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General Information

Location: SINGAPORE SGPICAO/IATA: WSSS / SINLat/Long: N01° 21.55', E103° 59.36'Elevation: 22 ft

Airport Use: PublicDaylight Savings: Not ObservedUTC Conversion: -8:00 = UTCMagnetic Variation: 0.0° E

Fuel Types: Jet A-1Repair Types: Major Airframe, Major EngineCustoms: YesAirport Type: IFRLanding Fee: NoControl Tower: YesJet Start Unit: NoLLWS Alert: YesBeacon: Yes

Sunrise: 2315 ZSunset: 1118 Z

Runway Information

Runway: 02CLength x Width: 13123 ft x 197 ftSurface Type: bituTDZ-Elev: 15 ftLighting: Edge, ALS, Centerline, REILStopway: 197 ft

Runway: 20CLength x Width: 13123 ft x 197 ftSurface Type: bituTDZ-Elev: 15 ftLighting: Edge, ALS, Centerline, REIL, TDZStopway: 197 ft

Runway: 20RLength x Width: 13123 ft x 197 ftSurface Type: bituTDZ-Elev: 14 ftLighting: Edge, ALS, Centerline, REILDisplaced Threshold: 2428 ftStopway: 197 ft

Runway: 02LLength x Width: 13123 ft x 197 ftSurface Type: bitu

TDZ-Elev: 22 ftLighting: Edge, ALS, Centerline, REIL, TDZStopway: 197 ft

Communication Information

ATIS: 128.600Singapore Tower: 118.600Singapore Tower: 118.250Singapore Ground: 121.850Singapore Ground: 122.550Singapore Ground: 124.300Singapore Ground: 125.650Singapore Ground: 129.950Singapore Ground: 121.725Changi Ramp/Taxi: 121.900Singapore Clearance Delivery: 121.650Singapore Approach: 120.300Singapore Approach: 124.600 SecondarySingapore Arrival: 119.300Singapore Radar: 135.800 Secondary Remote Communications Air-GroundSingapore Radio: 1139.600 Remote Communications Air-GroundSingapore Radar: 127.300 Secondary Remote Communications Air-GroundSingapore Radio: 565.500 Remote Communications Air-GroundSingapore Radio: 655.600 Remote Communications Air-GroundSingapore Radio: 894.200 Remote Communications Air-GroundSingapore Radio: 1129.700 Remote Communications Air-GroundSingapore Radar: 134.400 Remote Communications Air-GroundSingapore Radar: 134.200 Remote Communications Air-GroundSingapore Radar: 133.800 Remote Communications Air-GroundSingapore Radar: 123.700 Remote Communications Air-GroundSingapore Radar: 124.050 Remote Communications Air-GroundSingapore Radar: 133.350 Secondary Remote Communications Air-GroundSingapore Radar: 133.250 Remote Communications Air-GroundSingapore Radar: 128.100 Secondary Remote Communications Air-Ground

General Information





Runway Information





Airport Information For WSSSPrinted on 27 Jan 2018(c) JEPPESEN SANDERSON, INC., 2018, ALL RIGHTS RESERVED

jep=JEPPESEN

JeppView for Windows

General Information





Runway Information











Airport Information For WSSSPrinted on 27 Jan 2018(c) JEPPESEN SANDERSON, INC., 2018, ALL RIGHTS RESERVED

jep=JEPPESEN


WSSS/SIN10-1P

JEPPESEN

CHANGI 29 JUL 16SINGAPORE, SINGAPORE

FLIGHT AND GROUND PROCEDURES1. LOW VISIBILITY PROCEDURES (LVP) FOR CATEGORY II ILS OPERATIONS

1.1 INTRODUCTION1.1.1 Category II ILS approaches will be made available at Singapore Changi

1.2 AUTHORIZATION FOR CATEGORY II ILS APPROACHES 1.2.1 Operators who wish to conduct Category II ILS operations at Singapore

1.3 CATEGORY II ILS RUNWAYS1.3.1 At Singapore Changi Airport, Category II ILS approaches are available only

on RWY 02L and RWY 20C, which are also equipped with precision approachCategory II lighting system. When required, pilots making Category II ILSapproaches to Singapore Changi Airport should refer to the procedures in

1.4 INITIATION OF CATEGORY II ILS OPERATIONS1.4.1 Preparations will be made to implement LVP for Category II ILS operations

at Singapore Changi Airport during prolonged period of low visibility,

1.4.2 Availability of the Category II ILS approaches will be made known throughNOTAM and ATIS broadcasts as well as air traffic control radiocommunications.

1.4.3 During LVP operations, aircraft will not be cleared for Category II ILS

II requirements. Aircraft will not be cleared for landing if the Touchdown Zone RVR is unserviceable.

1.5 ILS SENSITIVE AREAS1.5.1 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 centerlines of Rapid ExitTaxiways and Cross Taxiways.

1.6 TERMINATION OF LVP FOR CATEGORY II ILS OPERATIONS1.6.1 LVP for Category II ILS operations will be terminated when RVR has

well as air traffic control radio communications.operations will be made known through NOTAM and ATIS broadcasts as

2.1 RUNWAY-IN-USE2.1.1 The runway-in-use (Departure/Arrival) is selected by Aerodrome Control

as the optimum for general purposes and to maximize runway utilization.

approach if any of the ILS or approach/runway lights fall below Category

If the assigned runway is unsuitable for a particular operation, the pilotcan obtain permission from ATC to use another runway but shouldanticipate delay.

except during thunderstorms, when the RVR drops below 2625' (800m).

improved above 2625' (800m). Termination of LVP for Category II ILS

Airport to authorized flights during prolonged periods of low visibility,

2. RUNWAY UTILIZATION

informed, ATC will be able to make changes in the departure sequence,

| JEPPESEN, 2011, 2016. ALL RIGHTS RESERVED.

except during thunderstorms. RVR minima for Cat II ILS operations is

on the airfield.limited to 1148' (350m) due to Rwy and Twy light spacing requirements

Text.

2.2.1 Pilots should arrange their taxi such that they are ready to depart withoutdelay on reaching the runway holding point. As standard ICAO waketurbulence separation is being applied, pilots are to advise ATC early ifmore time is needed for the aircraft to be ready for departure. When

if necessary, to minimize delays to other succeeding departures.

the Instrument Approach Charts and the Precision Approach Terrain Chartsfor RWY 02L and RWY 20C.

Changi Airport must have obtained operational approval from the relevant State of Operator and be authorized by the Civil Aviation Authorityof Singapore.

1.7 OPERATIONS OF FLIGHTS NOT AUTHORIZED FOR CATEGORY II ILS OPERATIONS

flights not authorized for Category II ILS operations may continue to makeapproaches and land. Airlines planning to operate flights not authorizedfor Category II ILS operations into Changi shall monitor the METARto ascertain the RVR values when launching their flights and be prepared

2.2 DEPARTURES

1.7.1 During Category II ILS operations, if the RVR is 1804' (550m) or above,

to divert if the RVR is below 1804' (550m).

CHANGES:

.AIRPORT.BRIEFING.

Printed from JeppView for Windows 5.3.0.0 on 27 Jan 2018; Terminal chart data cycle 01-2018 (Expired); Notice: After 25 Jan 2018, 0000Z, this chart may no longer be valid

WSSS/SIN10-1P1

JEPPESEN

CHANGI 29 JUL 16SINGAPORE, SINGAPORE

2.3 CLEARANCE FOR IMMEDIATE TAKE-OFF2.3.1 A pilot receiving the ATC instruction 'cleared for immediate take-off' is

required to act as follows:(a) if waiting clear of the runway, taxi immediately on to it and begin

take-off run immediately without stopping the aircraft;(b) if already lined-up on the runway, take-off without delay;(c) if unable to comply with the instruction, inform ATC immediately.

2.5 LAND AFTER PROCEDURES2.5.1 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 landbefore the first aircraft has cleared the runway-in-use provided:(a) the runway is long enough;(b) during daylight hours;(c) the second aircraft will be able to see the first aircraft clearly and

continuously until it is clear of the runway;(d) 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 inconditions shown as follows:(a) When the runway-in-use is temporarily occupied by other traffic,

landing clearance may be issued to an arriving aircraft provided thatat the time the aircraft crosses the threshold of the runway-in-use

2.4 ARRIVALS - MINIMUM RUNWAY OCCUPANCY TIME2.4.1 Arriving aircraft upon landing are reminded that it is imperative to vacate

the runway as quickly as practicable to enable ATC to apply minimum

2.4.5 Between 0830 - 1030 daily estimated delays of 15 minutes can be expectedfor arrivals into Changi Airport.


spacing on final approach and minimize the occurrence of "go-arounds".

2.2.2 Pilots should complete cockpit checks prior to line-up for departureand 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 taxiinto position promptly without delay. Unless given instruction to line-up and wait, pilots should be ready and prepared tp depart without stopping. Onreceipt of take-off clearance, pilots to commence take-off roll without delay.

2.4.2 To ensure minimum Runway Occupancy Time (ROT) and reduce missedapproaches due to occupied runway, pilots should vacate the runway via thefirst available exit taxiway corresponding to operational requirements,or as instructed by ATC. If an exit taxiway other than the first available

contact.exit taxiway is required, pilots shall advise the Tower Controller on first

2.4.3 To enhance planning, pilots can make reference to the Landing ExitDistance (LED), the distance from threshold to the furthest edge of the exittaxiway:

RWY TWY Exits LED

1948m,6391'

5423' 1655m,

9436' 2876m

3267m

6965' 2123m,

2391m,7844'

8173' 2491m,

2565m,8415'

3061m

3152m

6450' 1966m,

2055m,6742'

10,043'

10,341'

10,719'

12 12

21 12

21 12

21 12

1 2Recommended exit taxiways. Rapid Exit Taxiway (RET) and maximum design groundspeed for the exit taxiway is 50 KT.

2.4.4 Pilots can expect initial taxi instructions from the Runway Controller

should not stop on the exit taxiway until the entire aircraft has passed therunway holding point.

2

2

before clearing the exit taxiway. Aircraft vacating the runway-in-use

Rwy 20L/02R information removed.CHANGES:

20R

20C

02L

02C

W6, W7, W8

E6, E7, E8

W5,

E5,

W4, W3

E4, E3

.AIRPORT.BRIEFING.


WSSS/SIN10-1P2

JEPPESEN

CHANGI 22 SEP 17SINGAPORE, SINGAPORE

3.1 In VMC during daylight hours, if total radio communication failure occurs to an aircraft bound for Singapore Changi Airport, the pilot shall maintain VMC to land at the most suitable airfield and report to the appropriate air trafficcontrol unit by the most expeditious means.

shall:3.2 For IFR flights to Singapore Changi Airport, aircraft experiencing radio failure

Singapore ATC, or3.2.1 Proceed according to the last acknowledged clearance received from

Singapore ATC:3.2.2 If no specific instructions or clearance has been received from

b) Commence descent from SHA at or as close as possible to the ETA as

land on Rwy 02L/02C.

indicated on the flight plan.c) Carry out the appropriate instrument approach procedure from SHA to

3.2.3 If unable to effect a landing on:a) Rwy 02L

Carry out missed approach procedure to AKOMA (PU R-356/20DME). Leave AKOMA at 4,000' to NYLON Holding Area (NHA) and execute the appropriate instrument procedure from NHA to land on Rwy 20R or Rwy 20C, as appropriate.

b) Rwy 02CCarry out missed approach procedure to NYLON Holding Area (NHA) and execute the appropriate instrument procedure from NHA to land on Rwy 20R or Rwy 20C, as appropriate.

c) Rwy 20RCarry out missed approach procedure to SAMKO Holding Area (SHA) and execute the appropriate instrument procedure from SHA to land on Rwy 02L or Rwy 02C, as appropriate.

ARRIVALS3. TOTAL RADIO FAILURE - SPECIAL PROCEDURES - SINGAPORE CHANGI AP -


the following separation distances will exist:i) Landing following landing - The preceding landing aircraft will be

ii) Landing following departure - The departing aircraft will be

2.6.2 These procedures will be used only under the following conditions:(a) during daylight hours;(b) visibility of at least 5km;(c) cloud ceiling of 1,500ft in the departure/missed approach area;

be able to observe continuously the relevant traffic;(d) ATC is satisfied that the pilot of the next arriving aircraft will

tailwind, windshear, turbulence, etc);(e) no unfavourable surface wind conditions (including significant

no evidence that the braking action may be adversely affected.(f) when the runway is dry and free of all precipitants such that there is

2.7 PHRASEOLOGY2.7.1 When issuing a landing clearance following the application of these

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

instructions:procedures, ATC will issue the second aircraft with the following

the threshold of the runway-in-use.clear of the runway-in-use or will be at least 8202' (2500m) from

airborne and at least 8202' (2500m) from the threshold of the

from the threshold of the runway-in-use.runway-in-use, or if not airborne, will be at least 8202' (2500m)

a) Maintain the last assigned altitude or flight level and proceed via airway thereafter the appropriate STAR for Rwy 02L/02C to SAMKO Holding Area(SHA) except for the following STARS: KARTO 1A, MABAL 2A and ELALO 1Ashall proceed to SHA after SANAT.

STAR BELVA 1A removed (paragraph 3.2.2a).CHANGES:

.AIRPORT.BRIEFING.


WSSS/SIN10-1P3

JEPPESEN

CHANGI 22 SEP 17SINGAPORE, SINGAPORE

a) Proceed straight ahead to NYLON Holding Area (NHA) climbing to the last assigned altitude. At NHA, climb/descend to maintain 7,000'.

b) Hold at NHA for 4 minutes and leave NHA on track 203^. At 10 DME north of VTK, turn left for HOSBA Holding Area (HHA) to jettison fuel,maintaining 7,000'.

c) After fuel jettison, proceed to SAMKO Holding Area (SHA) via AWY G580 and SINJON DVOR. Maintain 7,000'. At SHA descend for an instrument approach on Rwy 02L/02C. Identify the runway-in-use in accordance with

a) Proceed straight ahead to SAMKO Holding Area (SHA) climbing to the last assigned altitude. At SHA climb/descend to maintain 7,000'.

5.3 When radio communication failure occurs immediately after the aircraft has departed on Rwy 20R/20C, the pilot shall proceed according to the following procedures:

c) After fuel jettison, proceed to NHA via Airway W401. Maintain 7,000'. On crossing VTK 042R turn right to intercept VTK 023R. At NHA descend to carry out an instrument approach on Rwy 20R/20C.

5.4 ATC action is based on the assumption that the aircraft will take a minimum of 10 min to jettison fuel. An aircraft therefore should not leave earlier than 10 min after arrival at HOSBA Holding Area even if fuel jettison is completed at a shorter time of if jettisoning is not necessary or possible unless circumstances require an immediate return.

5.5 Alternatively, aircraft may jettison fuel between HOSBA and point 90 NM from SJ DVOR/DME on airway G580.

5.2 When radio communication failure occurs immediately after the aircraft has departed on Rwy 02L/02C, the pilot shall proceed according to the following procedures:

b) Hold at SHA for 4 minutes. Leave SHA for HOSBA Holding Area (HHA) via SJ DVOR and Airway G580 to jettison fuel, maintaining 7,000'.

Based Navigation Manual (Doc 9613).


d) Rwy 20CCarry out missed approach procedure to EXOMO (VTK R-158/22DME). Leave EXOMO at 4,000' to SAMKO Holding Area (SHA) and execute the appropriate instrument procedure from SHA to land on Rwy 02L or Rwy 02C, as appropriate.

4. IDENTIFICATION OF RUNWAY-IN-USE

4.1 ATC will switch on the appropriate approach lights and the ILS serving the runway-in-use to assist the pilot in its identification. If the approach lights for the runway-in-use are sighted but the ILS frequency is not received, the pilot shall assume that the ILS is inoperative and shall proceed to land on the runway on which the approach lights have been sighted.

4.2 If unable to land within 30 minutes of EAT or ETA, if no EAT has been received

5. TOTAL RADIO FAILURE - SPECIAL PROCEDURES - SINGAPORE CHANGI AP - DEPARTURES

5.1 When an aircraft which has been cleared by ATC to an intermediate level experiences total radio communication failure immediately after departure from Singapore Changi Airport and it is deemed unsafe for it to continue to its destination, the pilot will set the aircraft transponder to Mode A/C Code 7600 and adhere to the procedures below.

and acknowledged, proceed to cross SAMKO Holding Area (SHA) at 4,000' then

FL 290 if Soekarno-Hatta is the nominated alternate or otherwise proceed at via A457 at FL200 if Kuala Lumpur is the nominated alternate or via B470 at

the planned flight level to other nominated alternate.

paragraph 4.

6.1 The SIDs and STARs for Singapore Changi Airport require aircraft to beGNSS-equipped and approved with navigation systems that meet theICAO RNAV-1 navigation specification in accordance to the ICAO Performance

6. SID/STAR OPERATIONS

SID/STAR operations.CHANGES:

.AIRPORT.BRIEFING.


WSSS/SIN

CHANGES:

10 FEB 17

JEPPESEN

TSAT displayed on ADGS may not be final and can be revised due to en-route clearance restrictions, ground congestion or flow measures.

will be maintained.

ATC clearance and TSAT will be cancelled. Pilot must notify the AO/GHA to update

in the pre-departure sequence. Delay can be expected as a result of re-sequencing based on new TOBT input.

can expect start-up/pushback approval.

at TOBT. Any updates to TOBT after receipt of ATC clearance will result incancellation of clearance issued as the ATC clearance validity is based onthe initial TOBT.

to maximise apron and runway capacity and reduce the overall delay to trafficas and when required.

should not expect an earlier departure time as the planned pre-departure sequence before the assigned time will be allowed to do so subject to traffic. However, the flight

10-1P4

7.1.2 Target Start Up Approval Time (TSAT) - The time provided by ATC that an aircraft

updating the TOBT. Notify the AO/GHA to update the TOBT if it is expected todiffer by 5 minutes or more.

7.2.1 Pilot shall ensure aircraft is ready for pushback at TOBT.

7.2.2 Pilot to maintain communication with the AO/GHA as they are responsible for

7.2.3 Pilot to contact Clearance Delivery and request for ATC clearance within 5 minutes

7.2.3.1 Pilot shall only request for ATC clearance provided aircraft is ready to pushback

7.2.5 ATC will update TSAT changes if any, during issuance of ATC clearances. Note that

7.2.6.1 ATC may swap pushback sequence based on real-time readiness of aircrafts

7.2.7 A flight issued with gate hold (TSAT TOBT) but chooses to commence pushback

7.2.8 If a flight is unable to pushback by TSAT + 5 minutes due to the aircraft being unready,

7.2.9 Non-compliance of initial TSAT may result in an aircraft losing its existing position

7.2.10 If delay in pusback is due to ground traffic movement or ATC clearance restrictions,

operation and usage of ADGS still remain the same for flight crew. Additionalinformation which includes TOBT, TSATand TOBT count-down timer will bedisplayed in local times as part of the improvements to support A-CDM operations.

7.3.1 All contact stands in Singapore Changi Airport will have ADGS. The fundamental

7.1.1 Target Off Block Time (TOBT) - The time an aircraft operator (AO) or ground handlingagent (GHA) estimates that an aircraft will be ready, all doors closed, boarding bridge

receipt of clearance from ATC.removed, pushback vehicle available and ready to start-up/pushback immediately upon


of TOBT using following phraseology:

- Callsign- Destination

- Parking position- Proposed flight level and alternate level if any

7.2.6.2 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-offas distances between aircraft stands and the departure rwy vary.

the TOBT for a new TSAT before requesting for a new ATC clearance. This also appliesto aircraft returning back to blocks after pushback.

before requesting for new clearence'.'(Callsign of acft) your ATC clearence and TSAT is cancelled (reason). Update TOBT

7.2.8.2 Flight may also have its ATC clearence cancelled if it develops a technical problemafter pushback and is unable to taxi for prolonged duration.

the ATC clearance will remain valid even if it exceeds TSAT + 5 minutes. TOBT neednot be updated for such situations.

7.2.4 ATC will advise the pilot whether the proposed or other alternate flight level is

with an adjacent unit or centre is required the pilot will be instructed to standby.available and an ATC clearence will be issued accordingly. If pre-departure coordination

TSAT after obtaining ATC clearance, or as directed by ATC.7.2.6 Pilot shall request for pushback from Ground Movement Control within 5 minutes of

7.2.11 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

(see 7.4).operator and a NOTAM will be issued by ATC. Pilot shall follow the non-CDM procedure

7.2.8.1 ATC will inform the aircraft when a clearence is cancelled using the phraseology:

Notes updated.

CHANGISINGAPORE, SINGAPORE

Definition of commonly used terms in A-CDM

7.1 Introduction

7. AIRPORT COLLABORATIVE DECISION MAKING (A-CDM) - SINGAPORE CHANGI AIRPORT

7.2 A-CDM start-up procedures

7.3 A-CDM information via Aircraft Docking Guidance System (ADGS)


WSSS/SIN

CHANGES:

10 FEB 17

JEPPESEN

- Airport Operations Centre System (AOCS) A-CDM web based portal; or

- AOCS A-CDM portal;- GMID;- ADGS at contact stands;- Radio communication with GHA or AO;- ATC - Upon issuance of ATC clearance (for flights parked at aircraft stands

without ADGS);

Aircraft arrival to stand

No change in existing functionality and display.

Description Display on ADGS

40 minutes prior to TOBT

ADGS will display TOBTsubmitted by AO/GHA anda count down timer (2 digits)to TOBT in minutes.

Timing displayed will be inLocal Time (LT).

TOBT timings will changeinstantly if there is an update done by AO/GHA.

As ADGS can only displayup to 7 characters per line, the displayed message willbe scrolling.

Snapshot 1 Snapshot 2

Snapshot 3

- Gate Message Input Display (GMID) at boarding rooms;

7.4.1 To non-CDM procedures are applicable for non-scheduled flights departing Changi Airport

due to system issues or maintenance.or when TOBT and TSAT references used in A-CDM mode of operations become unavailable

7.4.2 If TOBT cannot be submitted or it is unavailable through different channels:

a. Pilots shall notify ATC when the aircraft is ready to pushback within 5 minutes.

b. ATC will advise the pilot whether the proposed or alternate flight level is available and

adjacent unit or centre is requirded the pilot will be instructed to standby. an ATC clearence will be issued accordingly. If pre-departure coordination with an

c. 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 the5 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.

d. 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.

7.4.3 If TSAT is unavailable through different means stated below:

a. AO and GHA shall continue to submit TOBT and pilots shall request for ATC clearance

5 minutes within TOBT (see 7.2.3). b. ATC will revert to the gate hold procedures published on 10-9E chart and issue estimated

pushback times accordingly.

Non-CDM mode ops added. | JEPPESEN, 2016, 2017. ALL RIGHTS RESERVED.

B773

TOBT101

30

RG123 RG123

OBT1015

30

RG123

T1015LT

30


10-1P5

AIRCRAFT DOCKING GUIDANCE SYSTEM (ADGS)

7.4. Non-CDM mode of operations


WSSS/SIN

CHANGES:

JEPPESEN

| JEPPESEN, 2016. ALL RIGHTS RESERVED.

Description Display on ADGS


Snapshot 3


Snapshot 3

25 minutes prior to TOBT

Aircraft departure from stand

As ADGS can only displayup to 7 characters per line,the displayed message willbe scrolling.

ADGS will display TSATderived by PDS.

TSAT timings may change asthe PDS is continuoslyoptimising push back timesbased on real time trafficconditions.

ADGS will display the actualoff-block time (AOBT).

As ADGS can only displayup to 7 characters per line,the displayed message willbe scrolling.

TOBT, TSAT and TOBTcountdown timer will beremoved.

AOBT display will be removed3 minutes after AOBT.

7 APR 17

None.

AOBT101

RG123 RG123

BT1018L

RG123

TOBT101

25

RG123 RG123

BT1015L

25

RG123

25

TSAT101 AT1017L

1015LT1017LT

1018LT


10-1P6

AIRCRAFT DOCKING GUIDANCE SYSTEM (ADGS)


WSSS/SIN SINGAPORE, SINGAPORECHANGI

JEPPESEN

1. Introduction

CHANGES:

7 APR 17

SIMULTANEOUS INDEPENDENT PARALLEL APPROACHES

2.1 To ensure safe operations between aircraft on parallel approaches, Normal

Operating Zones (NOZs) are established for each extended runway centerline

and a No Transgression Zone (NTZ) is established between the NOZs.

2.2 ATC will vector arriving flights into Singapore Changi Airport from the final

waypoint of the respective STARs to the respective NOZs.

or 3NM surveillance separation between pairs of aircraft until both aircraft

are established on the ILS Localizer course.

2.4 ATC is not required to provide separation between aircraft on adjacent ILSLocalizers and will monitor aircraft for deviation from the approach path.

2.5 Aircraft can expect to maintain altitude 3500' till Glide Path Interception

2.3 Within the NOZ, ATC shall provide a minimum vertical separation of 1000'

for Runway 20R / 02L and 2500' till Glide Path Interception for

Runway 20C / 02C. This is to ensure the necessary vertical separation prior

to establishing on the respective ILS Localizer course.

2.6 Aircraft can expect the following radiotelephony phraseology when

intercepting the ILS:

a. to intercept the Localizer before clearing for ILS

followed by ...

"MAINTAIN (altitude), CLEARED FOR ILS APPROACH RUNWAY (number)

LEFT (CENTER / RIGHT)"

or

"TURN LEFT (RIGHT) HEADING (three digits) MAINTAIN (altitude)

b. to intercept ILS

2.7 Aircraft can expect to maintain speed 180KT at base turn or earlier till 8NMfrom touchdown.

3. Break-out maneuver

3.1 When an aircraft is observed to have not established on the appropriate

2. Procedures for simultaneous independent parallel approaches

Localizer course or deviated from its course towards the NTZ, ATC will

instruct the aircraft to return immediately to the correct Localizer course

with the following radiotelephony phraseology:

"YOU HAVE CROSSED THE LOCALIZER, TURN LEFT (or RIGHT)IMMEDIATELY AND RETURN TO THE LOCALIZER"

or

"TURN LEFT (or RIGHT) TO RETURN TO LOCALIZER COURSE"

3.2 When ATC observed aircraft to be penetrating or will penetrate the NTZ,

ATC will instruct the aircraft on the adjacent Localizer course to alter course

to avoid the deviating aircraft with the following radiotelephony phraseology:

"TRAFFIC ALERT, TURN LEFT (or RIGHT) IMMEDIATELY HEADING

4. Pilot notification and conditions for operations

4.1 Simultaneous approaches to parallel runways operation will be broadcasted

1.1 Simultaneous independent parallel approaches will be implemented daily between

0000UTC and 1500UTC to optimize runway utilization and enhance air traffic

efficiency.

"TURN LEFT (RIGHT) HEADING (three digits) MAINTAIN (altitude) REPORT

ESTABLISHED ON THE LOCALIZER RUNWAY (number) LEFT (CENTER / RIGHT)"

CLEARED FOR ILS APPROACH RUNWAY (number) LEFT (CENTER / RIGHT)"

on ATIS during the active period.

4.2 Simultaneous approaches to the parallel runways will be suspended in the event of

adverse weather or any other conditions that may affect the safe conduct of such

approaches to the parallel runways.

(degrees), CLIMB AND MAINTAIN (altitude)"

New chart. | JEPPESEN, 2017. ALL RIGHTS RESERVED.

10-1P7


COMMSLOST COMMSLOST COMMSLOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS LOSTCOMMS LOSTLOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

BATAM

Hang N

adim

WID

D

SIN

GAPORE

Paya L

ebar

WSAP

SIN

GAPORE

Sele

tar

WSSL

01-00

01-30

103-00

103-30

104-00

22

20

27

34

24

3500

RPA

10000

6000

4000

Cha

ngi

EAST

Rw

y 02

R/20

Lis

sol

ely

for

use

by t

heRe

publ

ic o

f Si

ngap

ore

Air

For

ce (

RSA

F) A

ircr

aft

1A

RA

MA

262^

082^

BO

BA

G

147^

BO

KIP

082^

168^

348^SA

MKO

MA

X 2

20 K

TM

AX F

L180

MHA

600

0

MA

X 2

20 K

TM

AX F

L140

MHA

400

0

1

CHANGES: | JEPPESEN, 2017. ALL RIGHTS RESERVED.

WSSS/SINCHANGI

SINGAPORE, SINGAPORE.RNAV.STAR.

JEPPESEN

10-25 MAY 17

1.

RA

DA

R r

equir

ed.

D-A

TIS

128.

6A

pt E

lev

2.

RNA

V 1

navig

ati

on s

pecif

icati

on G

NSS r

equir

ed.

(RWYS 02

L/C)

RNAV (GNSS) ARR

IVAL

Alt

Set

: hP

a T

rans

lev

el:

FL13

0

and

proc

eed

on A

RAM

A 1

A t

o SA

MKO

.

2. W

hen

clea

red

via

ARA

MA

1A

by

Sing

apor

e A

TC:

1. S

et t

rans

pond

er t

o M

ode

A/C

cod

e 76

00.

appr

opri

ate

land

ing

proc

edur

e fo

r Rw

y 02

as

clos

e as

pos

sibl

e to

EA

T or

ETA

.

Spec

ial

Proc

edur

es f

or m

isse

d ap

proa

ch p

roce

dure

.

b. F

rom

SA

MKO

com

men

ce d

esce

nt a

nd c

arry

out

c. I

f un

able

to

effe

ct a

lan

ding

, re

fer

to S

inga

pore

3. N

o cl

eara

nce

or i

nstr

ucti

on r

ecei

ved

from

Si

ngap

ore

ATC

:

a. M

AIN

TAIN

las

t as

sign

ed f

ligh

t le

vel

or a

ltit

ude

Refe

r to

10-

1P p

ages

for

rad

io c

omm

unic

atio

nsfa

ilur

e pr

oced

ure.

New format.

RO

UTIN

G

From

ARA

MA

, sp

eed

250

KT.

To

BO

BA

G a

t or

abo

ve 1

0000

,

SAM

KO

at

or a

bove

400

0, s

peed

190

KT.

spee

d 22

0 KT,

tur

n LE

FT.

To B

OKIP

at

or a

bove

600

0. T

o

22

1020

3040

500

515

2535

455

2347

41

14

9

ARA

MA 1

A [ARA

M1A

]

EXPE

CT

RAD

AR

appr

oach

Rw

y 02

vect

ors

for

ILS

At

250 K

T

At

220 K

T

At

190 K

T

CO

NTO

UR

INTE

RVA

LS

4000

2000


113.

5 SJ

SIN

JON

SJD

COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

LOST

COMMS COMMSLOST COMMSLOST LOST

COMMS LOSTCOMMS LOSTCOMMS LOST

COMMS

LOST

COMMS

LOST

LOST

COMMS

LOST

COMMS

COMMS

BATAM

Hang N

adim

WID

D

JOHOR B

AHRU

Senai In

tlW

MKJ

SIN

GAPORE

Paya L

ebar

WSAP

SIN

GAPORE

Sele

tar

WSSL

01-00

01-30

103-00

103-30

104-00

22

27

34

24

3500

R AP

10000

7000

4000

3000

2. W

hen

clea

red

via

ARA

MA

1B b

y Si

ngap

ore

ATC

:1.

Set

tra

nspo

nder

to

Mod

e A

/C c

ode

7600

.

appr

opri

ate

land

ing

proc

edur

e fo

r Rw

y 20

as

clos

e as

pos

sibl

e to

EA

T or

ETA

.

Spec

ial

Proc

edur

es f

or m

isse

d ap

proa

ch p

roce

dure

.

b. F

rom

NYLO

N c

omm

ence

des

cent

and

car

ry o

ut

c. I

f un

able

to

effe

ct a

lan

ding

, re

fer

to S

inga

pore

3. N

o cl

eara

nce

or i

nstr

ucti

on r

ecei

ved

from

Si

ngap

ore

ATC

:

and

proc

eed

on A

RAM

A 1

B t

o BIP

OP,

the

n di

rect

to

NYLO

N.

Cha

ngi

EAST

Rw

y 02

R/20

Lis

sol

ely

for

use

by t

heRe

publ

ic o

f Si

ngap

ore

Air

For

ce (

RSA

F) A

ircr

aft

1

a. M

AIN

TAIN

las

t as

sign

ed f

ligh

t le

vel

or a

ltit

ude

Refe

r to

10-

1P p

ages

for

rad

io c

omm

unic

atio

nsfa

ilur

e pr

oced

ure.

ARA

MA

MA

X 2

20 K

TM

AX F

L180

MHA

600

0

263^

083^

BO

BA

G

147^

SA

MKO

082^

BA

TAM

BTM

D

080^

DO

VA

N

023^

BIP

OP

348^

MA

X 2

20 K

TM

AX F

L140

MHA

300

0

023^

NYLO

N

203^

1

116.

0 BTM

WSSS/SINCHANGI

1.

RA

DA

R r

equir

ed.

D-A

TIS

128.

6A

pt E

lev

2.

RNA

V 1

navig

ati

on s

pecif

icati

on G

NSS r

equir

ed.

3. F

or f

ligh

t la

ndin

g at

Sin

gapo

re C

hang

i A

irpo

rt,

pilo

ts a

re t

o re

ques

t fo

rth

e ST

AR

from

Sin

gapo

re A

TC w

hen

the

flig

ht i

s w

ithi

n D

120.

0 SJ

and

RWY 2

0 is

in

use.

Fli

ght

shal

l st

ill

rem

ain

unde

r th

e co

ntro

l of

WM

KK A

TC.

CHANGES:

22

Alt

Set

: hP

a T

rans

lev

el:

FL13

0

010

2030

4050

10

SINGAPORE, SINGAPORE.RNAV.STAR.10-2A

JEPPESEN

5 MAY 17

RO

UTIN

G

To S

AM

KO

, tu

rn L

EFT.

To

BTM

at

or a

bove

700

0, s

peed

220

KT,

tur

n LE

FT.

To D

OVA

NFr

om A

RAM

A,

spee

d 25

0 KT.

To

BO

BA

G a

t or

abo

ve 1

0000

, sp

eed

220

KT,

tur

n LE

FT.

at o

r ab

ove

4000

, tu

rn L

EFT.

To

BIP

OP

at o

r ab

ove

3000

, sp

eed

190

KT.

| JEPPESEN, 2017. ALL RIGHTS RESERVED.New format.

appr

oach

Rw

y 20

vect

ors

for

ILS

EXPE

CT

RAD

AR

(RWYS 20

C/R

)RN

AV (GNSS) ARR

IVAL

2347

41

23

15

1212

ARA

MA 1

B [ARA

M1B

]

180^

360^

090^

2100

2500

3400

MSA

SJ

VO

R

At

250 K

T

At

220 K

TA

t 220 K

T

At

190 K

T

CO

NTO

UR

INTE

RVA

LS

4000

2000



COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST


COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

SIN

GAPORE

Paya L

ebar

WSAP

SIN

GAPORE

Sele

tar

WSSL

01-00

103-30

104-00

22

20

34

24

3500

R PA

10000

6000

4000

MA

X 2

20 K

TM

AX F

L180

MHA

600

0

262^

082^

BO

KIP

MA

X 2

20 K

TM

AX F

L140

MHA

400

0

168^

348^SA

MKO

ASUNA

BO

BA

G

1

CHANGES: | JEPPESEN, 2017. ALL RIGHTS RESERVED.New format.

WSSS/SINCHANGI


JEPPESEN

10-2B

D-A

TIS

128.

6A

pt E

lev

22A

lt S

et:

hPa

T

rans

lev

el:

FL13

0 1.

RA

DA

R r

equir

ed.

2.

RNA

V 1

navig

ati

on s

pecif

icati

on G

NSS r

equir

ed.

and

proc

eed

on A

SUN

A 1

A t

o SA

MKO

.

2. W

hen

clea

red

via

ASU

NA

1A

by

Sing

apor

e A

TC:

1. S

et t

rans

pond

er t

o M

ode

A/C

cod

e 76

00.

clos

e as

pos

sibl

e to

EA

T or

ETA

.

Spec

ial

Proc

edur

es f

or m

isse

d ap

proa

ch p

roce

dure

.

b. F

rom

SA

MKO

com

men

ce d

esce

nt a

nd c

arry

out

c. I

f un

able

to

effe

ct a

lan

ding

, re

fer

to S

inga

pore

3. N

o cl

eara

nce

or i

nstr

ucti

on r

ecei

ved

from

Si

ngap

ore

ATC

:

a. M

AIN

TAIN

las

t as

sign

ed f

ligh

t le

vel

or a

ltit

ude

Refe

r to

10-

1P p

ages

for

rad

io c

omm

unic

atio

nsfa

ilur

e pr

oced

ure.

appr

opri

ate

land

ing

proc

edur

e fo

r Rw

y 02

as

RO

UT

IN

G

From

ASU

NA

, sp

eed

250

KT.

