Changi

General Information

Location: Singapore SgpIATA Code: SINLat/Long: N01° 21.55' E103° 59.36'Elevation: 22 ft

Airport Use: PublicMagnetic Variation: 0.2°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: 2302 ZSunset: 1110 Z,

Runway Information

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

Runway: 02LLength x Width: 13123 ft x 197 ftSurface Type: bituTDZ-Elev: 22 ftLighting: Edge, ALS, Centerline, REIL, TDZStopway: 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 ft

Lighting: Edge, ALS, Centerline, REILDisplaced Threshold: 2428 ftStopway: 197 ft

Communication Information

ATIS 128.6 Singapore Tower 118.25 Singapore Tower 118.6 Singapore Ground Control 124.3 Singapore Ground Control 121.725 Singapore Ground Control 121.85 Changi Ramp/Taxi Control 121.9 Singapore Clearance Delivery 121.65 Singapore Pre-Taxi Clearance 121.65 Singapore Approach Control 124.6 Secondary Singapore Approach Control 120.3 Singapore Arrival Control 119.3 Singapore Radar 124.05 Arrival Service

General Information





Runway Information





Airport Information For WSSSPrinted on 10 Apr 2014Page 1(c) JEPPESEN SANDERSON, INC., 2014, ALL RIGHTS RESERVED

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General Information





Runway Information











Airport Information For WSSSPrinted on 10 Apr 2014Page 2(c) JEPPESEN SANDERSON, INC., 2014, ALL RIGHTS RESERVED

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JEPPESENWSSS/SIN10-1PCHANGI 16 MAR 12

SINGAPORE, 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

except during thunderstorms.

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

Changi Airport are required to submit the following documents to the Airworthiness/Flight Operations Division of the Civil Aviation Authority of Singapore at least one month before the commencement of the operations:

the State of Registry/Operator of the operators:a) Authorization for Category II ILS operations by the relevant authority of

b) Operators' minima for Category II ILS operations; andc) Operators' method of verifying its pilots' Category II qualification and

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 inthe Instrument Approach Charts WSSS AD 2-101 to WSSS AD 2-119 andthe Precision Approach Terrain Charts for RWY 02L and RWY 20C at WSSSAD 2-43 and WSSS AD 2-45 respectively.

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,

currency.

2. RUNWAY UTILIZATION

2.2.1 To maximize runway utilization and minimize runway occupancy time,departing aircraft when in receipt of line up clearance must inform ATC ifgreater wake vortex separation will be required behind the proceedingaircraft than that laid down in PANS ATM Doc 4444, else are required tocommence take-off roll as soon as take-off clearance is issued by ATC.Failure to do so may result in additional delay.

Departures text revised. | JEPPESEN, 2011, 2012. ALL RIGHTS RESERVED.

2.2 DEPARTURES - WAKE VORTEX SEPARATION

CHANGES:

.AIRPORT.BRIEFING.

JEPPESENWSSS/SIN10-1P1CHANGI 16 MAR 12


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.

multiple Rapid Exit Taxiways (RETs). Pilots should vacate via the first2.4.2 To ensure minimum Runway Occupancy Time (ROT), each runway has

by ATC.available RET corresponding to operational requirements, or as instructed

2.4.3 Aircraft vacating the runway-in-use should not stop on the exit taxiwayuntil the entire aircraft has passed the runway holding point.

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 that

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

at the time the aircraft crosses the threshold of the runway-in-use

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)

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

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

| JEPPESEN, 2011, 2012. ALL RIGHTS RESERVED.Arrivals text revised.

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

CHANGES:

.AIRPORT.BRIEFING.

WSSS/SIN10-1P2

JEPPESEN

CHANGI 14 MAR 14SINGAPORE, 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

thereafter the appropriate transition and STAR for Rwy 02L/02C to SAMKO Holding Area (SHA) except for the following STARS: LAVAX 1A and PASPU 1A shall proceed to SHA after SANAT.

a) Maintain the last assigned altitude or flight level and proceed via airways

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.

d) Rwy 20C

Carry 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.

ARRIVALS

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.

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

None. | JEPPESEN, 2013, 2014. ALL RIGHTS RESERVED.CHANGES:

.AIRPORT.BRIEFING.

WSSS/SIN10-1P3

JEPPESEN

CHANGI 14 MAR 14SINGAPORE, 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.

paragraph 4 on 10-1P2.

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'.

6. RNAV (GNSS) SID/STAR OPERATIONS

6.1 For RNAV (GNSS) SIDs and STARs operations, the aircraft shall be GNSS-equipped and the navigation systems shall meet ICAO RNP-1 standard of

Precision Area Navigation (P-RNAV).accuracy, or equivalent, such as JAA TGL 10 or FAA AC 90-96A Apendix 2 -

Paragraph 6. | JEPPESEN, 2013, 2014. ALL RIGHTS RESERVED.CHANGES:

.AIRPORT.BRIEFING.

1. Introduction

CHANGES:

WSSS/SINCHANGI

SINGAPORE, SINGAPORE.RNAV.STAR.

CONTINUOUS DESCENT OPERATION (CDO) FOR ARRIVALS

2. Conditions for conducting a CDO

3. Requirements for individual flights

4. Preparations for CDO

5. CDO Execution

C-D-O" "Request

| JEPPESEN, 2011, 2013. ALL RIGHTS RESERVED.

FIR entry point RWY STAR Transition

02L

20R

PASPU 1K

PASPU 1LVEPLI

MELAS02L

20R

PASPU 1K

PASPU 1LMABAL

20R

02L LAVAX 1K

LAVAX 1LTOMAN

02L

20R LAVAX 1L

LAVAX 1KOBDOS

SURGA02L LAVAX 1K

20R LAVAX 1LSURGA

PARDI02L REMES 1K

REMES 1L20R

TAROSBOBAG 1K02L

20R BOBAG 1L

ESPOB, IPRIX,

IGARI

TEGID, KAMIN,

AGOBA

KADAR, BAVUS

1.2 The vertical profile of CDO takes the form of a continuously descending path withminimum level flight segments to enable smooth aircraft deceleration and configuration

2.1 Pilots shall adhere to the instructions as depicted on the CDO RNAV STARs and the conditions for ILS procedures into Changi. In addition, the following conditions must be met:a) Changi Runway 02L/20R is open for landing;b) ILS for the intended runway of landing into Changi is in operation;c) Visibility is greater than or equal to 800m;

e) No other system degradation that may affect a GNSS or ILS operation.

3.1 Flights that fulfill the following requirements can be allowed to conduct a CDO subject to ATC and real-time traffic condition:a) Flight enters Singapore FIR via one of the following waypoints and ATS routes:

b) RNAV-equipped aircraft with FMC capable of:-LNAV and VNAV;

depicted on the charts;-continuing on planned vertical path from RNAV STAR onto ILS of intended runway of landing.

4.1 To ensure that the CDO procedures can be effectively carried out, pilots are

and landing runway-in-use. The landing runway-in-use is available from D-ATIS.

5.1 On first contact with Singapore RADAR, use the following when requesting for a CDO:

-Depending on the situation, Singapore ATC will make an early assessment to approve/disapprove your request accordingly. When it is obvious to ATC that the conduct of CDO flight will not reap any operational benefit, ATC shall disapprove your request and inform you accordingly.

prior to an ILS approach. New CDO RNAV STARs have been constructed in accordance

is facilitated by appropriate instrument flight procedure design and ATC procedures.

1.1 CDO is an aircraft operating technique which enables the pilot to execute anoptimized arrival descent profile utilizing the onboard capability of the aircraft. CDO

Aircraft Operations, to facilitate CDO into Singapore Changi Airport.

IGARI (N-891)

IPRIX (M-753)

ESPOB (L-642)

MELAS (N-892) TEGID (M-767)

KAMIN (B-348)

KADAR (M-774) SURGA (M-635)

PARDI (G-579)

advised to abide by the following:a) Check if conditions for conducting the CDO are met;b) Check if flight meets requirement for executing a CDO; and c) Plan the lateral route in your FMC as shown below based on FIR entry point

-flying Changi RNAV STARs and to abide by all speed and altitude restrictions

10-2JEPPESEN

15 FEB 13

Text.

BAVUS (L-504)

ATETI (G-580) VPK (B-469)

TAROS (R-469)

02L

20R PASPU 1L

PASPU 1KBIKTAVPK

with ICAO Doc 9931 CDO Manual and ICAO Doc 8168 Procedures for Air Navigation,

d) RVR is greater than or equal to 550m for runway-in-use; and

CHANGES:

WSSS/SINCHANGI


6. CDO Flight procedures

CONTINUOUS DESCENT OPERATION (CDO) FOR ARRIVALSCONTINUOUS DESCENT OPERATION (CDO) FOR ARRIVALS

"[flight callsign], EXPECT C-D-O and cleared to Singapore via [STAR] Arrival, MAINTAIN [cruising altitude],

report ready for descent"[transition, if any] transition, Runway [runway-in-use].

"Request descent"

"Singapore [ATC sector transferred to], [flight callsign], on C-D-Oto [last cleared altitude by ATC], Runway [runway-in-use]"


5.2 If CDO is approved, Singapore ATC shall reply using the following phraseology:

On receipt of this clearance from Singapore ATC, pilot shall plan the arrival route using the FMC and to report estimated time/distance for Top Of Descent (TOD) once the information is available. CDO RNAV STARs have been designed for arrivals into Runway 02L or Runway 20R and linking up to the ILS of these respective runways. As such, please refrain from requesting for a change in landing runway (i.e. 02C or 20C).

5.3 Prior to reaching TOD, pilot shall make another call to request CDO execution:

Once cleared for descent:

path;

5.4 When transferred to another ATC sector/frequency, always inform the next sector that flight is on CDO upon initial contact:

5.5 Once in contact with Singapore Arrival, ATC shall issue onward clearance to facilitatefinal phase of the CDO flight. Clearance would be in the following form:

-With this clearance, pilot may proceed on remaining route of CDO flight procedure to intercept on the appropriate ILS.

