing on the manoeuvring area will be regulated by ATC to avoid or reduce possible conflict and will be provided with traffic information and alerting service. ATC shall apply taxiing clearance limits whenever necessary.
16.3 The taxiway routes to be used by aircraft after landing or when taxiing for departure will be specified by ATC. The issuance by ATC of a taxi route to an aircraft does not relieve the pilot-in-command of the responsibility to maintain separation with other aircraft on the manoeuvring area or to comply with ATC directions intended to regulate aircraft on the manoeuvring area.
16.4 Pilots are reminded to always use minimum power when starting engines, when manoeuvring within the apron area or when manoeuvring from apron taxiways to other parts of the aerodrome. It is especially critical when commencing to taxi that break-away thrusts are kept to an absolute minimum and then be reduced to idle thrusts as soon as possible.

17 TAKE-OFF AND LANDING
17.1 Departing aircraft will normally be directed by ATC to use the full length of the runway for take-off. On obtaining an ATC clearance the aircraft shall enter the runway via designated taxiways:

RWY 02C - TWY E10 or E11

RWY 02L - TWY W8, W9 or W10

RWY 20C - TWY E1, E2

RWY 20R - TWY W1, W2

17.2 The pilot-in-command shall not take-off or land without a clearance from Aerodrome Control.
17.3 The pilot-in-command shall not run-up on the runway in use unless authorised by Aerodrome Control. Engine run-ups in the holding pan or taxiway holding point clear of the runway in use may be carried out subject to approval by Aerodrome Control.
17.4 After landing, the pilot-in-command shall vacate the runway by the shortest suitable route and to contact Ground Control who will issue specific taxi route instructions to its assigned aircraft stand.
17.5 Aircraft with radio communication failure shall vacate the runway and stop on the taxiway and watch for light signals from Aerodrome Control.
18 RNAV(GNSS) SIDs and STARs
18.1 INTRODUCTION
18.1.1 The RNAV(GNSS) SIDs and STARs are designed in accordance with the ICAO RNAV(GNSS) Departure and Arrival criteria as stipulated in the ICAO PANS-OPS (Doc 8168) Volume II.
18.1.2 For RNAV(GNSS) SIDs and STARs operations, the aircraft shall be GNSS-equipped and the navigation systems shall meet ICAO RNP-1 standard of accuracy, or equivalent, such as JAA TGL 10 or FAA AC 90-96A Appendix 2 - Precision Area Navigation (P-RNAV).
18.1.3 To avoid proliferation of SIDs and STARs, the basic RNAV SIDs and STARs have been modified to follow similar tracks as the RNAV(GNSS) SIDs and STARs using the same set of SIDs and STARs identification.
18.1.4 Operators/pilots who are not approved to fly the RNAV(GNSS) SIDs and STARs shall fly the alternate basic RNAV SIDs and STARs or expect radar vectors from ATC.
18.2 ARRIVALS
18.2.1 STARs are presented in diagrammatic and textual format on a chart which comprises two main elements:
  1. A TRANSITION route; and
  2. An ARRIVAL route.
18.2.2 A TRANSITION starts at a waypoint on the ATS route and then requires VOR/DME or RNAV tracking to position the aircraft for the ARRIVAL route.
18.2.3 All arriving aircraft are required to follow the appropriate TRANSITION and ARRIVAL routes. The TRANSITION routes are as follows:
ATS RouteTransitionTransition RouteRNAV STAR
B469 (southbound to Singapore)
L642
N892
BIKTA
VEPLI
MABAL
BIKTA-PIBAP-PASPU
VEPLI-VINIL-PIBAP-PASPU
MABAL-KILOT-VINIL-PIBAP-PASPU
PASPU
ARRIVAL
A464 (southbound to Singapore)
A576 (southbound to Singapore)
R469
ARAMA
REKOP
no transition
ARAMA-BOBAG
REKOP-BOBAG
no transition
BOBAG
ARRIVAL
G579no transitionno transitionREMES
ARRIVAL
L504
M635
M774
OBDOS
SURGA
OBDOS
OBDOS-IKAGO-IKIMA-IBULA-LAVAX
SURGA-IKAGO-IKIMA-IBULA-LAVAX
OBDOS-IKAGO-IKIMA-IBULA-LAVAX
LAVAX
ARRIVAL
M767 / G580
M646 / G580
G580
TOMANTOMAN-KARTO-KEXAS-LAVAX
Note: Aircraft landing at Singapore Changi Airport operating on N891, M753 and L642 shall flight plan only on L642 after ENREP
18.2.4 Additional elements on the STAR chart include the following:
  1. Vertical restrictions, designed to contain aircraft in controlled airspace and to separate aircraft from obstacles and to avoid, to the degree possible, conflict with departing traffic.
  2. Speed restrictions, designed for flow control purposes.
  3. Minimum safe altitude (MSA) within 25NM of VTK and SJ DVOR/DME. The MSA provides a minimum of 1000ft vertical clearance within 5NM of any obstacle.
18.2.5 Arrivals to Singapore Changi Airport can expect radar vectors to intercept the localizer for an ILS approach after the initial approach fix on the RNAV STARs.
18.2.6 STARs shall be issued by ATC in the following order:
  1. ARRIVAL identifier;
  2. TRANSITION identifier;
  3. Runway-in-use;
  4. An assigned level
Example:
<Callsign>cleared to Singapore via PASPU 1A ARRIVAL, VEPLI TRANSITION, Runway 02, maintain / descend to flight level one five zero.
18.3 DEPARTURES
18.3.1 All departing aircraft will be cleared on the appropriate RNAV(GNSS) SID and shall climb initially to 3,000ft.
18.3.2 Operators are to note that RNAV(GNSS)SIDs VENPA 1A and 1B will be assigned to departures from Singapore Changi Airport that flight plan to destinations south of Singapore on L504, M635 and M774.