To

BO

BA

G a

t or

abo

ve 1

0000

, sp

eed

220

KT.

To B

OKIP

at

or a

bove

600

0. T

o SA

MKO

at

or a

bove

400

0, s

peed

190

KT.

Cha

ngi

EAST

Rw

y 02

R/20

Lis

sol

ely

for

use

by t

heRe

publ

ic o

f Si

ngap

ore

Air

For

ce (

RSA

F) A

ircr

aft

1(RWYS 02

L/C)

RNAV (GNSS) ARR

IVAL

1020

300

515

2535

5

20

14

9

1411

EXPE

CT

RAD

AR

vect

ors

for

ILS

appr

oach

Rw

y 02

5 MAY 17

ASU

NA 1

A [ASU

N1A

]

At

250 K

T

At

220 K

TA

t 190 K

T



COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

LOST


LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

BATAM

Hang N

adim

WID

D

JOHOR B

AHRU

Senai In

tlW

MKJ

SIN

GAPORE

Paya L

ebar

WSAP

SIN

GAPORE

Sele

tar

WSSL

01-00

01-30

103-00

103-30

104-00

104-30

17

22

27

34

24

3500

RA

P

4000

7000

3000

10000


WSSS/SINCHANGI


JEPPESEN

10-2C

D-A

TIS

128.

6A

pt E

lev

22A

lt S

et:

hPa

T

rans

lev

el:

FL13

0 1.

RA

DA

R r

equir

ed.

2.

RNA

V 1

navig

ati

on s

pecif

icati

on G

NSS r

equir

ed.

RO

UTIN

G

From

ASU

NA

, sp

eed

250

KT.

To

BO

BA

G a

t or

abo

ve 1

0000

, sp

eed

220

KT.

To

SAM

KO

,tu

rn L

EFT.

To

BTM

at

or a

bove

700

0, s

peed

220

KT,

tur

n LE

FT.

To D

OVA

N a

t or

ab

ove

4000

, tu

rn L

EFT.

To

BIP

OP

at o

r ab

ove

3000

, sp

eed

190

KT.

2. W

hen

clea

red

via

ASU

NA

1B b

y Si

ngap

ore

ATC

:1.

Set

tra

nspo

nder

to

Mod

e A

/C c

ode

7600

.

clos

e as

pos

sibl

e to

EA

T or

ETA

.

Spec

ial

Proc

edur

es f

or m

isse

d ap

proa

ch p

roce

dure

.

b. F

rom

NYLO

N c

omm

ence

des

cent

and

car

ry o

ut

c. I

f un

able

to

effe

ct a

lan

ding

, re

fer

to S

inga

pore

3. N

o cl

eara

nce

or i

nstr

ucti

on r

ecei

ved

from

Si

ngap

ore

ATC

:

a. M

AIN

TAIN

las

t as

sign

ed f

ligh

t le

vel

or a

ltit

ude

Refe

r to

10-

1P p

ages

for

rad

io c

omm

unic

atio

nsfa

ilur

e pr

oced

ure.

appr

opri

ate

land

ing

proc

edur

e fo

r Rw

y 20

as

NYLO

N.

and

proc

eed

on A

SUN

A 1

B t

o BIP

OP,

the

n di

rect

to

Cha

ngi

EAST

Rw

y 02

R/20

Lis

sol

ely

for

use

by t

heRe

publ

ic o

f Si

ngap

ore

Air

For

ce (

RSA

F) A

ircr

aft

1

SA

MKO

080^

023^

DO

VA

N

BA

TAM

D

BTM

116.

0 BTM

348^BIP

OP

MA

X 2

20 K

TM

AX F

L140

MHA

300

0

023^

NYLO

N

203^

1

BO

BA

G

ASUNA

MA

X 2

20 K

TM

AX F

L180

MHA

600

0

263^

083^

082^

010

2030

4050

10

appr

oach

Rw

y 20

vect

ors

for

ILS

EXPE

CT

RAD

AR

RNAV (GNSS) ARR

IVAL

(RWYS 20

R/C)

2347

20

23

15

1212

ASU

NA 1

B [ASU

N1B

]

5 MAY 17

At

220 K

T

At

190 K

T

At

220 K

T

At

250 K

T

CO

NTO

UR

INTE

RVA

LS

4000

2000


COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMSLOST COMMSLOST COMMSLOST COMMSLOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMSLOST LOST COMMS LOST COMMS LOST COMMS

BATAM

WIDD

TANJUNG PINANGRaja Haji Fisabilillah

WIDN

JOHOR BAHRUSenai Intl

WMKJ

SINGAPOREPaya Lebar

WSAP

SINGAPORESeletarWSSL

01-00

01-30

02-00

02-30

103-30 104-00 104-3022 20

34 24

47 47

3500

RAP

FL210

4000

6000

PIBAP

PASPU

NYLON

MAX 300 KTMAX FL350MHA FL280354^

174^

ELALO

KANLA

174^

MAX 250 KTMAX FL270MHA FL220

047^

227^

KILOT

227^

180^

MAX 220 KTMAX FL140MHA 3000

023^

203^

172^

SANAT

203^

SAMKO


168^

348^



1. RADAR required.

10-2DJEPPESEN

D-ATIS

128.6Apt Elev

2. RNAV 1 navigation specification GNSS required.22Alt Set: hPa Trans level: FL130

ELALO 1A [ELAL1A]RNAV (GNSS) ARRIVAL (RWYS 02L/C)

WSSS/SINCHANGI

Changi EAST Rwy 02R/20Lis solely for use by theRepublic of Singapore

Air Force (RSAF) Aircraft

1

ROUTING

NOT TO SCALE

1

POSUB

1. Set transponder to Mode A/C code 7600.

3. No clearance or instruction received from Singapore ATC:

b. From SAMKO commence descent and carry out appropriate landing procedure for Rwy 02 as close as possible to EAT or ETA.c. If unable to effect a landing, refer to Singapore Special Procedures for missed approach procedure.

a. MAINTAIN last assigned flight level or

Refer to 10-1P pages for radiocommunications failure procedure.

altitude and proceed on ELALO 1A to SANAT,then direct to SAMKO.

2. When cleared via ELALO 1A by Singapore ATC:

010

2030

4050

10

21

10

2231

47

4427

3337

EXPECT RADARvectors for ILS

approach Rwy 02

From ELALO. To KANLA. To KILOT, turn RIGHT. To PIBAP at or below FL210, speed 250 KT, turn LEFT. To PASPU speed 220 KT. To NYLON, turn LEFT. To POSUB at or above 6000, speed 220 KT, turn RIGHT. ToSANAT at or above 4000, speed 190 KT.

19 MAY 17 .Eff.25.May.

Chart reindexed.

At 250 KT

At 220 KT

At 190 KT

At 220 KT

Hang Nadim

CONTOURINTERVALS

4000

2000


COMMS

LOST

COMMS

LOST

COMMS

LOST


COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMSLOST LOST COMMS LOST COMMS LOST COMMS


WMKJ

SINGAPOREPaya Lebar

WSAP


01-30

02-00

02-30

03-00

03-30

04-00

04-30

103-00 103-30 104-00 104-30 105-00

34 2410

47 47 30

4510 32

11

10

3500

RA

P3000

FL210

6000



b. From NYLON commence descent and carry out appropriate landing procedure for Rwy 20 as close as possible to EAT or ETA.c. If unable to effect a landing, refer to

2. When cleared via ELALO 1B by Singapore ATC:

Singapore Special Procedures for missed approach procedure.



altitude and proceed on ELALO 1B to NYLON.


354^

174^

ELALO

KANLA

174^


7^

227^

KILOT

PIBAP

227^

PASPU

180^


023^

203^

NYLON

1



1


WSSS/SINCHANGI


1. RADAR required.

10-2EJEPPESEN

D-ATIS

128.6Apt Elev

2. RNAV 1 navigation specification GNSS required.22Alt Set: hPa Trans level: FL130

ROUTING

From ELALO. To KANLA. To KILOT, turn RIGHT. To PIBAP at or below FL210, speed 250 KT, turn LEFT.To PASPU, at or above 6000, speed 220 KT. To NYLON at or above 3000, speed 190 KT.

ELALO 1B [ELAL1B]RNAV (GNSS) ARRIVAL (RWYS 20R/C)

approach Rwy 20vectors for ILSEXPECT RADAR

2744

47

3122

3337

010

2010

3040

50

19 MAY 17 .Eff.25.May.

Chart reindexed.

At 250 KT

At 220 KT

At 190 KT

CONTOURINTERVALS

4000

2000



COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST


COMMS

COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

LOST

BATAM

Hang N

adim

WID

D

TANJU

NG P

INANG

Raja

Haji F

isabililla

hW

IDN

SIN

GAPORE

Paya L

ebar

WSAP

SIN

GAPORE

Sele

tar

WSSL

00-30

01-00

01-30

104-00

104-30

105-00

105-30

22

20

34

24

10

3500

RA P

FL1

60

7000

4000

TO

MA

N

MA

X 2

80 K

TM

AX F

L310

MHA

FL2

6008

9^

269^

KA

RTO

233^

269^

MA

X 2

20 K

TM

AX F

L140

MHA

700

0

089^

IGNO

N

266^

SA

NA

T

1

KEXA

S

LAVA

X

SA

MKO

MA

X 2

20 K

TM

AX F

L140

MHA

400

0

348^

168^

Cha

ngi

EAST

Rw

y 02

R/20

Lis

sol

ely

for

use

by t

heRe

publ

ic o

f Si

ngap

ore

Air

For

ce (

RSA

F) A

ircr

aft

1

appr

oach

Rw

y 02

vect

ors

for

ILS

EXPE

CT

RAD

AR


WSSS/SINCHANGI

SINGAPORE, SINGAPORE.RNAV.STAR.10-2F

JEPPESEN

D-A

TIS

128.

6A

pt E

lev

2.

RNA

V 1

navig

ati

on s

pecif

icati

on G

NSS r

equir

ed.

1.

RA

DA

R r

equir

ed.

(RWYS

02L/C)

RNAV (GNSS) ARR

IVAL

Alt

Set

: hP

a T

rans

lev

el:

FL13

0

22

2. W

hen

clea

red

via

KA

RTO

1A

by

Sing

apor

e A

TC:

1. S

et t

rans

pond

er t

o M

ode

A/C

cod

e 76

00.

appr

opri

ate

land

ing

proc

edur

e fo

r Rw

y 02

as

clos

e as

pos

sibl

e to

EA

T or

ETA

.

Spec

ial

Proc

edur

es f

or m

isse

d ap

proa

ch p

roce

dure

.

b. F

rom

SA

MKO

com

men

ce d

esce

nt a

nd c

arry

out

c. I

f un

able

to

effe

ct a

lan

ding

, re

fer

to S

inga

pore

3. N

o cl

eara

nce

or i

nstr

ucti

on r

ecei

ved

from

Si

ngap

ore

ATC

:

and

proc

eed

on K

ART

O 1

A t

o SA

NA

T, t

hen

dire

ct

to S

AM

KO

.

a. M

AIN

TAIN

las

t as

sign

ed f

ligh

t le

vel

or a

ltit

ude

Refe

r to

10-

1P p

ages

for

rad

io c

omm

unic

atio

nsfa

ilur

e pr

oced

ure.

From

TO

MA

N.

To K

ART

O,

turn

RIG

HT.

To

KEX

AS

at o

r be

low

FL1

60,

spee

d25

0 KT.

To

LAVA

X,

spee

d 22

0 KT,

tur

n LE

FT.

To I

GN

ON

at

or a

bove

700

0.

RO

UTIN

G

To S

AN

AT

at o

r ab

ove

4000

, sp

eed

190

KT.

100

2030

4050

10

1414

2146

17

KART

O 1

A [KA

RT1A

]

1132

5 MAY 17

At

250 K

T

At

220 K

T

At

190 K

T


COMMSLOST COMMSLOST

LOST

COMMS LOSTCOMMS LOST

COMMS

COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

LOST

COMMS

COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

BATAM

Hang N

adim

WID

D

TANJU

NG P

INANG

Raja

Haji F

isabililla

hW

IDN

SIN

GAPORE

Paya L

ebar

WSAP

SIN

GAPORE

Sele

tar

WSSL

01-00

01-30

104-00

104-30

105-00

105-30

22

20

34

24

10

3500

RP

A

FL1

60

8000

4000

3000

2. W

hen

clea

red

via

KA

RTO

1B b

y Si

ngap

ore

ATC

:1.

Set

tra

nspo

nder

to

Mod

e A

/C c

ode

7600

.

RO

UTIN

G

a. M

AIN

TAIN

las

t as

sign

ed f

ligh

t le

vel

or a

ltit

ude

and

proc

eed

onKA

RTO

1B t

o BIP

OP,

the

n di

rect

to

NYLO

N.

b. F

rom

NYLO

N c

omm

ence

des

cent

and

car

ry o

ut a

ppro

pria

te l

andi

ngpr

oced

ure

for

Rwy

20 a

s cl

ose

as p

ossi

ble

to E

AT

or E

TA.

Proc

edur

es f

or m

isse

d ap

proa

ch p

roce

dure

.c.

If

unab

le t

o ef

fect

a l

andi

ng,

refe

r to

Sin

gapo

re S

peci

al

Refe

r to

10-

1P p

ages

for

rad

io c

omm

unic

atio

ns f

ailu

re p

roce

dure

.3.

No

clea

ranc

e or

ins

truc

tion

rec

eive

d fr

om S

inga

pore

ATC

:

TO

MA

N

MA

X 2

80 K

TM

AX F

L310

MH

A F

L260

089^

269^

KA

RTO

233^

KEXA

S

269^

MA

X 2

20 K

TM

AX F

L140

MH

A 7

000

089^

LAVA

XRUVIK

304^

DO

VA

N

BIP

OP

348^

NYLO

NM

AX 2

20 K

TM

AX F

L140

MH

A 3

000

023^

203^


WSSS/SINCHANGI

SINGAPORE, SINGAPORE.RNAV.STAR.10-2G

JEPPESEN

D-A

TIS

128.

6A

pt E

lev

222.

RNA

V 1

navig

ati

on s

pecif

icati

on G

NSS r

equir

ed.

1.

RA

DA

R r

equir

ed.

Alt

Set

: hP

a

Tra

ns l

evel

: FL

130

KART

O 1

B [KART

1B]

From

TO

MA

N.

To K

ART

O,

turn

RIG

HT.

To

KEX

AS

at o

r be

low

FL1

60,

spee

d 25

0 KT.

at o

r ab

ove

4000

, tu

rn R

IGHT.

To

BIP

OP

at o

r ab

ove

3000

, sp

eed

190

KT.

To L

AVA

X,

spee

d 22

0 KT,

tur

n RI

GHT.

To

RUVIK

at

or a

bove

800

0. T

o D

OVA

N

Cha

ngi

EAST

Rw

y 02

R/20

Lis

sol

ely

for

use

by t

heRe

publ

ic o

f Si

ngap

ore

Air

For

ce (

RSA

F) A

ircr

aft

1

vect

ors

for

ILS

EXPE

CT

RAD

AR

appr

oach

Rw

y 20

1

010

2030

4050

10

12

9

2146

RNAV (GNSS) ARR

IVAL (RWYS

20C/R

)

17

8 1132

5 MAY 17

At

250 K

T

At

220 K

T

At

190 K

T


COMMS

LOST

COMMS

LOST

COMMS

LOST

LOST COMMS COMMSLOST COMMSLOST COMMSLOST LOST

COMMS

COMMS

LOST

COMMS

LOST

LOST

LOST COMMSCOMMS LOST COMMS LOST COMMSLOST

SINGAPOREPaya Lebar

WSAP


01-30

104-00

34 24

3500MSA ARP

4000

7000

7000



altitude and proceed on LEBAR 2A to

b. From SAMKO commence descent and

c. If unable to effect a landing, refer to

2. When cleared via LEBAR 2A by Singapore ATC:


SAMKO.

Rwy 02L as close as possible to EAT or ETA.


Refer to 10-1P pages for radio communications failure procedure.

carry out appropriate landing procedure for

PASPU

197^

113.5 SJSINJON

SJD

202^

PALGA 234^

PAMSI

173^

SAMKO082^

115.1 PUPAPA UNIFORM

PUD

Deviation is not permitedbetween SJ and PU



1

1


WSSS/SINCHANGI


JEPPESEN

(RWY 02L)

D-ATIS

128.6

10-2H

Apt Elev

2. RNAV 1 navigation specification GNSS required.1. RADAR required.

RNAV (GNSS) ARRIVALLEBAR 2A [LEBA2A]

22Alt Set: hPa Trans level: FL130

To PALGA, speed 220 KT, turn LEFT. To PAMSI, turn LEFT. To SAMKO at or above 4000, speed 190 KT.From PASPU, speed 220 KT. To PU at or above 7000, turn RIGHT. To SJ at or above 7000, turn RIGHT.

ROUTING


NOT TO SCALE

05

1015

205

25

35

13

4

6

4

607

5 MAY 17

At 190 KT

At 220 KT

At 220 KT



COMMS

LOST

COMMS

LOST

COMMS

LOST

LOSTC

OMMS

COMMS

LOST

COMMS

LOST

COMMS

LOST

LOST COMMSCOMMSLOSTCOMMSLOST COMMSLOST

BATAMHang Nadim

WIDD


WMKJ

SINGAPOREPaya Lebar

WSAP

01-00

01-30

103-30

104-00

22 20

34 24

3500

RPA

7000

7000

3000

10000

BOBAG

113.5 SJSINJON

SJD

063^

BOBA

G

REMES

348^

REM

ES

115.1 PUPAPA UNIFORM

PUD

022^

BETBA342^

BIDUS

057^

1


WSSS/SINCHANGI


JEPPESEN

D-ATIS

128.6

10-2J

Apt Elev1. RADAR required.2. RNAV 1 navigation specification GNSS required.

(RWY 20R)RNAV (GNSS) ARRIVAL

22

Alt Set: hPa Trans level: FL130

LEBAR 2B [LEBA2B]

ROUTING

TRANSITIONS

BOBAG

REMES From REMES, speed 220 KT. To SJ at or above 7000, turn RIGHT. To PU.From BOBAG at or above 10000, speed 220 KT. To SJ at or above 7000, turn LEFT. To PU.

or altitude and proceed on LEBAR 2B

b. From NYLON commence descent and

Refer to 10-1P pages for radio communications failure procedure.

from Singapore ATC:3. No clearance or instruction received

to Singapore Special Proceduresfor missed approach procedure.

c. If unable to effect a landing, refer

for Rwy 20R as close as possible toEAT or ETA.

carry out appropriate landing procedures

a. MAINTAIN last assigned flight levelSingapore ATC:

2. When cleared via LEBAR 2B by

to BIDUS, then direct to NYLON.




1


1020

3040

500

515

2535

455

58

13

24

30

Deviation is not permitedbetween SJ and PU

speed 190 KT.From PU, at or above 7000, speed 220 KT, turn LEFT. To BETBA, turn RIGHT. To BIDUS at or above 3000,

5 MAY 17

NYLON

203^MAX 220 KT

023^

MAX FL140MHA 3000

2347

At 220 KT

At 220 KT

At 220 KT

At 190 KT

CONTOURINTERVALS

4000

2000


COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST



COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

BATAM

Hang N

adim

WID

D

JOHOR B

AHRU

Senai In

tlW

MKJ

SIN

GAPORE

Paya L

ebar

WSAP

SIN

GAPORE

Sele

tar

WSSL

01-30

103-00

103-30

104-00

27

34

24

3500

R

A

P

7000

6000

3000

10000

2. W

hen

clea

red

via

LELI

B 3

B b

y Si

ngap

ore

ATC

:1.

Set

tra

nspo

nder

to

Mod

e A

/C c

ode

7600

.

appr

opri

ate

land

ing

proc

edur

e fo

r Rw

y 20

as

clos

e as

pos

sibl

e to

EA

T or

ETA

.

Spec

ial

Proc

edur

es f

or m

isse

d ap

proa

ch p

roce

dure

.

b. F

rom

NYLO

N c

omm

ence

des

cent

and

car

ry o

ut

c. I

f un

able

to

effe

ct a

lan

ding

, re

fer

to S

inga

pore

3. N

o cl

eara

nce

or i

nstr

ucti

on r

ecei

ved

from

Si

ngap

ore

ATC

:

and

proc

eed

on L

ELIB

3B t

o BID

US,

the

n di

rect

to

NYLO

N.

(RWYS

20C/R

)

1.

RA

DA

R r

equir

ed.

a. M

AIN

TAIN

las

t as

sign

ed f

ligh

t le

vel

or a

ltit

ude

Refe

r to

10-

1P p

ages

for

rad

io c

omm

unic

atio

nsfa

ilur

e pr

oced

ure.

D-A

TIS

128.

6A

pt E

lev

2.

RNA

V 1

navig

ati

on s

pecif

icati

on G

NSS r

equir

ed.

RNAV (GNSS) ARR

IVAL

the

STA

R fr

om S

inga

pore

ATC

whe

n th

e fl

ight

is

wit

hin

D12

0.0

SJ a

ndRW

Y 2

0 is

in

use.

Fli

ght

shal

l st

ill

rem

ain

unde

r th

e co

ntro

l of

WM

KK A

TC.

3. F

or f

ligh

t la

ndin

g at

Sin

gapo

re C

hang

i A

irpo

rt,

pilo

ts a

re t

o re

ques

t fo

r

ARA

MA

LELI

B

118^

JAYBE

E40

0 JB

082^

086^

BID

US

057^

NYLO

NM

AX 2

20 K

TM

AX F

L140

203^ 023^

MHA

300

0

1

appr

oach

Rw

y 20

vect

ors

for

ILS

EXPE

CT

RAD

AR

Cha

ngi

EAST

Rw

y 02

R/20

Lis

sol

ely

for

use

by t

heRe

publ

ic o

f Si

ngap

ore

Air

For

ce (

RSA

F) A

ircr

aft

1

JB


WSSS/SINCHANGI

SINGAPORE, SINGAPORE.RNAV.STAR.10-2J1

JEPPESEN

22

Alt

Set

: hP

a T

rans

lev

el:

FL13

0 LELIB

3B [LELI3B

]

RO

UTIN

G

From

ARA

MA

, sp

eed

250

KT.

To

LELI

B a

t or

abo

ve 1

0000

, tu

rn L

EFT.

To

JAYBEE

at

or a

bove

700

0, s

peed

220

KT,

tur

n

at o

r ab

ove

3000

, sp

eed

190

KT.

RIG

HT.

To

ALF

A a

t or

abo

ve 6

000,

tur

n LE

FT.

To B

IDUS

1020

3040

500

515

2535

455

20

18

7

10

2347

ALF

A

5 MAY 17

At

190 K

T

At

250 K

T

At

220 K

T

CO

NTO

UR

INTE

RVA

LS

4000

2000



COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

LOST

LOST COMMS LOST COMMS LOST COMMS LOST COMMS

BATAMHang Nadim

WIDD


WMKJ

SINGAPOREPaya Lebar

WSAP


01-30

02-00

02-30

104-00

104-30 105-00

2220

34

24

10

4747

30

3500

RAP

4000

6000

FL210



altitude and proceed on MABAL 2A to

b. From SAMKO commence descent and carry out appropriate landing procedure for Rwy 02 as close as possible to EAT or ETA.c. If unable to effect a landing, refer to

2. When cleared via MABAL 2A by Singapore ATC:




SANAT, then direct to SAMKO.

SAMKO


168^

NYLONMAX 220 KTMAX FL140MHA 3000

023^

203^

172^

SANAT

203^ POSUB

PASPU

PIBAP

180^

348^

1

MAX 300 KT

MABAL

MAX 250 KT

KILOT

231^

227^



1

227^

231^

051^ MAX FL350

MHA FL280

MAX FL270MHA FL220


10-2J2WSSS/SINCHANGI


1. RADAR required.

JEPPESEN

D-ATIS

128.6Apt Elev

2. RNAV 1 navigation specification GNSS required.

MABAL 2A [MABA2A]

22

RNAV (GNSS) ARRIVAL (RWYS 02L/C)


ROUTING

From MABAL. To KILOT, turn LEFT. To PIBAP at or below FL210, speed 250KT, turn LEFT. To PASPU,speed 220 KT. To NYLON, turn LEFT. To POSUB at or above 6000, speed 220KT, turn RIGHT. To SANATat or above 4000, speed 190 KT.

NOT TO SCALE

010

2030

4050

10

2271

42

47

21

10

2231


approach Rwy 02

047^

5 MAY 17

At 220 KT

At 190 KT

At 220 KT

At 250 KT

CONTOURINTERVALS

4000

2000


COMMS

LOST

COMMS

LOST

COMMS

LOST

LOST

COMMS COMMSLOST COMMSLOST COMMSLOST LOST

COMMS

COMMS

LOST

COMMS

LOST

LOST

BATAMHang Nadim

WIDD


WMKJ

SINGAPOREPaya Lebar

WSAP


COMMS LOST COMMS LOSTLOST COMMS COMMS LOST

01-30

02-00

02-30

03-00

03-30

104-00 104-30

105-00 105-30

34

24

10

4747 30

45 10

32

3500

RP

A

6000

3000

FL210



altitude and proceed on MABAL 2B to

b. From NYLON commence descent and carry out appropriate landing procedure for Rwy 20 as close as possible to EAT or ETA.c. If unable to effect a landing, refer to

2. When cleared via MABAL 2B by Singapore ATC:




NYLON.

231^

051^


MABAL

227^


KILOT

231^

PIBAP

227^

PASPU

180^

203^

023^

MAX 220 KTMAX FL140NYLONMHA 3000

1


10-2KWSSS/SINCHANGI


1. RADAR required.

(RWYS 20R/C)

JEPPESEN

D-ATIS

128.6Apt Elev

2. RNAV 1 navigation specification GNSS required.

RNAV (GNSS) ARRIVALMABAL 2B [MABA2B]


22

ROUTING

From MABAL. To KILOT, turn LEFT. To PIBAP at or below FL210, speed 250KT, turn LEFT. To PASPU,at or above 6000, speed 220 KT. To NYLON at or above 3000, speed 190KT.

010

2030

4050

10



1


3334

42

47

3122

047^

5 MAY 17

At 250 KT

At 220 KT

At 190 KT

CONTOURINTERVALS

4000

2000


COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMSLOST COMMSLOST LOST


LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

COMMS

BATAM

Hang N

adim

WID

D

TANJU

NG P

INANG

Raja

Haji F

isabililla

hW

IDN

SIN

GAPORE

Paya L

ebar

WSAP

SIN

GAPORE

Sele

tar

WSSL

00-30

01-00

103-30

104-00

104-30

105-00

105-30

22

20

10

34

24

10

3500

R AP

7000

4000

FL1

80

2. W

hen

clea

red

via

OBD

OS

1A b

y Si

ngap

ore

ATC

:1.

Set

tra

nspo

nder

to

Mod

e A

/C c

ode

7600

.

appr

opri

ate

land

ing

proc

edur

e fo

r Rw

y 02

as

clos

e as

pos

sibl

e to

EA

T or

ETA

.

Spec

ial

Proc

edur

es f

or m

isse

d ap

proa

ch p

roce

dure

.

b. F

rom

SA

MKO

com

men

ce d

esce

nt a

nd c

arry

out

c. I

f un

able

to

effe

ct a

lan

ding

, re

fer

to S

inga

pore

3. N

o cl

eara

nce

or i

nstr

ucti

on r

ecei

ved

from

Si

ngap

ore

ATC

:

and

proc

eed

on O

BD

OS

1A t

o SA

NA

T, t

hen

dire

ct

to S

AM

KO

.

a. M

AIN

TAIN

las

t as

sign

ed f

ligh

t le

vel

or a

ltit

ude

Refe

r to

10-

1P p

ages

for

rad

io c

omm

unic

atio

nsfa

ilur

e pr

oced

ure.

291^

111^

MA

X 2

50 K

TM

AX F

L250

MH

A F

L150

IKIM

A

269^

089^

MA

X 2

20 K

TM

AX F

L140

LAVA

X

335^

IGNO

N

266^

SA

NA

TSA

MKO

MA

X 2

20 K

TM

AX F

L140

348^

168^

MH

A 7

000

MH

A 4

000

Cha

ngi

EAST

Rw

y 02

R/20

Lis

sol

ely

for

use

by t

heRe

publ

ic o

f Si

ngap

ore

Air

For

ce (

RSA

F) A

ircr

aft

1


WSSS/SINCHANGI

SINGAPORE, SINGAPORE.RNAV.STAR.10-2L

JEPPESEN

(RWYS 02

L/C)

D-A

TIS

128.

6A

pt E

lev

RNAV (GNSS) ARR

IVAL

2.

RNA

V 1

navig

ati

on s

pecif

icati

on G

NSS r

equir

ed.

1.

RA

DA

R r

equir

ed.

Alt

Set

: hP

a

Tra

ns l

evel

: FL

130

OBD

OS

1A [OBD

O1A

]

22

RO

UTIN

G

From

OBD

OS.

To

IKA

GO

. To

IKIM

A,

turn

RIG

HT.

To

IBULA

at

or

belo

w F

L180

, sp

eed

250

KT,

tur

n RI

GHT.

To

LAVA

X,

spee

d 22

0 KT,

tur

n LE

FT.

To I

GN

ON

at

or a

bove

700

0.To

SA

NA

T at

or

abov

e 40

00,

spee

d 19

0 KT.

NO

T TO

SCA

LE

279^

OBDO

S

IKA

GO

291^

IBULA

1

010

2030

4050

10

1414

21

20

35

87

appr

oach

Rw

y 02

vect

ors

for

ILS

EXPE

CT

RAD

AR

1132

5 MAY 17

At

220 K

T

At

190 K

T

At

250 K

T


COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST



COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

BATAM

Hang N

adim

WID

D

TANJU

NG P

INANG

Raja

Haji F

isabililla

hW

IDN

SIN

GAPORE

Paya L

ebar

WSAP

SIN

GAPORE

Sele

tar

WSSL

01-30

104-00

104-30

105-00

105-30

22

20

10

34

24

10

3500

RA

P

3000

8000

4000

FL1

80

2. W

hen

clea

red

via

OBD

OS

1B b

y Si

ngap

ore

ATC

:1.

Set

tra

nspo

nder

to

Mod

e A

/C c

ode

7600

.

appr

opri

ate

land

ing

proc

edur

e fo

r Rw

y 20

as

clos

e as

pos

sibl

e to

EA

T or

ETA

.

Spec

ial

Proc

edur

es f

or m

isse

d ap

proa

ch p

roce

dure

.

b. F

rom

NYLO

N c

omm

ence

des

cent

and

car

ry o

ut

c. I

f un

able

to

effe

ct a

lan

ding

, re

fer

to S

inga

pore

3. N

o cl

eara

nce

or i

nstr

ucti

on r

ecei

ved

from

Si

ngap

ore

ATC

:

and

proc

eed

on O

BD

OS

1B t

o BIP

OP,

then

dir

ect

to N

YLO

N.

(RWYS

20C/R

)

a. M

AIN

TAIN

las

t as

sign

ed f

ligh

t le

vel

or a

ltit

ude

Refe

r to

10-

1P p

ages

for

rad

io c

omm

unic

atio

nsfa

ilur

e pr

oced

ure.

D-A

TIS

128.

6A

pt E

lev

OBDO

S

IKA

GO

279^

291^

111^

MA

X 2

50 K

TM

AX F

L250

MH

A F

L150

IKIM

A

IBULA

291^

269^

089^

MA

X 2

20 K

TM

AX F

L140

LAVA

X

335^

RUVIK

304^

DO

VA

N

BIP

OP

348^

NYLO

N

MA

X 2

20 K

TM

AX F

L140

203^ 023^

MH

A 3

000

MH

A 7

000

1

Cha

ngi

EAST

Rw

y 02

R/20

Lis

sol

ely

for

use

by t

heRe

publ

ic o

f Si

ngap

ore

Air

For

ce (

RSA

F) A

ircr

aft

1


WSSS/SINCHANGI

SINGAPORE, SINGAPORE.RNAV.STAR.10-2M

JEPPESEN

2.

RNA

V 1

navig

ati

on s

pecif

icati

on G

NSS r

equir

ed.

1.

RA

DA

R r

equir

ed.

Alt

Set

: hP

a

Tra

ns l

evel

: FL

130

22

OBD

OS

1B [OBD

O1B

]

RO

UTIN

G

From

OBD

OS.

To

IKA

GO

. To

IKIM

A,

turn

RIG

HT.

To

IBULA

at

or

belo

w F

L180

, sp

eed

250

KT,

tur

n RI

GHT.

To

LAVA

X,

spee

d 22

0 KT,

tur

n LE

FT.

To R

UVIK

at

or a

bove

800

0. T

o

abov

e 30

00,

spee

d 19

0 KT.

DO

VA

N a

t or

abo

ve 4

000,

tur

n RI

GHT.

To

BIP

OP

at o

r

NO

T TO

SCA

LE

appr

oach

Rw

y 20

vect

ors

for

ILS

EXPE

CT

RAD

AR

010

2030

4050

10

12

9

8

21

20

35

87

2081

RNAV (GNSS) ARR

IVAL

5 MAY 17

At

250 K

T

At

220 K

T

At

190 K

T

01-00

CO

NTO

UR

INTE

RVA

LS

4000

2000


COMMSLOST COMMSLOST COMMSLOST COMMSLOST COMMSLOST

COMMS

LOST

COMMS

LOST

LOST

COMMS

LOST

COMMS

LOST

LOST

LOST COMMS LOST COMMS LOST COMMS LOST COMMS COMMS

BATAMHang Nadim

WIDD

SINGAPOREPaya Lebar

WSAP


00-30

01-00

103-30

104-00

22 20

34

24

3500

RPA

6000

4000

FL210

WSSS/SINCHANGI

SINGAPORE, SINGAPORE.RNAV.STAR.10-2N

(RWYS 02L/C)

2. When cleared via REPOV 1A by Singapore ATC:1. Set transponder to Mode A/C code 7600.

appropriate landing procedure for Rwy 02 as close as possible to EAT or ETA.

Special Procedures for missed approach procedure.

b. From SAMKO commence descent and carry out

c. If unable to effect a landing, refer to Singapore


and proceed on REPOV 1A to SAMKO.

JEPPESEN

a. MAINTAIN last assigned flight level or altitude

Refer to 10-1P pages for radio communicationsfailure procedure.

D-ATIS

128.6Apt Elev

RNAV (GNSS) ARRIVAL


348^

168^


REPOV

168^

MAX 220 KTMAX FL140

REMES

348^

168^

MAX 220 KTMAX FL140

SAMKO

MHA 6000

MHA 4000

1



1



REPOV 1A [REPO1A]

ROUTING

010

2030

4050

10

22

28

above 4000, speed 190 KT.From REPOV at or below FL210, speed 250 KT. To REMES at or above 6000, speed 220 KT. To SAMKO at or

1411


approach Rwy 02

5 MAY 17

At 190 KT

At 220 KT

At 250 KT


COMMSLOST COMMSLOST COMMSLOST COMMSLOST COMMSLOST

COMMS

LOST

COMMS

LOST

LOSTC

OMMS

LOST

COMMS

LOST

COMMS

LOST

COMMSLOST COMMS LOST COMMS LOST COMMS LOST COMMS LOST

BATAMHang Nadim

WIDD

TANJUNG PINANGRaja Haji Fisabilillah

WIDN

SINGAPOREPaya Lebar

WSAP


00-30

01-30

104-00

104-30

22

20

34

24

3500

RPA

3000

4000

FL210

7000

2. When cleared via REPOV 1B by Singapore ATC:1. Set transponder to Mode A/C code 7600.

appropriate landing procedure for Rwy 20 as close as possible to EAT or ETA.

Special Procedures for missed approach procedure.

b. From NYLON commence descent and carry out

c. If unable to effect a landing, refer to Singapore


(RWYS 20C/R)

and proceed on REPOV 1B to BIPOP, then direct to NYLON.

a. MAINTAIN last assigned flight level or altitude

Refer to 10-1P pages for radio communicationsfailure procedure.