NOTE:

you to an intermediate level which would still facilitate a CDO profile. In doing so,

reaching 3000' from last assigned altitude so as to prevent leveling off.-If CDO flight has commenced and in the course of the CDO execution, Changi changes direction of its runway-in-use, i.e. Rwy 02 to Rwy 20 or vice versa, ATC shall adviseif the CDO flight can resume and issue the necessary re-clearance. Pilot shall thenre-plan arrival route to the revised landing runway and advise ATC if the flight wouldstill be able to meet all the required speed/altitude restrictions.

5.6 Deviation from lateral or vertical path - At times, it may be necessary for ATC to take you off track temporarily or stop descent at an intermediate level due to a change in traffic situation. When instructed, pilot shall comply with ATC instructions until such a time when informed that the CDO flight can resume.

5.7 Termination of a CDO - In the event that traffic complexity reaches a stage where cancellation of the CDO flight becomes necessary, ATC shall issue a clearance to terminate the CDO flight. In doing so, ATC shall use the following phrase to terminate the CDO flight:

6.1 The CDO flight shall track along the CDO RNAV STARs up to the intermediate segment and ILS procedure for the final and missed approaches for the respective runways. The CDO RNAV STARs have been designed as closed approaches into Changi, special provisions have been made herein to facilitate CDO flight joining the ILS Approach from the RNAV STAR.

6.2 In the event that airborne RNAV equipment fails, pilot shall inform ATC as soon as practicable. ATC shall then terminate CDO operation and resume with RADAR vectors to aid pilot in landing into Changi.

6.3 For each set of RNAV STAR, information on distance to threshold has been added to

a) Start descent at the calculated FMC TOD based on the planned lateral and vertical

b) Use lateral and vertical navigation functions of the FMC throughout CDO execution.

"[flight callsign], descend to [altitude], cleared ILS approach

Runway [runway-in-use]"

ATC shall endeavor to issue further descent clearance prior to the CDO flight

"[callsign], [reason for CDO termination], C-D-O is now terminated.[other ATC instructions that may follow]..."

JEPPESEN

10-2A15 FEB 13

-During CDO, standard ATC procedures continue to apply. ATC may at times clear

5.8 Radio Communication Failure - In the event of a radio communication failure, CDOflight is to be terminated immediately and pilot is to apply the radio communication

Radio communication failure text.

between pilot and ATC.aid pilot in CDO planning and execution and to reduce radio voice transmissions

failure procedures.

244^

252^

235^243^

220^

D57.3

D43.6

D38

.6 D24.0

D11.

6

COMMSLOST COMMSLOST COMMSLOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS LOSTCOMMS LOSTLOST

CHANGES:

WSSS/SINCHANGI


TEKONG

116.5

VTK

VTK

N01

24.9 E10

4 01

.3

D

2

and p

roceed o

n B

OBAG 1

A t

o S

AMKO.

.RNAV.STAR.

Alt Set: hPa Trans level: FL130 Trans alt: 11000'

2. W

hen c

leare

d v

ia B

OBAG 1

A b

y S

ingapore

ATC:

N01

33.1

E103

05.4

REKO

P(S

J R-

293/

D50

.0)

(VTK

R-2

78/D

56.6

)

147^

141^

083^

083^

ASUNA

N00

59.8

E103

09.9

BO

BA

GN01

02.5

E103

29.9

BO

KIP

(VTK

R-2

21/D

27.0

)N01

04.4

E103

43.9

SA

MKO

N01

05.5

E103

52.9

263^

6000'

- FL1

80

MA

X 2

20 K

T

ARAMA

REKOP

41

39

20

14

9

SINJO

N

113.5

SJSJ

N01

13.4

E103

51.3

D

1. Set

transponder

to M

ode A

/C c

ode 7

600.

appro

priate

landin

g p

rocedure

for

Rwy 0

2 a

s

clo

se a

s p

ossib

le t

o E

AT o

r ETA.

Specia

l Pro

cedure

s f

or

mis

sed a

ppro

ach p

rocedure

.

b. Fro

m S

AMKO c

ommence d

escent

and c

arr

y o

ut

c. If

unable

to e

ffect

a landin

g, re

fer

to S

ingapore

3. No c

leara

nce o

r in

str

uction r

eceiv

ed f

rom

Sin

gapore

ATC:

ARA

MA

(SJ

R-29

8/D

50.0

)(V

TK R

-282

/D55

.5)

Dir

ect

dist

ance

fro

m S

AM

KO

to:

(SJ

R-16

8/D

8.0)

(VTK

R-2

04/D

21.1

)

4000'

- FL1

40

220 K

TM

AX

348^

168^

At

or a

bove

MA

X 2

20 K

T

4000'

EXPE

CT

RAD

AR

vect

ors

for

ILS

appr

oach

Rw

y 02

At

or a

bove

10000'

N01

36.9 E10

3 07

.2

At

or a

bove

6000'

JEPPESEN


10-2B

Changi EAST R

wy 0

2R/20L

is s

ole

ly for

use b

y the

Republic o

f Sin

gapore

Air F

orc

e (RSAF) Aircra

ft

2

1. RADAR required.

22 NOV 13

220 K

TM

AX

250 K

TM

AX

250 K

TM

AX

250 K

TM

AX.A.464.

.A.576.

.R.46

9.

(RWYS 02L/C)

[BOBA1A]

BOBAG ONE ALPHA (BOBAG1A) ARRIVAL

1RO

UTIN

G

Fro

m A

RAMA t

rack 1

47^

to B

OBAG.

Fro

m R

EKOP t

rack 1

41^

to B

OBAG.

1TRA

NSITIO

NS

EXPECT R

ADAR v

ecto

rs f

or

ILS a

ppro

ach R

wy 0

2.

At

BOBAG t

rack 0

83^

to B

OKIP

then t

o S

AMKO. Fro

m S

AMKO,

ARA

MA

(A

-464)

REK

OP

(A

-576)

a. MAIN

TAIN

last

assig

ned f

light

level or

altitude

Cha

ngi

Apt

17

NM

Refe

r to

10-1

P p

ages f

or

radio

communic

ations

failure

pro

cedure

.

2. Non-RNP-1/P-RNAV approved aircraft shall fly this as a basic RNAV (B-RNAV) procedure 1 or EXPECT RADAR vectors from ATC.

090^

180^ 360^

3400

'

2500

'21

00'

090^

180^ 360^

3400

'

2100

'19

00'

MSA

VTK

VO

RM

SA S

J VO

R

Apt Elev

22'D-ATIS

128.6

Airport elevation, lost comms.

NO

T TO

SCA

LE

244^

252^

235^243^

220^

168^

204^

115^

074^055^

047^

033^

D57.3

D43.6

D38

.6 D24.0

D11.

6

D21.1

D8.0

D12.7

D22.5

D11.0 D2

6.2

D30.0


COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS LOSTCOMMS LOSTCOMMS LOST

CHANGES:

WSSS/SINCHANGI


TEKONG

116.5

VTK

VTK

N01

24.9 E10

4 01

.3

D

2

.RNAV.STAR.

2. W

hen c

leare

d v

ia B

OBAG 1

B b

y S

ingapore

ATC:

1RO

UTIN

G

Fro

m A

RAMA t

rack 1

47^

to B

OBAG.

Fro

m R

EKOP t

rack 1

41^

to B

OBAG.

023^

BTM, th

en t

urn

LEFT a

nd t

rack 0

23^

to D

OVAN. Then t

urn

LEFT, tr

ack 3

48^

to

BIP

OP. Fro

m B

IPOP, EXPECT R

ADAR v

ecto

rs f

or

ILS a

ppro

ach R

wy 2

0.

3000'

- FL1

40

MA

X 2

20 K

T

N01

33.1

E103

05.4

REKO

P(S

J R-

293/

D50

.0)

(VTK

R-2

78/D

56.6

)

147^

141^

083^

083^

080^

023^

348^

ASUNA

N00

59.8

E103

09.9

BO

KIP

(VTK

R-2

21/D

27.0

)N01

04.4

E103

43.9

SA

MKO

N01

05.5

E103

52.9

DO

VA

NN01

19.6

E104

12.8

BIP

OP

N01

31.4

E104

10.3

At

or a

bove

MA

X 2

20 K

T

3000'

NYLO

N(V

TK R

-023

/D13

.0)

N01

37.0

E104

06.4

263^

6000'

- FL1

80

MA

X 2

20 K

T

203^

ARAMA

REKOP

41

39

20

14

9

15

1212

SINJO

N

113.5

SJSJ

N01

13.4

E103

51.3

D

BATA

M

*11

6.0

BTM

BTM

N01

08.2 E10

4 08

.0

D

1. Set

transponder

to M

ode A

/C c

ode 7

600.

appro

priate

landin

g p

rocedure

for

Rwy 2

0 a

s

clo

se a

s p

ossib

le t

o E

AT o

r ETA.

Specia

l Pro

cedure

s f

or

mis

sed a

ppro

ach p

rocedure

.

b. Fro

m N

YLON c

ommence d

escent

and c

arr

y o

ut

c. If

unable

to e

ffect

a landin

g, re

fer

to S

ingapore

3. No c

leara

nce o

r in

str

uction r

eceiv

ed f

rom

Sin

gapore

ATC:

ARA

MA

(SJ

R-29

8/D

50.0

)(V

TK R

-282

/D55

.5)

N01

36.9

E103

07.2

Dir

ect

dist

ance

fro

m B

IPO

P to

:

and p

roceed o

n B

OBAG 1

B t

o B

IPOP, th

en d

irect

to N

YLON.