There will be 3 Transitions as shown below:

ATS RouteTransitionTransition RouteRNAV SID
L504BAVUSVENPA-ATKAX-BAVUSVENPA DEPARTURE
M635SURGAVENPA-VENIX-SURGA
M774KADARVENPA-ATKAX-KADAR
18.3.3 A Transition will be issued by ATC in conjunction with the RNAV(GNSS)SID, for example a departure from Singapore to Brisbane via airway M774 will read as follows:

Example:

<Callsign> cleared to Brisbane via VENPA 1A departure Transition KADAR, airway M774, flight plan route, maintain FL330, squawk alfa 2234 on departure.

18.4 TRANSITION
18.4.1 Aircraft may be radar vectored off a Transition / RNAV SID / RNAV STAR. Such aircraft will subsequently be given an instruction to intercept the appropriate Transition / RNAV SID / RNAV STAR.
18.5 VERTICAL AND SPEED RESTRICTIONS
18.5.1 Pilots shall comply with an ATC assigned level. Pilots shall also adhere to the vertical and speed restrictions depicted on the cleared Transition and RNAV(GNSS)SIDs / STARs. ATC clearance will take precedence when the ATC clearance does not allow the pilots to adhere to the vertical and speed restrictions depicted on the Transition and RNAV(GNSS)SIDs / STARs.
18.6 OPERATORS’ PROCEDURES
18.6.1 The operator shall ensure that in-flight procedures, crew manuals and training programmes are established in accordance with RNAV requirements.
18.6.2 Pilots shall inform ATC when on-board equipment does not meet the requirements of RNAV. Pilots can then expect radar vector from ATC.
19 COORDINATES OF SID/STAR WAYPOINTS (WGS84 DATUM)
NameLatitudeLongitudeRadius/Distance from VTKRadius/DIstance from SJ
ABVIP010008N1035032EVTK R-203.5 / D27.0SJ R-183.5 / D13.2
ADMIM005733N1033033EVTK R-228.4 / D41.2SJ R-232.8 / D26.1
AGROT010108N1035808EVTK R-187.7 / D24.0SJ R-150.8 / D14.0
AGVAR014719N1034145EVTK R-318.8 / D29.8SJ R-344.3 / D35.3
AKMET015355N1034339EVTK R-328.6 / D34.0SJ R-349.3 / D41.3
AKOMA014522N1035443EVTK R-342.0 / D21.4SJ R-006.2 / D32.0
ALFA013033N1034942EVTK R-295.7 / D12.9SJ R-354.8 / D 17.2
ANITO001700S1045200EVTK R-153.4 / D113.4SJ R-146.0 / D108.6
ARAMA013654N1030712EVTK R-282.4 / D55.5SJ R-298.0 / D50.0
AROSO020846N1032421EVTK R-319.9 / D57.4SJ R-334.0/ D61.7
ASUNA005948N1030954EVTK R-244.1 / D57.3SJ R-252.0 / D43.6
ATKAX000512N1065946EVTK R-113.9 /D 195.5SJ R-109.7 / D200.6
ATRUM013256N1040057EVTK R-357.3 / D8.0SJ R-026.1 / D21.8
BAVUS000000N1090000EVTK R-105.9 / D310.5SJ R-103.4 / D317.3
BETBA013302N1035331EVTK R-316.1 / D11.3SJ R-006.3 / D19.8
BIDUS013554N1035755EVTK R-326.0 / D13.2SJ R-006.9 / D22.6
BIKTA024337N1034308EVTK R-346.9 / D80.4SJ R-355.0 / D90.2
BIPOP013122N1041018EVTK R-054.5 / D11.0SJ R-046.8 / D26.2
BOBAG010230N1032954EVTK R-234.7 / D38.6SJ R-243.2 / D24.0
BOKIP010421N1034353EVTK R-220.5 / D27.0SJ R-219.5 / D11.6
BTM010813N1040758EVTK R-158.2 / D17.9SJ R-107.0 / D17.5
DIVSA011105N1040303EVTK R-172.9 / D13.9SJ R-100.8 / D11.9
DOGRA010525N1041423EVTK R-146.2 / D23.5SJ R-108.9 / D24.4
DOKTA012606N1041040EVTK R-083.0 / D9.4SJ R-057.0 / D23.2
DONDI011252N1035855EVTK R-191.3/ D12.3SJ R-093.4 / D7.6
DOSNO004757N1041409EVTK R-160.8 / D39.0SJ R-137.8 / D34.1
DOSPA011459N1040441EVTK R-161.4 / D10.5SJ R-082.9 / D13.5
DOVAN011938N1041249EVTK R-114.6 / D12.7SJ R-073.9 / D22.5
HOSBA011948N1042418EVTK R-102.5 / D23.6SJ R-079.0 / D33.7
IBIBI011503N1035707EVTK R-203.1 / D10.7SJ R-073.4 / D6.0