D-ATIS

128.6Apt Elev

ROUTING

RNAV (GNSS) ARRIVAL


348^

168^


REPOV

168^

MAX 220 KTMAX FL140

REMES

348^BATAM

B T M116.0 BTMD

023^

DOVAN348^

NYLON

MAX 220 KTMAX FL14020

3^02

3^

1

BIPOPvectors for ILSEXPECT RADAR

approach Rwy 20

Changi EAST Rwy 02R/20L1

is solely for use by theRepublic of Singapore


MHA 3000

MHA 6000


WSSS/SINCHANGI

SINGAPORE, SINGAPORE.RNAV.STAR.10-2P

JEPPESEN


REPOV 1B [REPO1B]

From REPOV at or below FL210, speed 250 KT. To REMES, speed 220 KT, turn RIGHT. To BTM at or above 7000, speed 220 KT. To DOVAN at or above 4000, turn LEFT.To BIPOP at or above 3000, speed 190 KT.

010

2030

4050

10

12

12

27

281132

5 MAY 17

At 190 KT

At 250 KT

At 220 KT

At 220 KT01-00


COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST



LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

BATAM

Hang N

adim

WID

D

TANJU

NG P

INANG

Raja

Haji F

isabililla

hW

IDN

JOHOR B

AHRU

Senai In

tlW

MKJ

SIN

GAPORE

Paya L

ebar

WSAP

SIN

GAPORE

Sele

tar

WSSL

00-30

01-00

01-30

103-30

104-00

104-30

105-00

105-30

22

20

10

34

24

10

3500

RAP

4000

7000

FL1

80

1.

RA

DA

R r

equir

ed.

2. W

hen

clea

red

via

SURG

A 1

A b

y Si

ngap

ore

ATC

:1.

Set

tra

nspo

nder

to

Mod

e A

/C c

ode

7600

.

appr

opri

ate

land

ing

proc

edur

e fo

r Rw

y 02

as

clos

e as

pos

sibl

e to

EA

T or

ETA

.

Spec

ial

Proc

edur

es f

or m

isse

d ap

proa

ch p

roce

dure

.

b. F

rom

SA

MKO

com

men

ce d

esce

nt a

nd c

arry

out

c. I

f un

able

to

effe

ct a

lan

ding

, re

fer

to S

inga

pore

3. N

o cl

eara

nce

or i

nstr

ucti

on r

ecei

ved

from

Si

ngap

ore

ATC

:

and

proc

eed

on S

URG

A 1

A t

o SA

NA

T, t

hen

dire

ct

to S

AM

KO

.

(RWYS

02L/C)

a. M

AIN

TAIN

las

t as

sign

ed f

ligh

t le

vel

or a

ltit

ude

Refe

r to

10-

1P p

ages

for

rad

io c

omm

unic

atio

nsfa

ilur

e pr

oced

ure.

D-A

TIS

128.

6A

pt E

lev

2.

RNA

V 1

navig

ati

on s

pecif

icati

on G

NSS r

equir

ed.

RO

UTIN

G

RNAV (GNSS) ARR

IVAL

SURG

A

IKA

GO

320^

IKIM

A27

9^

291^

269^

089^

MA

X 2

20 K

TM

AX F

L140

335^

266^

SA

MKO

MA

X 2

20 K

TM

AX F

L140

348^

168^

1

SA

NA

T

IGNO

NLA

VA

X

IBULA

MH

A 7

000

MH

A 4

000

Cha

ngi

EAST

Rw

y 02

R/20

Lis

sol

ely

for

use

by t

heRe

publ

ic o

f Si

ngap

ore

Air

For

ce (

RSA

F) A

ircr

aft

1

MA

X 2

50 K

TM

AX F

L250

MH

A F

L150

111^

291^


WSSS/SINCHANGI

SINGAPORE, SINGAPORE.RNAV.STAR.10-2Q

JEPPESEN

Alt

Set

: hP

a

Tra

ns l

evel

: FL

130

22

SURG

A 1

A [SU

RG1A

]

From

SURG

A.

To I

KA

GO

, tu

rn L

EFT.

To

IKIM

A,

turn

RIG

HT.

To I

BULA

at

or b

elow

FL1

80,

spee

d 25

0 KT,

tur

n RI

GHT.

To

LAVA

X,

spee

d 22

0 KT,

tur

n LE

FT.

To I

GN

ON

at

or a

bove

700

0.To

SA

NA

T at

or

abov

e 40

00,

spee

d 19

0 KT.

NO

T TO

SCA

LE

010

2030

4050

10

1414

21

20

35

97

2347

appr

oach

Rw

y 02

vect

ors

for

ILS

EXPE

CT

RAD

AR

5 MAY 17

At

190 K

T

At

220 K

T

At

250 K

T

CO

NTO

UR

INTE

RVA

LS

4000

2000


COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

LOST



LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

COMMS

BATAM

Hang N

adim

WID

D TANJU

NG P

INANG

Raja

Haji F

isabililla

hW

IDN

JOHOR B

AHRU

Senai In

tlW

MKJ

SIN

GAPORE

Paya L

ebar

WSAP

SIN

GAPORE

Sele

tar

WSSL

00-30

01-00

01-30

103-30

104-00

104-30

105-00

105-30

20

10

34

24

10

3500

RA

P

FL1

80

3000

80004000

WSSS/SINCHANGI


1.

RA

DA

R r

equir

ed.

2. W

hen

clea

red

via

SURG

A 1

B b

y Si

ngap

ore

ATC

:1.

Set

tra

nspo

nder

to

Mod

e A

/C c

ode

7600

.

appr

opri

ate

land

ing

proc

edur

e fo

r Rw

y 20

as

clos

e as

pos

sibl

e to

EA

T or

ETA

.

Spec

ial

Proc

edur

es f

or m

isse

d ap

proa

ch p

roce

dure

.

b. F

rom

NYLO

N c

omm

ence

des

cent

and

car

ry o

ut

c. I

f un

able

to

effe

ct a

lan

ding

, re

fer

to S

inga

pore

3. N

o cl

eara

nce

or i

nstr

ucti

on r

ecei

ved

from

Si

ngap

ore

ATC

:

and

proc

eed

on S

URG

A 1

B t

o BIP

OP,

the

n di

rect

to

NYLO

N.

10-2SJEPPESEN

(RWYS

20C/R

)

a. M

AIN

TAIN

las

t as

sign

ed f

ligh

t le

vel

or a

ltit

ude

Refe

r to

10-

1P p

ages

for

rad

io c

omm

unic

atio

nsfa

ilur

e pr

oced

ure.

D-A

TIS

128.

6A

pt E

lev

2.

RNA

V 1

navig

ati

on s

pecif

icati

on G

NSS r

equir

ed.

RO

UTIN

G

RUVIK

304^

DO

VA

N

348^

1

SURG

A

IKA

GO

320^

IKIM

A27

9^

291^

269^

089^

MA

X 2

20 K

TM

AX F

L140

335^

LAVA

X

IBULA

MH

A 7

000

MA

X 2

50 K

TM

AX F

L250

MH

A F

L150

111^

291^

BIP

OP

vect

ors

for

ILS

EXPE

CT

RAD

AR

appr

oach

Rw

y 20

Cha

ngi

EAST

Rw

y 02

R/20

L1

is s

olel

y fo

r us

e by

the

Repu

blic

of

Sing

apor

e A

ir F

orce

(RS

AF)

Air

craf

t

MA

X 2

20 K

TM

AX F

L140

203^

MH

A 3

000

023^

NYLO

N


22A

lt S

et:

hPa

T

rans

lev

el:

FL13

0

SURG

A 1

B [SURG

1B]

RNAV (GNSS) ARR

IVAL

From

SURG

A.

To I

KA

GO

, tu

rn L

EFT.

To

IKIM

A,

turn

RIG

HT.

To

IBULA

at

or b

elow

FL1

80,

spee

d 25

0 KT,

tur

n RI

GHT.

To

LAVA

X,

spee

d 22

0 KT,

tur

n LE

FT.

To R

UVIK

at

or a

bove

80

00.

To D

OVA

N a

t or

abo

ve 4

000,

tur

n RI

GH

T. T

o BIP

OP

at o

r ab

ove

3000

, sp

eed

190

KT.

12

NO

T TO

SCA

LE

010

2030

4050

10

9

2120

35

97

2347

5 MAY 17

8A

t 220 K

T

At

250 K

T

At

190 K

TCO

NTO

UR

INTE

RVA

LS

4000

2000


CHANGES:

WSSS/SINCHANGI

SINGAPORE, SINGAPOREJEPPESEN


MINIMUM CLIMB GRADIENT CRITERIA

10-3

The Instrument Departure Procedures are only applicable for aircraft with all engines

obstacles throughout the areas concerned in relation to the certificated performance ofthe individual aircraft type. It is also the responsibility of the operator to ensure thatcontingency procedures comply fully with the airplane performance requirements ofAnnex 6.

RUNWAY 02L

When there are no reports of vessel movement along the northern shipping channel, orwhere the reported vessel height is less than 32m (105 ft) AMSL, the aircraft minimumnet climb gradient shall be at 3.3%.

Where the reported vessel height is 33m (108 ft) AMSL or higher, ATC shall advisedeparting pilots of the vessel height. Pilots, on receipt of this information, shall applythe minimum net climb gradient in accordance with the table below.

The specific routes to be followed are depicted in SID Charts pages. Altitude restrictions

procedures for the individual type of aircraft and to conduct the necessary examination ofoperating. It remains the responsibility of the operator to develop contingency

After the aircraft has reached or passed the minimum crossing altitude over vessel,the minimum net climb gradient shall be 3.3%.

RUNWAY 02C

When there are no reports of vessel movement along the northern shipping channel, orwhere the reported vessel height is less than 69m (226 ft) AMSL, the aircraft minimumnet climb gradient shall be at 3.3%.

Where the reported vessel height is 70m (230 ft) AMSL or higher, ATC shall advise

Minimum net climb gradient specifies obstacle clearance requirements.

at fixes and/or DME specify ATC/airspace requirements.

In the event that the minimum net climb gradient cannot be achieved, pilots shall informATC. ATC shall hold departures if pilots indicate that they are unable to meet therequired net climb gradient.

22 SEP 17

feetmeters

Minimum Crossing Altitude Over VesselGradient(%)

Ht of Vessel(meters AMSL)

33

40

50

60

70

80

90

100

140

110

120

130

9.7

10.7

11.7

12.7

13.7

39

49

59

69

79

89

99

109

119

129

139

149

355

388

421

454

486

3.4

4.0

4.9

5.8

6.8

7.8

8.8

125

158

191

224

257

290

322

Runway 02L minimum crossing altitude over vessel revised.

departing pilots of the vessel height. Pilots, on receipt of this information, shall applythe minimum net climb gradient in accordance with the following table.


CHANGES:

WSSS/SINCHANGI

SINGAPORE, SINGAPOREJEPPESEN


MINIMUM CLIMB GRADIENT CRITERIA

10-3A

After the aircraft has reached or passed the minimum crossing altitude over vessel,the minimum net climb gradient shall be 3.3%.

Refer to Standard Instrument Departures for Runways 20C and 20R.

DETERMINATION OF CLIMB GRADIENT BY OPERATORS

The minimum net climb gradients specified above need not apply to operators who wish

- The most penalizing obstacle is taken into account under both all-engines operatingprocedures as well as one-engine-out procedures; and

- The required minimum obstacle clearance (MOC) is met under all engines operatingprocedures.

For the above calculations, operators shall use the following information:

a. The most penalizing obstacle is a tall vessel which is on the extended center line ofthe runway. (ATC shall advise pilots of the height of the tall vessel.)

b. The required MOC is 0.8% of the distance (d) from the departure end of runway(DER) to the obstacle, in accordance with Volume II of ICAO Doc 8168:Procedures for Air Navigation Services Operations (PANS-OPS) where, in the caseof Singapore Changi Airport, the DER is defined as the end of the clearway.

c. The distance (d) for departure Runways 02L/02C is measured from the DER to theshipping channel north of Changi. The distance (d) for departure Runways 20C/20R ismeasured from the DER to the boundary of the restricted waters south of Changi

feetmeters

Minimum Crossing Altitude Over VesselGradient(%)

Ht of Vessel(meters AMSL)

70

80

90

100

140

110

120

130

4.7

5.1

5.5

6.0

6.4

89

99

119

129

139

149

159

390

423

456

489

522

3.4

3.8

4.3

292

325

358109

to calculate their own climb gradients based on actual lift-off point, provided thecalculation ensures the following:

RUNWAYS 20C AND 20R

All departures on Runway 20C shall be on a minimum net climb gradient of 7% untilreaching or passing 2500 ft. Thereafter, the minimum net climb gradient shall be 3.3%.

All departures on Runway 20R shall be on a minimum net climb gradient of 6% untilreaching or passing 2500 ft. Thereafter, the minimum net climb gradient shall be 3.3%.

wherein tall vessels of height above 49m (161 ft) AMSL are not permitted.The distance (d) for the various departure runways is as follows:

22 SEP 17

Departure Runway Distance (d)

02L

02C

1100m

2590m

20C

20R

9670m

12830m

None.


COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST



COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

BATAM

Hang N

adim

WID

D

SIN

GAPORE

Paya L

ebar

WSAP

SIN

GAPORE

Sele

tar

WSSL

01-00

01-30

104-0035

00

RPA

4000

6000

10000

6000

1500

2500

2000

Rwy

20C:

Dep

artu

res

shal

l be

on

a

Rwy

02C:

See

10-3

and

10-

3A.

2. C

omm

unic

atio

ns f

ailu

re o

ccur

s im

med

iate

ly a

fter

dep

artu

re o

n:

1. S

et t

rans

pond

er t

o M

ode

A/C

cod

e 76

00.

SID

INIT

IAL

CLI

MB

Rwy

02C:

Proc

eed

stra

ight

ahe

ad t

o N

ylon

Hol

ding

Are

a (N

HA

) cl

imbi

ng t

o th

e la

st

Rwy

20C:

Proc

eed

stra

ight

ahe

ad t

o Sa

mko

Hol

ding

Are

a (S

HA

) cl

imbi

ng t

o th

e la

st

assi

gned

alt

itud

e. T

here

afte

r re

fer

to10

-1P

page

s fo

r ra

dio

com

mun

icat

ions

assi

gned

alt

itud

e. T

here

afte

r re

fer

to10

-1P

page

s fo

r ra

dio

com

mun

icat

ions

fail

ure

proc

edur

e.

fail

ure

proc

edur

e.

1A

ADM

IM

RW

Y

02C

20C

unti

l re

achi

ng o

r pa

ssin

g 25

00.

min

imum

net

cli

mb

grad

ient

of

7.0%

Apt

Ele

v

5. A

ll S

IDs

incl

ude

nois

e pr

efer

enti

al r

oute

s.

1.

RA

DA

R r

equir

ed.

RNAV (GNSS) DEP

ART

URE

S

7.0%

V/V

(fp

m)

532

709

1063

1418

1772

2127

Gnd

spe

ed-K

T75

100

150

200

250

300

For

min

imum

cli

mb

grad

ient

cri

teri

a:

Cha

ngi

EAST

Rw

y 02

R/20

LA

clos

ed d

ue d

evel

opm

ent

wor

ks.

TO

KIM

115^

IBIX

U

203^

IBIV

A

A

AG

RO

T

DO

KTA DO

GRA

169^

255^

262^

ABVIP

ADM

IM

276^

ASUNA

204^

SA

MKO

023^

CHA

NG

ES:

WSSS/

SIN

| J

EPPE

SEN

, 20

17.

ALL

RIG

HTS

RES

ERVED

.

JEPPESEN

CHA

NG

I3

NO

V 1

710

-3B

.RNAV.SID.

Tran

s al

t: 1

1000

2.

RNA

V 1

Navig

ati

on S

pecif

icati

on G

NSS

requir

ed.

3. A

ircr

aft

unab

le t

o fl

y th

e SI

D p

rofi

le s

hall

RAD

AR

vect

orin

g, i

f ne

cess

ary.

info

rm A

TC p

rior

to

depa

rtur

e an

d to

EXPE

CT

4. C

ruis

ing

leve

ls w

ill

be i

ssue

d af

ter

take

-off

by S

inga

pore

RA

DA

R.

22

ADMIM

3B

[ADMI3B]

ADMIM

1A [ADMI1A]

or a

s di

rect

ed b

y A

TC

turn

RIG

HT.

To

DO

KTA

at

or a

bove

400

0,To

TO

KIM

on

cour

se 0

23^

at o

r ab

ove

2000

,

turn

RIG

HT.

To

DO

GRA

at

or b

elow

600

0,tu

rn R

IGH

T. T

o A

GRO

T, t

urn

RIG

HT.

To

ABVIP

. To

AD

MIM

at

or a

bove

100

00,

turn

RIG

HT.

To

ASU

NA

.To

IBIX

U o

n co

urse

203

^ at

or

abov

e 15

00.

To I

BIV

A a

t or

abo

ve 2

500.

To

SAM

KO

at

or

3000

Init

ial

clim

b cl

eara

nce

05101520 525

2120

8

6

17

9

4

9

21

630

SINGAPO

RE, SINGAPO

RE.Eff.9.Nov.

2.7

AD

MIM

2B r

epla

ced

by A

DM

IM 3

B,

IBIB

I w

aypo

int

wit

hdra

wn.

belo

w 6

000,

tur

n RI

GH

T. T

o A

BVIP

, tu

rnRI

GH

T. T

o A

DM

IM a

t or

abo

ve 1

0000

, tu

rnRI

GH

T. T

o A

SUN

A.

ADM

IM3B

ADM

IM 1

A

ADMIM 3B

262^

NO

T T

O S

CA

LE

22

20

34

24

UNTIL

PA

SSIN

G 4

000 A

ND N

OT E

XCEED

250 K

T U

NTIL

PA

SSIN

G 1

0000

SHA

LL N

OT E

XCEED 2

30 K

T

.SPEED

:


COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST


COMMSCOMMS LOSTCOMMS LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

BATAM

Hang N

adim

WID

D

SIN

GAPORE

Paya L

ebar

WSAP

SIN

GAPORE

Sele

tar

WSSL

01-00

01-30

104-00

3500

RP

A

2000

4000

1500

2500

6000

6000

10000

Cha

ngi

EAST

Rw

y 02

R/20

LA

clos

ed d

ue d

evel

opm

ent

wor

ks.

TO

PO

M

DO

KTA

115^

DO

GRA

169^

AG

RO

T

255^

ABVIP

262^

ADM

IM

ASUNA27

6^

LEDO

X

203^LE

TG

O

SA

MKO

197^

204^

023^

A

CHA

NG

ES:

WSS

S/SIN

| J

EPPE

SEN

, 20

17.

ALL

RIG

HTS

RES

ERVED

.

JEPPESEN

CHA

NG

I3

NO

V 1

710

-3C

SINGAPO

RE, SINGAPO

RE.RNAV.SID.

05101520 525

For

min

imum

cli

mb

grad

ient

cri

teri

a:

Rwy

20R:

Dep

artu

res

shal

l be

on

a

Rwy

02L:

See

10-

3 an

d 10

-3A

.

unti

l re

achi

ng o

r pa

ssin

g 25

00.

min

imum

net

cli

mb

grad

ient

of

6.0%

6.0%

V/V

(fp

m)

456

608

911

1215

1519

1823

Gnd

spe

ed-K

T75

100

150

200

250

300

2. C

omm

unic

atio

ns f

ailu

re o

ccur

s im

med

iate

ly a

fter

dep

artu

re o

n:

1. S

et t

rans

pond

er t

o M

ode

A/C

cod

e 76

00.

Rwy

02L:

Pro

ceed

str

aigh

t ah

ead

to N

ylon

Hol

ding

Are

a (N

HA

) cl

imbi

ng t

o th

e la

st

Rwy

20R:

Pro

ceed

str

aigh

t ah

ead

to S

amko

Hol

ding

Are

a (S

HA

) cl

imbi

ng t

o th

e la

st

assi

gned

alt

itud

e. T

here

afte

r re

fer

to10

-1P

page

s fo

r ra

dio

com

mun

icat

ions

assi

gned

alt

itud

e. T

here

afte

r re

fer

to10

-1P

page

s fo

r ra

dio

com

mun

icat

ions

fail

ure

proc

edur

e.

fail

ure

proc

edur

e.

SID

INIT

IAL

CLI

MB

RW

Y

02L

20R

5. A

ll S

IDs

incl

ude

nois

e pr

efer

enti

al r

oute

s.

RNAV (GNSS) DEP

ART

URE

S

RAD

AR

vect

orin

g, i

f ne

cess

ary.

info

rm A

TC p

rior

to

depa

rtur

e an

d to

EXPE

CT

4. C

ruis

ing

leve

ls w

ill

be i

ssue

d af

ter

take

-off

by S

inga

pore

RA

DA

R.

22

ADMIM

3F [ADMI3F]

ADMIM

1E [ADMI1E]

or a

s di

rect

ed b

y A

TC3000

Init

ial

clim

b cl

eara

nce

Apt

Ele

v3.

Air

craf

t un

able

to

fly

the

SID

pro

file

sha

ll

requir

ed.

2.

RNA

V 1

Navig

ati

on S

pecif

icati

on G

NSS

1.

RA

DA

R r

equir

ed.

Tran

s al

t: 1

1000

To T

OPO

M o

n co

urse

023

^ at

or

abov

e 20

00,

turn

RIG

HT.

To

DO

KTA

at

or a

bove

400

0,

turn

RIG

HT.

To

DO

GRA

at

or b

elow

600

0,tu

rn R

IGH

T. T

o A

GRO

T, t

urn

RIG

HT.

To

To A

BVIP

. To

AD

MIM

at

or a

bove

100

00,

turn

RIG

HT.

To

ASU

NA

.To

LED

OX o

n co

urse

203

^ at

or

abov

e 15

00.

ADM

IM1E

9

6

2021

8

17

21

9

4

630

.Eff.9.Nov.

2.7

AD

MIM

2F

repl

aced

by

AD

MIM

3F,

LEG

AS

way

poin

t w

ithd

raw

n.

To L

ETG

O a

t or

abo

ve 2

500,

tur

n LE

FT.

ToSA

MKO

at

or b

elow

600

0, t

urn

RIG

HT.

To

ABVIP

, tu

rn R

IGH

T. T

o A

DM

IM a

t or

abo

ve10

000,

tur

n RI

GH

T. T

o A

SUN

A.

ADM

IM3F

ADM

IM 1

E

ADMIM 3F

262^

NO

T T

O S

CA

LE

22

20

34

24

UNTIL

PA

SSIN

G 4

000 A

ND N

OT E

XCEED

250 K

T U

NTIL

PA

SSIN

G 1

0000

SHA

LL N

OT E

XCEED 2

30 K

T

.SPEED

:


COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST



COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

BATAM

Hang N

adim

WID

D

SIN

GAPORE

Paya L

ebar

WSAP

SIN

GAPORE

Sele

tar

WSSL

01-00

01-30

104-00

3500

RP

A

4000

2000

6000

1500

2500

4000

6. A

ll S

IDs

incl

ude

nois

e pr

efer

enti

al r

oute

s.

DO

NDI

113^

TO

KIM

115^

DO

KTA

169^

023^

A

DO

GRA

203^

IBIX

U

IBIV

A

Cha

ngi

EAST

Rw

y 02

R/20

LA

clos

ed d

ue d

evel

opm

ent

wor

ks.

DO

SNO

150^

ANIT

O

DIV

SA

120^ BA

TAM

B T

M11

6.0

BTM

D

180^

Apt

Ele

v

1.

RA

DA

R r

equir

ed.

RNAV (GNSS) DEP

ART

URE

S

JEPPESEN

10-3

D.RNAV.SID.

Tran

s al

t: 1

1000

2.

RNA

V 1

Navig

ati

on S

pecif

icati

on G

NSS

requir

ed.

3. A

ircr

aft

unab

le t

o fl

y th

e SI

D p

rofi

le s

hall

RAD

AR

vect

orin

g, i

f ne

cess

ary.

info

rm A

TC p

rior

to

depa

rtur

e an

d to

EXPE

CT

22

ANITO 7

B [ANIT7B

]ANITO 6

A [ANIT6A

]

05101520 525

INIT

IAL

CLI

MB

Rwy

20C:

Dep

artu

res

shal

l be

on

a

Rwy

02C:

See

10-3

and

10-

3A.

unti

l re

achi

ng o

r pa

ssin

g 25

00.

min

imum

net

cli

mb

grad

ient

of

7.0%

7.0%

V/V

(fp

m)

532

709

1063

1418

1772

2127

Gnd

spe

ed-K

T75

100

150

200

250

300

For

min

imum

cli

mb

grad

ient

cri

teri

a:

2. C

omm

unic

atio

ns f

ailu

re o

ccur

s im

med

iate

ly a

fter

dep

artu

re o

n:

1. S

et t

rans

pond

er t

o M

ode

A/C

cod

e 76

00.

Rwy

02C:

Proc

eed

stra

ight

ahe

ad t

o N

ylon

Hol

ding

Are

a (N

HA

) cl

imbi

ng t

o th

e la

st

Rwy

20C:

Proc

eed

stra

ight

ahe

ad t

o Sa

mko

Hol

ding

Are

a (S

HA

) cl

imbi

ng t

o th

e la

st

assi

gned

alt

itud

e. T

here

afte

r re

fer

to10

-1P

page

s fo

r ra

dio

com

mun

icat

ions

assi

gned

alt

itud

e. T

here

afte

r re

fer

to10

-1P

page

s fo

r ra

dio

com

mun

icat

ions

fail

ure

proc

edur

e.

fail

ure

proc

edur

e.

turn

RIG

HT.

To

DO

GRA

at

or b

elow

600

0,

To T

OKIM

on

cour

se 0

23^

at o

r ab

ove

2000

,

SID 6A

RW

Y

02C

turn

RIG

HT.

To

DO

KTA

at

or a

bove

400

0,

To I

BIX

U o

n co

urse

203

^ at

or

abov

e 15

00.

ANIT

O

ANIT

O7B

or a

s di

rect

ed b

y A

TC

20C

3000

Init

ial

clim

b cl

eara

nce

WSSS/

SIN

CHA

NG

I

CHA

NG

ES:

| J

EPPE

SEN

, 20

17.

ALL

RIG

HTS

RES

ERVED

.

turn

RIG

HT.

To

DO

SNO

, tu

rn L

EFT.

To

AN

ITO

.

4. O

n in

itia

l co

ntac

t w

hen

requ

esti

ng A

TC,

cros

s A

NIT

O.

info

rm A

TC o

f th

e fl

ight

lev

el a

ircr

aft

can

5. C

ruis

ing

leve

ls w

ill

be i

ssue

d af

ter

take

-off

by S

inga

pore

RA

DA

R.

3 N

OV 1

7

3

4

6

7

17

75

21

9

630

SINGAPO

RE, SINGAPO

RE.Eff.9.Nov.

2.7

ANITO 6A

ANIT

O 7

B

AN

ITO

6B r

epla

ced

by A

NIT

O 7

B,

IBIB

I w

aypo

int

wit

hdra

wn.

To I

BIV

A a

t or

abo

ve 2

500,

tur

n LE

FT.

ToD

ON

DI.

To

DIV

SA a

t or

abo

ve 4

000,

tur

nRI

GH

T. T

o BTM

VO

R, t

urn

LEFT

. To

DO

GRA

at o

r be

low

600

0, t

urn

RIG

HT.

To

DO

SNO

,tu

rn L

EFT.

To

AN

ITO

.

NO

T T

O S

CA

LE

113^

22

20

34

24

UNTIL

PA

SSIN

G 4

000 A

ND N

OT E

XCEED

250 K

T U

NTIL

PA

SSIN

G 1

0000

.SPEED

:SHA

LL N

OT E

XCEED 2

30 K

T


COMMS

LOST

COMMS

LOST

COMMS

LOST

LOST COMMSLOST COMMSLOST COMMSLOST

COMMSCOMMS LOSTCOMMS LOSTLOST

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

BATAM

Hang N

adim

WID

D

SIN

GAPORE

Paya L

ebar

WSAP

SIN

GAPORE

Sele

tar

WSSL

01-00

01-30

104-00

3500

R PA

2000

4000

25001

500

6000

4000

Rwy

02L:

Pro

ceed

str

aigh

t ah

ead

to

Nyl

on H

oldi

ng A

rea

(NH

A)

clim

bing

Rwy

20R:

Pro

ceed

str

aigh

t ah

ead

to

Sam

ko H

oldi

ng A

rea

(SH

A)

clim

bing

to t

he l

ast

assi

gned

alt

itud

e.

to t

he l

ast

assi

gned

alt

itud

e.

7600

.1.

Set

tra

nspo

nder

to

Mod

e A

/C c

ode

2. C

omm

unic

atio

ns f

ailu

re o

ccur

s im

med

iate

ly a

fter

dep

artu

re o

n:

Ther

eaft

er r

efer

to

10-1

P pa

ges

Ther

eaft

er r

efer

to

10-1

P pa

ges

for

proc

edur

e.ra

dio

com

mun

icat

ions

fai

lure

for

radi

o co

mm

unic

atio

ns f

ailu

repr

oced

ure.

6. A

ll S

IDs

incl

ude

nois

e pr

efer

enti

al r

oute

s.

1.

RA

DA

R r

equir

ed.

RNAV (GNSS) DEP

ART

URE

S

For

min

imum

cli

mb

grad

ient

cri

teri

a:Rw

y 02

L: S

ee 1

0-3

and

10-3

A.

Rwy

20R:

Dep

artu

res

shal

l be

on

a

6.0%

V/V

(fp

m)

456

608

911

1215

1519

1823

Gnd

spe

ed-K

T75

100

150

200

250

300

min

imum

net

cli

mb

grad

ient

of

6.0%

unti

l re

achi

ng o

r pa

ssin

g 25

00.

DO

SNO

180^

ANIT

O

150^

DIV

SA

113^

BATA

M

B T

M11

6.0

BTM

D

120^

A

TO

PO

M

115^

023^

169^DO

KTA

LETG

OLEDO

X

203^

DO

GRA

CHA

NG

ES:

WSS

S/SIN

| J

EPPE

SEN

, 20

17.

ALL

RIG

HTS

RES

ERVED

.

JEPPESEN

CHA

NG

I3

NO

V 1

710

-3E

SINGAPO

RE, SINGAPO

RE

Tran

s al

t: 1

1000

requir

ed.

2.

RNA

V 1

Navig

ati

on S

pecif

icati

on G

NSS

3. A

ircr

aft

unab

le t

o fl

y th

e SI

D p

rofi

le s

hall

in

form

ATC

pri

or t

o de

part

ure

and

to E

XPE

CT

RAD

AR

vect

orin

g, i

f ne

cess

ary.

4. O

n in

itia

l co

ntac

t w

hen

requ

esti

ng A

TC,

cros

s A

NIT

O.

info

rm A

TC o

f th

e fl

ight

lev

el a

ircr

aft

can

5. C

ruis

ing

leve

ls w

ill

be i

ssue

d af

ter

take

-off

by

Sin

gapo

re R

AD

AR.

Apt

Ele

v

22 SID

INIT

IAL

CLI

MB

6E

ANIT

O

7F

ANIT

O

RW

Y

02L

20R

or a

s di

rect

ed b

y A

TC3000

Init

ial

clim

b cl

eara

nce

To T

OPO

M o

n co

urse

023

^ at

or

abov

e 20

00,

turn

RIG

HT.

To

DO

KTA

at

or a

bove

400

0,

turn

RIG

HT.

To

DO

GRA

at

or b

elow

600

0,

To A

NIT

O.

turn

RIG

HT.

To

DO

SNO

, tu

rn L

EFT.

To L

EDO

X o

n co

urse

203

^ at

or

abov

e 15

00.

DIV

SA a

t or

abo

ve 4

000,

tur

n RI

GH

T. T

o

ANITO 7

F [ANIT7F

]ANITO 6

E [ANIT6E

]

Cha

ngi

EAST

Rw

y 02

R/20

LA

clos

ed d

ue d

evel

opm

ent

wor

ks.

05101520 525

.RNAV.SID.

9

21

8

6

7

17

75

630

.Eff.9.Nov.

2.7

ANITO 6E

ANIT

O 7

F

AN

ITO

6F

repl

aced

by

AN

ITO

7F,

LEG

AS

way

poin

t w

ithd

raw

n.

To L

ETG

O a

t or

abo

ve 2

500,

tur

n LE

FT.

To

BTM

VO

R, t

urn

LEFT

. To

DO

GRA

at

orbe

low

600

0, t

urn

RIG

HT.

To

DO

SNO

, tu

rnLE

FT.

To A

NIT

O.

NO

T T

O S

CA

LE

113^

22

20

34

24

UNTIL

PA

SSIN

G 4

000 A

ND N

OT E

XCEED

250 K

T U

NTIL

PA

SSIN

G 1

0000

SHA

LL N

OT E

XCEED 2

30 K

T

.SPEED

:



COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

LOST


COMMS


WMKJ

SINGAPOREPaya Lebar

WSAP

104-00

3500

RAP

11000

7000

7000

4000

1500

2500

2000

For minimum climb gradient criteria:

Rwy 20C: Departures shall be on a

Rwy 02C: See 10-3 and 10-3A.

until reaching or passing 2500.minimum net climb gradient of 7.0%

7.0% V/V (fpm) 532 709 1063 1418 1772 2127

Gnd speed-KT 75 100 150 200 250 300

Changi EAST Rwy 02R/20LA

closed due development works.

AROSO

2A

NOT TO SCALE

AROSO

AKMET

308^

AKOMAAROSO 2A:

ARO

SO

4B

TEKONG

V T K116.5 VTKD

DIVSA

DOSPA

023^

A

IBIXU

113^IBIVA

DONDI

TOKIM

023^

203^

332^

AROSO 4B:

342^

22Apt Elev

5. All SIDs include noise preferential routes.

2. RNAV 1 Navigation Specification GNSS required.1. RADAR required.

3. Aircraft unable to fly the SID profile shall inform ATC prior to departure and to EXPECT RADAR vectoring, if necessary.

Trans alt: 11000

4. Cruising levels will be issued after take-off by Singapore RADAR.

AROSO 2A [AROS2A], AROSO 4B [AROS4B]RNAV (GNSS) DEPARTURES

CHA

NG

ES:|

JEPPESEN, 2017. A

LL RIGHTS RESERV

ED.

SID INITIAL CLIMBRWY

02C

20C

To TOKIM on course 023^ at or above 2000, turn LEFT. To

To IBIXU on course 203^ at or above 1500. To IBIVA at or

Initial climb clearance or as directed by ATC3000

2. Communications failure occurs immediately after departure on:


Rwy 02C: Proceed straight ahead to NylonHolding Area (NHA) climbing to the lastassigned altitude. Thereafter refer to10-1P pages for radio communications failure procedure.Rwy 20C: Proceed straight ahead to Samko Holding Area (SHA) climbing to the last assigned altitude. Thereafter refer to 10-1P pages for radio communications failure procedure.

RNAV (G

NSS) D

EPARTU

RES

AROSO2A

AROSO4B

AKOMA at or above 7000, turn LEFT. To AKMET at or above11000. To AROSO.

0 5 10 15 205 25

JEPPESEN

10-3F.RNAV.SID.

ARO

SO 4B [A

ROS4B]

ARO

SO 2A

[ARO

S2A]

3 NO

V 17

24

14

21

18

10

4

5

3

WSSS/SIN

CHA

NG

I

637

SINGAPO

RE, SINGAPO

RE.Eff.9.N

ov.

2.7

above 2500, turn LEFT. To DONDI. To DIVSA at or above 4000,speed 230 KT, turn LEFT. To DOSPA, turn LEFT. To VTK VOR ator above 7000. To AKOMA, turn LEFT. To AKMET at or above11000. To AROSO.

ARO

SO 3B

replaced by ARO

SO 4B

, IBIB

I waypoint w

ithdrawn.

342^

34 24

At 230 KT

RWY 20C: SHALL NOT EXCEED 230 KT UNTIL DIVSAAND NOT EXCEED 250 KT UNTIL PASSING 10000

4000 AND NOT EXCEED 250 KT UNTIL PASSING 10000RWY 02C: SHALL NOT EXCEED 230 KT UNTIL PASSING.SPEED:

01-30



COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

LOST


COMMS


WMKJ

SINGAPOREPaya Lebar

WSAP

104-00

3500

RAP

2500

1500

4000

2000

7000

7000

11000


Rwy 20R: Departures shall be on aRwy 02L: See 10-3 and 10-3A.


4. Cruising levels will be issued after take-off by Singapore RADAR.5. All SIDs include noise preferential routes.


6.0% V/V (fpm) 456 608 911 1215 1519 1823

Gnd speed-KT 75 100 150 200 250 300


02L

20R



ATRUM

ARO

SO 2

E

AKOMA

333^

AKMET

AROSO

308^

ARO

SO 4

F

TEKONG

V T K116.5 VTKD

342^

342^

203^

A

113^

LEDOX

LETGO

023^

DIVSA

DOSPA

TOPOM

023^

AROSO 2E:

CHA

NG

ES:

WSSS/SIN

| JEPPESEN

, 2017. ALL RIG

HTS RESERV

ED.