10-2C

090^

180^ 360^

3400

'

2500

'21

00'

090^

180^ 360^

3400

'

2100

'19

00'

MSA

VTK

VO

R

MSA

SJ

VO

R

(RWYS 20C/R)

EXPE

CT

RAD

AR

vect

ors

for

ILS

appr

oach

Rw

y 20

(SJ

R-10

7/D

17.5

)(V

TK R

-158

/D17

.9)

1TRA

NSITIO

NS

At

BOBAG t

rack 0

83^

to B

OKIP

then t

o S

AMKO. Turn

LEFT, tr

ack 0

80^

to

At

or a

bove

7000'

or a

s di

rect

ed b

y A

TC

At

or a

bove

4000'

ARA

MA

(A

-464)

REK

OP (

A-576)

JEPPESEN



[BOBA1B]

BOBAG ONE BRAVO

Changi EAST R

wy 0

2R/20L

is s

ole

ly for

use b

y the

Republic o

f Sin

gapore

Air F

orc

e (RSAF) Aircra

ft

2

(BOBAG1B) ARRIVAL

BO

BA

GN01

02.5

E103

29.9

At

or a

bove

10000'

1. RADAR required.

1

22 NOV 13

MA

X 2

20 K

T

MA

X 2

20 K

T

.A.464.

.A.576.

.R.46

9.

250 K

TM

AX

250 K

TM

AX

250 K

TM

AX

Cha

ngi

Apt

15

NM

a. MAIN

TAIN

last

assig

ned f

light

level or

altitude

Refe

r to

10-1

P p

ages f

or

radio

communic

ations

failure

pro

cedure

.


2. Non-RNP-1/P-RNAV approved aircraft shall fly thisas a basic RNAV (B-RNAV) procedure or EXPECT RADAR vectors fromATC. 3. All SOUTHBOUND flights from the WEST landing at Singapore Changi Apt are to request for the STAR only from Singapore ATC on 133.25or 135.8 when Rwy 20 is in use and within SJ 120 DME. Flight shall remainunder the control of WMKK ATC.

22'Apt ElevD-ATIS

128.6

NO

T TO

SCA

LE


COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST


CHANGES:

WSSS/SINCHANGI


1

Apt Elev

22'and p

roceed o

n B

OBAG 1

K t

o A

DNIK

.

.RNAV.STAR.

2. W

hen c

leare

d v

ia B

OBAG 1

K b

y S

ingapore

ATC:

083^

ASUNA

N00

59.8

E103

09.9

BO

BA

GN01

02.5

E103

29.9

BO

KIP

N01

04.4

E103

43.9

SA

MKO

20

14

9SINJO

N11

3.5

SJSJ

N01

13.4

E103

51.3

D

1. Set

transponder

to M

ode A

/C c

ode 7

600.

clo

se a

s p

ossib

le t

o E

AT o

r ETA.

Specia

l Pro

cedure

s f

or

mis

sed a

ppro

ach p

rocedure

.

b. Fro

m A

DNIK

commence d

escent

and c

arr

y o

ut

c. If

unable

to e

ffect

a landin

g, re

fer

to S

ingapore

3. No c

leara

nce o

r in

str

uction r

eceiv

ed f

rom

Sin

gapore

ATC:

090^

180^ 360^

3400

'

2500

'

2100

'

MSA

SJ

VO

R

JEPPESEN

Fro

m A

SUNA t

o B

OBAG, to

BOKIP

, to

SAMKO, to

SADET,

RO

UTIN

G

At

or a

bove

6000'

015^023

^

MA

X 2

20 K

T

At

or a

bove

4000'

SA

DET

N01

10.1

E103

54.2

N01

05.5

E103

52.9

ADNIK

N01

16.9

E103

56.9

BOBAG ONE KILO (BOBAG1K) ARRIVAL[BOBA1K](RWY 02L)

5

7

D-ATIS

128.6

to A

DNIK

.

appro

priate

landin

g p

rocedure

for

Rwy 0

2L a

s

Changi EAST R

wy 0

2R/20L

is s

ole

ly for

use b

y the

Republic o

f Sin

gapore

Air F

orc

e (RSAF) Aircra

ft

1

MA

X 2

50 K

T

At

or a

bove

10000'


1. RNAV 1.2. RADAR required.


10-2D22 NOV 13

Lost comms.

4. Changi arrivals via ATS route A-464 shall flight plan BOBAG 1A ora. MAIN

TAIN

last

assig

ned f

light

level or

altitude

Refe

r to

10-1

P p

ages f

or

radio

communic

ations

failure

pro

cedure

.

3. RNAV (GNSS) CDO.

BOBAG 1B as STAR route. When traffic permits, BOBAG 1K, BOBAG 1L or LELIB 2B STAR will be issued to pilots.

NO

T TO

SCA

LE

ASUNA -

59.4

NM

BOBAG -

39.4

NM

BOKIP

- 2

5.4

NM

SADET -

11.7

NM

SAMKO -

16.4

NM

ADNIK

- 4

.5 N

M

WA

YPO

IN

T T

O

TH

RESH

OLD

DISTA

NC

E

COMMSLOST COMMSLOST LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMSCOMMS LOSTCOMMS LOST

CHANGES:

WSSS/SINCHANGI


TEKONG

116.5

VTK

VTK

N01

24.9 E10

4 01

.3

D

1

.RNAV.STAR.

2. W

hen c

leare

d v

ia B

OBAG 1

L b

y S

ingapore

ATC:

083^

080^

023^

ASUNA

N00

59.8

E103

09.9

BO

BA

GN01

02.5

E103

29.9

BO

KIP

N01

04.4

E103

43.9

SA

MKO

N01

05.5

E103

52.9

DO

VA

NN01

19.6

E104

12.8

BIP

OP

N01

31.4

E104

10.3

20

14

9

15

12

BATA

M*11

6.0

BTM

BTM

N01

08.2 E10

4 08

.0

D

1. Set

transponder

to M

ode A

/C c

ode 7

600.

clo

se a

s p

ossib

le t

o E

AT o

r ETA.

Specia

l Pro

cedure

s f

or

mis

sed a

ppro

ach p

rocedure

.

b. Fro

m I

DURO c

ommence d

escent

and c

arr

y o

ut

c. If

unable

to e

ffect

a landin

g, re

fer

to S

ingapore

3. No c

leara

nce o

r in

str

uction r

eceiv

ed f

rom

Sin

gapore

ATC:

090^

180^ 360^

3400

'

2100

'

1900

'

MSA

VTK

VO

R

At

or a

bove

4000'

JEPPESEN

RO

UTIN

G

BOBAG ONE LIMA (BOBAG1L) ARRIVAL[BOBA1L](RWY 20R)

BIP

AL

N01

33.1

E104

03.9

IDURO

N01

26.7

E104

01.1

285^

203^

At

or a

bove

10000'

MA

X 2

20 K

T

At

or a

bove

3000'

7

7

and p

roceed o

n B

OBAG 1

L t

o I

DURO.

appro

priate

landin

g p

rocedure

for

Rwy 2

0R a

s

348^

12

MA

X 2

50 K

TA

t or

abo

ve7000'

Changi EAST R

wy 0

2R/20L

is s

ole

ly for

use b

y the

Republic o

f Sin

gapore

Air F

orc

e (RSAF) Aircra

ft

1

Apt Elev

22'D-ATIS

128.6

to B

IPOP, to

BIP

AL, to

IDURO.

Fro

m A

SUNA t

o B

OBAG, to

BOKIP

, to

SAMKO, to

BTM, to

DOVAN,

1. RNAV (GNSS) CDO.Alt Set: hPa Trans level: FL130 Trans alt: 11000'

3. RADAR required.2. RNAV 1.

10-2E


22 NOV 13

Lost comms.

4. Changi arrivals via ATS route A-464 shall flight plan BOBAG 1A orBOBAG 1B as STAR route. When traffic permits, BOBAG 1K, BOBAG 1Lor LELIB 2B STAR will be issued to pilots.

a. MAIN

TAIN

last

assig

ned f

light

level or

altitude

Refe

r to

10-1

P p

ages f

or

radio

communic

ations

failure

pro

cedure

.

NO

T TO

SCA

LE

WA

YPO

IN

T T

O

TH

RESH

OLD

DISTA

NC

E

BIP

AL -

11.5

NM

BIP

OP -

18.2

NM

BOBAG -

80.2

NM

BOKIP

- 6

6.2

NM

DOVAN -

30.2

NM

SAMKO -

57.2

NM

ASUNA -

100.2

NM

BTM -

42.2

NM

IDURO -

4.5

NM


COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST


096^

D36.2

120^

D30

.0

D8.0168^

CHANGES:

WSSS/SINCHANGI


TEKONG

116.5

VTK

VTK

N01

24.9 E10

4 01

.3

D

3

1

.RNAV.STAR.

Alt Set: hPa Trans level: FL130 Trans alt: 11000'1. RADAR required.

2. W

hen c

leare

d v

ia L

AVAX 1

A b

y S

ingapore

ATC:

1RO

UTIN

G

1. Set

transponder

to M

ode A

/C c

ode 7

600.

appro

priate

landin

g p

rocedure

for

Rwy 0

2 a

s

clo

se a

s p

ossib

le t

o E

AT o

r ETA.

Specia

l Pro

cedure

s f

or

mis

sed a

ppro

ach p

rocedure

.

b. Fro

m S

AMKO c

ommence d

escent

and c

arr

y o

ut

c. If

unable

to e

ffect

a landin

g, re

fer

to S

ingapore

3. No c

leara

nce o

r in

str

uction r

eceiv

ed f

rom

Sin

gapore

ATC:

Dir

ect

dist

ance

fro

m S

AN

AT

to:

and p

roceed o

n L

AVAX 1

A t

o S

ANAT, th

en d

irect

to S

AMKO.

10-2F

TO

MA

NTra

ck 2

33^

from T

OMAN t

o K

ARTO, tu

rn R

IGHT t

rack 2

69^

to

KEXAS, th

en t

o L

AVAX.

090^

180^ 360^

3400

'

2500

'21

00'

090^

180^ 360^

3400

'

2100

'19

00'

MSA

VTK

VO

R

MSA

SJ

VO

R

SINJO

N11

3.5

SJSJ

N01

13.4

E103

51.3

D

168^

348^

IGNO

N(S

J R-

102/

D22

.2)

(VTK

R-1

44/D

19.8

)N01

08.8

E104

13.0

SA

NA

T(S

J R-

124/

D9.