IBIVA011351N1035637EVTK R-203.1/ D12.0SJ R-084.3 / D5.3
IBIXU011621N1035740EVTK R-203.2 / D9.3SJ R-064.4 / D7.0
IBULA005036N1043600EVTK R-134.5 / D48.7SJ R-116.8 / D50.2
IGNON010847N1041257EVTK R-144.1 / D19.8SJ R-101.8 / D22.2
IKAGO003816N1052931EVTK R-117.7 / D99.8SJ R-109.5 / D104.4
IKIMA004314N1045500EVTK R-127.6 / D67.9SJ R-115.1 / D70.5
JB (JAYBEE)013000N1034242EVTK R-285.1 / D19.3SJ R-332.6 / D18.6
KADAR000647S1074342EVTK R-112.4 / D240.5SJ R-109.0 / D245.8
KARTO011124N1053343EVTK R-098.3 / D93.5SJ R-091.1 / D102.6
KEXAS011019N1044818EVTK R-107.2 / D49.2SJ R-093.0 / D57.2
KILOT030217N1044023EVTK R-022.0 / D104.5SJ R-024.4 / D119.0
LAVAX010950N1042714EVTK R-120.1 / D30.0SJ R-095.5 / D36.2
LEDOX011642N1035651EVTK R-208.6 / D9.4SJ R-058.5 / D6.5
LEGAS011524N1035618EVTK R-207.9 / D10.8SJ R-067.3 / D5.4
LELIB012729N1032450EVTK R-274.0 / D36.6SJ R-298.0 / D30.0
LETGO011411N1035548EVTK R-207.3 / D12.1SJ R-079.1 / D4.6
MABAL032826N1051236EVTK R-030.1 / D142.1SJ R-031.2 / D157.2
MASBO020248N1025251EVTK R-299.0 / D78.3SJ R-310.2 / D76.6
NYLON013657N1040624EVTK R-023.0 / D13.0SJ R-032.9 / D30.0
OBDOS002503N1065551EVTK R-108.9 / D184.5SJ R-104.7 / D190.7
PALGA011059N1034759EVTK R-223.8 / D19.3SJ R-235.1 / D4.1
PAMSI010459N1034845EVTK R-212.3 / D23.6SJ R-197.2 / D8.7
PASPU015915N1040618EVTK R-008.3 / D34.5SJ R-018.3 / D48.1
PIBAP023023N1040618EVTK R-004.4 / D65.3SJ R-011.1 / D78.1
POSUB012725N1040748EVTK R-069.0 / D6.9SJ R-049.8 / D21.7
PU012524N1035600EVTK R-275.2 / D5.4SJ R-021.1 / D13.0
REMES004342N1035735EVTK R-185.2 / D41.2SJ R-167.9 / D30.2
REPOV001623N1040300EVTK R-178.6 / D68.2SJ R-168.3 / D57.9
RUVIK011422N1042033EVTK R-118.8 / D21.9SJ R-088.0 / D29.2
RWY 02C DER012152N1040000EVTK R-203.5 / D3.3SJ R-046.0 / D12.2
RWY 02L DER012305N1035933EVTK R-224.1 / D2.5SJ R-040.6 / D12.8
RWY 20C DER011935N1035902EVTK R-203.3 / D5.8SJ R-051.5 / D10.0
RWY 20R DER012047N1035835EVTK R-213.7 / D4.9SJ R-044.8 / D10.4
SABKA015051N1031713EVTK R-300.4 / D51.2SJ R-317.7 / D50.7
SAMKO010530N1035255EVTK R-203.5 / D21.1SJ R-168.0 / D8.0
SANAT010749N1035930EVTK R-186.1 / D17.1SJ R-123.7 / D9.9
SJ (SINJON)011319N1035120E--
SURGA003657S1063119EVTK R-129.1 / D193.3SJ R-124.6 / D194.3
TOKIM012933N1040315EVTK R-022.7 / D5.0SJ R-036.7 / D20.1
TOMAN012147N1054717EVTK R-091.7 / D106.2SJ R-085.9 / D116.5
TOPOM012955N1040227EVTK R-012.8 / D5.1SJ R-034.2 / D20.0
VENIX002156S1060521EVTK R-130.6 / D163.5 SJ R-125.3 / D164.3
VENPA002141N1044955EVTK R-142.3 / D79.6SJ R-131.2 / D78.1
VEPLI035223N1040542EVTK R-001.7 / D146.8SJ R-005.2 / D158.9
VINIL025500N1040618EVTK R-003.2 / D89.8SJ R-008.5 / D102.3
VMR022318N1035218EVTK R-351.2 / D58.8SJ R-000.9 / D69.6
VTK (TEKONG)012455N1040120E--
20 ARRIVING AIRCRAFT
20.1 The pilot-in-command of an arriving aircraft shall contact the appropriate Approach Control Unit 10 minutes before entering the CTR or ATZ.
21 LIGHT AIRCRAFT OPERATIONS
21.1 Light aircraft operations into and out of Singapore Changi Airport may be approved subject to the following conditions:
  1. Prior permission has been granted;
  2. Aircraft is suitably equipped;
  3. Pilot is appropriately rated;
  4. Subject to ATC.
21.2 Flight notification shall be given by filing a flight plan.
21.3 All such operations will be regulated in accordance with IFR procedures.