JEPPESEN

CHA

NG

I3 N

OV 17

10-3GSIN

GAPO

RE, SINGAPO

RE.RNAV.SID.

ARO

SO 2E [A

ROS2E], A

ROSO

4F [ARO

S4F]RN

AV (G

NSS) D

EPARTU

RESApt Elev

22 3. Aircraft unable to fly the SID profile shall inform ATC prior to departure and to EXPECT RADAR vectoring, if necessary.

Trans alt: 11000 AROSO 2E [AROS2E], AROSO 4F [AROS4F]RNAV (GNSS) DEPARTURES

NOT TO SCALE

To TOPOM on course 023^ at or above 2000, turn LEFT. To

at or above 11000. To AROSO.ATRUM. To AKOMA at or above 7000, turn LEFT. To AKMET

To LEDOX on course 203^ at or above 1500. To LETGO at or

AROSO2E



Rwy 02L: Proceed straight ahead to NylonHolding Area (NHA) climbing to the lastassigned altitude. Thereafter refer to10-1P pages for radio communications failure procedure.Rwy 20R: Proceed straight ahead to Samko Holding Area (SHA) climbing to the last assigned altitude. Thereafter refer to 10-1P pages for radio communications failure procedure.

0 5 10 15 205 25

24

14

1421

3

8 5

10


637

.Eff.9.Nov.

AROSO4F

above 2500, turn LEFT. To DIVSA at or above 4000, speed230 KT, turn LEFT. To DOSPA, turn LEFT. To VTK VOR at orabove 7000. To AKOMA, turn LEFT. To AKMET at or above11000. To AROSO.

ARO

SO 3F replaced by A

ROSO

4F, LEGA

S waypoint w

ithdrawn.

2.7

34 24

At 230 KT

RWY 20R: SHALL NOT EXCEED 230 KT UNTIL DIVSAAND NOT EXCEED 250 KT UNTIL PASSING 10000

4000 AND NOT EXCEED 250 KT UNTIL PASSING 10000RWY 02L: SHALL NOT EXCEED 230 KT UNTIL PASSING.SPEED:

01-30


COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST



COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

BATAM

Hang N

adim

WID

D

SIN

GAPORE

Paya L

ebar

WSAP

SIN

GAPORE

Sele

tar

WSSL

01-00

01-30

104-00

3500

RP

A

4000

2000

1500

2500

4000

6000

Cha

ngi

EAST

Rw

y 02

R/20

LA

clos

ed d

ue d

evel

opm

ent

wor

ks.

TO

KIM

115^

DO

KTA

169^

A023^

203^

113^

IBIX

U

IBIV

ADO

NDI DIV

SA

120^ BATA

M

B T

M11

6.0

BTM

D

DO

GRA

VENPA

126^

ATKA

X

097^

BA

VUS

092^

DO

SNO

180^

2. C

omm

unic

atio

ns f

ailu

re o

ccur

s im

med

iate

ly a

fter

dep

artu

re o

n:

1. S

et t

rans

pond

er t

o M

ode

A/C

cod

e 76

00.

Rwy

02C:

Proc

eed

stra

ight

ahe

ad t

o N

ylon

Hol

ding

Are

a (N

HA

) cl

imbi

ng t

o th

e la

st

Rwy

20C:

Proc

eed

stra

ight

ahe

ad t

o Sa

mko

Hol

ding

Are

a (S

HA

) cl

imbi

ng t

o th

e la

st

assi

gned

alt

itud

e. T

here

afte

r re

fer

to10

-1P

page

s fo

r ra

dio

com

mun

icat

ions

assi

gned

alt

itud

e. T

here

afte

r re

fer

to10

-1P

page

s fo

r ra

dio

com

mun

icat

ions

fail

ure

proc

edur

e.

fail

ure

proc

edur

e.

Apt

Ele

v

5. A

ll S

IDs

incl

ude

nois

e pr

efer

enti

al r

oute

s.

1.

RA

DA

R r

equir

ed.

RNAV (GNSS) DEP

ART

URE

S

JEPPESEN

10-3

H.RNAV.SID.

Tran

s al

t: 1

1000

2.

RNA

V 1

Navig

ati

on S

pecif

icati

on G

NSS

requir

ed.

3. A

ircr

aft

unab

le t

o fl

y th

e SI

D p

rofi

le s

hall

RAD

AR

vect

orin

g, i

f ne

cess

ary.

info

rm A

TC p

rior

to

depa

rtur

e an

d to

EXPE

CT

4. C

ruis

ing

leve

ls w

ill

be i

ssue

d af

ter

take

-off

by S

inga

pore

RA

DA

R.

22

BAVUS 3B

[BA

VU3B

]BA

VUS 1A

[BA

VU1A

]

Rwy

20C:

Dep

artu

res

shal

l be

on

a

Rwy

02C:

See

10-3

and

10-

3A.

unti

l re

achi

ng o

r pa

ssin

g 25

00.

min

imum

net

cli

mb

grad

ient

of

7.0%

7.0%

V/V

(fp

m)

532

709

1063

1418

1772

2127

Gnd

spe

ed-K

T75

100

150

200

250

300

For

min

imum

cli

mb

grad

ient

cri

teri

a:

SID

INIT

IAL

CLI

MB

RW

Y

02C

20C

or a

s di

rect

ed b

y A

TC

turn

RIG

HT.

To

DO

KTA

at

or a

bove

400

0,To

TO

KIM

on

cour

se 0

23^

at o

r ab

ove

2000

,

turn

RIG

HT.

To

DO

GRA

at

or b

elow

600

0,

To I

BIX

U o

n co

urse

203

^ at

or

abov

e 15

00.

3000

Init

ial

clim

b cl

eara

nce

05101520 525

WSSS/

SIN

CHA

NG

I

CHA

NG

ES:

| J

EPPE

SEN

, 20

17.

ALL

RIG

HTS

RES

ERVED

.

3 N

OV 1

7

turn

RIG

HT.

To

DO

SNO

, tu

rn L

EFT.

To

VEN

PA,

turn

LEF

T. T

o A

TKA

X,

turn

LEF

T.To

BA

VUS.

1A

BA

VUS

7

6

4

3

9

21

17 44

131

121

1132

SINGAPO

RE, SINGAPO

RE.Eff.9.Nov.

BA

VUS

2B r

epla

ced

by B

AVUS

3B,

IBIB

I w

aypo

int

wit

hdra

wn.

To I

BIV

A a

t or

abo

ve 2

500,

tur

n LE

FT.

ToD

ON

DI.

To

DIV

SA a

t or

abo

ve 4

000,

tur

nRI

GH

T. T

o BTM

VO

R, t

urn

LEFT

. To

DO

GRA

at o

r be

low

600

0, t

urn

RIG

HT.

To

DO

SNO

,tu

rn L

EFT.

To

VEN

PA,

turn

LEF

T. T

o A

TKA

X,

turn

LEF

T. T

o BA

VUS.

3B

BA

VUS

BAVUS 1A

BAVUS

3B

2.7

113^

NO

T T

O S

CA

LE

22

20

34

24

SHA

LL N

OT E

XCEED 2

30 K

T

.SPEED

:

250 K

T U

NTIL

PA

SSIN

G 1

0000

UNTIL

PA

SSIN

G 4

000 A

ND N

OT E

XCEED


COMMS

LOST

COMMS

LOST

COMMS

LOST



LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

BATAM

Hang N

adim

WID

D

SIN

GAPORE

Paya L

ebar

WSAP

SIN

GAPORE

Sele

tar

WSSL

01-00

01-30

104-00

3500

RP

A

2000

4000

6000

4000

25001

500

Rwy

02L:

Pro

ceed

str

aigh

t ah

ead

to

Nyl

on H

oldi

ng A

rea

(NH

A)

clim

bing

Rwy

20R:

Pro

ceed

str

aigh

t ah

ead

to

Sam

ko H

oldi

ng A

rea

(SH

A)

clim

bing

to t

he l

ast

assi

gned

alt

itud

e.

to t

he l

ast

assi

gned

alt

itud

e.

7600

.1.

Set

tra

nspo

nder

to

Mod

e A

/C c

ode

2. C

omm

unic

atio

ns f

ailu

re o

ccur

s im

med

iate

ly a

fter

dep

artu

re o

n:

Ther

eaft

er r

efer

to

10-1

P pa

ges

for

Ther

eaft

er r

efer

to

10-1

P pa

ges

for

proc

edur

e.ra

dio

com

mun

icat

ions

fai

lure

radi

o co

mm

unic

atio

ns f

ailu

repr

oced

ure.

VENPA

126^

ATKA

X

097^

BA

VUS

092^

TO

PO

M

115^

023^

169^DO

KTA

180^

DIV

SA

BATA

M

B T

M11

6.0

BTM

D

DO

GRA

113^

120^

LETG

OLEDO

X

203^

A

DO

SNO

WSS

S/SIN

CHA

NG

I

JEPPESEN

3 N

OV 1

710

-3J

SINGAPO

RE, SINGAPO

RE.RNAV.SID.

5. A

ll S

IDs

incl

ude

nois

e pr

efer

enti

al r

oute

s.

1.

RA

DA

R r

equir

ed.

Tran

s al

t: 1

1000

requir

ed.

2.

RNA

V 1

Navig

ati

on S

pecif

icati

on G

NSS

3. A

ircr

aft

unab

le t

o fl

y th

e SI

D p

rofi

le s

hall

in

form

ATC

pri

or t

o de

part

ure

and

to E

XPE

CT

RAD

AR

vect

orin

g, i

f ne

cess

ary.

4. C

ruis

ing

leve

ls w

ill

be i

ssue

d af

ter

take

-off

by

Sin

gapo

re R

AD

AR.

RNAV (GNSS) DEP

ART

URE

S

For

min

imum

cli

mb

grad

ient

cri

teri

a:Rw

y 02

L: S

ee 1

0-3

and

10-3

A.

Rwy

20R:

Dep

artu

res

shal

l be

on

a

6.0%

V/V

(fp

m)

456

608

911

1215

1519

1823

Gnd

spe

ed-K

T75

100

150

200

250

300

min

imum

net

cli

mb

grad

ient

of

6.0%

unti

l re

achi

ng o

r pa

ssin

g 25

00.

| J

EPPE

SEN

, 20

17.

ALL

RIG

HTS

RES

ERVED

.

SID

INIT

IAL

CLI

MB

RW

Y

02L

20R

or a

s di

rect

ed b

y A

TC3000

Init

ial

clim

b cl

eara

nce

To T

OPO

M o

n co

urse

023

^ at

or

abov

e 20

00,

turn

RIG

HT.

To

DO

KTA

at

or a

bove

400

0,

turn

RIG

HT.

To

DO

GRA

at

or b

elow

600

0,tu

rn R

IGH

T. T

o D

OSN

O,

turn

LEF

T.

To L

EDO

X o

n co

urse

203

^ at

or

abov

e 15

00.

6000

, tu

rn R

IGH

T. T

o D

OSN

O,

turn

LEF

T.

BAVUS 3F

[BA

VU3F

]BA

VUS 1E

[BA

VU1E

]

05101520 525 CHA

NG

ES:

22A

pt E

lev

To V

ENPA

, tu

rn L

EFT.

To

ATK

AX,

turn

LEF

T.

To B

AVUS.

To V

ENPA

, tu

rn L

EFT.

To

ATK

AX,

turn

LEF

T.1E

BA

VUS

Cha

ngi

EAST

Rw

y 02

R/20

LA

clos

ed d

ue d

evel

opm

ent

wor

ks.

8

6

7

17 44

131

121

21

9

1132

.Eff.9.Nov.

3F

BA

VUS

To L

ETG

O a

t or

abo

ve 2

500,

tur

n LE

FT.

ToD

IVSA

at

or a

bove

400

0, t

urn

RIG

HT.

To

BTM

VO

R, t

urn

LEFT

. To

DO

GRA

at

or b

elow

To B

AVUS.

2.7

BAVUS 1E

BAVUS 3

F

BA

VUS

2F r

epla

ced

by B

AVUS

3F,

LEG

AS

way

poin

t w

ithd

raw

n.

NO

T T

O S

CA

LE

113^

22

20

34

24

UNTIL

PA

SSIN

G 4

000 A

ND N

OT E

XCEED

250 K

T U

NTIL

PA

SSIN

G 1

0000

SHA

LL N

OT E

XCEED 2

30 K

T

.SPEED

:


COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST



COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

BATAM

Hang N

adim

WID

D

SIN

GAPORE

Paya L

ebar

WSAP

SIN

GAPORE

Sele

tar

WSSL

01-00

01-30

104-00

3500 R

PA

4000

2000

1500

2500

4000

6000

For

min

imum

cli

mb

grad

ient

cri

teri

a:

Rwy

20C:

Dep

artu

res

shal

l be

on

a

Rwy

02C:

See

10-3

and

10-

3A.

7.0%

V/V

(fp

m)

532

709

1063

1418

1772

2127

Gnd

spe

ed-K

T75

100

150

200

250

300

min

imum

net

cli

mb

grad

ient

of

7.0%

unti

l re

achi

ng o

r pa

ssin

g 25

00.

KA

DA

R

105^

TO

KIM

115^

DO

KTA

169^

A023^

203^

113^

IBIX

U

IBIV

ADO

NDI DIV

SA

120^

BATA

M

B T

M11

6.0

BTM

D

DO

GRA

Cha

ngi

EAST

Rw

y 02

R/20

LA

clos

ed d

ue d

evel

opm

ent

wor

ks.

VENPA

126^

ATKA

X

097^

DO

SNO

180^

2. C

omm

unic

atio

ns f

ailu

re o

ccur

s im

med

iate

ly a

fter

dep

artu

re o

n:

1. S

et t

rans

pond

er t

o M

ode

A/C

cod

e 76

00.

Rwy

02C:

Proc

eed

stra

ight

ahe

ad t

o N

ylon

Hol

ding

Are

a (N

HA

) cl

imbi

ng t

o th

e la

st

Rwy

20C:

Proc

eed

stra

ight

ahe

ad t

o Sa

mko

Hol

ding

Are

a (S

HA

) cl

imbi

ng t

o th

e la

st

assi

gned

alt

itud

e. T

here

afte

r re

fer

to10

-1P

page

s fo

r ra

dio

com

mun

icat

ions

assi

gned

alt

itud

e. T

here

afte

r re

fer

to10

-1P

page

s fo

r ra

dio

com

mun

icat

ions

fail

ure

proc

edur

e.

fail

ure

proc

edur

e.

Apt

Ele

v

5. A

ll S

IDs

incl

ude

nois

e pr

efer

enti

al r

oute

s.

1.

RA

DA

R r

equir

ed.

RNAV (GNSS) DEP

ART

URE

S

JEPPESEN

10-3

K.RNAV.SID.

Tran

s al

t: 1

1000

2.

RNA

V 1

Navig

ati

on S

pecif

icati

on G

NSS

requir

ed.

3. A

ircr

aft

unab

le t

o fl

y th

e SI

D p

rofi

le s

hall

RAD

AR

vect

orin

g, i

f ne

cess

ary.

info

rm A

TC p

rior

to

depa

rtur

e an

d to

EXPE

CT

4. C

ruis

ing

leve

ls w

ill

be i

ssue

d af

ter

take

-off

by S

inga

pore

RA

DA

R.

22

KADAR

3B [KADA3B

]KADAR

1A [KADA1A

]

SID

INIT

IAL

CLI

MB

RW

Y

02C

20C

or a

s di

rect

ed b

y A

TC

turn

RIG

HT.

To

DO

KTA

at

or a

bove

400

0,To

TO

KIM

on

cour

se 0

23^

at o

r ab

ove

2000

,

turn

RIG

HT.

To

DO

GRA

at

or b

elow

600

0,

To I

BIX

U o

n co

urse

203

^ at

or

abov

e 15

00.

3000

Init

ial

clim

b cl

eara

nce

| J

EPPE

SEN

, 20

17.

ALL

RIG

HTS

RES

ERVED

.

3 N

OV 1

7

turn

RIG

HT.

To

DO

SNO

, tu

rn L

EFT.

To

To K

AD

AR.

05101520 525 CHA

NG

ES:

WSSS/

SIN

CHA

NG

I

1A

KA

DA

R

VEN

PA,

turn

LEF

T. T

o A

TKA

X,

turn

RIG

HT.

46

131

4417

7

6

4

3

9

2111

32

SINGAPO

RE, SINGAPO

RE.Eff.9.Nov.

To I

BIV

A a

t or

abo

ve 2

500,

tur

n LE

FT.

ToD

ON

DI.

To

DIV

SA a

t or

abo

ve 4

000,

tur

nRI

GH

T. T

o BTM

VO

R, t

urn

LEFT

. To

DO

GRA

at o

r be

low

600

0, t

urn

RIG

HT.

To

DO

SNO

,tu

rn L

EFT.

To

VEN

PA,

turn

LEF

T. T

o A

TKA

X,

turn

RIG

HT.

To

KA

DA

R.

KA

DA

R3B

KA

DA

R 2B

rep

lace

d by

KA

DA

R 3B

, IB

IBI

way

poin

t w

ithd

raw

n.

2.7

KADAR 1A

KADAR 3

B

NO

T T

O S

CA

LE

113^

22

20

34

24

UNTIL

PA

SSIN

G 4

000 A

ND N

OT E

XCEED

250 K

T U

NTIL

PA

SSIN

G 1

0000

SHA

LL N

OT E

XCEED 2

30 K

T

.SPEED

:


COMMS

LOST

COMMS

LOST

COMMS

LOST



LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

BATAM

Hang N

adim

WID

D

SIN

GAPORE

Paya L

ebar

WSAP

SIN

GAPORE

Sele

tar

WSSL

01-00

01-30

104-00

3500

RP

A

2000

4000

25001

500

6000

4000

For

min

imum

cli

mb

grad

ient

cri

teri

a:

Rwy

20R:

Dep

artu

res

shal

l be

on

a

Rwy

02L:

Pro

ceed

str

aigh

t ah

ead

to

Nyl

on H

oldi

ng A

rea

(NH

A)

clim

bing

Rwy

20R:

Pro

ceed

str

aigh

t ah

ead

to

Sam

ko H

oldi

ng A

rea

(SH

A)

clim

bing

to t

he l

ast

assi

gned

alt

itud

e.

to t

he l

ast

assi

gned

alt

itud

e.

7600

.1.

Set

tra

nspo

nder

to

Mod

e A

/C c

ode

2. C

omm

unic

atio

ns f

ailu

re o

ccur

s im

med

iate

ly a

fter

dep

artu

re o

n:

Rwy

02L:

See

10-

3 an

d 10

-3A

.

Ther

eaft

er r

efer

to

10-1

P pa

ges

for

Ther

eaft

er r

efer

to

10-1

P pa

ges

for

proc

edur

e.ra

dio

com

mun

icat

ions

fai

lure

radi

o co

mm

unic

atio

ns f

ailu

repr

oced

ure.

6.0%

V/V

(fp

m)

456

608

911

1215

1519

1823

Gnd

spe

ed-K

T75

100

150

200

250

300

unti

l re

achi

ng o

r pa

ssin

g 25

00.

min

imum

net

cli

mb

grad

ient

of

6.0%

KA

DA

R

105^

TO

PO

M

115^

023^

169^DO

KTA

A

113^

LETG

OLEDO

X

203^

DIV

SA

BATA

M

B T

M11

6.0

BTM

D

DO

GRA

120^

126^

180^

VENPA

ATKA

X

097^

DO

SNO

Cha

ngi

EAST

Rw

y 02

R/20

LA

clos

ed d

ue d

evel

opm

ent

wor

ks.

WSS

S/SIN

CHA

NG

I

JEPPESEN

3 N

OV 1

710

-3L

SINGAPO

RE, SINGAPO

RE.RNAV.SID.

5. A

ll S

IDs

incl

ude

nois

e pr

efer

enti

al r

oute

s.

1.

RA

DA

R r

equir

ed.

requir

ed.

2.

RNA

V 1

Navig

ati

on S

pecif

icati

on G

NSS

3. A

ircr

aft

unab

le t

o fl

y th

e SI

D p

rofi

le s

hall

RAD

AR

vect

orin

g, i

f ne

cess

ary.

by S

inga

pore

RA

DA

R.

RNAV (GNSS) DEP

ART

URE

S

SID

INIT

IAL

CLI

MB

RW

Y

02L

20R

or a

s di

rect

ed b

y A

TC3000

Init

ial

clim

b cl

eara

nce

turn

RIG

HT.

To

DO

KTA

at

or a

bove

400

0,

turn

RIG

HT.

To

DO

GRA

at

or b

elow

600

0,

KADAR

3F [KADA3F

]KADAR

1E [KADA1E

]

To K

AD

AR.

To T

OPO

M o

n co

urse

023

^ at

or

abov

e 20

00,

To L

EDO

X o

n co

urse

203

^ at

or

abov

e 15

00.

| J

EPPE

SEN

, 20

17.

ALL

RIG

HTS

RES

ERVED

.

info

rm A

TC p

rior

to

depa

rtur

e an

d to

EXPE

CT

4. C

ruis

ing

leve

ls w

ill

be i

ssue

d af

ter

take

-off

Tran

s al

t: 1

1000

22A

pt E

lev

CHA

NG

ES:

05101520 525

1E

KA

DA

R

3F

KA

DA

R

9

21

8

6

7

17 44

131

46tu

rn R

IGH

T. T

o D

OSN

O,

turn

LEF

T. T

o VEN

PA,

turn

LEF

T. T

o A

TKA

X,

turn

RIG

HT.

1132

.Eff.9.Nov.

To L

ETG

O a

t or

abo

ve 2

500,

tur

n LE

FT.

ToD

IVSA

at

or a

bove

400

0, t

urn

RIG

HT.

To

BTM

VO

R, t

urn

LEFT

. To

DO

GRA

at

orbe

low

600

0, t

urn

RIG

HT.

To

DO

SNO

, tu

rn

LEFT

. To

VEN

PA,

turn

LEF

T. T

o A

TKA

X,

turn

RIG

HT.

To

KA

DA

R.

KA

DA

R 2F

rep

lace

d by

KA

DA

R 3F

, LE

GA

S w

aypo

int

wit

hdra

wn.

2.7

KADAR 1E

KADAR 3

F

NO

T T

O S

CA

LE

113^

22

20

34

24

UNTIL

PA

SSIN

G 4

000 A

ND N

OT E

XCEED

250 K

T U

NTIL

PA

SSIN

G 1

0000

SHA

LL N

OT E

XCEED 2

30 K

T

.SPEED

:



COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

LOST


COMMS


WMKJ

SINGAPOREPaya Lebar

WSAP


01-30

104-00

3500

RAP

1500

2500

4000

7000

2000

7000

11000



Rwy 02C: See 10-3 and 10-3A.


7.0% V/V (fpm) 532 709 1063 1418 1772 2127

Gnd speed-KT 75 100 150 200 250 300

IBIXU

113^IBIVA

203^

DIVSA

DOSPA

023^

DONDI

342^

TEKONG

V T K116.5 VTKD

MASBO 4B:

A

023^

TOKIM

332^

MASB

O 2

A

MA

SBO

4B

MASBO 2A:AKOMA

SABKA

MASBO

296^ AGVAR

278^

| JEPPESEN

, 2017. ALL RIG

HTS RESERV

ED.


02C

20C






MASBO2A



RNAV (G

NSS) D

EPARTU

RES

JEPPESEN

10-3M.RNAV.SID.

MASBO

4B [MASB4B]

MASBO

2A [M

ASB2A

]MASBO 2A [MASB2A], MASBO 4B [MASB4B]

RNAV (GNSS) DEPARTURES



Apt Elev22 3. Aircraft unable to fly the SID profile shall inform ATC prior to

departure and to EXPECT RADAR vectoring, if necessary.

Trans alt: 11000


CHA

NG

ES:

0 5 10 15 205 253 N

OV 17

AKOMA at or above 7000, turn LEFT. To AGVAR at or above11000. To SABKA, turn RIGHT. To MASBO.

27

25

13

18

21

3

5

10

4

2347


WSSS/SIN

CHA

NG

ISIN

GAPO

RE, SINGAPO

RE.Eff.9.N

ov.

above 2500, turn LEFT. To DONDI. To DIVSA at or above 4000,speed 230 KT, turn LEFT. To DOSPA, turn LEFT. To VTK VORat or above 7000. To AKOMA, turn LEFT. To AGVAR at orabove 11000. To SABKA, turn RIGHT. To MASBO.

MASBO4B

2.7

MA

SBO

3B replaced by M

ASB

O 4B

, IBIB

I waypoint w

ithdrawn.

NOT TO SCALE

342^

34 24

At 230 KT

AND NOT EXCEED 250 KT UNTIL PASSING 10000RWY 20C: SHALL NOT EXCEED 230 KT UNTIL DIVSA


CONTOURINTERVALS

4000

2000


COMMS

LOST

COMMSLOST COMMSLOST

COMMS COMMSLOST COMMSLOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

LOST



WMKJ

SINGAPOREPaya Lebar

WSAP


01-30

104-00

3500

RAP

2500

1500

4000

7000

2000

7000

11000


Rwy 20R: Departures shall be on a

Rwy 02L: See 10-3 and 10-3A.


6.0% V/V (fpm) 456 608 911 1215 1519 1823

Gnd speed-KT 75 100 150 200 250 300

AGVAR

278^

SABKA

MASBO

296^

113^

LEDOX

LETGO

DIVSA

DOSPA

023^

342^

A

023^

203^

TEKONG

V T K116.5 VTKD

342^

ATRUM

333^

TOPOM

MASBO

4F

MASB

O 2

E

AKOMAMASBO 2E:

MASBO 2E [MASB2E], MASBO 4F [MASB4F]RNAV (GNSS) DEPARTURES





Trans alt: 11000


CHA

NG

ES:

0 5 10 15 205 25

| JEPPESEN

, 2017. ALL RIG

HTS RESERV

ED.


02L

20R

To TOPOM on course 023^ at or above 2000, turn LEFT. To ATRUM. To AKOMA at or above 7000, turn LEFT. To AGVAR




MASBO2E

MASBO4F

SINGAPO

RE, SINGAPO

RE.RNAV.SID.

MASBO

2E [MASB2E], M

ASBO

4F [MASB4F]

RNAV (G

NSS) D

EPARTU

RES

JEPPESEN

WSSS/SIN

CHA

NG

I



10-3N3 N

OV 17

at or above 11000. To SABKA, turn RIGHT. To MASBO.

27

25

13

1421

3

8 5

10

2347


.Eff.9.Nov.

To LEDOX on course 203^ at or above 1500. To LETGO at orabove 2500, turn LEFT. To DIVSA at or above 4000, speed230 KT, turn LEFT. To DOSPA, turn LEFT. To VTK VOR at orabove 7000. To AKOMA, turn LEFT. To AGVAR at or above11000. To SABKA, turn RIGHT. To MASBO.

2.7

MA

SBO

3F replaced by MA

SBO

4F, LEGA

S waypoint w

ithdrawn.

NOT TO SCALE

34 24

At 230 KT

AND NOT EXCEED 250 KT UNTIL PASSING 10000RWY 20R: SHALL NOT EXCEED 230 KT UNTIL DIVSA


CONTOURINTERVALS

4000

2000


COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

LOST


COMMS COMMSLOST COMMSLOST COMMSLOST COMMSLOST


WMKJ

SINGAPOREPaya Lebar

WSAP


01-30

104-00

3500

RAP

1500

2500

4000

7000

2000

7000



Rwy 02C: See 10-3 and 10-3A.


7.0% V/V (fpm) 532 709 1063 1418 1772 2127

Gnd speed-KT 75 100 150 200 250 300

IBIXU

113^IBIVA

203^

DIVSA

DOSPA

023^

DONDI

342^

A

TEKONG

V T K116.5 VTKD

023^

TOKIM

332^

AKOMA

| JEPPESEN

, 2017. ALL RIG

HTS RESERV

ED.



RNAV (G

NSS) D

EPARTU

RES

JEPPESEN

10-3P.RNAV.SID.

3 NO

V 17




Apt Elev

22 3. Aircraft unable to fly the SID profile shall inform ATC prior to departure and to EXPECT RADAR vectoring, if necessary.

Trans alt: 11000


0 5 10 15 205 25CHA

NG

ES:



116.8 VMRXXXDMERSING

356^

MERSING 8B:

MERSIN

G 5

A

MERSIN

G 8

B

(VM

R 8B)

(VMR 5A

)

MERSING 5A:

MERSING 5A (VMR 5A), MERSING 8B (VMR 8B)MERSIN

G 5A

(VMR 5A

)MERSIN

G 8B (V

MR 8B)


02C

20C


8BMERSING

AKOMA at or above 7000, turn RIGHT. To VMR VOR.MERSING

5A




38

18

21

3

4

5

10

WSSS/SIN

CHA

NG

I

637

SINGAPO

RE, SINGAPO

RE.Eff.9.N

ov.

MERSIN

G 7B

replaced by MERSIN

G 8B

, IBIB

I waypoint w

ithdrawn.

above 2500, turn LEFT. To DONDI. To DIVSA at or above 4000,speed 230 KT, turn LEFT. To DOSPA, turn LEFT. To VTK VORat or above 7000. To AKOMA, turn RIGHT. To VMR VOR.

NOT TO SCALE

342^

34 24

At 230 KT

AND NOT EXCEED 250 KT UNTIL PASSING 10000RWY 20C: SHALL NOT EXCEED 230 KT UNTIL DIVSA


2.7



COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

LOST


COMMS


WMKJ

SINGAPOREPaya Lebar

WSAP


01-30

104-00

3500

RAP

2500

1500

4000

7000

2000

7000


Rwy 20R: Departures shall be on a

Rwy 02L: See 10-3 and 10-3A.


6.0% V/V (fpm) 456 608 911 1215 1519 1823

Gnd speed-KT 75 100 150 200 250 300



356^

113^

LEDOX

LETGO

DIVSA

DOSPA

023^

342^

TEKONG

A

203^

V T K116.5 VTKD

023^

342^

ATRUM

333^

TOPOM

AKOMAMERSING 5E:

MER

SING 5

E

MERSIN

G 8

F

(VMR 5E)

(VM

R 8F)

116.8 VMRXXXDMERSING






Trans alt: 11000


CHA

NG

ES:

0 5 10 15 205 2510-3Q

SINGAPO

RE, SINGAPO

RE.RNAV.SID.

JEPPESEN

WSSS/SIN

CHA

NG

I

RNAV (G

NSS) D

EPARTU

RES

| JEPPESEN

, 2017. ALL RIG

HTS RESERV

ED.


02L

20R

To TOPOM on course 023^ at or above 2000, turn LEFT. To

To LEDOX on course 203^ at or above 1500. To LETGO at or

5E

8F

MERSING 5E (VMR 5E), MERSING 8F (VMR 8F)

3 NO

V 17

MERSIN

G 8F (V

MR 8F)

MERSIN

G 5E (V

MR 5E)

MERSING

MERSING




VOR.ATRUM. To AKOMA at or above 7000, turn RIGHT. To VMR

38

1421

3

8 5

10


637

.Eff.9.Nov.

above 2500, turn LEFT. To DIVSA at or above 4000, speed230 KT, turn LEFT. To DOSPA, turn LEFT. To VTK VOR at orabove 7000. To AKOMA, turn RIGHT. To VMR VOR.

MERSIN

G 7F replaced by M

ERSING

8F, LEGA

S waypoint w

ithdrawn.

NOT TO SCALE

34 24

At 230 KT

AND NOT EXCEED 250 KT UNTIL PASSING 10000RWY 20R: SHALL NOT EXCEED 230 KT UNTIL DIVSA


2.7


COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST


COMMS LOSTCOMMS LOSTLOST LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

COMMS

BATAM

Hang N

adim

WID

D

SIN

GAPORE

Paya L

ebar

WSAP

SIN

GAPORE

Sele

tar

WSSL

01-00

01-30

104-00

3500

RP

A

1500

2500

4000

6000

2000

4000

7000

7000

For

min

imum

cli

mb

grad

ient

cri

teri

a:

Rwy

20C:

Dep

artu

res

shal

l be

on

a

Rwy

02C:

See

10-3

and

10-

3A.

unti

l re

achi

ng o

r pa

ssin

g 25

00.

min

imum

net

cli

mb

grad

ient

of

7.0%

7.0%

V/V

(fp

m)

532

709

1063

1418

1772

2127

Gnd

spe

ed-K

T75

100

150

200

250

300

203^

113^

IBIX

U

IBIV

ADO

NDI

A

DIV

SA

120^

BATA

M

B T

M11

6.0

BTM

D

DO

GRA

TO

KIM

115^

023^

DO

KTA

TO

MA

N08

9^

HO

SBA

RUVIK

035^

5. A

ll S

IDs

incl

ude

nois

e pr

efer

enti

al r

oute

s.

1.

RA

DA

R r

equir

ed.

requir

ed.

2.

RNA

V 1

Navig

ati

on S

pecif

icati

on G

NSS

3. A

ircr

aft

unab

le t

o fl

y th

e SI

D p

rofi

le s

hall

RAD

AR

vect

orin

g, i

f ne

cess

ary.

by S

inga

pore

RA

DA

R.

RNAV (GNSS) DEP

ART

URE

STO

MAN 4

B [TOMA4B

]TO

MAN 2

A [TO

MA2A

]

info

rm A

TC p

rior

to

depa

rtur

e an

d to

EXPE

CT

4. C

ruis

ing

leve

ls w

ill

be i

ssue

d af

ter

take

-off

Tran

s al

t: 1

1000

22A

pt E

lev

SID

INIT

IAL

CLI

MB

RW

Y

02C

20C

or a

s di

rect

ed b

y A

TC3000

Init

ial

clim

b cl

eara

nce

| J

EPPE

SEN

, 20

17.

ALL

RIG

HTS

RES

ERVED

.

4B

2. C

omm

unic

atio

ns f

ailu

re o

ccur

s im

med

iate

ly a

fter

dep

artu

re o

n:

1. S

et t

rans

pond

er t

o M

ode

A/C

cod

e 76

00.

Rwy

02C:

Proc

eed

stra

ight

ahe

ad t

o N

ylon

Hol

ding

Are

a (N

HA

) cl

imbi

ng t

o th

e la

stas

sign

ed a

ltit

ude.

The

reaf

ter

refe

r to

10-1

P pa

ges

for

radi

o co

mm

unic

atio

ns

fail

ure

proc

edur

e.Rw

y 20

C:

Proc

eed

stra

ight

ahe

ad t

o Sa

mko

H

oldi

ng A

rea

(SH

A)

clim

bing

to

the

last

as

sign

ed a

ltit

ude.

The

reaf

ter

refe

r to

10

-1P

page

s fo

r ra

dio

com

mun

icat

ions

fa

ilur

e pr

oced

ure.

TO

MA

N

05101520 525 CHA

NG

ES:

Cha

ngi

EAST

Rw

y 02

R/20

LA

clos

ed d

ue d

evel

opm

ent

wor

ks.

JEPPESEN

WSSS/

SIN

CHA

NG

I3

NO

V 1

710

-3S

.RNAV.SID.

TO

MA

N2A

To T

OKIM

on

cour

se 0

23^

at o

r ab

ove

2000

, tu

rn R

IGH

T. T

o D

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at

or a

bove

400

0.

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OM

AN

.To

IBIX

U o

n co

urse

203

^ at

or

abov

e 15

00.

or b

elow

700

0. T

o H

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t or

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ve 7

000,

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t or

abo

ve 7

000,

tur

n LE

FT.

83

6

11

7

6

4

3

9

15

1132

SINGAPO

RE, SINGAPO

RE.Eff.9.Nov.

To I

BIV

A a

t or

abo

ve 2

500,

tur

n LE

FT.

ToD

ON

DI.

To

DIV

SA a

t or

abo

ve 4

000,

tur

nRI

GH

T. T

o BTM

VO

R, t

urn

LEFT

. To

DO

GRA

at o

r be

low

600

0, t

urn

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. To

RUVIK

at

turn

RIG

HT.

To

TOM

AN

.

TOMAN 4

B

TOM

AN 2

A2.7

TOM

AN

3B r

epla

ced

by T

OM

AN

4B,

IBIB

I w

aypo

int

wit

hdra

wn.