9)(V

TK R

-186

/D17

.1)

N01

07.8

E103

59.5

At

or a

bove

4000'

266^

14

14

1TRA

NSITIO

NS

At

LAVAX t

rack 2

66^

to I

GNON a

nd t

hen t

o S

ANAT. Fro

m S

ANAT,

EXPECT R

ADAR v

ecto

rs f

or

ILS a

ppro

ach R

wy 0

2.

SA

MKO

(VTK

R-2

04/D

21.1

)N01

05.5

E103

52.9

or EXPECT RADAR vectors from ATC.

MA

X 2

20 K

T

SU

RG

A(M

-635)

JEPPESEN

then t

rack 2

91^

to I

BULA, th

en t

rack 3

35^

to L

AVAX.

Tra

ck 2

79^

from O

BDOS t

o I

KAGO, th

en t

rack 2

79^

to I

KIM

A,

then t

rack 2

91^

to I

BULA. Then t

rack 3

35^

to L

AVAX.

Tra

ck 3

20^

from S

URGA t

o I

KAGO, th

en t

rack 2

79^

to I

KIM

A,

OBD

OS

(L-504/

M-774)


EXPE

CT

RAD

AR

vect

ors

for

ILS

appr

oach

Rw

y 02

4000'

- FL1

40

220 K

TM

AX

(SJ

R-11

7/D

50.2

)(V

TK R

-135

/D48

.7)

279^

291^

335^

233^

269^

21

20

17

46

21

TOMAN

OBDO

S

N01

09.8

E104

27.2

LAVA

XN01

10.3

E104

48.3

(VTK

R-1

07/D

49.2

)

KEXA

S(S

J R-

093/

D57

.2)

N00

50.6

E104

36.0

IBULA

IKIM

A(S

J R-

115/

D70

.5)

(VTK

R-1

28/D

67.9

)N00

43.2 E10

4 55

.0

SURG

A(S

J R-

124/

D19

4)

S00

37.0 E10

6 31

.3(V

TK R

-129

/D19

3)

OBDO

S(S

J R-

105/

D19

1)(V

TK R

-109

/D18

5)N00

25.1

E106

55.9

089^

089^

111^

291^

269^

KA

RTO

(SJ

R-09

1/D

103)

N01

11.4

E105

33.7

(VTK

R-0

98/D

93.5

)

TO

MA

N(S

J R-

086/

D11

7)

N01

21.8

E105

47.3

(VTK

R-0

92/D

106)

SURG

A

97

320^

IKA

GO

(SJ

R-11

0/D

104)

N00

38.3

E105

29.5

(VTK

R-1

18/D

99.8

)

87

.M.635.

.L.504.

.M.774.

3527

9^

2FL1

50 -

FL2

50

MA

X 2

50 K

TFL2

60 -

FL3

10

MA

X 2

80 K

T

27000'

- FL1

40

MA

X 2

20 K

T

(RWYS 02L/C)

LAVAX ONE ALPHA(LAVAX1A) ARRIVAL

[LAVA1A]

7000'

At

or a

bove

or a

s di

rect

edby

ATC

Changi EAST R

wy 0

2R/20L

is s

ole

ly for

use b

y the

Republic o

f Sin

gapore

Air F

orc

e (RSAF) Aircra

ft

3

At

250 K

T

At

or b

elow

FL1

60

At 2

20 K

T

At

250 K

T

At

or b

elow

FL1

80

22 NOV 13

Cha

ngi

Apt

14

NM

a. MAIN

TAIN

last

assig

ned f

light

level or

altitude

Refe

r to

10-1

P p

ages f

or

radio

communic

ations

failure

pro

cedure

.


2. Non-RNP-1/P-RNAV approved aircraft shall fly this as a basic RNAV (B-RNAV) procedure

Apt Elev

22'D-ATIS

128.6

NO

T TO

SCA

LE

074^

055^03

3^

D22.5

D11.0

D30.0

COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST


096^

087^

D36.2

D28.6

LOSTCOMMSLOSTCOMMSLOST COMMS

CHANGES:

WSSS/SINCHANGI


TEKONG

116.5

VTK

VTK

N01

24.9 E10

4 01

.3

D

3

1

.RNAV.STAR.


2. W

hen c

leare

d v

ia L

AVAX 1

B b

y S

ingapore

ATC:

023^

348^

DO

VA

N

BIP

OP

N01

31.4

E104

10.3

NYLO

N(V

TK R

-023

/D13

.0)

N01

37.0

E104

06.4

203^

12

1. Set

transponder

to M

ode A

/C c

ode 7

600.

appro

priate

landin

g p

rocedure

for

Rwy 2

0 a

s

clo

se a

s p

ossib

le t

o E

AT o

r ETA.

Specia

l Pro

cedure

s f

or

mis

sed a

ppro

ach p

rocedure

.

b. Fro

m N

YLON c

ommence d

escent

and c

arr

y o

ut

c. If

unable

to e

ffect

a landin

g, re

fer

to S

ingapore

3. No c

leara

nce o

r in

str

uction r

eceiv

ed f

rom

Sin

gapore

ATC:

Dir

ect

dist

ance

fro

m B

IPO

P to

:

and p

roceed o

n L

AVAX 1

B t

o B

IPOP, th

en d

irect

to N

YLON.

10-2G

304^

9

8N01

14.9

E104

19.8

RUTO

T(V

TK R

-118

/D21

.0)

3000'

- FL1

40

MA

X 2

20 K

T

SINJO

N

113.5

SJSJ

N01

13.4

E103

51.3

D

(SJ

R-04

7/D

26.2

)

N01

19.6 E10

4 12

.8(V

TK R

-115

/D12

.7)


4000'

At

or a

bove

JEPPESEN


090^

180^ 360^

3400

'

2500

'21

00'

090^

180^ 360^

3400

'

2100

'19

00'

MSA

VTK

VO

RM

SA S

J VO

R

1RO

UTIN

G

TO

MA

NTra

ck 2

33^

from T

OMAN t

o K

ARTO, tu

rn R

IGHT t

rack 2

69^

to

KEXAS, th

en t

o L

AVAX.

1TRA

NSITIO

NS

SU

RG

A(M

-635)

then t

rack 2

91^

to I

BULA, th

en t

rack 3

35^

to L

AVAX.

Tra

ck 2

79^

from O

BDOS t

o I

KAGO, th

en t

rack 2

79^

to I

KIM

A,

then t

rack 2

91^

to I

BULA. Then t

rack 3

35^

to L

AVAX.

Tra

ck 3

20^

from S

URGA t

o I

KAGO, th

en t

rack 2

79^

to I

KIM

A,

OBD

OS

(L-504/

M-774)

At

LAVAX t

rack 3

04^

to R

UTOT a

nd t

hen t

o D

OVAN. Then t

rack 3

48^

to

BIP

OP. Fro

m B

IPOP, EXPECT R

ADAR v

ecto

rs f

or

ILS a

ppro

ach R

wy 2

0.

(SJ

R-11

7/D

50.2

)(V

TK R

-135

/D48

.7)

279^

291^

335^

233^

269^

21

20

17

46

21

TOMAN

OBDO

S

N01

09.8

E104

27.2

N01

10.3

E104

48.3

(VTK

R-1

07/D

49.2

)

KEXA

S(S

J R-

093/

D57

.2)

N00

50.6

E104

36.0

IBULA

IKIM

A(S

J R-

115/

D70

.5)

(VTK

R-1

28/D

67.9

)N00

43.2 E10

4 55

.0SURG

A(S

J R-

124/

D19

4)

S00

37.0 E10

6 31

.3(V

TK R

-129

/D19

3)

OBDO

S(S

J R-

105/

D19

1)(V

TK R

-109

/D18

5)N00

25.1

E106

55.9

089^

089^

111^

291^

269^

KA

RTO

(SJ

R-09

1/D

103)

N01

11.4

E105

33.7

(VTK

R-0

98/D

93.5

)

TO

MA

N(S

J R-

086/

D11

7)

N01

21.8

E105

47.3

(VTK

R-0

92/D

106)

SURG

A

97

320^

IKA

GO

(SJ

R-11

0/D

104)

N00

38.3

E105

29.5

(VTK

R-1

18/D

99.8

)

87

.M.635.

.L.504.

.M.774.

3527

9^

2FL1

50 -

FL2

50

MA

X 2

50 K

TFL2

60 -

FL3

10

MA

X 2

80 K

T

27000'

- FL1

40

MA

X 2

20 K

T

(RWYS 20C/R)

LAVAX ONE BRAVO(LAVAX1B) ARRIVAL

[LAVA1B]EX

PECT

RAD

AR

vect

ors

for

ILS

appr

oach

Rw

y 20

(VTK

R-1

20/D

30.0

)LA

VA

Xor

as

dire

cted

by A

TC

At

or a

bove

8000'

MA

X 2

20 K

T

At

or a

bove

3000'

Changi EAST R

wy 0

2R/20L

is s

ole

ly for

use b

y the

Republic o

f Sin

gapore

Air F

orc

e (RSAF) Aircra

ft

3

At 2

20 K

TA

t 250 K

T

At

or b

elow

FL1

60

At

or b

elow

At

250 K

T

FL1

80

22 NOV 13

Cha

ngi

Apt

15

NM

a. MAIN

TAIN

last

assig

ned f

light

level or

altitude

Refe

r to

10-1

P p

ages f

or

radio

communic

ations

failure

pro

cedure

.



Apt Elev

22'D-ATIS

128.6

NO

T TO

SCA

LE

COMMSLOST COMMSLOST LOSTCOMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMSCOMMS LOSTCOMMS LOST

CHANGES:

WSSS/SINCHANGI


1

.RNAV.STAR.

2. W

hen c

leare

d v

ia L

AVAX 1

K b

y S

ingapore

ATC:

1. Set

transponder

to M

ode A

/C c

ode 7

600.

clo

se a

s p

ossib

le t

o E

AT o

r ETA.