WSSS AD 2.23 ADDITIONAL INFORMATION

1 BIRD CONCENTRATION IN THE VICINITY OF THE AIRPORT
1.1 A number of varieties of birds are found in Singapore throughout the year. The larger birds commonly found in Singapore Changi Airport include the following:
-cattle egrets(weighing approximately 300g each)
-grey herons(weighing approximately 500g each)
-brahminy kites(weighing approximately 600g each)
1.2 There could be an increase in bird activities during the migratory months of September to April. During this period, migratory birds may use the airport as their feeding ground. Handheld laser device, long range acoustic device and alternating amplified bird cries of distress are used for bird dispersal within Singapore Changi Airport.

WSSS AD 2.24 CHARTS RELATED TO AN AERODROME

Location of RWY 02R/20L in relation to RWY 02L/20/R and RWY 02C/20C
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Aerodrome Chart - ICAO
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Aerodrome Advisory Chart - ICAO
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Aerodrome Obstacle Chart - ICAO - TYPE A - RWY 02L/20R
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Aerodrome Obstacle Chart - ICAO - TYPE A - RWY 02C/20C
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Aerodrome Obstacle Chart - ICAO - TYPE B
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Precision Approach Terrain Chart - ICAO - RWY 02L
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Precision Approach Terrain Chart - ICAO - RWY 20C
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RNAV(GNSS) SIDs and STARs - Introduction