113^

NO

T T

O S

CA

LE

22

20

34

24

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PA

SSIN

G 4

000 A

ND N

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XCEED

250 K

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NTIL

PA

SSIN

G 1

0000

SHA

LL N

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30 K

T

.SPEED

:


COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST



COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

COMMS

BATAM

Hang N

adim

WID

D

SIN

GAPORE

Paya L

ebar

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GAPORE

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tar

WSSL

01-00

01-30

104-00

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RP

A

2000

1500

2500

4000

6000

4000

7000

7000

For

min

imum

cli

mb

grad

ient

cri

teri

a:

Rwy

20R:

Dep

artu

res

shal

l be

on

a

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02L:

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10-

3 an

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unti

l re

achi

ng o

r pa

ssin

g 25

00.

min

imum

net

cli

mb

grad

ient

of

6.0%

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m)

456

608

911

1215

1519

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spe

ed-K

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100

150

200

250

300

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MA

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9^83

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PO

M

115^

023^

A

113^

203^

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X

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M

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ngi

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y 02

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ent

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ks.

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WSS

S/SIN

CHA

NG

I

JEPPESEN

3 N

OV 1

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SINGAPO

RE, SINGAPO

RE.RNAV.SID.

5. A

ll S

IDs

incl

ude

nois

e pr

efer

enti

al r

oute

s.

1.

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DA

R r

equir

ed.

requir

ed.

2.

RNA

V 1

Navig

ati

on S

pecif

icati

on G

NSS

3. A

ircr

aft

unab

le t

o fl

y th

e SI

D p

rofi

le s

hall

RAD

AR

vect

orin

g, i

f ne

cess

ary.

by S

inga

pore

RA

DA

R.

RNAV (GNSS) DEP

ART

URE

S

SID

INIT

IAL

CLI

MB

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Y

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or a

s di

rect

ed b

y A

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ial

clim

b cl

eara

nce

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t or

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ve 4

000,

tur

n RI

GH

T. T

o

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F [TOMA4F

]TO

MAN 2

E [TOMA2E

]

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OPO

M o

n co

urse

023

^ at

or

abov

e 20

00,

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EDO

X o

n co

urse

203

^ at

or

abov

e 15

00.

| J

EPPE

SEN

, 20

17.

ALL

RIG

HTS

RES

ERVED

.

info

rm A

TC p

rior

to

depa

rtur

e an

d to

EXPE

CT

4. C

ruis

ing

leve

ls w

ill

be i

ssue

d af

ter

take

-off

Tran

s al

t: 1

1000

22A

pt E

lev

4F

TO

MA

N

CHA

NG

ES:

05101520 525

2. C

omm

unic

atio

ns f

ailu

re o

ccur

s im

med

iate

ly a

fter

dep

artu

re o

n:

1. S

et t

rans

pond

er t

o M

ode

A/C

cod

e 76

00.

Rwy

02L:

Pro

ceed

str

aigh

t ah

ead

to N

ylon

Hol

ding

Are

a (N

HA

) cl

imbi

ng t

o th

e la

stas

sign

ed a

ltit

ude.

The

reaf

ter

refe

r to

10-1

P pa

ges

for

radi

o co

mm

unic

atio

ns

fail

ure

proc

edur

e.Rw

y 20

R: P

roce

ed s

trai

ght

ahea

d to

Sam

ko

Hol

ding

Are

a (S

HA

) cl

imbi

ng t

o th

e la

st

assi

gned

alt

itud

e. T

here

afte

r re

fer

to

10-1

P pa

ges

for

radi

o co

mm

unic

atio

ns

fail

ure

proc

edur

e.

turn

RIG

HT.

To

DO

KTA

at

or a

bove

400

0.To

HO

SBA

at

or a

bove

700

0, t

urn

LEFT

. To

TO

MA

N.

TO

MA

N2E

9

15

6

11

7

6

8

1132

.Eff.9.Nov.

To L

ETG

O a

t or

abo

ve 2

500,

tur

n LE

FT.

To

BTM

VO

R, t

urn

LEFT

. To

DO

GRA

at

or b

elow

6000

, tu

rn L

EFT.

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RUVIK

at

or b

elow

700

0.To

HO

SBA

at

or a

bove

700

0, t

urn

RIG

HT.

To T

OM

AN

.

TOMAN 4

F

TOM

AN 2

E

2.7

TOM

AN

3F

repl

aced

by

TOM

AN

4F,

LEG

AS

way

poin

t w

ithd

raw

n.

NO

T T

O S

CA

LE

113^

22

20

34

24

UNTIL

PA

SSIN

G 4

000 A

ND N

OT E

XCEED

250 K

T U

NTIL

PA

SSIN

G 1

0000

SHA

LL N

OT E

XCEED 2

30 K

T

.SPEED

:


COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST



COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

BATAM

Hang N

adim

WID

D

SIN

GAPORE

Paya L

ebar

WSAP

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GAPORE

Sele

tar

WSSL

01-00

01-30

104-00

3500

RP

A

1500

2500

4000

2000

4000

6000

For

min

imum

cli

mb

grad

ient

cri

teri

a:

Rwy

20C:

Dep

artu

res

shal

l be

on

a

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and

10-

3A.

unti

l re

achi

ng o

r pa

ssin

g 25

00.

min

imum

net

cli

mb

grad

ient

of

7.0%

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m)

532

709

1063

1418

1772

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Gnd

spe

ed-K

T75

100

150

200

250

300

203^

113^

IBIX

U

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NDI DIV

SA

120^ BA

TAM

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M11

6.0

BTM

D

A

TO

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115^

023^

DO

KTA

169^

DO

GRA

180^

VENIX

120^

SURG

A

VENPA

126^

DO

SNO

2. C

omm

unic

atio

ns f

ailu

re o

ccur

s im

med

iate

ly a

fter

dep

artu

re o

n:

1. S

et t

rans

pond

er t

o M

ode

A/C

cod

e 76

00.

Rwy

02C:

Proc

eed

stra

ight

ahe

ad t

o N

ylon

Hol

ding

Are

a (N

HA

) cl

imbi

ng t

o th

e la

st

Rwy

20C:

Proc

eed

stra

ight

ahe

ad t

o Sa

mko

Hol

ding

Are

a (S

HA

) cl

imbi

ng t

o th

e la

st

assi

gned

alt

itud

e. T

here

afte

r re

fer

to10

-1P

page

s fo

r ra

dio

com

mun

icat

ions

assi

gned

alt

itud

e. T

here

afte

r re

fer

to10

-1P

page

s fo

r ra

dio

com

mun

icat

ions

fail

ure

proc

edur

e.

fail

ure

proc

edur

e.

5. A

ll S

IDs

incl

ude

nois

e pr

efer

enti

al r

oute

s.

1.

RA

DA

R r

equir

ed.

RNAV (GNSS) DEP

ART

URE

S

Tran

s al

t: 1

1000

2.

RNA

V 1

Navig

ati

on S

pecif

icati

on G

NSS

requir

ed.

3. A

ircr

aft

unab

le t

o fl

y th

e SI

D p

rofi

le s

hall

RAD

AR

vect

orin

g, i

f ne

cess

ary.

info

rm A

TC p

rior

to

depa

rtur

e an

d to

EXPE

CT

4. C

ruis

ing

leve

ls w

ill

be i

ssue

d af

ter

take

-off

by S

inga

pore

RA

DA

R.

22

VEN

IX 3

B [VEN

I3B]

VEN

IX 1

A [VEN

I1A]

SID

INIT

IAL

CLI

MB

RW

Y

02C

20C

or a

s di

rect

ed b

y A

TC

turn

RIG

HT.

To

DO

KTA

at

or a

bove

400

0,To

TO

KIM

on

cour

se 0

23^

at o

r ab

ove

2000

,

turn

RIG

HT.

To

DO

GRA

at

or b

elow

600

0,

To I

BIX

U o

n co

urse

203

^ at

or

abov

e 15

00.

3000

Init

ial

clim

b cl

eara

nce

| J

EPPE

SEN

, 20

17.

ALL

RIG

HTS

RES

ERVED

.

3 N

OV 1

7

turn

RIG

HT.

To

DO

SNO

, tu

rn L

EFT.

To

JEPPESEN

10-3

U.RNAV.SID.

Apt

Ele

v

CHA

NG

ES:

05101520 525

WSSS/

SIN

CHA

NG

I

Cha

ngi

EAST

Rw

y 02

R/20

LA

clos

ed d

ue d

evel

opm

ent

wor

ks.

VEN

PA,

turn

LEF

T. T

o VEN

IX.

To S

URG

A.

1A

VENIX

3

4

6

7

21

9

17 44

87

30

1132

SINGAPO

RE, SINGAPO

RE.Eff.9.Nov.

VENIX

3B

To I

BIV

A a

t or

abo

ve 2

500,

tur

n LE

FT.

ToD

ON

DI.

To

DIV

SA a

t or

abo

ve 4

000,

tur

nRI

GH

T. T

o BTM

VO

R, t

urn

LEFT

. To

DO

GRA

at o

r be

low

600

0, t

urn

RIG

HT.

To

DO

SNO

, tu

rn L

EFT.

To

VEN

PA,

turn

LEF

T. T

o VEN

IX.

To S

URG

A.

VENIX 1A

VEN

IX 3

B

2.7

VEN

IX 2

B r

epla

ced

by V

ENIX

3B,

IBIB

I w

aypo

int

wit

hdra

wn.

113^

NO

T T

O S

CA

LE

22

20

34

24

UNTIL

PA

SSIN

G 4

000 A

ND N

OT E

XCEED

250 K

T U

NTIL

PA

SSIN

G 1

0000

SHA

LL N

OT E

XCEED 2

30 K

T

.SPEED

:


COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST



COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

COMMS

BATAM

Hang N

adim

WID

D

SIN

GAPORE

Paya L

ebar

WSAP

SIN

GAPORE

Sele

tar

WSSL

01-00

01-30

104-00

3500

RP

A

25001

500

4000

2000

4000

6000

For

min

imum

cli

mb

grad

ient

cri

teri

a:

Rwy

20R:

Dep

artu

res

shal

l be

on

a

Rwy

02L:

See

10-

3 an

d 10

-3A

.

6.0%

V/V

(fp

m)

456

608

911

1215

1519

1823

Gnd

spe

ed-K

T75

100

150

200

250

300

unti

l re

achi

ng o

r pa

ssin

g 25

00.

min

imum

net

cli

mb

grad

ient

of

6.0%

VENIX

120^

SURG

A

113^

LETG

OLEDO

X

DIV

SA

BATA

M

B T

M11

6.0

BTM

D

120^

Cha

ngi

EAST

Rw

y 02

R/20

LA

clos

ed d

ue d

evel

opm

ent

wor

ks.

A

203^

TO

PO

M

115^

023^

169^DO

KTA

DO

GRA

DO

SNO

180^

VENPA

126^

05101520 525

WSS

S/SIN

CHA

NG

I

JEPPESEN

3 N

OV 1

710

-3V

SINGAPO

RE, SINGAPO

RE.RNAV.SID.

SID

INIT

IAL

CLI

MB

RW

Y

02L

20R

or a

s di

rect

ed b

y A

TC3000

Init

ial

clim

b cl

eara

nce

turn

RIG

HT.

To

DO

KTA

at

or a

bove

400

0,

turn

RIG

HT.

To

DO

GRA

at

or b

elow

600

0,tu

rn R

IGH

T. T

o D

OSN

O,

turn

LEF

T.

DIV

SA a

t or

abo

ve 4

000,

tur

n RI

GH

T. T

o

To T

OPO

M o

n co

urse

023

^ at

or

abov

e 20

00,

To L

EDO

X o

n co

urse

203

^ at

or

abov

e 15

00.

| J

EPPE

SEN

, 20

17.

ALL

RIG

HTS

RES

ERVED

.

3F

VENIX

5. A

ll S

IDs

incl

ude

nois

e pr

efer

enti

al r

oute

s.

1.

RA

DA

R r

equir

ed.

requir

ed.

2.

RNA

V 1

Navig

ati

on S

pecif

icati

on G

NSS

3. A

ircr

aft

unab

le t

o fl

y th

e SI

D p

rofi

le s

hall

RAD

AR

vect

orin

g, i

f ne

cess

ary.

by S

inga

pore

RA

DA

R.

RNAV (GNSS) DEP

ART

URE

SVEN

IX 3

F [VEN

I3F]

VEN

IX 1

E [VEN

I1E]

info

rm A

TC p

rior

to

depa

rtur

e an

d to

EXPE

CT

4. C

ruis

ing

leve

ls w

ill

be i

ssue

d af

ter

take

-off

Tran

s al

t: 1

1000

22A

pt E

lev

CHA

NG

ES:

2. C

omm

unic

atio

ns f

ailu

re o

ccur

s im

med

iate

ly a

fter

dep

artu

re o

n:

1. S

et t

rans

pond

er t

o M

ode

A/C

cod

e 76

00.

Rwy

02L:

Pro

ceed

str

aigh

t ah

ead

to N

ylon

Hol

ding

Are

a (N

HA

) cl

imbi

ng t

o th

e la

stas

sign

ed a

ltit

ude.

The

reaf

ter

refe

r to

10-1

P pa

ges

for

radi

o co

mm

unic

atio

ns

fail

ure

proc

edur

e.Rw

y 20

R: P

roce

ed s

trai

ght

ahea

d to

Sam

ko

Hol

ding

Are

a (S

HA

) cl

imbi

ng t

o th

e la

st

assi

gned

alt

itud

e. T

here

afte

r re

fer

to

10-1

P pa

ges

for

radi

o co

mm

unic

atio

ns

fail

ure

proc

edur

e.

To V

ENPA

, tu

rn L

EFT.

To

VEN

IX.

To S

URG

A.

VENIX

1E

9

21

8

6

7

17 44

87

30

1132

.Eff.9.Nov.

To L

ETG

O a

t or

abo

ve 2

500,

tur

n LE

FT.

To

BTM

VO

R, t

urn

LEFT

. To

DO

GRA

at

orbe

low

600

0, t

urn

RIG

HT.

To

DO

SNO

, tu

rnLE

FT.

To V

ENPA

, tu

rn L

EFT.

To

VEN

IX.

To S

URG

A.

VENIX 1E

VEN

IX 3

F

2.7

VEN

IX 2

F re

plac

ed b

y VEN

IX 3

F, L

EGA

S w

aypo

int

wit

hdra

wn.

113^

NO

T T

O S

CA

LE

22

20

34

24

UNTIL

PA

SSIN

G 4

000 A

ND N

OT E

XCEED

250 K

T U

NTIL

PA

SSIN

G 1

0000

SHA

LL N

OT E

XCEED 2

30 K

T

.SPEED

:


WSSS/SIN

CHANGES:

JEPPESEN


nightly from 28 October 2017 to 24 March 2018 for works and maintenance as follows:Runway 02L/20R and Runway 02C/20C will be closed between 1630 UTC and 2200 UTC

Month Runway 02L/20R Runway 02C/20C

For Runway 02C/20C closure from 1630 UTC to 2200 UTC, Taxiway EP betweenTaxiway L9 and Taxiway E11 will also be closed due to work in progress.

1, 4, 8, 11, 15, 18, 22, 25 and 29.

Any changes will be notified through NOTAM.

30 and 31.

October 2017

November 2017

December 2017

January 2018

February 2018

March 2018

30.

2, 6, 9, 13, 16, 20, 23, 27 and 30.

4, 7, 11, 14, 18, 21, 25 and 28.

1, 5, 8, 12, 15, 19, 22 and 26.

1, 5, 8, 12, 15, 19 and 22.

28, 29 and 31

1, 3, 4, 5, 7, 8, 10, 11, 12, 14, 15,17, 18, 19, 21, 22, 24, 25, 26, 28and 29.

1, 2, 3, 5, 6, 8, 9, 10, 12, 13, 15,

29, 30 and 31.

2, 3, 5, 6, 7, 9, 10, 12, 13, 14, 16,17, 19, 20, 21, 23, 24, 26, 27, 28,

2, 3, 4, 6, 7, 9, 10, 11, 13, 14, 16,17, 18, 20, 21, 23, 24, 25, 27 and28.

2, 3, 4, 6, 7, 9, 10, 11, 13, 14, 16,17, 18, 20, 21, 23 and 24.

16, 17, 19, 20, 22, 23, 24, 26, 27,

15 DEC 17

All aircraft operating during closure periods are to plan to carry sufficient contingencyfuel as only one runway will be available.

1) Between 1630-2200 on first, second and fourth Wednesday of the month

re-opened within 30 minutes.2) Between 0300-0315, 0650-0655, 1020-1025, 2315-2330 daily (inspection). In the

event of an emergency, Runway will be re-opened within 5 minutes.

maintenance work). In the event of an emergency, Runway will be re-openedwithin 30 minutes.

2) Between 0225-0240, 0630-0635, 1000-1005, 2300-2315 daily (inspection). In theevent of an emergency, Runway will be re-opened within 5 minutes.

Scheduled closure of Rwy 02C/20C:

Scheduled closure of Rwy 02L/20R:

(preventive maintenance work). In the event of an emergency, Runway will be

1) Between 1630-2200 on every Monday and Thursday of the month (preventive

Notes.


10-8

SINGAPORE CHANGI AIRPORT - WORKS SCHEDULE AND MOVEMENTAREA RESTRICTIONS PERTAINING TO DIVERSION OF AIRSIDE

SERVICES AND SOIL IMPROVEMENT WORKS


Apt Elev

104-00103-59

Elev 14'

FOR PARKING POSITIONS

01-20 01-20

01-21

01-22

01-23

Rw

y 0

2R/20LT2

SO

UTH A

PRO

N

SERVICEAPRON

NORTH

SOUTH-EASTREMOTE APRON

APRON

L8

L5

L6

L7

L4

Taxiway centerline along Twy EP

Pilots are advised to applyminimum thrust when turning


1

1

JEPPESEN

aircraft stands E7 and F36.

202C/20C - (0000 to 1600).For ACFT operating on Rwy

between Twys B1 and B3 offseteastward by 8'eastward by 8' (2.5m) away from

into Twy WA from Taxilane V6.

Taxilane A6 (behind aircraft stands E20 to E24) and taxilane

C6 (behind aircraft stands F50 to F54) can only be used by

aircraft with maximum

pushback exempted).

Pilots are advised to apply

taxiing along Twy South Cross 1 and South Cross 2.

wingspan 213' 65m (towing and

stands A18 to A21) can onlybe used by aircraft with

For AIRPORT BRIEFINGrefer to 10-1P pages.

Taxilane U4 (behind aircraft

maximum wingspan of200' (61m).

Pilots are advised to apply minimum thrust when turning intoTwy A1, A3, A4 and taxilane A5 while taxiing either Northwardsor Southwards on taxilane A6, and thereafter when taxiingalong Twy A1 up to and including the Twy A7/A1 junction.This is in view of apron activities at aircraft stands D40, D41, D47, D48, D49, E22, E24, E27 and E28.

L9

L10

Pilots are advised to exercisecaution when taxiing near Twys

VAR 0^

Frangible poles are installed for the purpose of identifying 295' (90m) away from the centerline of Rwy 02L/20R and Rwy 02C/20C.

L8, L9 and L10 and taxilane L5.

Taxiways M4, M5, M6 and M7are solely for use by Republicof Singapore Air Force(RSAF) aircraft.

(RSAF) aircraft.

Twy located Western side of Rwy 02L/20R, between Twy M5 andTwy M6 are solely for use by Republic of Singapore Air Force

CAUTION: Runway 02R/20L closed due to development works.

Taxilane L5 can only be used by aircraft with maximumwingspan of 118' (36m). Twys L8, L9, and L10 can onlybe used by aircraft with maximum wingspan 213' (65m).

1 DEC 17

Taxilane N1 (behind aircraftstands C16 to C19 and betweenTwy NC2 and Twy NC3), TaxilaneN2 and Taxilane N3 (behindaircraft stands D35 to D38 andbetween Twy NC2 and Twy NC3)can only be used by aircraft withmaximum wingspan of 213' (65m).

speed limit of 20 KT when

SEE 10-9B, 10-9C1 & 10-9C2

Twy NC3 (between Twy WA and Twy A6)can only be used by aircraft with a maximum wingspan of 213' (65m).

T4 APRON

SOUTHAPRON

Communications.

APR

ON

WES

T

N01 21.6 E103 59.4 CHANGI10-922'SINGAPORE, SINGAPORE

CHANGES:

WSSS/SIN

02L

EP

Elev 22'

E11

E10

E9

E8

E7

197' Stopway

60m

5 min, see 10-9D and 10-9E.

023^

13,123

'40

00m

197'60mStopway

023^

02C

T2 CENTRAL APRON

T2 NORTH APRON

REMOTE APRON

CHANGI EAST(MILITARY ONLY)

C6

E3

E4

EP

279'

WPWA

TERMINAL2

E5

13,123

' 400

0m

A4

C3

C1C2

B2

B1

B3

C7 EP

C1

A5

T1 E

AST

APR

ON

W10

W6

V6W7

V7

V8W8

W9

WA

U2

SC2

SC1

SC1

SC2

20C

Elev 15'

197'60m Stopway

20R

Elev 13'

164'

WP

EA

EASTCARGOAPRON

WCW3

W2

W1

APRONCARGOWEST

197'60m Stopway

203^

203^

FuelFarm

NC1

SERVICEAPRON

EAST

V3

V4

WP

WA

ARP

CENTRALAPRON

1TERMINAL

E1E2

W4NC2

EA

AIS

MET

A1

A2 A6

A3

NC2

NC1NORTHREMOTE APRON

T1

T1 W

EST

APR

ON N1

N2 N3

N3

N1

NC3W5

VY

VZU1

U1

Feet

Meters

0

0

1000

1000

2000 3000 4000 5000

1500500

A7

A7A3

SC1E6

SC2

NORTH-EAST

A6

EAST REMOTE

T3

U3

Pushback clearance expires in

Control Tower

ENEP

EP

U4

EC

SA

SASCOHANGAR

Max wingspan 213' (65m)

M5

M4

WC

V1V2

WD

M6

M7

M

S1

TERMINAL 4

S2S3

S4

118.252

D-ATIS

128.6

ACARS:D-ATIS

121.65 124.3

Ground

121.72

Tower

118.6Terminal 3West of

Terminal 2*East of

Emergency

129.95

*North of Terminal 1

121.85

SINGAPOREDelivery (Cpt)

125.65 122.55

ControllerController4 West 4 East


applicable when Runway 20C/02C is unavailable because of maintenance work or for other reasons.Departures on Runway 20R are not permitted between 1600/2200 UTC. However, this restriction is not


JEPPESEN

Runway 02L/20R between 1600/2200 UTC may not exceed idle reverse thrust.Unless it is necessary for operational or safety reasons, when using engine reverse, arrivals on

To maximize runway utilization and minimize runway occupancy time, departing aircraft, wheninstructed to enter the runway, shall commence the maneuver without delay. Pilots are required tocommence take-off roll as soon as take-off clearance is issued by ATC. Arriving aircraft uponlanding shall vacate the runway as quickly as practicable to enable ATC to apply minimum spacingon final approach and minimize the occurence of go-arounds.

1 DEC 17

None.

RWY

ADDITIONAL RUNWAY INFORMATION

ThresholdLANDING BEYOND

USABLE LENGTHS

WIDTHTAKE-OFFGlide Slope

GENERAL

RVR RVR

RVR RVR

02L20R

02C20C

11

1 Angle 3.0^.

Angle 3.0^.

11,995' 197'

197'

3656m

2929m 60m

60m

All Rwys

Eng

3 & 4Eng

TAKE-OFF

All Rwys

AIR CARRIER (FAR 121)

400m

ABCD

2 TDZ RVR

MID RVR

Rollout RVR

RVR

VIS

175m

CL & RCLM

CHANGI10-9A

Due to close proximity of Paya Lebar and Seletar airports, correct approach is vital.

2

2

500m

SINGAPORE, SINGAPORE

any RVR out, Adequate Vis Ref

250m (200m)

200m (150m) 250m

300m

Low-level wind shear alert system.

3661m

3662m12,014'12,012'

other two required

2

Maritime vessels of variable heights off Changi Apt.Birds in vicinity of airport.

3260m 9610'

CHANGES:

HIRL CL ALSF-II TDZ REILHIRL CL HIALS REIL PAPI

HIRL CL ALSF-I REILHIRL CL ALSF-II TDZ REIL PAPI-L

10,696'PAPI

PAPI

RL & CL

400m

RCLM (DAY only)or RL

RCLM (DAY only)or RL

AIR CARRIER (JAA) LVP must be in Force

All RwysAll Rwys

WSSS/SIN

175m

175m

20R Not applicableW2W3W4W5

02L Not applicableW8W7W6

20C Not applicableE2E3E4E5

02C Not applicable

E9E8E7

E10

E6

02R Not applicable

20L Not applicable

Rwy Designator Intersection Departures TORA

4000m3850m3050m2600m2150m

4000m3850m3050m2600m

4000m3850m3425m2750m2250m

4000m3850m3345m3205m2555m2105m

2750m

2750m

8,530'7,054'

8,530'

9,022'7,382'

8,383'6,906'

9,022'

9,022'

13,123'12,631'10,007'

13,123'12,631'10,007'

13,123'12,631'11,237'

13,123'12,631'10,974'10,515'

DECLARED DISTANCES

Intersection departures are allowed subject to the following:(a) Initiated by pilot and approved by ATC, traffic permitting.(b) ATC is able to keep aircraft visual at all times.


JEPPESEN


205

206

207 2

082

09

200

201

202

203

F60

F59

F58

F56

F54

F52

F50

F42

F41

F40

F37

F30

F31

F32

E1

E2

E3

B2

SC1

SC1

E6

EP

E5

C7

C3

C1

F33

F34

F35

F36

E4

E5

E6

E7

B3

B1

B2

EP

E4

A21

A20

A19

A18

A17 A

16A

15 A14

U4

U4

SC2

W10

W9

W8

WP

WA

V8

SC1

A13

A12

A11

A9

A10

A5

A4

A3

A2

A1

V6

V6

W6

W7

WP

WP

WA

WA

V7

B1

B2

B3

B4

B5

B6

B7

B8

B9

B10

C1

C20

WA

WA

W5

VY

VZ

VZ

U1

U1

C22

C23

C24

C25

C26

C11

C13

C15

D30

D32

D34

N2

D35

D36 D37 D

38

C16C

17C

18C

19

300

301

302

303

304

305

306

307

308

309

310N

1

N3

D41

D42

D40

E28

E27

E26

E24

E22

E20

E10

E11

E12

E8

D44

D46

D47D48 D

49

400

401402

404

403

W4

NC2

NC2

NC3

NC3

N1

N3

NC3

NC2

WP

EN

EPEP

EP

A6

A7 EP

E1E2

E3

A7

A1

A1

A2

A3

A4

A4

C1

C3

C6

C6

C2

SC2

EP

A6

A6

A5

A6

TERM

INA

L 1

SO

UTHEA

ST

REM

OTE A

PRO

N

C7

T2 S

OUTH

APRO

N

T2 N

ORTH

APRO

NT1 E

AST

APRO

N

NO

RTHEA

ST

REM

OTE A

PRO

N

T1 W

EST A

PRO

N

T3 W

EST

APRO

N

NO

RTH

REM

OTE

APRO

N

T1 C

ENTRA

LA

PRO

N

T2 C

ENTRA

LA

PRO

N

SC2

EA

ST R

EM

OTE

APRO

N

U2

U3

F52L

F52R

F59L

F59R

F56R

F56L

E24LE

24R

200L200R

Pilo

ts t

urni

ng a

ircr

aft

into

bay

A2

or b

ay B

2ar

e ad

vise

d to

wai

t fo

r an

y ai

rcra

ft h

oldi

ngat

tax

ilan

e V6,

at

the

inne

r cu

l-de

-sac

por

tion

of t

he t

erm

inal

bui

ldin

g to

vac

ate

this

port

ion

befo

re t

urni

ng i

nto

bay

A2

or b

ay B

2.

202L202R

461

462L

462462R

463L

463

463R

S1

L6

D42L D42R

F35LF35R

E27LE

27R

D40LD

40R

8 SEP 17

S2 S3

T3 W

EST

APRO

N

Twy S2,S3 added, T3 West apron.

RWY 0

2L-2

0R

RWY 0

2C-2

0C

TERM

INA

L 2

TERM

INA

L 3

WSSS/SIN SINGAPORE, SINGAPORE10-9B CHANGI

CHANGES:


N01 21.9 E103 59.4

N01 22.0 E103 59.5N01 22.1 E103 59.5

C18C19

N01 21.9 E103 59.5C15

C16, C17

C26 N01 22.0 E103 59.5


JEPPESEN

304305, 306

307 thru 309

310

N01 22.0 E103 59.7N01 22.1 E103 59.7

N01 22.0 E103 59.8

8 SEP 17

Apron update, note withdrawn.

CHANGI

PARKING BAY COORDINATES

COORDINATES COORDINATESBAY No.BAY No.

SINGAPORE, SINGAPORE10-9C

CHANGES:

WSSS/SIN

N01 21.0 E103 59.4F42F40, F41

F37 N01 21.0 E103 59.4N01 21.1 E103 59.4

N01 21.2 E103 59.4N01 21.0 E103 59.3

N01 21.0 E103 59.3

F50

T2 South Apron

400

North-East Remote Apron

404

N01 21.6 E103 59.7N01 21.7 E103 59.7N01 21.8 E103 59.7

401 thru 403

South-East Remote Apron

205206 thru 208

209 N01 20.9 E103 59.3N01 20.8 E103 59.3N01 20.7 E103 59.3

E11

E8E10

E12E20, E22

T2 North Apron

N01 21.5 E103 59.6

N01 21.4 E103 59.6N01 21.4 E103 59.5

N01 21.5 E103 59.6N01 21.4 E103 59.5

N01 21.5 E103 59.5

N01 21.6 E103 59.5

N01 21.3 E103 59.4N01 21.3 E103 59.5N01 21.3 E103 59.6N01 21.4 E103 59.6

E1E2 thru E4

E5E6, E7

F30, F31 N01 21.2 E103 59.4

N01 21.2 E103 59.5N01 21.1 E103 59.5

T2 Central Apron

F32, F33

T1 East Apron

N01 21.8 E103 59.6N01 21.8 E103 59.8

N01 21.9 E103 59.8

N01 21.7 E103 59.6D41, D42, D42L

D46D47, D48

N01 21.6 E103 59.5

D49

T1 Central Apron

N01 21.8 E103 59.4C11, C13

D30 N01 21.7 E103 59.5N01 21.8 E103 59.5N01 21.9 E103 59.7D35 thru D38

D32, D34

N01 21.8 E103 59.3C22 N01 21.9 E103 59.3

N01 21.9 E103 59.4C23N01 21.9 E103 59.5N01 22.0 E103 59.4

C24C25

N01 21.3 E103 59.0

N01 21.5 E103 59.1

A3, A4

B2 thru B4N01 21.6 E103 59.2

East Remote Apron

N01 20.9 E103 59.2

N01 20.8 E103 59.2

N01 21.2 E103 59.0A10

N01 21.1 E103 59.0A14 N01 21.0 E103 59.0

N01 21.0 E103 58.9A15 thru A17A18 N01 20.9 E103 58.9

N01 20.9 E103 59.0A19, A20

A21 N01 21.0 E103 59.0

N01 21.4 E103 59.1A1, A2

N01 21.3 E103 59.1A5N01 21.2 E103 59.1A9

A11 thru A13

N01 21.4 E103 59.1B1

N01 21.7 E103 59.3B8 thru B10

C1, C20

T3 West Apron

T1 West Apron

North Remote Apron

302, 303300, 301 N01 22.1 E103 59.5

N01 22.1 E103 59.6

N01 22.0 E103 59.9

N01 21.1 E103 59.3

F52L, F52R

B5 thru B7

N01 21.0 E103 59.3F58, F59, F59R

F59L, F60

E24 thru E26

F52, F56R, F56LN01 21.1 E103 59.3F54, F56

N01 20.8 E103 59.2200, 200L, 200R

201

N01 20.9 E103 59.2202, 202L, 202R

203

N01 21.7 E103 59.6D42R, D44

N01 20.7 E103 58.8N01 20.7 E103 58.8463, 463R

461, 462L N01 20.7 E103 58.9462, 462R, 463L

F34 thru F36

N01 21.5 E103 59.5E27, E27R, E28

E27L

D40, D40L, D40R

South Apron


509 N01 22.7 E103 59.6

505

506

504

503

502

507

508

604

603

602

601

606

609

JEPPESEN


EA

EA

WP

WP

W3

V3

V4

WC

WC

EC

611612

W2

W1V1

515

516

517517L517R516L516R

515 N01 22.9 E103 59.7N01 22.9 E103 59.7516L, 516, 516R

1

432

1234

509

WD

V2

510

511

512

513

514

517L, 517R517 N01 23.0 E103 59.8

N01 23.0 E103 59.7

605

600

600L

600R

15 DEC 17

NC1 NC1 NC1

N1 N3WA A7

None.

RWY 0

2L-2

0R



CHANGES:

WSSS/SIN

West Cargo Apron

505, 506507, 508

N01 22.4 E103 59.6

N01 22.5 E103 59.6N01 22.6 E103 59.6

N01 22.4 E103 59.5502

East Service Apron

606609

N01 22.2 E103 59.9N01 22.2 E103 59.9

601, 602 N01 22.3 E103 59.8N01 22.4 E103 59.9

East Cargo Apron

SERVICEAPRON

EASTCARGOAPRON

APRONCARGOWEST NORTH

SERVICEAPRON

EAST

10-9C1

COORDINATESBAY No.

N01 22.4 E104 00.0611, 612

N01 22.5 E103 59.6504503

Fuel Farm

N01 22.7 E103 59.7N01 22.8 E103 59.7

510, 511512 thru 514

603, 604, 605

N01 22.2 E103 59.8600, 600L, 600R


JEPPESEN


G19 G18

G9G8

E8L9

L5

L7

L6

L4

SC2 SC2

EP

EP

E7

E6

SC1

E9

EPC7C6SC1

G4G5G6G7 L8

L10

G21R

G21 G20

G20R

G21L

G3G2G1

G17G16G15G14G13G12G11G10

G20L

G18L

G18R

G19R

G19L

S2 S3

S4

467468469

464465466

Airportpolicestation

15 DEC 17

Taxiways L8 and L9, construction area, south apron depiction.

RWY 0

2C-2

0C

TERM

INA

L 4


CHANGES:

WSSS/SIN10-9C2

APRON


BAY No.

N01 20.6 E103 59.1

COORDINATES

N01 20.5 E103 59.2

N01 20.4 E103 59.1N01 20.3 E103 59.1

South-East Remote Apron

N01 20.2 E103 59.1N01 20.2 E103 59.0

G5, G6

N01 20.6 E103 59.1

N01 20.5 E103 59.2G18, G19

G21, G21L, G21RG20, G20L, G20R

N01 20.1 E103 59.0G1, G2G3, G4

G7 thru G11G12 thru G15

G16, G17N01 20.5 E103 59.2G18, G18L, G18R

N01 20.6 E103 59.2N01 20.5 E103 59.2

N01 20.5 E103 59.1

G19G19LG19R

T4

T4 Apron


BAY No. COORDINATES

N01 20.5 E103 58.7N01 20.6 E103 58.8N01 20.5 E103 58.8

SouthApron

464, 467465, 466468, 469

South Apron


JEPPESEN


TAXIING GUIDANCE SYSTEM AT SINGAPORE CHANGI AIRPORT

The taxiing guidance system at Singapore Changi Airport consists of stop bars and

selectable segments of green taxiway centerline lights. The system is designed to providepilots with visual guidance while taxiing during night operations and during periodsof low visibility. It is controlled by the Ground Movement Controller (GMC) at Changi

Route Selection and Priority

centerline lights on the maneuvering area are switched on automatically. When two ormore routes are selected, the system will give priority to the first route and activatered stopbar lights across conflicting routes, as necessary. A segment of the centerlinelights of the conflicting routes that cut across the first route will also be suppressed.The GMC has the option of overriding the taxiing route priority by selecting or deselecting the appropriate stopbar lights.

holding positions where, by default, red stopbar lights remain on unless deselected bythe runway controller. When deselected, these stopbar lights will re-activate

When following the directional guidance provided by the green taxiway centerline

lights and red stopbar lights, pilots are advised to also navigate their taxi route with

to maintain situational awareness of their whereabouts at all times.

CHANGES:

Information and Mandatory Signs/Markings

Control Tower using the Airfield Lighting Control and Monitoring System (AGLCMS).

When a taxiing route is selected on the AGLCMS, corresponding segments of taxiway

automatically after 50 seconds. Pilots shall not cross any lighted red stopbar lights.

reference to information and mandatory signs/markings provided at the airport so as

Pilots shall enter/cross the runway or taxiway only when both the following conditionsare met:The crew havea. received positive ATC clearance to enter/cross the runway or taxiway, andb. observed that the red stopbar lights are turned off.