Specia

l Pro

cedure

s f

or

mis

sed a

ppro

ach p

rocedure

.

b. Fro

m A

DNIK

commence d

escent

and c

arr

y o

ut

c. If

unable

to e

ffect

a landin

g, re

fer

to S

ingapore

3. No c

leara

nce o

r in

str

uction r

eceiv

ed f

rom

Sin

gapore

ATC:

TO

MA

N

291^

335^

233^

269^

21

20

17

46

21

TOMAN

090^

180^ 360^

3400

'

2500

'

2100

'

N01

09.8

E104

27.2

LAVA

X

N01

10.3

E104

48.3

KEXA

S

N00

50.6

E104

36.0

IBULA

IKIM

A

KA

RTO

TO

MA

N

SINJO

N11

3.5

SJSJ

N01

13.4

E103

51.3

D

IGNO

NN01

08.8

E104

13.0

SA

NA

T

266^

14

14

JEPPESEN

[LAVA1K](RWY 02L)

LAVAX ONE KILO (LAVAX1K) ARRIVAL

MSA

SJ

VO

R

Fro

m T

OMAN t

o K

ARTO, to

KEXAS, to

LAVAX.

OBD

OS

SU

RG

A

TRA

NSITIO

NS

RO

UTIN

G

N00

43.2

E104

55.0

N01

11.4

E105

33.7

N01

21.8

E105

47.3

At

or a

bove

7000'

N01

07.8

E103

59.5

SA

DET

N01

10.1

E103

54.2

ADNIK

N01

16.9

E103

56.9

293^

023^

6

7

appro

priate

landin

g p

rocedure

for

Rwy 0

2L a

s

Fro

m L

AVAX t

o I

GNON, to

SANAT, to

SADET, to

ADNIK

.

and p

roceed o

n L

AVAX 1

K t

o A

DNIK

.

Changi EAST R

wy 0

2R/20L

is s

ole

ly for

use b

y the

Republic o

f Sin

gapore

Air F

orc

e (RSAF) Aircra

ft

1

Apt Elev

22'D-ATIS

128.6

MA

X 2

20 K

T

At

or a

bove

4000'

MA

X 2

50 K

T

At

or b

elow

FL1

40

IKAGO -

121.5

NM

OBDOS -

208.5

NM

SURGA -

218.5

NM

2. RADAR required.1. RNAV 1.

3. RNAV (GNSS) CDO.


10-2H


OBDO

SN00

25.1

E106

55.9

IKA

GO

N00

38.3

E105

29.5

SURG

AS0

0 37

.0E1

06 3

1.3

279^

320^

87

97

3527

9^O

BDO

S

SURG

A

Fro

m O

BDOS t

o I

KAGO, to

IKIM

A, to

IBULA, to

LAVAX.

Fro

m S

URGA t

o I

KAGO, to

IKIM

A, to

IBULA, to

LAVAX.

22 NOV 13

a. MAIN

TAIN

last

assig

ned f

light

level or

altitude

Refe

r to

10-1

P p

ages f

or

radio

communic

ations

failure

pro

cedure

.

Lost comms.

NO

T TO

SCA

LE

WA

YPO

IN

T T

O T

HRESH

OLD

DISTA

NC

E

IBULA -

68.2

NM

IGNON -

31.5

NM

IKIM

A -

88.2

NM

ADNIK

- 4

.5 N

M

KARTO -

114.2

NM

KEXAS -

68.2

NM

LAVAX -

47.2

NM

SADET -

11.7

NM

SANAT -

17.6

NM

TOMAN -

131.2

NM


COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST


CHANGES:

WSSS/SINCHANGI


TEKONG

116.5

VTK

VTK

N01

24.9 E10

4 01

.3

D

1

.RNAV.STAR.

2. W

hen c

leare

d v

ia L

AVAX 1

L b

y S

ingapore

ATC:

348^

DO

VA

N

BIP

OP

N01

31.4

E104

10.3

12

1. Set

transponder

to M

ode A

/C c

ode 7

600.

clo

se a

s p

ossib

le t

o E

AT o

r ETA.

Specia

l Pro

cedure

s f

or

mis

sed a

ppro

ach p

rocedure

.

b. Fro

m I

DURO c

ommence d

escent

and c

arr

y o

ut

c. If

unable

to e

ffect

a landin

g, re

fer

to S

ingapore

3. No c

leara

nce o

r in

str

uction r

eceiv

ed f

rom

Sin

gapore

ATC:

TO

MA

N

304^

9

8

090^

180^ 360^

3400

'

2100

'

1900

'

MSA

VTK

VO

R

N01

14.9

E104

19.8

RUTO

T

N01

09.8

E104

27.2

LAVA

X

21

335^

21

N00

50.6

E104

36.0

IBULA

291^

20

At

or a

bove

8000'

4000'

At

or a

bove

JEPPESEN

(RWY 20R)

[LAVA1L]285^

203^

7

7

BIP

AL

N01

33.1

E104

03.9

Fro

m T

OMAN t

o K

ARTO, to

KEXAS, to

LAVAX.

Fro

m L

AVAX t

o R

UTOT, to

DOVAN, to

BIP

OP, to

BIP

AL, to

IDURO.

TRA

NSITIO

NS

RO

UTIN

G

and p

roceed o

n L

AVAX 1

L t

o I

DURO.

appro

priate

landin

g p

rocedure

for

Rwy 2

0R a

s

IDURO

N01

26.7

E104

01.1

N01

19.6

E104

12.8

LAVAX ONE LIMA (LAVAX1L) ARRIVAL

Changi EAST R

wy 0

2R/20L

is s

ole

ly for

use b

y the

Republic o

f Sin

gapore

Air F

orc

e (RSAF) Aircra

ft

1

Apt Elev

22'D-ATIS

128.6

MA

X 2

50 K

T

At

or b

elow

FL1

40

MA

X 2

20 K

T

At

or a

bove

3000'

IKAGO -

123.2

NM

SURGA -

220.2

NM

OBDOS -

210.2

NM

10-2J


KEXA

SN01

10.3

E104

48.3

46

269^

KA

RTO

N01

11.4

E105

33.7TO

MAN 17233^

TO

MA

NN01

21.8

E105

47.3

OBDO

SN00

25.1

E106

55.9

279^

IKA

GO

N00

38.3

E105

29.5

SURG

AS0

0 37

.0E1

06 3

1.3

320^

87

97

279^

OBDO

S

SURG

A

35

IKIM

AN00

43.2

E104

55.0

OBD

OS

Fro

m O

BDOS t

o I

KAGO, to

IKIM

A, to

IBULA, to

LAVAX.

Fro

m S

URGA t

o I

KAGO, to

IKIM

A, to

IBULA, to

LAVAX.

SU

RG

A

22 NOV 13

a. MAIN

TAIN

last

assig

ned f

light

level or

altitude

Refe

r to

10-1

P p

ages f

or

radio

communic

ations

failure

pro

cedure

.

Lost comms.

2. RADAR required.


3. RNAV (GNSS) CDO.

1. RNAV 1.

NO

T TO

SCA

LE

WA

YPO

IN

T T

O T

HRESH

OLD

DISTA

NC

EBIP

AL -

11.5

NM

BIP

OP -

18.2

NM

DOVAN -

30.2

NM

IBULA -

68.2

NM

TOMAN -

131.2

NM

IKIM

A -

88.2

NM

KARTO -

114.2

NM

KEXAS -

68.2

NM

LAVAX -

47.2

NM

RUTOT -

38.2

NM

IDURO -

4.5

NM


COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST


282^

274^

298^

296^

355^

326^

007^

033^

023^

D55.5

D36.6

D30.0

D12.9

D17.2

D22.6

D13.2

D30.0

D13.0

VTK

116.5

CHANGES:

WSSS/SINCHANGI


TEKONG

116.5

VTK

VTK

N01

24.9 E10

4 01

.3

D

2

.RNAV.STAR.

2. W

hen c

leare

d v

ia L

ELIB

2B b

y S

ingapore

ATC:

1RO

UTIN

G

023^

NYLO

NN01

37.0

E104

06.4

203^

1. Set

transponder

to M

ode A

/C c

ode 7

600.

appro

priate

landin

g p

rocedure

for

Rwy 2

0 a

s

clo

se a

s p

ossib

le t

o E

AT o

r ETA.

Specia

l Pro

cedure

s f

or

mis

sed a

ppro

ach p

rocedure

.

b. Fro

m N

YLON c

ommence d

escent

and c

arr

y o

ut

c. If

unable

to e

ffect

a landin

g, re

fer

to S

ingapore

3. No c

leara

nce o

r in

str

uction r

eceiv

ed f

rom

Sin

gapore

ATC:

ARA

MA

(SJ

R-29

8/D

50.0

)

Dir

ect

dist

ance

fro

m B

IDUS

to:

and p

roceed o

n L

ELIB

2B t

o B

IDUS, th

en d

irect

to N

YLON.

10-2K

090^

180^ 360^

3400

'

2500

'21

00'

090^

180^ 360^

3400

'

2100

'19

00'

MSA

VTK

VO

RM

SA S

J VO

R

(RWYS 20C/R)

118^

082^

086^

057^

20

18

7

10

LELI

BN01

27.5

E103

24.8

N01

30.6

E103

49.7

ALF

A

At

or a

bove

6000'

N01

35.9

E103

57.9

BID

US

SINJO

N11

3.5

SJSJ

N01

13.4

E103

51.3

DJAYBE

E

400

JBJ

BN01

30.0

E103

42.7

(SJ

R-33

3/D

18.6

)(V

TK R

-285

/D19

.3)

EXPE

CT

RAD

AR

vect

ors

for

ILS

appr

oach

Rw

y 20

.A464.

N01

36.9 E10

3 07

.2

LELIB TWO BRAVO

At

or a

bove

10000'

At

or a

bove

7000'

At

or a

bove

220 K

TM

AX 3000'

JEPPESEN

3000'

- FL1

40

MA

X 2

20 K

T



[LELI2B]

Changi EAST R

wy 0

2R/20L

is s

ole

ly for

use b

y the

Republic o

f Sin

gapore

Air F

orc

e (RSAF) Aircra

ft

2

(LELIB2B) ARRIVAL

1. RADAR required.

At

220 K

T

At

250 K

T

22 NOV 13

turn

LEFT a

nd t

rack 0

57^

to B

IDUS. Fro

m B

IDUS, EXPECT R

ADAR v

ecto

rsfo

r IL

S a

ppro

ach R

wy 2

0.