RNAV (GNSS) SID - RWY 02L/20R - ANITO 6E/ANITO 5F
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RNAV(GNSS) SID - RWY 02C/20C - ANITO 6A / ANITO 5B
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RNAV(GNSS) SID - RWY 02L/20R - ADMIM 1E / ADMIM 1F
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RNAV (GNSS) SID - RWY 02C/20C - ADMIM 1A / ADMIM 1B
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RNAV (GNSS) SID - RWY 02L/20R - TOMAN 2E / TOMAN 2F
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RNAV (GNSS) SID - RWY 02C/20C - TOMAN 2A / TOMAN 2B
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RNAV (GNSS) SID - RWY 02L/20R - BAVUS 1E / BAVUS 1F
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RNAV (GNSS) SID - RWY 02C/20C - BAVUS 1A / BAVUS 1B
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RNAV (GNSS) SID - RWY 02L/20R - AROSO 2E / AROSO 2F
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RNAV (GNSS) SID - RWY 02L/20R - MASBO 2E / MASBO 2F
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RNAV (GNSS) SID - RWY 02C/20C - AROSO 2A / AROSO 2B
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RNAV (GNSS) SID - RWY 02C/20C - MASBO 2A / MASBO 2B
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RNAV (GNSS) SID - RWY 02L/20R - MERSING 5E / MERSING 6F
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RNAV (GNSS) SID - RWY 02C/20C - MERSING 5A / MERSING 6B
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RNAV (GNSS) SID - RWY 02C/20C - VENIX 1A / VENIX 1B
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RNAV (GNSS) SID - RWY 02L/20R - VENIX 1E / VENIX 1F
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RNAV (GNSS) SID - RWY 02C/20C - KADAR 1A / KADAR 1B
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RNAV (GNSS) SID - RWY 02L/20R - KADAR 1E / KADAR 1F
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RNAV(GNSS) STAR - RWY 02L/02C - ARAMA 1A
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RNAV(GNSS) STAR - RWY 02L/02C - ASUNA 1A
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RNAV(GNSS) STAR - RWY 20R/20C - ARAMA 1B
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RNAV(GNSS) STAR - RWY 20R/20C - ASUNA 1B
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RNAV(GNSS) STAR - RWY 02L/02C - KARTO 1A
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RNAV(GNSS) STAR - RWY 02L/02C - OBDOS 1A
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RNAV(GNSS) STAR - RWY 20R/20C - KARTO 1B
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RNAV(GNSS) STAR - RWY 20R/20C - OBDOS 1B
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RNAV(GNSS) STAR - RWY 20R/20C - LELIB 3B
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RNAV(GNSS) STAR - RWY 02L/02C - BIKTA 1A
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RNAV(GNSS) STAR - RWY 02L/02C - MABAL 1A
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RNAV(GNSS) STAR - RWY 20R/20C - BIKTA 1B
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RNAV(GNSS) STAR - RWY 20R/20C - MABAL 1B
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RNAV(GNSS) STAR - RWY 02L - LEBAR 2A
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RNAV(GNSS) STAR - RWY 02L - LEBAR 2B
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RNAV(GNSS) STAR - RWY 02L/02C - REPOV 1A
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RNAV(GNSS) STAR - RWY 02L/02C - SURGA 1A
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RNAV(GNSS) STAR - RWY 20R/20C - REPOV 1B
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RNAV(GNSS) STAR - RWY 20R/20C - SURGA 1B
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RNAV(GNSS) STAR - RWY 02L/02C - VEPLI 1A
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RNAV(GNSS) STAR - RWY 20R/20C - VEPLI 1B
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Instrument Approach Chart - ICAO - RWY 02L - ICW ILS/DME
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Instrument Approach Chart - ICAO - RWY 02C - ICE ILS/DME
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Instrument Approach Chart - ICAO - RWY 20R - ICH ILS/DME
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Instrument Approach Chart - ICAO - RWY 20C - ICC ILS/DME
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Instrument Approach Chart - ICAO - RWY 20C - VTK DVOR/DME
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Instrument Approach Chart - ICAO - RWY 02L - RNAV(GNSS)
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Instrument Approach Chart - ICAO - RWY 02C - RNAV(GNSS)
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Instrument Approach Chart - ICAO - RWY 20R - RNAV(GNSS)
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Instrument Approach Chart - ICAO - RWY 20C - RNAV(GNSS)
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Visual Approach Chart - ICAO
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