All taxiing guidance lights on taxiways leading to the runways terminate at the runway

Reindexing.

8 SEP 17 CHANGISINGAPORE, SINGAPOREWSSS/SIN

10-9C3


JEPPESEN

| JEPPESEN, 2007, 2017. ALL RIGHTS RESERVED.CHANGES:

8 SEP 17

1.1

New format, reindexing.

ADVANCED- SURFACE MOVEMENT GUIDANCEAND CONTROL SYSTEM

(A-SMGCS)- MULTILATERATION SYSTEM DEPLOYMENTAT SINGAPORE CHANGI AIRPORT

1 Introduction

The Multilateration System is a new surveillance system which is able to detectand identify all Mode S equipped aircraft and vehicles moving on the airportsurface even during bad weather conditions such as heavy rain. It will integratewith the current radar-based ground surveillance system as a part of theAdvanced- Surface Movement Guidance and Control System (A-SMGCS) atSingapore Changi Airport. This will enhance the efficiency and safety at theairport.

2 Carriage of Mode-S SSR Transponder

2.1 Carriage and operation of Mode-S transponder is required for all civil aircraftoperating at Singapore Changi Airport. The Mode-S transponder shall comply, atleast, to the requirements of Level 2 as prescribed in ICAO Annex 10 Volume IV(Amendment 77 or later) Standards and Recommended Practices.

3 Multilateration System Outline

3.1

3.2 The system will derive the identity of an aircraft by selectively interrogating itstransponder to receive its assigned Mode A code or extracting its aircraftidentification (that is, the ICAO callsign used in flight and inserted in the FlightManagement System (FMS) or Transponder Control Panel), if available, from itssquitter. For transponder equipped vehicles, the system will derive theirrespective identities from the unique Mode S addresses contained in theirsquitters.

4

4.1

4.2

Aircraft Requirements

The Multilateration System is essentially passive. It relies on aircrafttransponders squittering at all times when moving on the airfield. At present,some aircraft checklist procedures instruct pilots to turn off the transpondershortly after leaving the runway on arrival and, not to switch it on until reachingthe runway holding point for departure. This is in line with the requirement thatMode A/C transponders should not transmit on the ground, which does not applyto Mode S transmissions.

For the Multilateration System to work effectively, all aircraft Mode Stransponders need to transmit Mode S squitters at all times when moving on theairfield, starting immediately prior to pushback, and for arrival aircraft untilthey are stationary at the aircraft stands. The Mode S transponders should notrespond to All-Call interrogations, but should respond to addressedinterrogations.

The Multilateration System uses multiple receivers to pick up 'squitters'transmitted by aircraft or vehicle Mode S transponders. It calculates the positionof an aircraft or a vehicle by comparing the time its 'squitte' arrives at eachreceiver.

CHANGISINGAPORE, SINGAPOREWSSS/SIN

10-9C4


JEPPESEN


8 SEP 17

5.1 The Multilateration System needs to receive squitters and to acquire the Mode Acode of a Mode S equipped aircraft at all times when it is on the ground. This isto enable detection and identification of the aircraft (from its Mode A code orICAO callsign) as soon as it pushes back. Hence, the following actions frompilots are required.

5.2 Pre-Push back / Taxi

a) Pilots will be required to enter an assigned Mode A code at start-up. This codewill be either a discrete or non-discrete code (a conspicuity code, e.g. 1000).

b) Pilots shall ensure that the aircraft transponder is operating (that is, XPNDRor the equivalent according to specific installation, AUTO if available, notOFF or STBY) and the assigned Mode A code is selected prior to the requestfor pushback or taxi, whichever is earlier.

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

5.3 After Landing

a) Pilots shall ensure that the aircraft transponder is operating (that is, XPNDRor the equivalent according to specific installation, AUTO if available, notOFF or STBY) after landing, and continuously until the aircraft is stationaryat the aircraft stand.

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

New format, reindexing.

5 Procedures / Actions Required By Pilots

CHANGISINGAPORE, SINGAPOREWSSS/SIN

10-9C5


CHANGES: | JEPPESEN, 1998, 2013. ALL RIGHTS RESERVED.

WSSS/SINJEPPESEN

10-9DSINGAPORE, SINGAPORE

CHANGI

FLIGHT LEVELS TO DEPARTING AIRCRAFT

GENERAL

b. 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 offeredafter coordination with the adjacent ATC centers.

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 orN571/N877, the Kuala Lumpur/Bangkok FIR boundary on M770 or L759 and VPL on P628can expect its requested flight level.

d. To avoid confusion, pilots shall use the correct phraseology as detailed in

PROCEDURES paragraph a. when ready for push back.

PROCEDURES

the following phraseology:

- call sign

- destination

- propsed flight level and alternate level, if any

- parking position

b. On receipt of the 'ready to push back' call, ATC will advise the pilot whether the proposedflight level or other alternate flight level is available and an ATC clearance will be issuedaccordingly. If pre-departure coordination with an adjacent unit or center is required, thepilot will be instructed to standby.

c. Once the fight level is accepted by the pilot and an ATC clearance issued, the aircraftmust be pushed back within 5 minutes from the time the ATC clearance is acceptedunless other ATC restrictions are imposed. The ATC clearance will be cancelled upon expiration of the 5 minute grace period.

PROCEDURES FOR PUSH BACK AND ASSIGMENT OF

N571/N877 or P628 will be cleared as follows:

separation provided there is no closing speed with the preceding aircraft.

a. Aircraft departing Singapore Changi Airport shall adhere to the procedures for push back

d. At the end of the push back, the departing aircraft must have all engines started and beready to taxi immediately, unless otherwise instructed by ATC.

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

and assignment of flight levels.

c. Departing flights from Singapore requesting FL280 or FL320 on L759, M770, N571,

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

a. The pilot shall notify ATC when the aircraft is ready to push back within 5 min using

29 DEC 17

None.


WSSS/SINJEPPESEN

10-9ESINGAPORE, SINGAPORE

CHANGI


Delays may be expected for the second aircraft to push back and to taxi when two or moreaircraft are parked either adjacent to one another or close together. However, it will retainits ATC clearance even if the 5 minutes grace period allowed for under PROCEDURES paragraph c. 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 specific time

and level or to depart a number of minutes behind a preceding traffic to establishlongitudinal separation. Such a delay will not deprive a departing aircraft of its ATC clearanceeven though the 5 minutes grace period would have been exceeded.

DELAY DUE TO OVERFLIGHTS

These are flights operating through Singapore FIR without landing at Changi Airport. Dependingon 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.

a. A departing aircraft may have its ATC clearance cancelled under the following circumstances:

1. on expiry of the 5 minutes grace period under

PROCEDURES

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.

'(Call sign of aircraft) your ATC clearance is cancelled (reason)'.

normal procedures as if it is the first time they are ready to depart.

paragraph c., it is still unable to push back; or

DELAY IN PUSH BACK AND/OR TAXI DUE TO OTHER AIRCRAFT

b. ATC will inform the aircraft when a clearance is cancelled using the following phraseology:

GATE HOLD PROCEDURES FOR DEPARTING AIRCRAFT

subsequent push backs of departures will be regulated such that the Ground Movement Planner (GMP) on frequency 121.65 will start to issue pilots with Expected Pushback 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.

a. Whenever there are about five to seven departing aircraft at the Rwy holding point,

b. When an EPT is issued, pilots will be instructed to either remain on GMP frequency

c. A flight issued with an EPT but chooses to commence pushback 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.

d. In a situation when a departing aircraft is occupying a gate that has been assigned

Singapore Ground for pushback for the purpose of better gate utilization.

e. To maximize runway utilization, departure sequence will be planned on the basis of increasing runway throughput so as to enhance overall efficiency.

CANCELLATION OF ATC CLEARANCE/ OBTAINING A FRESH CLEARANCE

c. Pilots who are ready to depart following the cancellation of an ATC clearance will adopt the

GROUND MOVEMENT PLANNER ON VHF 121.65

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 of the frequency.

to an arriving aircraft, the departing aircraft will be instructed by the GMP to contact

29 DEC 17

or to monitor Singapore Ground Control (frequencies 121.725, 121.85, 122.55, 124.3 or125.65). 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

for pushback instruction. This is to prevent unnecessary frequency congestion.maintain a listening watch on the assigned Singapore Ground Control frequency and wait

Singapore Ground Control frequencies.


WSSS/SINJEPPESEN

10-9E1SINGAPORE, SINGAPORE

CHANGI

CHANGES:

a. This frequency shall be used for aircraft start-up/push-back clearance.

b. Unless otherwise instructed by ATC, the pilot-in-command shall prior to starting engines

c. 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.

TAXIING

a. Taxi clearance given by Ground Movement Control will relate to movement on the maneuvering area, but excluding the marshalling area.

b. Aircraft taxiing on the maneuvering 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.

c. 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 maneuvering area or to comply with ATC directions intended to regulate aircraft on the maneuvering area.

d. Pilots are reminded to always use minimum power when starting engines, when maneuvering within the apron area or when maneuvering 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.

TAKE-OFF AND LANDING

a. 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, E2Rwy 20R - Twy W1. W2

c. The pilot-in-command shall not run-up on the runway in use unless authorized by Aerodrome Control. Engines 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.

d. 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.

e. Aircraft with radio communication failure shall vacate the runway and stop on the taxiway and watch for light signals from Aerodrome Control.

ARRIVING AIRCRAFT

The pilot-in-command of an arriving aircraft shall contact the appropriate Approach Control Unit 10 minutes before entering the CTR or ATZ.

b. The pilot-in-command shall not take-off or land without a clearance from Aerodrome Control.

29 DEC 17

2. Change from Ground Movement Control frequency to the Runway Control frequency wheninstructed (118.6 or 118.25). 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 forinstruction. This is to prevent unnecessary frequency congestion.

d. Departing aircraft will be instructed when to change from 118.6 or 118.25 to Singapore

Departure frequency 120.3.

e. In the case of the aircraft having landed, the pilot-in-command shall change from 118.6 or


GROUND MOVEMENT CONTROL ON 121.725, 121.85, 122.55, 124.3 and 125.65.

125.65.listen out on the Ground Movement Control frequency on 121.75, 121.85, 122.55, 124.3 or

118.25 to 121.85, 122.55, 124.3 or 125.65 immediately upon instructed by ATC after clearing

and parking instructions until he arrives at his aircraft stand.

the runway. He shall maintain watch on 121.725, 121.85, 122.55, 124.3 or 125.65 for taxiing

Ground Movement Control frequency.



JEPPESEN

CHANGES:

1.

2.

3.

A1

A2

A3 Pushback approved,to face North(or South).

A4

Pushback approved,to face North(or South).

A5, A9

Pushback approved,to face North.

OR

Pushback approved,to face South.

Standard pushback approved.

Standard pushback approved.

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.

When the pilot is ready for start-up and pushback, he/she shall seek confirmation from the ground crew that there is no hazard to the aircraft starting up. The pilot shall then notify the Ground Movement Controller (Callsign: Singapore Ground) that the aircraft is ready for pushback. On beinginformed by Singapore Ground that pushback is approved, the pilot should coordinate with the groundcrew for the start-up and pushback of the aircraft.

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.

This alternate pushback procedure can only be exercisedif the auxiliary power unit of aircraft is unserviceable.

A10

ORPushback approved,to face South.


The aircraft (on idle thrust) shall be pushed back onto TWY U2to face North until the nose of the aircraft is behind the stopbarbehind aircraft stand A10. The aircraft may breakaway fromthere.

10 MAR 17

The aircraft (on idle thrust) shall be pushed back onto TaxilaneV6,following Taxilane V6 centreline onto TWY WA, to face Northuntil the nose of the aircraft is behind the stopbar behindaircraft stand A2. The aircraft may breakaway from there.

Pushback approved,to face Northon TWY WA.

Alternate Pushback Procedure (To Face North)

Alternate Pushback Procedure (To Face South)

The aircraft (on idle thrust) shall be pushed back onto TaxilaneV6,following Taxilane V6 centreline onto TWY WA, to face Southuntil the nose of the aircraft is behind the stopbar behindaircraft stand B2. The aircraft may breakaway from there.This alternate pushback procedure can only be exercisedif the auxiliary power unit of aircraft is unserviceable.

Pushback approved,to face Southon TWY WA.

The aircraft shall be pushed back following the pushback lineonto Taxilane V6 until its nosewheel is at the "EOP A1" positionThe aircraft shall then be towed forward onto Taxilane V6 toface West until its nosewheel is at the "EOT A1, A2, B1, B2"position. The aircraft may breakaway from there. Engine start up is not permitted during standard pushback.

The aircraft (on idle thrust) shall be pushed back following thepushback line onto Taxilane V6 to face West until its nosewheelis at the "EOP A2, B2" position. The aircraft shall then be towedforward until its nosewheel is at the "EOT A1, A2, B1, B2"position. The aircraft may breakaway from there.Alternate Pushback Procedure (To Face North)


The aircraft (on idle thrust) shall be pushed back onto TWY WA,to face North until the nose of the aircraft is behind the stopbarbehind aircraft stand A2. The aircraft may breakaway from there.


The aircraft (on idle thrust) shall be pushed back onto TWY WA,to face South until the nose of the aircraft is behind the stopbarbehind aircraft stand B2. The aircraft may breakaway from there.This alternate pushback procedure can only be exercisedif the auxiliary power unit of aircraft is unserviceable.



The aircraft (on idle thrust) shall be pushed back onto TWY WAto face North (or South) its nosewheel is at the intersection ofthe aircraft stand lead-in line and TWY WA centerline. Theaircraft may breakaway from there.

The aircraft (on idle thrust) shall be pushed back following thepushback line onto TWY WA to face North (or South) until itsnosewheel is at the intersection of the aircraft stand lead-in lineand TWY WA centerline. The aircraft may breakaway from there.

The aircraft (on idle thrust) shall be pushed back following thepushback line onto TWY U2 to face North until the nose of theairrcaft is behind the stopbar behind aircraft stand A10. Theaircraft may breakaway from there.

The aircraft (on idle thrust) shall be pushed back onto TWY U2followed by TWY WA to face South until nose of the aircraft isbehind the stopbar behind aircraft stand A4. The aircraft maybreakaway from there.

The aircraft (on idle thrust) shall be pushed back onto TWY U2followed by TWY WA to face South until the nose of the aircraftis behind the stopbar behind aircraft stand A4. The aircraft maybreakaway from there.

Text.


10-9FWSSS/SIN

PROCEDURES FOR START-UP AND PUSHBACK OF AIRCRAFT

APRON/ACFTSTANDS

PUSHBACK PROCEDURESPHRASEOLOGY USED

BY SINGAPOREGROUND

TERMINAL 3 - WEST APRON



JEPPESEN

CHANGES:

A11 Pushback approved,to face North.


A12 Pushback approved,to face North.



A13, A14, A15


A16 Pushback approved,to face North(or South).

A17 Pushback approved,to face West.


A18 Standard pushbackapproved.

The aircraft (on idle thrust) shall be pushed back onto TWY WAto face South until the nose of the aircraft is behind thestopbar behind aircraft stand A16. The aircraft may breakawayfrom there.




10 MAR 17

The aircraft (on idle thrust) shall be pushed back onto TWY U2to face North until its nosewheel is at the intersection of theaircraft stand lead-in line and TWY U2 centerline. The aircraftshall then be towed forward until the nose of the aircraft isbehind the stopbar behind aircraft stand A10. The aircraft maybreakaway from there.

The aircraft (on idle thrust) shall be pushed back onto TWY U2to face South until its nosewheel is at the intersection of theaircraft stand lead-in line and TWY U2 centerline. The aircraftshall then be towed forward until the nose of the aircraft isbehind the stopbar behind aircraft stand A12. The aircraft maybreakaway from there.

The aircraft (on idle thrust) shall be pushed back onto TWY U2to face North until its nosewheel is at the intersection of theaircraft stand lead-in line and TWY U2 centerline. The aircraftshall then be towed forward until the nose of the aircraft isbehind the stopbar behind aircraft stand A10. The aircraft maybreakaway from there.

The aircraft (on idle thrust) shall be pushed back onto TWY U2to face South until its nosewheel is at the intersection of theaircraft stand lead-in line and TWY U2 centerline. The aircraftmay breakaway from there.

The aircraft (on idle thrust) shall be pushed back onto TWY U2to face South until the nose of the aircraft is behind the stopbarbehind aircraft stand A12. The aircraft may breakaway fromthere.

OR

The aircraft (on idle thrust) shall be pushed back onto TWY U2followed by TWY WA to face North until the nose of the aircraftis behind the stopbar behind aircraft stand A16. The aircraft maybreakaway from there.

The aircraft (on idle thrust) shall be pushed back onto TWY WAto face North (South) until its nosewheel is at the intersectionof the aircraft stand lead-in line and TWY WA centerline. Theaircraft may breakaway from there.

OR

The aircraft (on idle thrust) shall be pushed back following thepushback line onto Taxilane U4 to face West until the nose ofthe aircraft is behind the stopbar behind aircraft stand A18. Theaircraft may breakaway from there.

The aircraft (on idle thrust) shall be pushed back following thepushback line onto Taxilane U4 to face West until its nosewheelis at the "EOP A19" position behind aircraft stand A19. Theaircraft may breakaway from there.

The aircraft (on idle thrust) shall be pushed back following thepushback line onto Taxilane U4 to face West until its nosewheelis at the "EOP A20" position behind aircraft stand A20. Theaircraft may breakaway from there.

The aircraft (on idle thrust) shall be pushed back following thepushback line onto Taxilane U4 until its nosewheel is at the"EOP A21" position.The aircraft shall then be towed forward toface West until the nose of the aircraft is behind the stopbarbehind aircraft stand A18. The aircraft may breakaway fromthere.

Text.

The aircraft (on idle thrust) shall be pushed back onto TWY V8to face West until its nosewheel is at the "EOP A17" positionbehind aircraft stand A17. The aircraft may breakaway fromthere.


10-9GWSSS/SIN

APRON/ACFTSTANDS


BY SINGAPOREGROUND



JEPPESEN

CHANGES:

Standard pushbackapproved.

B1

B2




The aircraft (on idle thrust) shall be pushed back onto TaxilaneV6,following Taxilane V6 centerline onto TWY WA, to face Southuntil the nose of the aircraft is behind the stopbar behindaircraft stand B2. The aircraft may breakaway from there.This alternate pushback procedure can only be exercisedif the auxiliary power unit of aircraft is unserviceable.

The aircraft shall be pushed back following the pushback lineuntil its nosewheel at the "EOP B1" position. The aircraft shallthen be towed forward onto Taxilane V6 to face West until itsnosewheel is at the "EOT A1, A2, B1, B2" position. The aircraftmay breakaway from there. Engine start up is not permittedduring standard pushback.

The aircraft (on idle thrust) shall be pushed back onto TaxilaneV6, following Taxilane V6 centerline onto TWY WA, to faceNorth until the nose of the aircraft is behind the stopbar behindaircraft stand A2. The aircraft may breakaway from there.










The aircraft (on idle trust) shall be pushed back following thepushback line onto Taxilane V6 to face West until its nosewheelis at the "EOP A2, B2" position. The aircraft shall then be towedforward until its nosewheel is at the "EOT A1, A2, B1, B2"position. The aircraft may breakway from there.

The aircraft (on idle thrust) shall be pushed back onto TWY WAto face North until the nose of the aircraft is behind the stopbarbehind aircraft stand A2. The aircraft may breakaway from there.

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

B5, B6 Pushback approved,to face North.



B7 Pushback approved,to face North.

B8


OR



B9, B10

The aircraft (on idle thrust) shall be pushed back onto TWY U1to face South until the nose of the aircraft is behind thestopbar behind aircraft stand B7. The aircraft may breakawayfrom there.

B3

B4 Pushback approved,to face North(or South).

The aircraft (on idle thrust) shall be pushed back onto TWY WAto face North (or South) until its nosewheel is at theintersection of the aircraft stand lead-in line and TWY WAcenterline. The aircraft may breakaway from there.

The aircraft (on idle thrust) shall be pushed back following thepushback line onto TWY WA to face North (or South) until itsnosewheel is at the intersection of the aircraft stand pushbackline and TWY WA centerline. The aircraft may breakaway fromthere.

The aircraft (on idle thrust) shall be pushed back onto TWY U1to face North following TWY U1 centerline onto TWY WA untilthe nose of the aircraft is behind the stopbar behind aircraftstand B4. The aircraft may breakaway from there.

The aircraft (on idle thrust) shall be pushed back following thepushback line onto TWY U1 to face South until the nose of theaircraft is behind the stopbar behind aircraft stand B7. Theaircraft may breakaway from there.

The aircraft (on idle thrust) shall be pushed back onto TWY U1to face North following TWY U1 centerline onto TWY WA untilthe nose of the aircraft is behind the stopbar behind aircraftstand B4. The aircraft may breakaway from there.

OR

The aircraft (on idle thrust) shall be pushed back onto TWY U1to face North (or South) until its nosewheel is at theintersection of the aircraft stand lead-in line and TWY U1centerline. The aircraft may breakaway from there.

The aircraft (on idle thrust) shall be pushed back onto TWY U1to face North until its nosewheel is at the intersection of theaircraft stand lead-in line and TWY U1 centerline. The aircraftshall then be towed forward until its nosewheel is at theintersection of aircraft stand B9 lead-in line and TWY U1centerline.The aircraft may breakaway from there.

The aircraft (on idle thrust) shall be pushed back onto TWY U1to face South until its nosewheel is at the intersection of theaircraft stand lead-in line and TWY U1 centerline. Theaircraft may breakaway from there.


None.

15 DEC 17 CHANGISINGAPORE, SINGAPORE

10-9HWSSS/SIN

APRON/ACFTSTANDS PUSHBACK PROCEDURES

PHRASEOLOGY USEDBY SINGAPORE

GROUND



JEPPESEN

CHANGES:

461

462

Pushback approvedto face West.

Pushback approvedto face West.

462L Pushback approvedto face West.

462R Pushback approvedto face West.

463 Pushback approvedto face West.

463L Pushback approvedto face West.

463R Pushback approvedto face West.

The aircraft (on idle thrust) shall be pushed back onto taxiwayS1 to face west until the nose of the aircraft is behind the stopbar behind aircraft stand 463L. The aircraft may breakawayfrom there. There shall be no simultaneous aircraft pushbackfrom aircraft stands 461, 462, 462L, 462R, 463 and 463L.

The aircraft (on idle thrust) shall be pushed back onto taxiwayS1 to face west until its nosewheel is at the intersection of theaircraft stand pushback line and taxiway S1 centerline. Theaircraft may breakaway from there. There shall be nosimultaneous aircraft pushback from aircraft stands 461, 462L,462R, 463, 463L and 463R.The aircraft (on idle thrust) shall be pushed back onto taxiwayS1 to face west until its nosewheel is at the intersection of theaircraft stand pushback line and taxiway S1 centerline. Theaircraft may breakaway from there. There shall be nosimultaneous aircraft pushback from aircraft stands 461, 462,462R, 463, 463L and 463R.The aircraft (on idle thrust) shall be pushed back onto taxiwayS1 to face west until its nosewheel is at the intersection of theaircraft stand pushback line and taxiway S1 centerline. Theaircraft may breakaway from there. There shall be nosimultaneous aircraft pushback from aircraft stands 461, 462,462L, 463, 463L and 463R.The aircraft (on idle thrust) shall be pushed back onto taxiwayS1 to face west until its nosewheel is at the intersection of theaircraft stand pushback line and taxiway S1 centerline. Theaircraft may break away from there. There shall be nosimultaneous aircraft pushback from aircraft stands 461, 462,462L, 462R, 463L and 463R.The aircraft (on idle thrust) shall be pushed back onto taxiwayS1 to face west until its nosewheel is at the intersection of theaircraft stand pushback line and taxiway S1 centerline. Theaircraft may break away from there. There shall be nosimultaneous aircraft pushback from aircraft stands 461, 462,462L, 462R, 463 and 463R.

The aircraft (on idle thrust) shall be pushed back onto taxiwayS1 to face west until its nosewheel is at the EOP position. Theaircraft shall then be towed forward until its nosewheel is at the EOT position. The aircraft may break away from there.There shall be no simultaneous aircraft pushback from aircraftstands 462, 462L, 462R, 463, 463L and 463R.

464 Standard pushbackapproved.



465, 467

The aircraft (on idle thrust) shall be pushed back following thepushback line until its nose wheel is at "EOP 464" position. Theaircraft shall then be towed forward onto Taxilane S4 to face westuntil its nose wheel is at "EOT 464" position. The aircraft maybreak away from there.

The aircraft (on idle thrust) shall be pushed back following thepushback line onto Taxilane S4 to face west until its nose wheel isat intersection of the aircraft stand pushback line and TaxilaneS4 centerline. The aircraft may break away from there.

15 DEC 17


466, 469

468

The aircraft (on idle thrust) shall be pushed back following thepushback line onto Taxilane S4 to face west until its nose wheel isat "EOP 465, 467, 468" position. The aircraft may break awayfrom there.

T4 Apron moved to 10-9L9 page, 465, 467 and 468 pushback proc.

The aircraft (on idle thrust) shall be pushed back following thepushback line onto Taxilane S4 to face west until its nose wheel isat "EOP 465, 467, 468" position. The aircraft may break away fromthere.


10-9JWSSS/SIN

APRON/ACFTSTANDS


GROUND

PUSHBACK PROCEDURES

SOUTH APRON



JEPPESEN

CHANGES:

200Pushback approved,to face North.

OR


The aircraft (on idle thrust) shall be pushed back onto TaxilaneC6 to face North until its nosewheel is at the intersection of theaircraft stand lead-in line and Taxilane C6 centerline. Theaircraft shall then be towed forward until its nosewheel is atthe intersection of aircraft stand 201 lead-in line and TaxilaneC6 centreline.The aircraft may breakaway from there.

The aircraft (on idle thrust) shall be pushed back onto TaxilaneC6 to face South until its nosewheel is at the intersection ofthe aircraft stand lead-in line and Taxilane C6 centerline. Theaircraft may breakaway from there.

200R The aircraft (on idle thrust) shall be pushed back following thepushback line onto Taxilane C6 to face North (or South) until itsnosewheel is at the intersection of the aircraft stand pushbackline and Taxilane C6 centreline. The aircraft may breakawayfrom there.

Pushback approved, to face North (or South).

201 The aircraft (on idle thrust) shall be pushed back onto TaxilaneC6 to face North (or South) until the nosewheel is at theintersection of the aircraft stand lead-in line and Taxilane C6centreline. The aircraft may breakaway from there.


202 The aircraft (on idle thrust) shall be pushed back onto TaxilaneC6 to face North until its nosewheel is at the intersection of theaircraft stand lead-in line and Taxilane C6 centreline. Theaircraft may breakaway from there.

203 The aircraft (on idle thrust) shall be pushed back onto TaxilaneC6 to face North until the nose of the aircraft is behind thestopbar behind aircraft stand 203. The aircraft may breakawayfrom there.


ORThe aircraft (on idle thrust) shall be pushed back onto TaxilaneC6 to face South until its nosewheel is at the intersection of theaircraft stand lead-in line and Taxilane C6 centreline. Theaircraft may breakaway from there.


202L, 202R

OR

Pushback approved, to face North.

The aircraft (on idle thrust) shall be pushed back onto TaxilaneC6 to face South until its nosewheel is at the intersection of theaircraft stand lead-in line and Taxilane C6 centreline. Theaircraft may breakaway from there.

Pushback approved, to face South.


The aircraft (on idle thrust) shall be pushed back onto TaxilaneC6 to face North (or South) until its nosewheel is at theintersection of the aircraft stand pushback line and Taxilane C6centreline. The aircraft may breakaway from there.

200L The aircraft (on idle thrust) shall be pushed back following the pushback line onto Taxilane C6 to face North until its nose wheel is at the intersection of the aircraft stand pushback line and Taxilane C6 centerline. The aircraft shall then be towed forward until its nose wheel is abeam aircraft stand 200. The aircraft may breakaway from there.

ORThe aircraft (on idle thrust) shall be pushed back following the pushback line onto Taxilane C6 to face South until its nose wheel is at the intersection of the aircraft stand pushback line and Taxilane C6 centreline. The aircraft may breakaway from there.


Pushback approved, to face South.

T4 Apron moved to 10-9L9 page.


10-9KWSSS/SIN

APRON/ACFTSTANDS


BY SINGAPOREGROUND

EAST REMOTE APRON



JEPPESEN

CHANGES:

300

OR

The aircraft (on idle thrust) shall be pushed back onto TWY NC2to face East until the nosewheel is at the intersection of theaircraft stand lead-in line and TWY NC2 centreline. The aircraftshall then be towed forward until its nosewheel is at theintersection of aircraft stand 301 lead-in line and TWY NC2centreline.The aircraft may breakaway from there.

Pushback approved, to face East.

The aircraft (on idle thrust) shall be pushed back onto TWY NC2to face West until its nosewheel is at the intersection of theaircraft stand lead-in line and TWY NC2 centreline. The aircraftmay breakaway from there.

Pushback approved, to face West.

301 The aircraft (on idle thrust) shall be pushed back onto TWY NC2 to face East (or West) until the nosewheel is at the intersectionof the aircraft stand lead-in line and TWY NC2 centreline. Theaircraft may breakaway from there.

Pushback approved,to face East (or West).

302

OR

Pushback approved,to face East.

The aircraft (on idle thrust) shall be pushed back onto TWY NC2 to face East until the nosewheel is at the intersection of theaircraft stand lead-in line and TWY NC2 centreline. The aircraftmay breakaway from there.

The aircraft (on idle thrust) shall be pushed back onto TWY NC2 to face West until the nosewheel is at the intersection of theaircraft stand lead-in line and TWY NC2 centreline. The aircraftshall then be towed forward until the nosewheel is at theintersection of aircraft stand 301 lead-in line and TWY NC2centreline. The aircraft may breakaway from there.

Pushback approved,to face West.

303 The aircraft (on idle thrust) shall be pushed back onto TWY NC2 to face East until the nosewheel is at the intersection of theaircraft stand lead-in line and TWY NC2 centreline. The aircraftshall then be towed forward until the nosewheel is at theintersection of aircraft stand 304 lead-in line and TWY NC2centreline. The aircraft may breakaway from there.


The aircraft (on idle thrust) shall be pushed back onto TWY NC2 to face West until the nosewheel is at the intersection of theaircraft stand lead-in line and TWY NC2 centreline. The aircraftmay breakaway from there.

ORPushback approved,to face West.

304, 305 The aircraft (on idle thrust) shall be pushed back onto TWY NC2 to face East (or West) until the nosewheel is at the intersectionof the aircraft stand lead-in line and TWY NC2 centreline. Theaircraft may breakaway from there.

Pushback approved,to face East (or West).

306 The aircraft (on idle thrust) shall be pushed back onto TWY NC2 to face East until the nosewheel is at the intersection of theaircraft stand lead-in line and TWY NC2 centreline. The aircraftmay breakaway from there.


ORThe aircraft (on idle thrust) shall be pushed back onto TWY NC2 to face West until the nosewheel is at the intersection of theaircraft stand lead-in line and TWY NC2 centreline. The aircraftshall then be towed forward until the nosewheel is at theintersection of aircraft stand 305 lead-in line and TWY NC2centreline. The aircraft may breakaway from there.


307, 308

OR

The aircraft (on idle thrust) shall be pushed back onto TWY NC2 to face West until its nosewheel is at the intersection of theaircraft stand lead-in line and TWY NC2 centreline. The aircraftmay breakaway from there.

The aircraft (on idle thrust) shall be pushed back onto TWY NC2 to face East until the nosewheel is at the intersection of theaircraft stand lead-in line and TWY NC2 centreline. The aircraftshall then be towed forward until the nose of aircraft is behindthe stopbar behind aircraft stand 309.The aircraft maybreakaway from there.



309 The aircraft (on idle thrust) shall be pushed back onto TWY NC2 to face East until its nosewheel is at the intersection of theaircraft stand lead-in line and TWY NC2 centreline. The aircraftmay breakaway from there.


OR

The aircraft (on idle thrust) shall be pushed back onto TWY NC2 to face West until the nosewheel is at the intersection of theaircraft stand lead-in line and TWY NC2 centreline. The aircraftshall then be towed forward until the nose of aircraft is behindthe stopbar behind aircraft stand 307.The aircraft maybreakaway from there.


310 The aircraft (on idle thrust) shall be pushed back onto TWY NC2 to face East until the nose of the aircraft is behind the stopbarbehind aircraft stand 309. The aircraft may breakaway fromthere. ORThe aircraft (on idle thrust) shall be pushed back onto TWY NC2 to face West until the nosewheel is at the intersection of theaircraft stand lead-in line and TWY NC2 centreline. The aircraftshall then be towed forward until the nose of aircraft is behindthe stopbar behind aircraft stand 307.The aircraft maybreakaway from there.



None.


10-9LWSSS/SIN

APRON/ACFTSTANDS


BY SINGAPOREGROUND

NORTH REMOTE APRON



JEPPESEN

CHANGES:

400, 401, 402,403, 404

The aircraft (on idle thrust) shall be pushed back onto TaxilaneA6 to face North (or South) until its nosewheel is at theintersection of the aircraft stand lead-in line and Taxilane A6centerline.

Pushback approved,to face North (or South).

D32

C23 The aircraft (on idle thrust) shall be pushed back onto TWY U1to face North until the nose of the aircraft is behind the stopbarline behind the aircraft stand C22. The aircraft may break awayfrom there.

Pushback approved, toface North.

ORThe aircraft (on idle thrust) shall be pushed back onto Twy U1to face South until its nosewheel is at the intersection ofthe aircraft stand lead-in line and TWY U1 centreline. Theaircraft may break away from there.

Pushback approved, toface South.

C24, C25 The aircraft (on idle thrust) shall be pushed back onto Twy U1to face North (or South) until its nosewheel is at the intersectionof the aircraft stand lead-in line and TWY U1 centreline. Theaircraft may break away from there.

Pushback approved, toface North (or South).

C26

OR

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




D30


D34 The aircraft (on idle thrust) shall be pushed back following thepushback line onto Taxilane N2 to face North until the nosewheelis at the intersection of the aircraft stand lead-in line andTaxilane N2 centerline. The aircraft may breakaway from there.


Alternate Pushback Procedure

The aircraft (on idle thrust) shall be pushed back onto TaxilaneN2 to face South followed by Taxilane N3 until the nose of theaircraft is behind the stopbar line behind the aircraft stand D35.The aircraft may break away from there.

Pushback approved,to face South onTaxilane N3.

The aircraft (on idle thrust) shall be pushed back onto TWY WA to face South until its nosewheel is at the intersection of theaircraft stand lead-in line and TWY WA centreline. The aircraftshall then be towed forward until its nosewheel is at the "EOTC26" position behind aircraft stand C26. The aircraft maybreakaway from there.

29 DEC 17

The aircraft (on idle thrust) shall be pushed back onto Twy U1to face North (South) until its nosewheel is at the intersection ofthe aircraft stand lead-in line and TWY U1 centreline. Theaircraft may break away from there.

Pushback approved, toface North (South).

C1

C20

C22

The aircraft (on idle thrust) shall be pushed back onto Twy U1to face North until its nose wheel is at the "EOP C1" positionbehind aircraft stand C1. The aircraft may break away fromthere.


ORThe aircraft (on idle thrust) shall be pushed back onto Twy U1to face South until its nose wheel is at the intersection ofthe aircraft stand lead-in line and TWY U1 centreline. Theaircraft may break away from there.


The aircraft (on idle thrust) shall be pushed back onto Twy U1to face South until its nose wheel is at the "EOP C20" positionbehind aircraft stand C22. The aircraft may breakaway fromthere.

ORPushback approved, toface South.

The aircraft (on idle thrust) shall be pushed back onto Twy U1to face North until its nose wheel is at the intersection ofthe aircraft stand lead-in line and TWY U1 centreline. Theaircraft may break away from there.


The aircraft (on idle thrust) shall be pushed back following thepushback line onto Taxilane N2 to face North until its nosewheelis at the "EOP C13, D32" position. The aircraft shall then betowed forward until its nosewheel is at the "EOT C13, D32"position. The aircraft may breakaway from there.

The aircraft (on idle thrust) shall be pushed back following thepushback line to face North until the nosewheel is at the"EOP D30" position. The aircraft shall then be towed forwardfollowing the tow line onto Taxilane N2 until its nosewheel isat the "EOT C11, D30" position. The aircraft may breakawayfrom there.




The aircraft (on idle thrust) shall be pushed back onto TaxilaneN2 to face South followed by Taxilane N1 until the nose of theaircraft is behind the stopbar line behind aircraft stand C16.The aircraft may break away from there.