At

LELIB

, tu

rn L

EFT a

nd t

rack 0

82^

to J

B. Then t

rack 0

86^

to A

LFA, th

en

Cha

ngi

Apt

14

NM

a. MAIN

TAIN

last

assig

ned f

light

level or

altitude

Refe

r to

10-1

P p

ages f

or

radio

communic

ations

failure

pro

cedure

.

Lost comms.

procedure2. Non-RNP-1/P-RNAV approved aircraft shall fly this

as a basic RNAV (B-RNAV) 1 or EXPECT RADAR vectors fromATC. 3. All SOUTHBOUND flights from the WEST landing at SingaporeChangi Apt are to request the STAR only from Singapore ATC on 133.25 or135.8 when Rwy 20 is in use and within 120 DME SJ. Flight shall remainunder the control of WMKK ATC. 4. Changi arrivals via ATS route A-464shall flight plan BOBAG 1A or BOBAG 1B as STAR route. When trafficpermits, BOBAG 1K, BOBAG 1L or LELIB 2B STAR will be issued to pilots.

Apt Elev

22'D-ATIS

128.6

NO

T TO

SCA

LE

347^

355^D90.2

D80.4

069^

D6.9

D9.9

D8.0

124^168^

COMMS

COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMSLOST COMMSLOST COMMSLOST COMMSLOST


CHANGES:

WSSS/SINCHANGI


TEKONG116.5 VTKVTK

N01 24.9 E104 01.3

D

2

1

.RNAV.STAR.


1 ROUTING

023^

NYLON

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

3. No clearance or instruction received from Singapore ATC:

Direct distance from SANAT to:

10-2L

SANAT. From SANAT, EXPECT RADAR vectors for ILS approach Rwy 02.

090^

180^

360^

3400'

2500'2100'090^

180^

360^

3400'

2100'1900'

MSA VTK VOR MSA SJ VOR

VEPLI

N03 52.4 E104 05.7(VTK R-002/D147)

SINJON

113.5 SJSJN01 13.4 E103 51.3

D

(RWYS 02L/C)

At PASPU track 180^ to NYLON then track 172^ to POSUB. Turn RIGHT and track 203^ to

At BIKTA track 120^ to PIBAP, then turn RIGHT and track 180^ to PASPU.

At VEPLI track 180^ to PIBAP then to PASPU.

At MABAL track 231^ to KILOT, then turn RIGHT to track 258^ to VINIL. Turn LEFT and track 180^ to PIBAP and then to PASPU.

348^

168^

180^180^

231^

258^

120^

172^

203^

4235

57

27

25

31

22

10

21

MABAL

VEPLI

BIKTA

VINIL

MABAL

(VTK R-030/D142)N03 28.4 E105 12.6

KILOT

N03 02.3 E104 40.4

PIBAP

N02 30.4 E104 06.3(VTK R-004/D65.3)(SJ R-011/D78.1)

BIKTAN02 43.6E103 43.1

(VTK R-008/D34.5)(SJ R-018/D48.1)

PASPU

N01 59.3 E104 06.3

N01 37.0 E104 06.4

POSUB

N01 27.4 E104 07.8(SJ R-050/D21.7)

N01 07.8 E103 59.5

SANAT(VTK R-186/D17.1)

At or above4000'

360^360^

(VTK R-003/D89.8)(SJ R-009/D102)

051^

231^

(SJ R-024/D119)(VTK R-022/D105)

FL280 - FL350MAX 300 KT

N02 55.0E104 06.3

180^

203^

(VTK R-023/D13.0)(SJ R-033/D30.0)

SAMKO(VTK R-204/D21.1)

N01 05.5E103 52.9

4000' - FL140 220 KTMAX

3000' - FL140MAX 220 KT

altitude and proceed on PASPU 1A to SANAT, then direct to SAMKO.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 PASPU 1A by Singapore ATC:

Singapore Special Procedures for missed approach procedure.

(SJ R-031/D157)

(SJ R-005/D159)

EXPECT RADARvectors for ILS

approach Rwy 02

1 TRANSITIONS

.N892.

.B469..M751.

FL160 - FL260MAX 250 KT

.L642

.

FL280 - FL350MAX 300 KT

At or above6000'

or as directedby ATC

180^


MAX 220 KT

BIKTA(M-751/B-469)

MABAL(N-892)

VEPLI(L-642)

JEPPESEN


[PASP1A]

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

Air Force (RSAF) Aircraft

2

PASPU ONE ALPHA (PASPU1A) ARRIVAL

220 KTAt

At or belowFL210

250 KTAt

At 220 KT

22 NOV 13

Changi Apt 14 NM

a. MAINTAIN last assigned flight level or

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

Lost comms.


Apt Elev

22'D-ATIS

128.6

NOT TO SCALE

COMMS

COMMS

LOST

COMMS

LOST

COMMS

LOST



D90.2

D80.4

347^

355^

CHANGES:

WSSS/SINCHANGI


TEKONG116.5 VTKVTK

N01 24.9 E104 01.3

D

2

1

.RNAV.STAR.


1 ROUTING



Direct distance from NYLON to:

10-2M

090^

180^

360^

3400'

2500'2100'090^

180^

360^

3400'

2100'1900'


SINJON113.5 SJSJ

N01 13.4 E103 51.3

D

(RWYS 20C/R)

At BIKTA track 120^ to PIBAP, then turn RIGHT and track 180^ to PASPU.

At VEPLI track 180^ to PIBAP then to PASPU.

At MABAL track 231^ to KILOT, then turn RIGHT to track 258^ to VINIL. Turn LEFT and track 180^ to PIBAP and then to PASPU.

altitude and proceed on PASPU 1B 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 PASPU 1B by Singapore ATC:


NYLON.

At PASPU track 180^ to NYLON. From NYLON, EXPECT RADAR vectors for ILS approach Rwy 20.

(VTK R-008/D34.5)(SJ R-018/D48.1)

PASPU

N01 59.3 E104 06.3

At or above6000'

NYLON

N01 37.0 E104 06.4(VTK R-023/D13.0)(SJ R-033/D30.0)

VEPLI

N03 52.4 E104 05.7(VTK R-002/D147)

180^

120^

57

27

25

VEPLI

BIKTA

VINILBIKTA

N02 43.6E103 43.1

360^360^

(VTK R-003/D89.8)(SJ R-009/D102)

N02 55.0E104 06.3

180^

(SJ R-005/D159)

.B469..M751.

FL160 - FL260MAX 250 KT

.L642

.

180^

258^35

31

PIBAP

203^

FL280 - FL350MAX 300 KT

231^

MABAL

(VTK R-030/D142)N03 28.4 E105 12.6

051^

231^

FL280 - FL350MAX 300 KT

(SJ R-031/D157)

.N892.42MABA

L

KILOT

N03 02.3 E104 40.4

(SJ R-024/D119)(VTK R-022/D105)

N02 30.4 E104 06.3(VTK R-004/D65.3)(SJ R-011/D78.1)

3000' - FL140MAX 220 KT

023^

22

1 TRANSITIONS


approach Rwy 20

180^


At or above3000' 220 KTMAX

or as directed by ATC

BIKTA(M-751/B-469)

MABAL(N-892)

VEPLI(L-642)

JEPPESEN




2

PASPU ONE BRAVO (PASPU1B) ARRIVAL[PASP1B]

At 220 KT

At or belowFL210

At 250 KT

22 NOV 13

Changi Apt 17 NM




2. Non-RNP-1/P-RNAV approved aircraft shall fly this as a basic RNAV(B-RNAV) procedure

Apt Elev

22'D-ATIS

128.6

NOT TO SCALE

COMMS

COMMS

LOST

COMMS

LOST

COMMS

LOST



CHANGES:

WSSS/SINCHANGI


1

.RNAV.STAR.

NYLON



090^

180^

360^

3400'

2500'

2100'

MSA SJ VORVEPLI

SINJON113.5 SJSJ

N01 13.4 E103 51.3

D

180^180^

231^

120^

203^

42

35

57

27

25

31

22

21

VEPLI

BIKTA

VINIL

MABAL

KILOT

PIBAP

BIKTAN02 43.6E103 43.1

PASPU

POSUB

SANAT

N02 55.0E104 06.3

180^

altitude and proceed on PASPU 1K to

b. From ADNIK commence descent and carry out appropriate landing procedure for

c. If unable to effect a landing, refer to

2. When cleared via PASPU 1K by Singapore ATC:


At or belowFL270

JEPPESEN

[PASP1K](RWY 02L)

258^

N03 52.4E104 05.7

N03 28.4E105 12.6

MABAL

N03 02.3E104 40.4

N02 30.4E104 06.3

N01 59.3E104 06.3

N01 37.0E104 06.4

N01 27.4E104 07.8

N01 07.8E103 59.5

TRANSITIONS

ROUTING

BIKTA

MABAL

VEPLI

ADNIK.

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

SADETN01 10.1E103 54.2

ADNIKN01 16.9E103 56.9

293^

023^

6

7

PASPU ONE KILO (PASPU1K) ARRIVAL



1

D-ATIS

128.6

MAX 250 KT

At or above6000'

MAX 220 KT

At or above4000'

172^10

3. RNAV (GNSS) CDO.

Alt Set: hPa Trans level: FL130 Trans alt: 11000'1. RADAR required. 2. RNAV 1.

From BIKTA to PIBAP.

From MABAL to KILOT, to VINIL , to PIBAP.

From VEPLI to VINIL, to PIBAP.

From BIPAP to PASPU, to NYLON, to POSUB, to SANAT, to SADET, to ADNIK.

10-2N


Apt Elev

22'

22 NOV 13


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


NOT TO SCALE

THRESHOLD DISTANCEWAYPOINT TO

BIKTA - 128.6 NMKILOT - 161.6 NMMABAL - 203.6 NMNYLON - 48.6 NMPASPU - 70.6 NM

ADNIK - 4.5 NM

POSUB - 38.6 NMSADET - 11.7 NMSANAT - 17.6 NMVEPLI - 183.6 NM

PIBAP - 101.6 NM

VINIL - 126.6 NM

COMMS

COMMS

LOST

COMMS

LOST

COMMS

LOST



CHANGES:

WSSS/SINCHANGI


TEKONG116.5 VTKVTK

N01 24.9 E104 01.3

D

1

.RNAV.STAR.



090^

180^

360^

3400'

2100'

1900'

MSA VTK VOR

altitude and proceed on PASPU 1L to

b. From IDURO commence descent and carry out appropriate landing procedure for

c. If unable to effect a landing, refer to

2. When cleared via PASPU 1L by Singapore ATC:

IDURO.

PASPU

NYLON

VEPLI 180^

120^

57

27

25

VEPLI

BIKTA

VINILBIKTA

N02 43.6E103 43.1

N02 55.0E104 06.3 180^

180^

258^35

31

PIBAP

231^

MABAL

42MABA

L

KILOT

22

At or belowFL250

JEPPESEN

PASPU ONE LIMA (PASPU1L) ARRIVAL

(RWY 20R)[PASP1L]

N03 52.4E104 05.7

N03 28.4E105 12.6

BIKTA

MABAL

VEPLI

TRANSITIONS

ROUTING

Rwy 20R as close as possible to EAT or ETA.

N01 37.0E104 06.4

MAX 220 KTAt or above

3000'

BIPALN01 33.1E104 03.9

IDURON01 26.7E104 01.1

N01 59.3E104 06.3

214^

203^

5

7

N03 02.3E104 40.4

N02 30.4E104 06.3

Singapore Special Procedures for missedapproach procedure.



1

MAX 250 KT

At or above6000'

3. RNAV (GNSS) CDO.

Alt Set: hPa Trans level: FL130 Trans alt: 11000'1. RADAR required. 2. RNAV 1.

From BIKTA to PIBAP.

From MABAL to KILOT, to VINIL, to PIBAP.

From VEPLI to VINIL, to PIBAP.

From BIPAP to PASPU, to NYLON, to BIPAL, to IDURO.

10-2P


Apt Elev

22'

22 NOV 13

D-ATIS

128.6




NOT TO SCALE


BIPAL - 11.5 NM

KILOT - 129.1 NMMABAL - 171.1 NMNYLON - 16.1 NM

PIBAP - 69.1 NMVEPLI - 151.1 NM

PASPU - 38.1 NM

BIKTA - 96.1 NM

IDURO - 4.5 NM

VINIL - 94.1 NM

COMMSLOST COMMSLOST COMMSLOST COMMSLOST COMMSLOST

COMMS

LOST

COMMS

LOST

LOSTC

OMMS

COMMS

LOST

COMMS

LOST

CHANGES:

WSSS/SINCHANGI


090^

180^

360^

3400'

2500'

2100'

MSA SJ VOR

SINJON113.5 SJSJ

N01 13.4 E103 51.3

D

28

REPOV

REMESN00 43.7E103 57.6

348^

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

close as possible to EAT or ETA.

Special Procedures for missed approach procedure.

b. From ADNIK commence descent and carry out

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


and proceed on REMES 1K to ADNIK.

22

N01 05.5E103 52.9

SAMKO

N00 16.4E104 03.0

JEPPESEN

[REME1K](RWY 02L)

SADETN01 10.1E103 54.2

ADNIKN01 16.9E103 56.9

015^

023^

5

7

ROUTING

appropriate landing procedure for Rwy 02L as

REMES ONE KILO (REMES1K) ARRIVAL

MAX 220 KT

At or above4000'

From REPOV to REMES, to SAMKO, to SADET, to ADNIK.

1



1

D-ATIS

128.6 3. RNAV (GNSS) CDO.


At or belowFL250

MAX 250 KT

At or above6000'

1. RADAR required. 2. RNAV 1.

10-2Q

| JEPPESEN 2011, 2013. ALL RIGHTS RESERVED.

22 NOV 13

Apt Elev

22'

a. MAINTAIN last assigned flight level or altitude

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


NOT TO SCALE

WAYPOINT TO THRESHOLD DISTANCE

REMES - 38.4 NMREPOV - 66.4 NMSADET - 11.7 NMSAMKO - 16.4 NM

ADNIK - 4.5 NM


COMMS

COMMS

LOST

COMMS

LOST


CHANGES:

WSSS/SINCHANGI


TEKONG116.5 VTKVTK

N01 24.9 E104 01.3

D

1

.RNAV.STAR.

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

close as possible to EAT or ETA.


b. From IDURO commence descent and carry out



090^

180^

360^

3400'

2100'

1900'

MSA VTK VOR023^

28

27

12

BATAM*116.0 BTMBTM

N01 08.2 E104 08.0

D

REPOV

REMES

DOVANN01 19.6E104 12.8

N01 31.4E104 10.3

BIPOP

348^

023^

N00 16.4E104 03.0

At or above4000'

JEPPESEN

REMES ONE LIMA (REMES1L) ARRIVAL[REME1L](RWY 20R)


3000'


7000'

N00 43.7E103 57.6

348^

12

285^

203^

77

BIPALN01 33.1E104 03.9

IDURON01 26.7E104 01.1

At or belowFL270

and proceed on REMES 1L to IDURO.

appropriate landing procedure for Rwy 20R as

ROUTING

From REPOV to REMES, to BTM, to DOVAN, to BIPOP, to BIPAL, to IDURO.

D-ATIS

128.6



1

3. RNAV (GNSS) CDO.

Alt Set: hPa Trans level: FL130 Trans alt: 11000'1. RADAR required. 2.RNAV 1.

10-2S


22 NOV 13

Apt Elev

22'




NOT TO SCALE


BIPOP - 18.2 NM

DOVAN - 30.2 NM

REMES - 69.2 NMREPOV - 97.2 NM

BIPAL - 11.5 NM

BTM - 42.2 NM

IDURO - 4.5 NM

179^

185^

D41.2

D68.2

204^

D21.1


COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS COMMSLOST COMMSLOST COMMSLOST COMMSLOST

CHANGES:

WSSS/SINCHANGI


TEKONG116.5 VTKVTK

N01 24.9 E104 01.3

D

2

1

.RNAV.STAR.


1 ROUTING

Direct distance from SAMKO to:

10-2T

090^

180^

360^

3400'

2500'2100'090^

180^

360^

3400'

2100'1900'


(RWYS 02L/C)

SINJON113.5 SJSJ

N01 13.4 E103 51.3

D

FRO

M P

ARDI

348^

51

28

REPOV(SJ R-168/D57.9)

REMESN00 43.7E103 57.6

348^

2. When cleared via REMES 5A 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.


b. From SAMKO commence descent and carry out



and proceed on REMES 5A to SAMKO.

6000' - FL140MAX 220 KT

168^168^

22

168^

(SJ R-168/D30.2)

4000' - FL140MAX 220 KT


approach Rwy 02

N01 05.5E103 52.9

(SJ R-168/D8.0)SAMKO

FL150 - FL250 250 KTMAX

N00 16.4E104 03.0

RADAR vectors for ILS approach Rwy 02.At PARDI track 348^ to REPOV, then to REMES, then to SAMKO. From SAMKO, EXPECT


6000'At or above

At or belowFL210

JEPPESEN

REMES FIVE ALPHA (REMES5A) ARRIVAL[REME5A]




2

At 220 KT

At 250 KT

MAX 220 KT

At or above4000'

22 NOV 13

.G.579.

Changi Apt 17 NM





Apt Elev

22'D-ATIS

128.6

NOT TO SCALE


COMMS

LOST

COMMS

LOST

COMMS

LOST

179^

185^168^

115^

074^

047^

055^

D26.

2D11.0

D12.7

D22.5

D41.2

D30.2

D68.2


CHANGES:

WSSS/SINCHANGI


TEKONG116.5 VTKVTK

N01 24.9 E104 01.3

D

2

1

.RNAV.STAR.


2. When cleared via REMES 6B by Singapore ATC:

1 ROUTING

023^

203^


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


b. From NYLON commence descent and carry out



Direct distance from BIPOP to:

10-2U

090^

180^

360^

3400'

2500'2100'090^

180^

360^

3400'

2100'1900'


(RWYS 20C/R)

SINJON

113.5 SJSJN01 13.4 E103 51.3

D

FRO

M P

ARDI

348^

023^

348^

51

28

27

12

12

BATAM*116.0 BTMBTM

N01 08.2 E104 08.0

D

REPOV(SJ R-168/D57.9)

REMES

DOVANN01 19.6E104 12.8

N01 31.4E104 10.3

BIPOP

NYLON

N01 37.0 E104 06.4

(SJ R-033/D30.0)(VTK R-023/D13.0)

348^

and proceed on REMES 6B to BIPOP, then direct to NYLON.

3000' - FL140MAX 220 KT

6000' - FL140MAX 220 KT

168^168^

FL150 - FL250 250 KTMAX

023^

then to DOVAN. Turn LEFT and track 348^ to BIPOP. From BIPOP, EXPECT RADAR vectors for ILS approach Rwy 20.


approach Rwy 20

(SJ R-107/D17.5)(VTK R-158/D17.9)

N00 16.4E104 03.0

At PARDI track 348^ to REPOV, then to REMES. Then turn RIGHT and track 023^ to BTM,


N00 43.7 E103 57.6

At or above7000'


At or above4000'

JEPPESEN


[REME6B]



2

REMES SIX BRAVO (REMES6B) ARRIVAL


3000'

At 220 KT

At 220 KT

250 KTAtAt or below

FL210

22 NOV 13

.G.579.


Changi Apt 15 NM




Apt Elev

22'D-ATIS

128.6

NOT TO SCALE

| JEPPESEN SANDERSON, INC., 1998, 2007. ALL RIGHTS RESERVED.

SINGAPORE, SINGAPORECHANGI

WSSS/SIN JEPPESEN+

MINIMUM CLIMB GRADIENT CRITERIAThe Instrument Departure Procedures are only applicable for aircraft with all enginesoperating. It remains the responsibility of the operator to develop contingency proce-dures for the individual type of aircraft and to conduct the necessary examination ofobstacles 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.