The aircraft (on idle thrust) shall be pushed back onto TaxilaneN2 to face South followed by Taxilane N3 until the nose of theaircraft is behind the stopbar line behind aircraft stand D35.The aircraft may break away from there.

Stand D32 pushback procedure, part of D34 moved to reverse page.


10-9L1WSSS/SIN

APRON/ACFTSTANDS

PUSHBACK PROCEDURES

NORTH-EAST REMOTE APRON

TERMINAL 1 - WEST APRON

TERMINAL 1 - CENTRAL APRON

PHRASEOLOGY USEDBY SINGAPORE GROUND



JEPPESEN

CHANGES:

Pushback approvedto face North on Taxilane N2.

D35 The aircraft (on idle thrust) shall be pushed back onto TaxilaneN3 to face North until its nosewheel is at the intersection of theaircraft stand lead-in line and Taxilane N3 centreline. Theaircraft may breakaway from there.


ORThe aircraft (on idle thrust) shall be pushed back onto TaxilaneN3 to face South until the nose of the aircraft is behind thestopbar line behind aircraft stand D35. The aircraftmay breakaway from there.



The aircraft (on idle thrust) shall be pushed back onto TaxilaneN3 to face North until the nose of the aircraft is behind thestopbar behind aircraft stand D34 on taxilane N2.The aircraft may break away from there.


Pushback approved,to face North on Taxilane N2.

Pushback approved,to face North on Taxilane N2.

D37 Standard pushbackapproved.

D36 The aircraft (on idle thrust) shall be pushed back onto TaxilaneN3 to face North (or South) until its nosewheel is at theintersection of the aircraft stand lead-in line and Taxilane N3centreline. The aircraft may breakaway from there.

The aircraft (on idle thrust) shall be pushed back onto TaxilaneN3 to face North until the nose of the aircraft is behind thestopbar behind aircraft stand D34 on Taxilane N2. Theaircraft may breakaway from there.



The aircraft (on idle thrust) shall be pushed back onto TaxilaneN3 to face North until its nosewheel is at the intersection ofthe aircraft stand lead-in line and Taxilane N3 centreline. Theaircraft may breakaway from there.

The aircraft (on idle thrust) shall be pushed back onto TaxilaneN3 to face North until the nose of the aircraft is behind thestopbar behind aircraft stand D34 on Taxilane N2. Theaircraft may breakaway from there.


D38 The aircraft (on idle thrust) shall be pushed back onto TaxilaneN3 to face North until the nose of the aircraft is behind thestopbar behind aircraft stand D37. The aircraft may breakawayfrom there.

C11 Standard pushbackapproved.

C13 Standard pushbackapproved.

C15 The aircraft (on idle thrust) shall be pushed back following thepushback line onto Taxilane N2 to face North until its nosewheelis at the intersection of the aircraft stand lead-in line andTaxilane N2 centreline.The aircraft may breakaway from there.






The aircraft (on idle thrust) shall be pushed back onto TaxilaneN2 to face South followed by Taxilane N1 until the nose of theaircraft is behind the stopbar line behind the aircraft stand C16.The aircraft may break away from there.


29 DEC 17

The aircraft (on idle thrust) shall be pushed back following thepushback line to face North until its nosewheel is at the"EOP C11" position. The aircraft shall then be towed forwardfollowing the tow line onto Taxilane N2 until its nosewheel isat the "EOT C11, D30" position. The aircraft may breakawayfrom there.

The aircraft (on idle thrust) shall be pushed back following thepushback line onto Taxilane N2 to face North until its nosewheelis at the "EOP C13, D32" position. The aircraft shall then betowed forward until its nosewheel is at the "EOT C13, D32" position. The aircraft may breakaway from there.




The aircraft (on idle thrust) shall be pushed back onto TaxilaneN2 to face South followed by Taxilane N1 until the nose of theaircraft is behind the stopbar line behind the aircraft stand C16.The aircraft may break away from there.



Alternate Pushback ProcedureThe aircraft (on idle thrust) shall be pushed back onto TaxilaneN2 to face South followed by Taxilane N1 until the nose of theaircraft is behind the stopbar line behind aircraft stand C16.The aircraft may break away from there.


D34 (contd.)

Stand C13 pushback procedure, part of D34 moved from front page.


10-9L2WSSS/SIN

APRON/ACFTSTANDS


BY SINGAPOREGROUND



JEPPESEN

CHANGES:

C16 The aircraft (on idle thrust) shall be pushed back onto TaxilaneN1 to face North until its nosewheel is at the intersection ofthe aircraft stand lead-in line and Taxilane N1 centreline. Theaircraft may breakaway from there.


ORThe aircraft (on idle thrust) shall be pushed back onto TaxilaneN1 to face South until the nose of the aircraft is behind thestopbar line behind aircraft stand C16. The aircraft may breakaway from there.



The aircraft (on idle thrust) shall be pushed back onto TaxilaneN1 to face North until the nose of the aircraft is behind thestopbar behind aircraft stand C15 on Taxilane N2. Theaircraft may breakaway from there.

Pushback approved, toface North onTaxilane N2.


C17 The aircraft (on idle thrust) shall be pushed back onto TaxilaneN1 to face North (or South) until its nosewheel is at theintersection of the aircraft stand lead-in line and Taxilane N1centreline. The aircraft may break away from there.



The aircraft (on idle thrust) shall be pushed back onto TaxilaneN1 to face North until the nose of the aircraft is behind thestopbar behind aircraft stand C15 on Taxilane N2. The aircraftmay break away from there.

Pushback approved, toface North on TaxilaneN2.

C18 The aircraft (on idle thrust) shall be pushed back onto TaxilaneN1 to face North until its nosewheel is at the intersection ofthe aircraft stand lead-in line and Taxilane N1 centreline. Theaircraft may break away from there.Alternate Pushback ProcedureThe aircraft (on idle thrust) shall be pushed back onto TaxilaneN1 to face North until the nose of the aircraft is behind thestopbar behind aircraft stand C15 on Taxilane N2. The aircraftmay break away from there.

Pushback approved, toface North on TaxilaneN2.

C19The aircraft (on idle thrust) shall be pushed back onto TaxilaneN1 to face North until the nose of the aircraft is behind thestopbar behind aircraft stand C18. The aircraft may break awayfrom there.


The aircraft (on idle thrust) shall be pushed back following thepushback line onto Taxilane A6 to face North (or South) untilits nosewheel is at the intersection of the aircraft standpushback line and Taxilane A6 centreline. The aircraft maybreak away from there.

The aircraft (on idle thrust) shall be pushed back onto TaxilaneA6 to face North (or South) until its nosewheel is at theintersection of the aircraft stand lead-in line and Taxilane A6centreline. The aircraft may break away from there.


D42L, D42R Pushback approved, toface North (or South).

The aircraft (on idle thrust) shall be pushed back onto TaxilaneA6 to face North (or South) until its nosewheel is at theintersection of the aircraft stand lead-in line and Taxilane A6centreline. The aircraft may break away from there.


D44, D46, D47

D48 Pushback approved, toface North.

The aircraft (on idle thrust) shall be pushed back onto TaxilaneA6 to face North until the nose of the aircraft is behind thestopbar line behind aircraft stand D48. The aircraft may breakaway from there.

OR

The aircraft (on idle thrust) shall be pushed back onto TaxilaneA6 to face or South until its nosewheel is at theintersection of the aircraft stand lead-in line and Taxilane A6centreline. The aircraft may break away from there.



D40


D40L, D40R

D41, D42

The aircraft (on idle thrust) shall be pushed back onto TaxilaneA6 to face North until its nosewheel is at EOP B D40, D40L,D40R position. The aircraft may breakaway from there.

The aircraft (on idle thrust) shall be pushed back onto TaxilaneA6 to face South until its nosewheel is at EOP A D40, D40L,D40R position. The aircraft may breakaway from there.

OR

The aircraft (on idle thrust) shall be pushed back following thepushback line onto Taxilane A6 to face North until itsnosewheel is at EOP B D40, D40L, D40R position. The aircraftmay breakaway from there.

The aircraft (on idle thrust) shall be pushed back following thepushback line onto Taxilane A6 to face South until itsnosewheel is at EOP A D40, D40L, D40R position. The aircraftmay breakaway from there.

OR

22 SEP 17

None.


10-9L3WSSS/SIN

APRON/ACFTSTANDS


BY SINGAPOREGROUND

TERMINAL 1 - EAST APRON



JEPPESEN

CHANGES:

E1 Standard pushbackapproved.

D49 Pushback approved, toface North.

ORThe aircraft (on idle thrust) shall be pushed back onto TaxilaneA6 to face South until its nosewheel is at the intersection ofthe aircraft stand lead-in line and Taxilane A6 centreline.The aircraft shall then be towed forward until its nosewheelis on the "EOT D49" position behind aircraft stand D49.The aircraft may break away from there.


The aircraft (on idle thrust) shall be pushed back onto TaxilaneA6 to face North until its nosewheel is at the "EOP D49"position. The aircraft may break away from there.

The aircraft (on idle thrust) shall be pushed back following thepushback line to face East until its nosewheel is at the"EOP E1" position.The aircraft shall then be towed forwardonto Taxilane B2 until its nosewheel is at the"EOT E1, E2, F30, F31" position.The aircraft may breakawayfrom there.


E5, E6


F30 Standard pushbackapproved.

F31

F32

F33






Pushback approved, toface South onTaxilane B1.

Pushback approved, toface North onTaxilane B3.




Pushback approved, toface South on TaxilaneB1.

Pushback approved, toface North on TaxilaneB3.

E3 The aircraft (on idle thrust) shall be pushed back following thepushback line onto Taxilane B2 to face East until its nosewheelis at the intersection of the aircraft stand pushback line andTaxilane B2 centreline. The aircraft may breakaway from there.



E4 The aircraft (on idle thrust) shall be pushed back following thepushback line onto Taxilane B2 to face East until its nosewheelis at the "EOP E4, F33" position. The aircraft may breakawayfrom there.

The aircraft (on idle thrust) shall be pushed back onto TaxilaneB1 to face South until its nosewheel is at the "EOP A E4, F33"position. The aircraft may break away from there.

The aircraft (on idle thrust) shall be pushed back onto TaxilaneB3 to face North until its nosewheel is at the "EOP B E4, F33"position. The aircraft may break away from there.

The aircraft (on idle thrust) shall be pushed back following thepushback line onto Taxilane B2 to face East until its nosewheelis at the "EOP F31" position. The aircraft shall then be towedforward to "EOT E1, E2, F30, F31" position. The aircraft maybreakaway from there.

The aircraft (on idle thrust) shall be pushed back following thepushback line onto Taxilane B2 to face East until its nosewheelis at the intersection of the aircraft stand pushback line andTaxilane B2 centerline. The aircraft may breakaway from there.

The aircraft (on idle thrust) shall be pushed back following thepushback line onto Taxilane B2 to face East until its nosewheelis at the "EOP E4, F33" position. The aircraft may breakawayfrom there.

The aircraft (on idle thrust) shall be pushed back onto TaxilaneB1 to face South until its nosewheel is at the "EOP A E4, F33"position. The aircraft may breakaway from there.

The aircraft (on idle thrust) shall be pushed back onto TaxilaneB3 to face North until its nosewheel is at the "EOP B E4, F33"position. The aircraft may breakaway from there.

The aircraft (on idle thrust) shall be pushed back following thepushback line to face East until its nosewheel is at the"EOP F30" position. The aircraft shall then be towed forwardonto Taxilane B2 until its nosewheel is at the"EOT E1, E2, F30, F31" position. The aircraft may breakawayfrom there.


The aircraft (on idle thrust) shall be pushed back following thepushback line onto Taxilane B2 to face East until its nosewheelis at the intersection of the aircraft stand pushback line andTaxilane B2 centreline.The aircraft shall then be towed forwardto "EOT E1, E2, F30, F31" position. The aircraft may breakawayfrom there.

22 SEP 17

The aircraft (on idle thrust) shall be pushed back onto TaxilaneB1 to face North until its nosewheel is at the intersection of theaircraft stand lead-in line and Taxilane B1 centreline. Theaircraft shall then be towed forward until its nose wheel is atthe EOT E5, E6, E7 position behind aircraft stand E6. Theaircraft may breakaway from there.

The aircraft (on idle thrust) shall be pushed back onto TaxilaneB1 to face North until its nose wheel is at the EOT E5, E6, E7position behind aircraft stand E6. The aircraft may breakawayfrom there.

The aircraft (on idle thrust) shall be pushed back onto TaxilaneB3 to face South until its nosewheel is at the intersection of theaircraft stand lead-in line and Taxilane B3 centreline. Theaircraft shall then be towed forward until its nose wheel is atthe EOT F34, F35L, F36 position behind aircraft stand F35.The aircraft may breakaway from there.

Pushback procedures for stands E5, E6, E7 and F34.


10-9L4WSSS/SIN

APRON/ACFTSTANDS


BY SINGAPOREGROUND

TERMINAL 2 - CENTRAL APRON



JEPPESEN

F35, F35R The aircraft (on idle thrust) shall be pushed back following thepushback line onto Taxilane B3 to face South until its nosewheelis at the intersection of the aircraft stand pushback line andTaxilane B3 centreline. The aircraft may breakaway from there.


F35L, F36



E8 The aircraft (on idle thrust) shall be pushed back onto TWY A4to face East until its nosewheel is at "EOP 14" position. Theaircraft shall then be towed forward to "EOT 15" position.The aircraft may breakaway from there.


The aircraft (on idle thrust) shall be pushed back following thepushback line onto Taxilane A6 to face North until its nosewheelis at the "EOP 19" position. The aircraft may breakaway fromthere.


F37

E12



Pushback approved, toface North onTaxilane A6.

E20 The aircraft (on idle thrust) shall be pushed back following thepushback line until its nosewheel is at the "EOP 17" position.The aircraft shall then be towed forward following the tow lineonto Taxilane A6 to face North until its nosewheel is at the"EOT 18A" position. The aircraft may breakaway from there.

E22 The aircraft (on idle thrust) shall be pushed back following thepushback line onto Taxilane A6 to face North until its nosewheelis at "EOP 19" position.The aircraft shall then be towed forwarduntil its nosewheel is at the "EOT 18" position. The aircraft maybreakaway from there.



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


E24, E24L,E24R, E26

E27, E28 Pushback approved, toface North (or South).

The aircraft (on idle thrust) shall be pushed back onto TaxilaneA6 to face North (or South) until its nosewheel is at theintersection of the aircraft stand lead-in line and Taxilane A6centreline. The aircraft may breakaway from there.


Pushback approved, toface East on Twy C1.



E27L, E27R The aircraft (on idle thrust) shall be pushed back following thepusback line onto Taxilane A6 to face North (or South) until itsnosewheel is at the intersection of the aircraft stand pushbackline and Taxilane A6 centreline. The aircraft may breakaway fromthere.

The aircraft (on idle thrust) shall be pushed back following thepushback line onto Taxilane C2 to face South until its nosewheelis at the "EOT 4" position. The aircraft may breakaway from there.

The aircraft (on idle thrust) shall be pushed back onto TWY C1to face East until its nosewheel is at the "EOP 5" position. Theaircraft may breakaway from there.

The aircraft (on idle thrust) shall be pushed back following thepushback line onto Taxilane A5 followed by Taxilane A6 to faceNorth until its nosewheel is at the intersection of Taxilane A6and Taxilane A5 centreline. The aircraft may breakaway from there.

E11 The aircraft (on idle thrust) shall be pushed back following thepushback line onto Taxilane A6 to face North until its nosewheelis at the intersection of Taxilane A6 and TWY A5 centreline.The aircraft shall then be towed forward following TWY A5centreline to "EOT 16" position. The aircraft may breakawayfrom there.Alternate Pushback Procedure


Pushback approved, toface North onTaxilane A6.

The aircraft (on idle thrust) shall be pushed back following thepushback line onto Taxilane A6 to face North until its nosewheelis at the "EOP 19A" position behind aircraft stand E24. Theaircraft shall then be towed forward to "EOT 18B" positionbehind aircraft stand E26. The aircraft may breakaway fromthere.The aircraft (on idle thrust) shall be pushed back following thepushback line onto TWY A5 to face North until its nosewheel isat the intersection of the aircraft stand pushback line andTaxilane A5 centreline. The aircraft shall then be towed forwarduntil its nosewheel is at the "EOT 16" position. The aircraft maybreakaway from there.

The aircraft (on idle thrust) shall be pushed back onto TaxilaneB3 to face South until its nose wheel is at the EOT F34, F35L, F36position behind aircraft stand F35. The aircraft may breakawayfrom there.

The aircraft (on idle thrust) shall be pushed back following thethe pushback line onto Taxilane C6 to face South until itsnosewheel is at the "EOP F40, F52" position. The aircraft shallthen be towed forward until its nosewheel is at the "EOT F40,F50, F52, F52R" position. The aircraft may breakaway from there.

Stand F40 pushback procedure.


10-9L5

CHANGES:

WSSS/SIN

APRON/ACFTSTANDS


GROUNDPUSHBACK PROCEDURES

TERMINAL 2 - NORTH APRON

TERMINAL 2 - SOUTH APRON


JEPPESEN



F52L The aircraft (on idle thrust) shall be pushed back following thepushback line onto Taxilane C6 to face South until its nosewheelis at the intersection of the aircraft stand pushback line andTaxilane C6 centreline. The aircraft may breakaway from there.

F52R




The aircraft (on idle thrust) shall be pushed back following thepushback line onto Taxilane C6 to face South until its nosewheelis at the intersection of Taxilane C2 and Taxilane C6 centreline.The aircraft may breakaway from there.

F56 The aircraft (on idle thrust) shall be pushed back onto Taxilane C6to face South until its nosewheel is at the intersection of theaircraft stand lead-in line and Taxilane C6 centreline. The aircraft may breakaway from there.



F56L, F56R The aircraft (on idle thrust) shall be pushed back following thepushback line onto Taxilane C6 to face South until its nosewheelis at the intersection of the aircraft stand pushback line andTaxilane C6 centreline. The aircraft may breakaway from there.

The aircraft (on idle thrust) shall be pushed back onto Taxilane C6to face North (or South) until its nosewheel is at the intersectionof the aircraft stand lead-in line and Taxilane C6 centreline. Theaircraft may breakaway from there.


F58, F59

F59L, F59R The aircraft (on idle thrust) shall be pushed back following thepushback line onto Taxilane C6 to face North (or South) until itsnosewheel is at the intersection of the aircraft stand pushbackline and Taxilane C6 centreline. The aircraft may breakaway fromthere.


The aircraft (on idle thrust) shall be pushed back onto Taxilane C6to face North (or South) until its nosewheel is at the intersectionof the aircraft stand lead-in line and Taxilane C6 centreline. Theaircraft may breakaway from there.


F60


F50


F42 Main pushback procedure (for all aircraft wingspan)

The aircraft (on idle thrust) shall be pushed back following thepushback line onto Taxilane C2 to face South until its nosewheelis at the intersection of the aircraft stand pushback line andTaxilane C2 centreline. The aircraft shall then be towed forward until its nosewheel is at the "EOT 4" position. The aircraft maybreakaway from there.Alternate pushback procedure (for all aircraft types except A380)

The aircraft (on idle thrust) shall be pushed back following thepushback line onto Taxilane C2 to face South, following TaxilaneC2 centreline onto Taxilane C6 until its nosewheel is at theintersection of Taxilane C2 and Taxilane C6 centreline. Theaircraft may breakaway from there.

Pushback approved, topushback ontoTaxilane C6.

Alternate pushback procedure (for A380 aircraft)The aircraft (on idle thrust) shall be pushed back following thepushback line onto Taxilane C2 to face South until its nosewheelis at the "EOP 4A" position. The aircraft shall then be towedforward following the tow line until its nosewheel is at the"EOT 4B" position on Taxilane C6,behind aircraft stand F59.The aircraft may breakaway from there.


F41


The aircraft (on idle thrust) shall be pushed back following thepushback line onto Taxilane C2 to face South until its nosewheel isat the intersection of the aircraft stand pushback line and TaxilaneC2 centreline. The aircraft shall then be towed forward until itsnosewheel is at the "EOT 4" position. The aircraft may breakawayfrom there.


The aircraft (on idle thrust) shall be pushed back following thepushback line onto Taxilane C2 to face South, following TaxilaneC2 centreline onto Taxilane C6 until its nosewheel is at theintersection of Taxilane C2 and Taxilane C6 centreline. Theaircraft may breakaway from there.


The aircraft (on idle thrust) shall be pushed back following thepushback line until its nosewheel is at the "EOP F50" position. Theaircraft shall then be towed forward following the tow line ontoTaxilane C6 to face South until its nosewheel is at the "EOT F40,F50, F52, F52R" position. The aircraft may breakaway from there.

The aircraft (on idle thrust) shall be pushed back following thepushback line onto Taxilane C6 to face South until its nosewheelis at the "EOP F40, F52" position. The aircraft shall then be towedforward until its nosewheel is at the "EOT F40, F50, F52, F52R"position. The aircraft may breakaway from there.

The aircraft (on idle thrust) shall be pushed back following thepushback line onto Taxilane C6 to face South until its nosewheelis at the intersection of the aircraft stand pushback line andTaxilane C6 centreline. The aircraft shall then be towed forwarduntil its nosewheel is at the "EOT F40, F50, F52, F52R"position. The aircraft may breakaway from there.

Pushback procedures for stands F50, F52 and F52R.


10-9L6

CHANGES:

WSSS/SIN

APRON/ACFTSTANDS




JEPPESEN




ORPushback approvedto face South.

502, 503, 504,505,506,507,508,509,510

The aircraft (on idle thrust) shall be pushed back onto TWY WCto face North (or South) until its nosewheel is at the intersectionof the aircraft stand lead-in line and TWY WC centreline. Theaircraft may breakaway from there.

Pushback approved to face North.

513

The aircraft (on idle thrust) shall be pushed back onto TWY WC to face South until the nosewheel of the aircraft is at the intersection of the aircraft stand lead-in line and TWY 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.

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 TWY WC centreline. The aircraft may breakaway from there.

ORThe aircraft (on idle thrust) shall be pushed back onto TWY WC to face South following TWY WC centreline onto Taxilane WDuntil the nose of the aircraft is behind the stopbar behind aircraftstand 515 on Taxilane WD.The aircraft may breakaway from there.

Pushback approvedto face South.


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

OR


The aircraft (on idle thrust) shall be pushed back onto TWY WC to face South following TWY WC centreline onto Taxilane WDuntil the nose of the aircraft is behind the stopbar behind aircraftstand 515 on Taxilane WD.The aircraft may breakaway from there.

Pushback approvedto face South.

515 The aircraft (on idle thrust) shall be pushed back onto TaxilaneWD to face South until the nose of the aircraft is behind thestopbar behind aircraft stand 515. The aircraft may breakawayfrom there.


516L, 516R The aircraft (on idle thrust) shall be pushed back following thepushback line onto Taxilane WD to face South until its nosewheelis at the intersection of the aircraft stand pushback line andTaxilane WD centreline. The aircraft shall then be towed forwarduntil the nose of the aircraft is behind the stopbar behind aircraftstand 515. The aircraft may breakaway from there.

The aircraft (on idle thrust) shall be pushed back onto TaxilaneWD to face South until its nosewheel is at the intersection of theaircraft stand lead-in line and Taxilane WD centreline. Theaircraft shall then be towed forward until the nose of the aircraftis behind the stopbar behind aircraft stand 515. The aircraft maybreakaway from there.


517 The aircraft (on idle thrust) shall be pushed back onto TaxilaneWD to face South until its nosewheel is at the "EOP 517"position. The aircraft shall then be towed forward until the noseof the aircraft is behind the stopbar behind aircraft stand 515.The aircraft may breakaway from there.


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

511, 512

517L Standard pushbackapproved.

The aircraft (on idle thrust) shall be pushed back onto TaxilaneWD to face South until its nosewheel is at the "EOP 517L"position. The aircraft shall then be towed forward until the noseof the aircraft is behind the stopbar behind aircraft stand 515.The aircraft may breakaway from there.

8 SEP 17

517R The aircraft (on idle thrust) shall be pushed back following thepushback line onto Taxilane WD to face South until its nosewheelis at the intersection of the aircraft stand pushback line andTaxilane WD centreline. The aircraft shall then be towed forwarduntil the nose of the aircraft is behind the stopbar behind aircraftstand 515. The aircraft may breakaway from there.


Layout.


10-9L7WSSS/SIN

APRON/ACFTSTANDS



CHANGES:

WEST CARGO APRON


JEPPESEN



The aircraft (on idle thrust) shall be pushed back onto TaxilaneEA to face South until its nosewheel is at the "EOP" positionbehind aircraft stand 604. The aircraft shall then be towedforward until its nosewheel is at the "EOT" position behindaircraft stand 602. The aircraft may breakaway from there.


The aircraft (on idle thrust) shall be pushed back onto TaxilaneEC to face West until its nosewheel is at the "EOP" position onTaxilane EC. The aircraft shall then be towed forward followingTaxilane EC centreline onto Taxilane EA until its nosewheel is atthe "EOT" position behind aircraft stand 602. The aircraft maybreakaway from there.


611, 612 The aircraft (on idle thrust) shall be pushed back to face Northuntil its nosewheel is at the "EOP" position. The aircraft shallthen be towed forward following Taxilane EC centreline ontoTaxilane EA until its nosewheel is at the "EOT" position behindaircraft stand 602. The aircraft may breakaway from there.Engine start-up is not permitted during stand pushback.

Alternate pushback procedure

The aircraft (on idle thrust) shall be pushed back to face Northuntil its nosewheel is at the "EOP" position. Engine start -up ispermitted only on the port engine. The aircraft shall then betowed forward following Taxilane EC centreline onto TaxilaneEA until its nosewheel is at the "EOT" position behindaircraft stand 602. The aircraft may breakaway from there.

This alternate pushback procedure can only be exercised if theauxiliary power unit of the aircraft is unserviceable.

Alternate pushbackapproved.


The aircraft (on idle thrust) shall be pushed back onto TaxilaneEA to face South until its nosewheel is at the intersection of theaircraft stand lead-in line and Taxilane EA centreline. The aircraftshall then be towed forward until its nosewheel is at the "EOT"position behind aircraft stand 602. The aircraft may breakawayfrom there.


600, 600L, 600R, 601,602

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

8 SEP 17

Layout.

205 The aircraft (on idle thrust) shall be pushed back onto TWY C7to face North until the nosewheel is at the intersection of theaircraft stand lead-in line and TWY C7 centreline. The aircraftshall then be towed forward until its nosewheel is at theintersection of aircraft stand 206 lead-in line and TWY C7centreline.The aircraft may breakaway from there.


206, 207, 208

ORThe aircraft (on idle thrust) shall be pushed back onto TWY C7to face South until its nosewheel is at the intersection of theaircraft stand lead-in line and TWY C7 centreline. The aircraftmay breakaway from there.


The aircraft (on idle thrust) shall be pushed back onto TWY C7to face North (or South) until its nosewheel is at theintersection of the aircraft stand lead-in line and TWY C7centreline. The aircraft may breakaway from there.


209 The aircraft (on idle thrust) shall be pushed back onto TWY C7to face North until its nosewheel is at the intersection of theaircraft stand lead-in line and TWY C7 centreline. The aircraftmay breakaway from there.


ORThe aircraft (on idle thrust) shall be pushed back onto TWY C7to face South until the nosewheel is at the intersection of theaircraft stand lead-in line and TWY C7 centreline. The aircraftshall then be towed forward until its nosewheel is at theintersection of aircraft stand 208 lead-in line and TWY C7centreline.The aircraft may breakaway from there.



10-9L8WSSS/SIN

APRON/ACFTSTANDS



CHANGES:

EAST CARGO APRON

SOUTH-EAST REMOTE APRON


JEPPESEN

G2

G3, G4

G1 Pushback approved,to face South.

G5, G6, G7, G8,G9, G10, G11,G12, G13

G14, G15

OR

The aircraft (on idle thrust) shall be pushed back following thepushback line onto Taxilane L5 to face south until the nose of theaircraft is behind the stopbar behind aircraft stand G6 on TaxilaneL5. The aircraft may breakaway from there.


The aircraft (on idle thrust) shall be pushed back following thepushback line onto Taxilane L5 to face North until its nose wheel isat the intersection of the aircraft stand pushback line and TaxilaneL5 centerline. The aircraft may breakaway from there.


The aircraft (on idle thrust) shall be pushed back following thepushback line onto Taxilane L5 to face North or South until its nosewheel is at the intersection of the aircraft stand pushback lineand Taxilane L5 centerline. The aircraft may breakaway from there.

Pushback approved,to face North or South.

The aircraft (on idle thrust) shall be pushed back following thepushback line onto Taxilane L5 to face North until its nose wheel isat the intersection of the aircraft stand pushback line and TaxilaneL5 centerline. The aircraft may breakaway from there.


The aircraft (on idle thrust) shall be pushed back following thepushback line onto Taxilane L5 to face South until its nose wheel isat the intersection of the aircraft stand pushback line and TaxilaneL5 centerline. The aircraft shall then be towed forward until itsnose wheel is at the "EOT-G14, G15" position behind aircraftstand G14. The aircraft may breakway from there.

The aircraft (on idle thrust) shall be pushed back following thepushback line onto Taxilane L5 to face North until its nose wheel isat the "EOP-G2" position. The aircraft may breakaway from there.


G16, G17 The aircraft (on idle thrust) shall be pushed back following thepushback line onto Taxilane L5 to face North until the nose ofthe aircraft is behind the stopbar behind aircraft stand G15.The aircraft may breakway from there.


G18,G18L,G18R


G19,G19R

G19L

G20,G20L,G20R

The aircraft (on idle thrust) shall be pushed back following thepushback line onto Taxilane L4 to face West, followed by TaxiwayC6 onto Taxiway SC2 to face East (West) until the nose of theaircraft is behind the stopbar on Taxiway SC2. The aircraft may breakaway from there.

Pushback approved,to face East (West)on Taxiway SC2.

29 DEC 17


The aircraft (on idle thrust) shall be pushed back following thepushback line onto Taxilane L4 to face East until its nosewheel isat the intersection of the aircraft stand pushback line andTaxilane L4 centerline. The aircraft may breakaway from there.


Pushback approved,to face East (West) onTaxiway SC2.





The aircraft (on idle thrust) shall be pushed back following thepushback line onto Taxiway C6 followed by Taxiway SC2 to faceEast (West) until the nose of the aircraft is behind the stopbaron Taxiway SC2.The aircraft may break away from there.






The aircraft (on idle thrust) shall be pushed back following thepushback line onto Taxilane L4 to face East until its nosewheelis at the intersection of the aircraft stand pushback line andTaxilane L4 centerline. The aircraft may breakaway from there.


Stands G18 thru G20R pushback procedures.

The aircraft (on idle thrust) shall be pushed back following thepushback line onto Taxilane L4 to face East, followed by TaxiwayC6 onto Taxiway SC2 to face East (West) until the nose of theaircraft is behind the stopbar on Taxiway SC2. The aircraft maybreak away from there.

The aircraft (on idle thrust) shall be pushed back following thepushback line onto Taxilane L4 to face East, followed by TaxiwayC6 onto Taxiway SC2 to face East (West) until the nose of theaircraft is behind the stopbar on Taxiway SC2. The aircraft maybreak away from there.


10-9L9

CHANGES:

WSSS/SIN

APRON/ACFTSTANDS



T4 APRON


JEPPESEN

New chart. | JEPPESEN, 2017. ALL RIGHTS RESERVED.

29 DEC 17


G21 The aircraft (on idle thrust) shall be pushed back following thepushback line onto Taxilane L4 to face East until its nosewheelis at the "EOP G21" position. The aircraft shall then be towedforward until its nosewheel is at the "EOT G21, G21L, G21R"position on Taxilane L4 centerline. The aircraft may breakawayfrom there.




G21L Pushback approved,to face East.




The aircraft (on idle thrust) shall be pushed back following thepushback line onto Taxilane L4 to face East until its nosewheelis at the intersection of the aircraft stand pushback lineand Taxilane L4 centerline. The aircraft shall then be towedforward until its nosewheel is at the "EOT G21, G21L, G21R"position. The aircraft may breakaway from there.

G21R Pushback approved,to face East.




The aircraft (on idle thrust) shall be pushed back following thepushback line onto Taxilane L4 to face East until its nosewheelis at the "EOP G21R" position. The aircraft shall then be towedforward until its nosewheel is at the "EOT G21, G21L, G21R"position. The aircraft may breakaway from there.


CHANGES:

WSSS/SIN

APRON/ACFTSTANDS



10-9L10


Apt ElevJEPPESEN

AERO

DRO

ME A

DVIS

ORY C

HA

RT

Rwy

02L/

20R

Rwy

02C/2

0C


3 NOV 17

Adv

isor

y 1

Pilo

ts t

axii

ng o

n Tw

y C1

are

tom

aint

ain

a lo

okou

t to

ens

ure

suff

icie

nt w

ing

tip

clea

ranc

e.

Adv

isor

y 2

Pilo

ts t

axii

ng o

n Tw

y EP

are

to

mai

ntai

n a

look

out

to e

nsur

e

suff

icie

nt w

ing

tip

clea

ranc

e.

Adv

isor

y 3

Pilo

ts t

axii

ng o

n Tw

y N

C1

or N

C2

to h

oldi

ng p

oint

EN o

r E1

via

Tw

y EP

are

to

pay

extr

a at

tent

ion

to

grou

nd s

igna

ges

and

ligh

ting

s to

pre

vent

the

mis

take

n id

enti

fica

tion

of

Twy

EP a

s Rw

y 20

C.

Adv

isor

y 4

Pilo

ts t

axii

ng o

n Tw

y W

A a

re t

om

aint

ain

a lo

okou

t to

ens

ure

suff

icie

nt w

ing

tip

clea

ranc

e.

Advisory notes.

N01 21.6 E103 59.4 CHANGI22'SINGAPORE, SINGAPORE

CHANGES:

WSSS/SIN10-9M


C6

C3

C1

C7

E5

EP

B3

B2

E4

B1

203

F60

F59

F58

F58

F56

F54

F52

F50

F40

F41

F42

F37

F36

F35

F34

F33

F32

F31

F30

E1 E2 E3

E4

11

10

9 8

7

5

4

32

1

12

3A

JEPPESEN

7A

T2 C

ENTR

AL

APR

ON

T2 S

OUTH

APR

ON

C2

13A

F52L

F52R F3

5L

F35R

3 NOV 17

SOUT

H EA

ST P

IER

TERM

INA

L 2

CHANGES:

SINGAPORE, SINGAPORECHANGI

10-9M1

PUSHBACK PROCEDURES

WSSS/SIN

| JEPPESEN, 2008, 2016. ALL RIGHTS RESERVED.None.


D40

E28

E27

E26

E24

E22

E20

18 18A

17

19

E10

E11

E12

E8A

7

16

14

15

E7

E6

E5

E4

E3E2E1F3

0

F31

F32 F3

3

11

12

10 9 8

A6

T2 N

ORT

H A

PRO

N

T2 N

ORT

H A

PRO

N

T2 C

ENTR

AL

APR

ON

JEPPESEN

EP

7A

B1

B3

B2

E4

A5

A4

A3 E3

13

13A

2 DEC 16

NO

RTH

EAST

PIE

R

TERM

INA

L 2

CHANGES:


10-9M2

PUSHBACK PROCEDURES

WSSS/SIN

| JEPPESEN, 2008, 2016. ALL RIGHTS RESERVED.Chart re-indexed.


WSSS/SIN 10-9N SINGAPORE, SINGAPORECHANGI

.PARKING.JEPPESEN


SAFEGATE AIRCRAFT DOCKING GUIDANCE SYSTEM - SAFEDOCK1. INTRODUCTION

1.1 The Safegate Aircraft Docking Guidance System - SAFEDOCK is a fully

2. DESCRIPTION OF SYSTEM

lateral and longitudinal position of the aircraft. This 3D technique allows thesystem to identify the incoming aircraft and check it against the oneselected by the operator to ensure that the pilot is provided with the correctstop indication for the aircraft.

aircraft is to be marshalled into the stand manually.2.2 The system is operated only in Automatic Mode. When the system fails, the

2.3 Azimuth guidance, continuous closing rate information, aircraft type, etc., areshown to the pilot on a single display clearly visible for both pilot andco-pilots. Figure A shows the Display and Laser Scanning Unit mounted on the

B7679 M

Aircraft Type

Lead-in line

B747

3. DOCKING PROCEDURES

2.1 The system is based on a laser scanning technique and it tracks both the

CHANGES:

B7679 M

LED DISPLAY AND LASER SCANNING UNIT

Azimuth Guidance

Digital Countdown

A380

terminal or pole in front of the aircraft stand.

Figure A

Safedock Safedock

Safedock Type 1 Safedock Type 2

LED Closing Rate Bar

Type 1 Type 2

Check that the correct aircraft type is displayed. The scrollingarrows indicate that the system isactivated.Follow the lead-in line.

Checking of Aircraft Type

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 guidanceinformation. When the solid yellowclosing rate bar appears, the aircraftis being tracked by the system.

Capture of Correct Aircraft Type

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 centerline.

Steering and Alignment of Aircraft

A380 B747

A380 B747

17 NOV 17

automatic aircraft docking guidance system installed at the contact aircraft

Apron of Singapore Changi Airport. There are two types of ADGS inSingapore Changi Airport, Safedock Type 1 ADGS and Safedock Type 2 ADGS.

stands at Terminals 1, 2, 3 and 4, and at the remote aircraft stands at South

Introduction.


STOPSTOP

WAIT

WAIT

STOPSTOP

STOP ID

FAIL

WSSS/SIN 10-9N1 SINGAPORE, SINGAPORECHANGI

.PARKING.JEPPESEN

OK

WAIT


SAFEDOCK-Continued.

CHANGES:

OK

TOO FAR

TOO FAR

the approaching aircraft or the detected aircraft is lost before 12m to the correctstop position, the system will show "WAIT"

before the correct stop position. Otherwise, the display will show "WAIT", "STOP" and

A380 B74710.0m 10.0m

Distance of Aircraft from STOP Position

STOP Position

Checking of STOP Position

"OK" will be displayed after a few seconds.If the aircraft stops at the correct position,

Object Blocking the View

Overshooting of STOP Position

If the aircraft has gone past the correct stopposition, the display will show "TOO FAR" afterthe aircraft comes to a complete stop.

If some object is blocking the view towards

Identification of Aircraft

The aircraft must be identified at least 12m

"ID FAIL".

WAIT

SafedockType 1

SafedockType 2

When the aircraft is 15m from the stop position, closingrate information is given. "Distance to go" is indicatedby turning off one row of LEDs (Laser ElectronicDisplays) for every half meter that the aircraft advancestowards the stop position. From 15m to the stop position,

position for every 1m. At 3m from the stop position,

position for every 0.2m.the display will indicate the distance from the stop

When the correct stop position is reached, all of theLEDs for the closing rate bar will be off, the word"STOP" will appear in the display. For Safedock Type 1ADGS, the word "STOP" will be displayed in red with redborder. For Safedock Type 2 ADGS, the word "STOP" willbe displayed in yellow and two red, rectangular fieldswill light in the azimuth guidance area of the display.

ID

FAIL

the display will indicate the distance from the stop

17 NOV 17

None.


STOPSTOP

WAIT

WSSS/SIN 10-9N2SINGAPORE, SINGAPORE

CHANGI

.PARKING.JEPPESEN

CHANGES:

SAFEDOCK-Continued.

approach the stop position slowly and observe theclosing rate information displayed. Pilots shouldstop the aircraft immediately when seeing the

sign by the aircraft marshaller or is unsure of


7 APR 17

4. SAFETY MEASURES

the pilot if the aircraft's taxiing speed

taxi into the aircraft stand at minimum speed.The system will display "SLOW" to inform

exercise caution.

ADGS Blank / Wrong Aircraft Type

Pilot should not turn an aircraft into the aircraft standif the docking system is not activated or on seeinga wrong aircraft type displayed on the system.

SafedockType 1

SafedockType 2

B747Proceeding beyond Passenger Loading Bridges

Figure 1

A380

Figure 1

A380 B747

Figure 2 Figure 2

When using the docking system, pilots are to

Minimum Speed

exceeded 1.2 m/s.

SLOW B747SLOW7.0m

Slow Down (In Abnormal Situations) A380 B747SLOWSLOW

Figure 1 Figure 2

In bad weather conditions, the docking system may gointo downgrade mode. The display will show the aircrafttype and "SLOW" and the scrolling arrows are disabled(see figures 1 & 2). When the system has detected theaircraft, the solid yellow closing rate bar appears.Docking process is allowed to continue but pilot should

Overshooting

WAIT"STOP" or "WAIT" display or when given the stop

Figure 2 Figure 2

Figure 1 Figure 1

No Display

To avoid overshooting, pilots are advised to

the information displayed during the docking process.

Pilot should stop the aircraft immediately if the displaygoes black, for power failure (see figure 1) or systemfailure (see figure 2), during the docking process.The aircraft is to be manually marshalled into theaircraft stand.

Safety measures.

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


MALAYSIA

INDONESIA

168^

INDONESIASINGAPORE

356^

356^PU

115. 1

SINGA-PORE

MALAYSIA

BATAMHang Nadim

WIDD

SINGAPOREPaya Lebar

WSAP

SINGAPORE

WSSLSeletarWS(D)-35

WS(D)-4

WS(D)-5

WS(P)-24

WS(P)-3

WS(R)-38

WS(R)-2

WS(P)-49

WS(R)-31

WS(D)-34

DSINJON

113.5 SJS J

SAMKO

ILS DME

023^ 110.9 ICWI C WANUMA

D16.6 ICW

023^

4000

3500023^

SINGAPORE, SINGAPOREILS DME Rwy 02L

Ground

124.3

MISSED APCH:

CHANGI 11-1SINGAPORE Approach (R) SINGAPORE Arrival (R)

128.6 119.3LOC

110.9ICW

FinalApch Crs023^

GS

(3478')

ILSDA(H)

222'3500'

120.3SINGAPORE Tower

118.6

(200')

PA

NS O

PS

D-ATIS

Alt Set: hPa Rwy Elev: 1 hPa Trans level: FL 130 Trans alt: 11000'

(GS out)ICW DMELOC 2.04.0

1290'

WSSS/SIN

348^

168^

01-10

103-50 104-00 104-10

ALTITUDE


3.0

CAUTION: Changi East Rwy02R/20L is solely for use bythe Republic of Singapore

D116.5 VTKTEKONG

V T K

D11.1 ICW

AKIPOD7.8 ICW

ADNIKD4.6 ICW

ABVOND0.7 ICW

D16.0 ICWAPIPA

Gnd speed-Kts

REILPAPI PAPI

GS 3.00^FAF to MAP 3.9

MAP at ABVON/D0.7 ICW1

70 90 100 120 140 160

3:21 2:36 2:20 1:57 1:40 1:28

A

B

C

D

ILS

FULL ALS out

1200m

LOC (GS out)

ALS out

ALSF-II

1 Timing not authorized when GS inop.

CIRCLE-TO-LAND

NA

A

B

C

D

660'970'

ANUMA

Climb to 1000', then climbing LEFT turn to 4000' via

335^

hdg

AKOMA

356^

176^

D20.0 PU

4000

BRIE

FIN

G S

TRIP

TM0

55

1015

20

hdg

335^1000'

LT

4000'

STRAIGHT-IN LANDING RWY02L

or CL outTDZ

APCH FIXMISSED

directed by ATC.heading 335^ and PU R-356 to AKOMA (PU R-356/D20.0) and hold or as

01-20

3500'

3.3 3.2 3.9

TCH 58'

Rwy 22'1500'

ANUMAD11.1 ICW AKIPO

ADNIKABVON

D7.8 ICW

D4.6 ICWD0.7 ICW2500'

0.5

023^

PAPA UNIFORM115.1 PUPUD

4.9

via

3500

D8.0 SJ/R-168

JEPPESEN


372 478 531 637 743 849

1. RADAR required. 2. Simultaneous approaches authorized with Rwy 02R or 02C. 3. ILS DME co-located with glideslope. 4. Maritime vessels of variable heights in water north and south of Rwy.

Rwy 22'

DA(H) 222'(200') MDA(H) 420'(398')

RVR 550mVIS 800m

RVR 720mVIS 800m

RVR 720mVIS 800m

1200m

RVR 1500mVIS 1600m

RVR 1800mVIS 2000m

Apt Elev 22'

29 DEC 17

620'

637'

920'

611'

602'

538'

942'430'

427'

656'

None.

MSA VTK VOR

360^

090^

180^

3400

2100

1900

CHANGES:


MALAYSIA

INDONESIA

168^

INDONESIASINGAPORE

356^

356^PU

115. 1

SINGA-PORE

MALAYSIA

BATAMHang Nadim

WIDD

SINGAPOREPaya Lebar

WSAP

WSSL

SINGAPORESeletar

WS(D)-35

WS(D)-4

WS(D)-5

WS(P)-24

WS(P)-3

WS(R)-38 WS(R)-31

WS(R)-2

WS(P)-49

WS(D)-34

ILS DME Rwy 02L CAT II

CAT II ILS

DSINJON

113.5 SJS J

SAMKO

ILS DME

023^ 110.9 ICWI C WANUMA

D16.6 ICW

023^

4000

3500023^


MISSED APCH:

CHANGI

LOC

110.9ICW

FinalApch Crs023^

GS

(3478')3500'

PA

NS O

PS


WSSS/SIN

348^

168^

01-10

103-50 104-00 104-10



D116.5 VTKTEKONG

V T K

D11.1 ICW

D16.0 ICWAPIPA

Gnd speed-Kts

REILPAPI PAPI

GS 3.00^70 90 100 120 140 160 ALSF-II

ANUMA

Climb to 1000', then climbing LEFT turn to 4000' via

335^

hdg

AKOMA

356^

176^

D20.0 PU

4000

BRIE

FIN

G S

TRIP

TM

hdg

335^1000'

LT

4000'

APCH FIXMISSED

directed by ATC.heading 335^ and PU R-356 to AKOMA (PU R-356/D20.0) and hold or as

01-20

3500'

10.9

TCH 58'

Rwy 22'

ANUMAD11.1 ICW

023^

PAPA UNIFORM115.1 PUPUD

DA(H) 122'(100')

STRAIGHT-IN LANDING RWY

DA(H) 127'(105')

350m

02L

4.9

via

3500

D8.0 SJ/R-168

29 DEC 17

3. Simultaneous approaches authorized with Rwy 2R or 2C. 4. ILS DME co-located withglideslope. 5. Maritime vessels of variable heights in water north and south of Rwy.

05

510

1520

1. Special Aircrew and Acft Certificaton Required. 2. RADAR requried.

JEPPESEN


350m

Ground

124.3SINGAPORE Approach (R) SINGAPORE Arrival (R)

128.6 119.3120.3SINGAPORE Tower

118.6D-ATIS

372 478 531 637 743 849

CAT A B C CAT D

Refer toMinimums Rwy 22'

11-1A

RA values.

620'

637' 920'

611'

602'

538'

942'430'

427'

656'

MSA VTK VOR

360^

090^

180^

3400

2100

1900

Apt Elev 22'

CHANGES:

RA 104'CAT II ILS

RA 109'

RVRRVR


SINGAPORE

INDONESIA

MALAYSIA

168^SJ

113.5

023^

VTK

116.

5WS(D)-34

WS(R)-38

Paya Lebar

Seletar

Hang Nadim

LOC(GS out)

348^

168^

023^1.8

023^

SAMKO

4000

4500 436'

440'

ALT

LOC

(GS out)

611'

DSINJON

113.5 SJS J

TEKONG116.5 VTKV T KD

ICE DME

ILS DME

023^ 108.3 ICEI C E

680'

4.0

1290' 970'

3.0

LEPNA

D15.6 ICED8.0 SJ

MISSED APCH:

SINGAPORE, SINGAPORECHANGI ILS DME Rwy 02C

LOC

108.3ICE

FinalApch Crs023^

GS

4500'(4486')

ILSDA(H)

214'(200')

SINGAPORE Approach (R) SINGAPORE Arrival (R) SINGAPORE Tower Ground

128.6 120.3 119.3 118.6 124.3

1200m

ILS LOC (GS out)

ALS outALS outALS outFULL

1200m2800m

3200m2400m

NOT TOSCALE

1017'

1

1

11-2


01-20

104-00 104-10

WSSS/SIN

PA

NS O

PS

D-ATIS

CAUTION: Changi East Rwy02R/20L is solely for use bythe Republic of Singapore Air Force (RSAF) Aircraft

203^

023^

3000

22 APR 16

LEPNA

Climb to 3000' via heading 023^ and VTK R-023 to NYLON(VTK R-023/D13.0) and hold or as directed by ATC.

023^

hdg

NYLOND13.0 VTK

MISSEDAPCH FIX

co-located with glide slope. 4. Maritime vessels of variable heights in water north and south

LELOND7.8 ICE

LASIND4.6 ICE

LUXOLD2.0 ICE

D0.7 ICELAGUS

D14.2 ICE

LIDVAD16.0 ICE

4500'

6.4 3.2 1.3

TCH 59'2500'

0.5

023^D0.7 ICE

D2.0 ICE

LASIND4.6 ICE

LELOND7.8 ICE

LEPNAD14.2 ICE

2.6

Gnd speed-KtsGS

FAF to MAP 3.9MAP at LAGUS/D0.7 ICE1

70 90 100 120 140 160

3:21 2:36 2:20 1:57 1:40 1:28 PAPIREIL

PAPI

ALSF-I VTK

R-023116.5via and

3000'


CIRCLE-TO-LAND

NA

With LUXOL/D2.0 ICE Without LUXOL/D2.0 ICE

A

B

C

D

A

B

C

D

MDA(H) 420'(406') MDA(H) 660'(646')

LAGUSLUXOL

05

510

BRIE

FIN

G S

TRIP

TM

hdg

023^

STRAIGHT-IN LANDING RWY02C

FMS required for holdingduring SJ VOR outage.

4500

01-10

JEPPESEN

*118.25

of Rwy.


372 478 531 637 743 8493.00^

1. RADAR required. 2. Simultaneous approaches authorized with Rwy 2R or 2L. 3. ILS DME

MSA VTK VOR

3400'

090^

180^

360^

1900'

2100'

DA(H) 214'(200')

RVR

VIS 800m

720mRVRVIS 800m

720m RVR 1500mVIS 1600m 800mVIS

RVR 720m

2000mRVR 1800mVIS

1800m2000mVIS

RVR

RVR 1500mVIS 1600m

Apt Elev

Rwy

Rwy

14'

22'

14'

Rwy elevation, minimums.CHANGES:

523'

1500'


SINGAPORE

MALAYSIA

INDONESIA

SIN

GAPORE

MA

LAYSIA

158^VTK

116.5

023^

VTK

116.

5

158^VTK

116.5

WS(D)-34

WS(R)-38

Seletar

Paya Lebar

203^

PA

NS O

PS

D 116.5 VTKTEKONG

V T K

I C C ILS DME

203^ 109.7 ICC

MISSED APCH:

SINGAPORE, SINGAPORECHANGI ILS DME Rwy 20C11-3

LOC

109.7ICC

FinalApch Crs203^

GS

4500'(4485')

DA(H)

215'(200')


01-20

01-30

WSSS/SIN



ELALU

Climb to 4000' via VTK R-203 to ESLUX (D6.7 VTK). At

1. RADAR required. 2. Simultaneous approaches authorized with Rwy 20L or 20R. 3. ILS DME

ELBEBD7.8 ICC

ELMIN

D0.7 ICCESBIT

NYLOND16.7 ICCD13.0 VTK

1.8

4500203^ 023^

300020

3^

ELALUD14.2 ICC

EGORAD16.0 ICC

05

510

BRIE

FIN

G S

TRIP

TM

(GS out)LOC

ALTITUDEICC DME

660'2.0

980'3.0

1290'4.0

MISSEDAPCH FIX

104-10

EXOMOD22.0 VTK

338^4000

158^

104-00

PAPIREIL

ELALUD14.2 ICCELBEB

D7.8 ICC

6.43.23.9TCH 58' 1500'

2500'

0.5

203^ 4500'ELMIN

D0.7 ICCESBIT

Gnd speed-KtsGS 3.00^

FAF to MAP 3.9MAP at ESBIT/D0.7 ICC1

70 90 100 120 140 160

3:21 2:36 2:20 1:57 1:40 1:28

A

BC

D

ILS

FULL ALS out

1200m

LOC (GS out)

ALS out


CIRCLE-TO-LAND

NAA

BC

D

4000'

R-203

VTK

116.5via ESLUX

ALSF-II


DA(H) 215'(200') MDA(H) 420'(405')

1200m

NOT TOSCALE

130^hdg

Rwy 15'

ESLUXD6.7 VTK

TDZ or CL out

RVR 550m

4500

D4.6 ICC

D4.6 ICC

JEPPESEN

Ground


119.3120.3SINGAPORE Tower

118.6D-ATIS

*118.25128.6

of Rwy.


372 478 531 637 743 849

RVR 720m

RVR 1800mVIS 2000m

VIS 800m VIS 800mVIS 800mRVR 720m

VIS 1600mRVR 1500m

920'

611'

602'

627'

430'

427'

755'

573'

15'

22'Apt Elev

Rwy

(VTK R-158/D22.0) and hold or as directed by ATC.ESLUX turn LEFT heading 130^ to intercept VTK R-158 to EXOMO

FULL ALS out

1400m

DA(H) 315'(300')TDZ or CL out

Missed approach climb gradientmim 2.8% to 2000'

(CONDITIONAL)

090^

180^

360^

1900'

2100'

3400'

MSA VTK VOR

900m

18 NOV 16

Missed approach climb gradientmim 2.5%

Missed approach climb gradient note.CHANGES:


SINGAPORE

MALAYSIA

INDONESIA

SING

APORE

MA

LAYSIA

158^VTK

116.5

023^

VTK

116.

5

158^VTK116.5

WS(D)-34

WS(R)-38

Seletar

Paya Lebar

CAT II ILSRA 102'

ILS DME Rwy 20C CAT II

4500'

14.0

203^

203^

PA

NS O

PS

D 116.5 VTKTEKONG

V T K

I C C ILS DME

203^ 109.7 ICC

MISSED APCH:


LOC

109.7ICC

FinalApch Crs203^

GS

4500'(4485')


01-20

01-30

WSSS/SIN



ELALU

Climb to 4000' via VTK R-203 to ESLUX (D6.7 VTK). At

1. RADAR required. 2. Simultaneous approaches authorized with Rwy 20L or 20R. 3. ILS DME

NYLOND16.7 ICCD13.0 VTK

1.8

4500203^ 023^

300020

3^

ELALUD14.2 ICC

EGORAD16.0 ICC

05

510

BRIE

FIN

G S

TRIP

TM

MISSEDAPCH FIX

104-10

EXOMOD22.0 VTK

338^

4000158^

104-00

PAPIREIL

ELALUD14.2 ICC

TCH 58'


70 90 100 120 140 160 4000'

R-203

VTK

116.5via ESLUX

ALSF-II

NOT TOSCALE

130^hdg

Rwy 15'

ESLUXD6.7 VTK

11-3A


115'DA(H) (100')

350m

4500

JEPPESEN


Ground


128.6 119.3120.3SINGAPORE Tower

118.6D-ATIS

*118.25

of Rwy.

372 478 531 637 743 849

920'

611'

602'

627'

430'

427'

755'

573'

090^

180^

360^

1900'

2100'

3400'

MSA VTK VOR

115'(100')DA(H) 15'

22'Apt Elev

Rwy

(VTK R-158/D22.0) and hold or as directed by ATC.ESLUX turn LEFT heading 130^ to intercept VTK R-158 to EXOMO

18 NOV 16

None.CHANGES:

CAT II ILS

RA 102'

RVR


VTK

023^

116.

5

JS168^SJ113.5

146^

113.5SJJS

MALA

YSIA

SINGAPORE

MALAYSIA

SINGAPORE WS(D)-34

WS(R)-38

Seletar

Paya Lebar Aero

203^

TEKONG

116.5 VTKDV T K

ILS DME

203^ 108.9 ICHI C H

(GS out) ALTITUDE 650' 970' 1290'

PA

NS O

PS

4.03.02.0ICH DMELOC

2100'

090^

180^

360^

3400'

1900'MISSED APCH:

SINGAPORE, SINGAPORECHANGI ILS DME Rwy 20R11-4

LOC

108.9 ICH

FinalApch Crs203^

GS

3500'(3487')

DA(H)

213'(200')

MSA VTK VOR


128.6 120.3 119.3 118.6 124.3

FMS required for holdingduring SJ VOR outage.

1

Rwy Elev: 1 hPa Trans level: FL 130 Trans alt: 11000'

01-20

01-30

104-00

104-10

WSSS/SIN

D-ATIS


Alt Set: hPa


IGULA

Climb straight ahead to 5000'. On crossing SJ R-146,proceed direct SAMKO holding area and hold or as directed by ATC.

IDUNAD0.8 ICH

IDUROD4.6 ICH

IDVASD7.8 ICH

IGULAD11.1 ICH

05

510

BRIE

FIN

G S

TRIP

TM

NYLOND16.2 ICHD13.0 VTK

203^

023^

3000

D16.0 ICHIPNAK

203^

3500

NOT TO SCALE

348^

SAMKOD8.0 SJ

15000

168^

MISSEDAPCH FIX

1200m

ILS LOC (GS out)

ALS outALS outFULL

1200m


FAF to MAP 3.9MAP at IDUNA/D0.8 ICH1

70 90 100 120 140 160372 478 531 637 743 8493:21 2:36 2:20 1:57 1:40 1:28


CIRCLE-TO-LAND

NAABCD

ABCD

5000'PAPIREIL

PAPI

R-146

SJ

113.5 SAMKODon

crossing

DA(H) 213'(200')

3500'

3.33.2

2500'

0.6

203^

3.8

TCH 57'

IDUNAD0.8 ICH

IDUROD4.6 ICH

IGULAD11.1 ICHIDVAS

D7.8 ICH

STRAIGHT-IN LANDING RWY20R

4.9

3500

JEPPESEN


HIALS

MDA(H) 420'(407')

*118.25

of rwy.

1. RADAR required. 2. Simultaneous approaches authorized with Rwy 20L or 20C. 3. ILS DME

RVR

VIS 800m

720mRVRVIS 800m

720m RVR 1500mVIS 1600m

2000mRVR 1800mVIS

Apt Elev 22'

Rwy 13'

13'Rwy

430'

3600m

ALS outFULLDA(H) 693'(680')

Missed approach climb gradientmim 3.7% to 2500'

(CONDITIONAL)

611'

602'

427'

573'

3200m3200m

18 NOV 16

Missed approach climb gradientmim 2.5%

Missed approach climb gradient note.CHANGES:

1500'


SINGAPORE

INDONESIA

MALAYSIA

INDONESIA

SINGAPO

RE

WS(D)-35

WS(D)-4

WS(D)-5

WS(P)-24

WS(P)-3

WS(P)-36

WS(P)-49

WS(R)-2

WS(R)-31

WS(R)-38

Hang Nadim

Seletar

Paya Lebar


Ground

124.3

MISSED APCH:


128.6 119.3

RNAVFinal

Apch Crs023^ (1378')

DA(H)450'1400'


118.6

(428')

PA

NS O

PS

D-ATIS


WSSS/SIN

01-10

104-00 104-10



Gnd speed-Kts

REILPAPI PAPI

70 90 100 120 140 160

A

B

C

D

ALS out

2200m

ALS out

ALSF-II

CIRCLE-TO-LAND

NA

A

B

C

D

EMTAP

AKOMA

356^

176^

4000

01-20

6.1 4.322'

ERVOTEMTAP

RWY~2L

1300'

023^

STRAIGHT-IN LANDING RWY02L

22'

22'Apt Elev

RNAV (GNSS) Rwy 02L

LNAV/VNAV

LNAV/VNAV LNAVDA(H) 450'(428') MDA(H) 540'(518')

4.3 3:41 2:52 2:35 2:09 1:51 1:37

Descent angle 372 478 531 637 743 849

04.310.4

2. Maritime vessels of variable heights in water north and south of runway.

1 1

Procedure Alt

EMTAP to MAP

RVRRVR1400m

01-00

BRIE

FIN

G S

TRIP

TM0

55

1015

20

APCH FIXMISSED

540'


JEPPESEN

*118.25

21 APR 17

ERVOT(IF)

EMTAP

023^

RWY~2L

ENSUN

5.5

20.2

SAMKO(IAF)

016^6.1

2800

SANAT(IAF)305^

6.02800

342^

14000

4000

4000

1. Minimum temperature for which Baro-VNAV operations are authorized: 5^C (41^F).

3.00^TCH 50'

3.00^

Climb direct to ENSUN. Turn LEFT to AKOMA to join theholding at 4000' or above or as directed by ATC.

D ENSUN

1200m1200m

RVR

VIS1600mRVR

2400mRVR

2800mRVR2000mRVR

1600mRVR

103-50

1400'

2800'

4000'

348^

168^

620'

637' 920'

611'

602'

538'

942'

427'

430'

427'

755' 624'

MAP at RWY~2L

[RW~2L]

[RW~2L]

All arrivals into WSSS will be issued instructions by ATCto maintain 180KT till 8NM from touchdownand thereafter 150KT till 4NM from touchdown.

MSA ARP

Rwy

Rwy

3500

None.

Max 220 KT.

NOT TO SCALE

WS(D)-34

CHANGES:


SINGAPORE

INDONESIA

MALAYSIA

INDONESIA

SINGAPO

RE

WS(D)-34

WS(D)-35WS(D)-5

WS(P)-24

WS(P)-3

WS(P)-36

WS(R)-31

WS(R)-38

WS(D)-4

WS(R)-2

Hang Nadim

Seletar

Paya Lebar


Ground

124.3

MISSED APCH:


128.6 119.3

RNAVFinal

Apch Crs023^ (1586')

DA(H)360'1600'

120.3

SINGAPORE Tower

118.6

(346')

PA

NS O

PS

D-ATIS


WSSS/SIN

REILPAPI PAPI

A

B

C

D

ALS out ALS out

CIRCLE-TO-LAND

NA

A

B

C

D

KASPO


14'

22'Apt Elev

RNAV (GNSS) Rwy 02C

LNAV/VNAV

LNAV/VNAV LNAV

DA(H) 360'(346') MDA(H) 490'(476')

Descent angle 372 478 531 637 743 849


Procedure Alt

KASPO to MAP

RVRRVR 2000m

RVR 2400m

1200m

5.0 4:17 3:20 3:00 2:30 2:09 1:52

BRIE

FIN

G S

TRIP

TM0

55

1015

20

Gnd speed-Kts 70 90 100 120 140 160

JEPPESEN

*118.25

HIALS

21 APR 17

above or as directed by ATC.Climb direct to NYLON to join the holding at 3000' or

3.00^

MDA(H) 890'(876')

RVR 1600m

without KAKSA

RVR 1800mRVR 1200m

1200mVIS

RVRVIS

1500m1600m RVR 4400m

4000mRVR

RVR 1600m

RVR 2000m

RVRVIS

1200m1200m

RVR 3200m

3600mRVR

ALS out

3000'D NYLON

0

14'

TCH 50'

4.4 2.9

KIMERKASPO

RWY~2C

1000'

023^

5.09.4

490'

3.00^

KAKSA

890'

2.92.1

990'

KIMER(IF)

KASPO

023^

KAKSA

RWY~2C

18.6

SAMKO(IAF)

024^6.

1

2000

168^ 348^

4000


01-10

01-20

01-30

103-50 104-00 104-10

114000

1600'

2000'


620'

637' 920'

611'

602'

538'

942'

627'

427'

430'

427'

755'

624'

MAP at RWY~2C

[RW~2C]

[RW~2C]


MSA ARP

Rwy

Rwy

3500


Note.

Max 220 KT.

203^

023^

MISSED APCH FIX

NYLON

3000

NOT TO SCALE

CHANGES:


WS(R)-31SINGAPORE

INDONESIA

MALAYSIA

WS(D)-34

WS(D)-35

WS(P)-24

WS(P)-36

WS(R)-31WS(R)-38

Paya Lebar

Seletar


Ground

124.3

MISSED APCH:


128.6 119.3

RNAVFinal

Apch Crs203^ (1985')

DA(H)490'2000'


118.6

(475')

PA

NS O

PS

D-ATIS


WSSS/SIN

Gnd speed-Kts

REILPAPI PAPI

70 90 100 120 140 160

A

B

C

D

ALS out

2400m

ALS out

ALSF-II

CIRCLE-TO-LAND

NA

A

B

C

D

VILEV

4.16.215'

VABRIVILEV

RWY2~C203^


15'

22'Apt Elev

RNAV (GNSS) Rwy 20C

LNAV/VNAV

LNAV/VNAV LNAVDA(H) 490'(475') MDA(H) 540'(525')

6.2 5:19 4:08 3:43 3:06 2:39 2:20

Descent angle 372 478 531 637 743 849

0 6.2 10.3


Procedure Alt

VILEV to MAP

RVR 1600m

2800m

2400m

RVRVIS

RVR 1600m

RVR 2000m

1600m

BRIE

FIN

G S

TRIP

TM0

55

1015

20

540'

JEPPESEN

*118.25

21 APR 17

Climb direct to ESLUX. Turn LEFT to magnetic course 142^to join the holding at 3600' or above or as directed by ATC.

RVR RVR

1200m1200m

RVR

RVR

3600'3.00^

TCH 50'

3.00^ 2000'

25

VABRI(IF)

VILEV

203^

RWY2~C

ESLUX

3.2

NYLON(IAF)

203^6.2

2000


01-20

01-30

01-40

103-50 104-00 104-10

104-20

142^

1

1

3000

D ESLUX

203^

023^

2000'

600'

920'

611'

602'

535'

627'430'

427'

755'

MAP at RWY2~C

[RW2~C]

[RW2~C]



MSA ARP

Rwy

Rwy

3500


Note.

Max 220 KT.

EXOMO

158^

338^

NOT TO SCALE

MISSEDAPCH FIX

3600

3000

CHANGES:

142^142^


SINGAPORE

INDONESIA

MALAYSIA

WS(D)-34WS(D)-35

WS(D)-5

WS(P)-24

WS(P)-3

WS(P)-36

WS(R)-31

WS(R)-38

Paya Lebar

Seletar


Ground

124.3

MISSED APCH:


128.6 119.3

RNAVFinal

Apch Crs203^ (1987')

DA(H)690'2000'


118.6

(677')

PA

NS O

PS

D-ATIS


WSSS/SIN

Gnd speed-Kts

REILPAPI PAPI

70 90 100 120 140 160

A

B

C

D

ALS out

3600m

ALS out

ALSF-II

CIRCLE-TO-LAND

NA

A

B

C

D

ELGAP

3.86.213'

ELBEXELGAP

RWY2~R 203^

STRAIGHT-IN LANDING RWY20R

13'

22'Apt Elev

RNAV (GNSS) Rwy 20R

LNAV/VNAV

LNAV/VNAV LNAVDA(H) 690'(677') MDA(H) 690'(677)

6.2 5:19 4:08 3:43 3:06 2:39 2:20

Descent angle 372 478 531 637 743 849

0 6.2 10.0


Procedure Alt

ELGAP to MAP

RVR 1600m

3600m

3200mRVR

VIS

RVR 2400m

RVR 2800m

2800m

BRIE

FIN

G S

TRIP

TM0

55

1015

20

690'


JEPPESEN

*118.25

21 APR 17

Climb direct to ENLES. Turn LEFT to SAMKO to join theholding at 3200' or above or as directed by ATC.

25

RVR

RVR 1200m1200m

RVRRVR

RVR

D ENLES3200'3.00^

TCH 50'

3.00^2000'

690'

ELBEX(IF)

ELGAP203^

RWY2~R

14.1

BIDUS(IAF)

127^

6.72000

BIPOP(IAF)

273^7.1

2000

NYLON(IAF)

211^6.

020

00

01-20

01-30

01-40

103-50 104-00 104-10

104-20

1

1

3400

203^

11

3000

3000


203^

023^

2000'

620'

637'

920'

611'

602'

538'

942'

627'430'

427'

755'

MAP at RWY2~R

[RW2~R]

[RW2~R]


MSA ARP

Rwy

Rwy

3500


Max 220 KT.

Note.

ENLES

SAMKO4.

1

168^ 348^

3200

MISSEDAPCH FIX

NOT TO SCALE

3000

203^

192^

14.1

CHANGES:


MALAYSIA

SINGAPORE

INDONESIA

SING

APO

RE

MA

LAYSIA

158^VTK116.5

116.5VTK

158^

WS(D)-34

WS(R)-38

Seletar

Paya Lebar

V T K

203^

(IF)

627'

440'

611'

602'

920'

3000

023^

203^

2000203^

NYLOND13.0 VTK

680'

VTKD9.1

VTKD2.6

203^

D3.0 VTK

MISSED APCH:

SINGAPORE, SINGAPORECHANGI VOR DME Rwy 20C13-1


128.6 120.3 119.3 118.6 124.3VOR

116.5 VTK

FinalApch Crs203^

Minimum Alt

2000'(1985')

MDA(H)

580'(565')D2.6 VTK

090^

180^

360^

1900'

2100'

3400'

MSA VTK VOR

PA

NS O

PS

20C

A

B

C

D

STRAIGHT-IN LANDING RWYMDA(H) 580'(565')

ALS out

1500mRVRVIS 1600m

2400m

2800m

RVR 720m800mVIS

RVR1500m1600mVIS

RVRVIS 2000m

1800m

PAPIREIL

VTK DME D1.0 AFTER VTK860' 1820'

D2.0 BEFORE VTK

573'

D116.5 VTKTEKONG

ALTITUDE

01-20

01-30

104-00

WSSS/SIN

D-ATIS

500'


05

510

ALSF-II

BRIE

FIN

G S

TRIP

TM

MISSEDAPCH FIX

EXOMOD22.0 VTK

338^4000

158^

104-10

ESLUX130^hdg

1180'VTK D1.0 BEFORE VTK

1500'

4000'

R-203

VTK

116.5via ESLUX

Climb to 4000' via VTK R-203 to ESLUX (D6.7 VTK).

directed by ATC.

At ESLUX (1000' or above) turn LEFT heading 130^ to intercept

3.9

NOT TOSCALE

3.0 2.6

2000'

6.5

203^ 2000'203^

0.5

1180'

VTKD3.0 VTKD2.6 VTKD9.1

VTK R-023

VTK R-158 to EXOMO (VTK R-158/D22.0) and hold or as

D6.7 VTK

JEPPESEN

*118.25

1. Maritime vessels of variable heights in water north and south of Rwy.


22'

15'Rwy

Apt Elev

Rwy 15'

1 JUL 16

[FD20C]

[MD20C]

[CD20C]

[MD20C][FD20C] [CD20C]

TCH 58'

Gnd speed-KtsDescent Angle 3.00^

70 90 100 120 140 160372 478 531 637 743 849

MAP at D3.0 VTK or

FAF to MAP 5.6 4:48 3:44 3:22 2:48 2:24 2:06

3.00^

CAUTION: Changi East Rwy 02R/20Lis solely for use by the Republic ofSingapore Air Force (RSAF) Aircraft.Closed due to development works.

Reindexing, VNAV data, VNAV angle.CHANGES:

VOR


TERMINAL CHART CHANGE NOTICES

Chart Change Notices for Airport WSSS

Type: TerminalEffectivity: PermanentBegin Date: ImmediatelyEnd Date: No end date

CAUTION. Rwy 02R-20L closed due to development works.

Type: TerminalEffectivity: TemporaryBegin Date: ImmediatelyEnd Date: 20200430

Runway 02C approach lighting reduced from 900m to 810m


Speed Control Procedures for Arrivals. All arrivals into Singapore Changi Airport will be issued instructions by ATC to maintain 180 KT till 8 NM from touchdown and thereafter 150 KT till 4 NM from touchdown.

Type: TerminalEffectivity: PermanentBegin Date: 20171117End Date: No end date

(10-9) Terminal 4 construction completed. South Apron under construction.

TERMINAL CHART CHANGE NOTICES

Chart Change Notices for Airport WSSS


CAUTION. Rwy 02R-20L closed due to development works.

Type: TerminalEffectivity: TemporaryBegin Date: ImmediatelyEnd Date: 20200430

Runway 02C approach lighting reduced from 900m to 810m


Speed Control Procedures for Arrivals. All arrivals into Singapore Changi Airport will be issued instructions by ATC to maintain 180 KT till 8 NM from touchdown and thereafter 150 KT till 4 NM from touchdown.

Type: TerminalEffectivity: PermanentBegin Date: 20171117End Date: No end date

(10-9) Terminal 4 construction completed. South Apron under construction.

Terminal Chart Change NoticesPage 1 - Printed on 27 Jan 2018Notice: After 25 Jan 2018, 0000Z, this data may no longer be valid(c) JEPPESEN SANDERSON, INC., 2018, ALL RIGHTS RESERVED

jep=JEPPESEN


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