The specific routes to be followed are depicted in SID Charts pages. Altitude restric-tions at fixes and/or DME specify ATC/airspace requirements. Minimum net climb gra-dient specifies obstacle clearance requirements.

In the event that the minimum net climb gradient cannot be achieved, pilots shallinform ATC and ATC shall hold departures if pilots indicate that they are unable tomeet the required net climb gradient.

RUNWAY 02L

When there are no reports of vessel movement along the northern shipping channel, orwhere the reported vessel height is less than 35m (115 ft) AMSL, the aircraft minimumnet climb gradient shall be at 3.3%.

Where the reported vessel height is 35m (115 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.

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 70m (230 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 advisepilots of the vessel height. Pilots, on receipt of this information, shall apply the mini-mum net climb gradient in accordance with the following table.

Ht of Vessel(meters AMSL)

Gradient (%)

Minimum Crossing Altitude Over Vessel

meters feet

35 3.4 44 142

40 3.9 49 158

50 4.8 59 191

60 5.8 69 224

70 6.8 79 257

80 7.8 89 290

90 8.8 99 322

100 9.7 109 355

110 10.7 119 388

120 11.7 129 421

130 12.7 139 454

140 13.7 149 486

10-326 JAN 07

| JEPPESEN SANDERSON, INC., 1998, 2007. ALL RIGHTS RESERVED.


WSSS/SIN JEPPESEN+

MINIMUM CLIMB GRADIENT CRITERIA

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

RUNWAYS 20C/20R

All departures on Runway 20C/20R shall be on a minimum net climb gradient of 5%until reaching or passing 400 ft. Thereafter, the minimum net climb gradient shall be3.3%.

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 wishto calculate their own climb gradients based on actual lift-off point, provided the cal-culation ensures the following:

^ 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 Changiwherein tall vessels of height above 49m (161 ft) AMSL are not permitted. The dis-tance (d) for the various departure runways is as follows:

Ht of Vessel(meters AMSL)

Gradient (%)

Minimum Crossing Altitude Over Vessel

meters feet

70 3.4 89 292

80 3.8 99 325

90 4.3 109 358

100 4.7 119 390

110 5.1 129 423

120 5.5 139 456

130 6.0 149 489

140 6.4 159 522

Departure Runway Distance (d)

02L 1020m

02C 2360m

20C 5945m

20R 8370m

10-3A26 JAN 07

COMMSLOST COMMSLOST COMMSLOST COMMSLOSTLOST

COMMSLOST COMMSLOST COMMSLOST COMMSLOST LOSTCOMMS

COMMS

LOST

CHANGES:

WSSS/SINCHANGI


SID

.RNAV.SID.Trans level: FL130 Trans alt: 11000'

ROUTING


2. Communications failure occurs immediately

INITIAL CLIMB

JEPPESEN

022^

023^

001^

001^

266^297^

VIDAX

NUGSI

TOREKN01 43.3 E104 01.6

ADPAXN01 44.0 E103 15.6

2

16

24

30

FL140

FL140

MAA FL240

MAA FL240

ADPAX 1

U

ADPAX 1W

TEKONG116.5 VTKVTK

N01 24.9 E104 01.3

D

N01 31.3E104 06.4

N01 27.4E104 01.4

At or above6000'

after departure on Rwys 02L/C:Proceed straight ahead to Nylon HoldingArea (NHA) climbing to the last assigned

To VIDAX on course 022^.

To VTK on course 023^.

JB (JAYBEE), to ADPAX.

At or aboveFL140

For minimum climb gradient criteria:Rwys 02L/C- See 10-3 and 10-3A.

SINJON113.5 SJSJ

N01 13.4 E103 51.3

D



JAYBEE

400 JBJBN01 30.0 E103 42.7

22 NOV 13


DEPARTURES

ADPAX 1UADPAX 1W

[ADPA1U], [ADPA1W]

(RWYS 02L, 02C)

090^

180^

360^

3400'

2100'1900'

MSA VTK VOR

090^

180^

360^

3400'

2500'2100'

MSA SJ VORMAX 220 KT UNTIL PASSING 4000' AND250 KT UNTIL PASSING 10000'

10-3B

RWY

02L

02C

ADPAX 1U

ADPAX 1W

Direct distance from Changi Apt(Rwy 02L) to: VIDAX 6 NM(Rwy 02C) to: VTK 4 NM

Initial climb clearance 3000' or as directed by ATC

To TOREK. Climb on track 001^, at or above 6000' turn RIGHT direct to NUGSI. Then to

altitude. Thereafter refer to 10-1P pages


for radio communications failure procedure.

1. These SIDs will be assigned during air defense exercises.2. RADAR required. 3. RNAV 1 (GNSS, DME/DME).4. All SIDs include noise preferential routes. 5. Cruising levelswill be issued after take-off by Singapore RADAR. 6. Aircraftunable to fly SID profile shall inform ATC prior to departure andto EXPECT RADAR vectoring, if necessary.

Apt Elev

22'

SPEED:

NOT TO SCALE


COMMS

LOST

COMMSLOST COMMSLOST COMMSLOST COMMSLOST LOST

LOST

CHANGES:

WSSS/SINCHANGI

SINGAPORE, SINGAPORE.RNAV.SID.



A

ROUTING

Direct distance from Changi Apt

75 100 150 200 250 300Gnd speed-KT

minimum net climb gradient of 5.0% untilRwys 20C/R: Departures shall be on a


2. Communications failure occurs immediately

INITIAL CLIMB

JEPPESEN

A

203^

180^5

N01 17.5E103 58.1

SUDPO

DUNAL

11

271^

28

FL140At or above

SUNVAN01 17.9E103 57.4 20

3^

171^5

180^

N01 01.6E103 58.1

ADPAX 1

V

ADPA

X 1

X

SINJON113.5 SJSJ

N01 13.4 E103 51.3

D

TEKONG116.5 VTKVTK

N01 24.9 E104 01.3

D

326^

344^9

35

MA

A F

L240

FL1

40

MAA FL2

40

FL140

ADPAXN01 44.0E103 15.6

BASIXN01 10.0E103 24.9

after departure on Rwys 20C/R:Proceed straight ahead to Samko HoldingArea (SHA) climbing to the last assigned

To SUNVA on course 203^, then to SUSIN.

To SUDPO on course 203^, then to SUSIN.

1At or above

2000'

At SUSIN to DUNAL, BOBAG, BASIX, ADPAX.

22 NOV 13

DEPARTURES

ADPAX 1VADPAX 1X

[ADPA1V], [ADPA1X]

MAX 220 KT UNTIL PASSING4000' AND 250 KT UNTILPASSING 10000'


090^

180^

360^

3400'

2500'2100'090^

180^

360^

3400'

2100'1900'


1At or above

2000'

10-3C

(RWYS 20C/R)

SID RWY

20R

20C

ADPAX 1V

ADPAX 1X

(Rwy 20C) to: SUDPO 4 NM(Rwy 20R) to: SUNVA 4 NM

reaching or passing 400'.

5.0% V/V (fpm) 380 506 760 1013 1266 1519


altitude. Thereafter refer to 10-1P pagesfor radio communications failure procedure.

SUSINN01 12.5E103 58.1

BOBAGN01 02.5E103 29.9

Trans level: FL130 Trans alt: 11000'1. These SIDs will be assigned during air defense exercises.

4. 12. RADAR required. 3. RNAV 1 (GNSS, DME/DME). The restriction to crossSUDPO or SUNVA at or above 2000' is applicable between 2301-1100 UTC. Alldeparture aircraft on Runways 20C/R issued with heading instructions by ATC shall

restriction cannot be complied with, the pilot-in-command of an aircraft departing onRunways 20C/R shall inform ATC during the time when the aircraft commences taxiing

6. Cruising levels will be issued after take-off by Singapore RADAR. 7. Aircraft unableto fly SID profile shall inform ATC prior to departure and to EXPECT RADAR

vectoring, if necessary.

Apt Elev

22'


also cross VTK 8 DME at or above 2000' between 2301-1100 UTC. If the altitude

to the holding point for departure. 5. All SIDs include noise preferential routes.

SPEED:

NOT TO SCALE

083^

057^

059^

097^

195^

150^

D9.4

D23.2

D24.2

D8.0

D6.9

D12.8

COMMSLOST COMMSLOST COMMSLOST LOST

COMMS

COMMS

LOST

COMMS

LOST

LOST


161^D39.0

138^D34.1

CHANGES:

WSSS/SINCHANGI


SID

10-3D

A

115^173^

120^

203^

180^

150^

9

22

16

75

17

5

N01 17.5E103 58.1

(VTK R-203/D8.0)SUDPO

N01 12.5E103 58.1

SUSIN

At or above4000'

N01 26.1E104 10.7

DOKTA

.RNAV.SID.

1 INITIAL CLIMB

1 ROUTING

ANITO FIVE ALPHA (ANI5A),

DOSNO

ANITO

N00 48.0 E104 14.2

S00 17.0 E104 52.0

ANIT

O F

IVE A

LPHA

(ANI5A

)

(ANI4B)

ANITO FOUR BRAVO

TOKIM(SJ R-037/D20.1)(VTK R-023/D5.0)

(SJ R-113/D24.0)DOBLU

N01 03.8 E104 13.3

At or belowor as directed by ATC

6000'

Rwy 02C: Proceed straight ahead to Nylon Holding Area (NHA) climbing

Rwy 20C: Proceed straight ahead to Samko Holding Area (SHA) climbing

to the last assigned altitude.


7600.1. Set transponder to Mode A/C code

2. Communications failure occurs immediately after departure on:

177^

(VTK R-153/D113)(SJ R-146/D109)

(RWYS 02C, 20C)

22 NOV 13

4000'At or above

JEPPESEN

ANITO FOUR BRAVO (ANI4B) DEPARTURES

N01 29.6 E104 03.3

2At or above

2000'


2000'At or above

75 100 150 200 250 300


Gnd speed-KT

For minimum climb gradient criteria:

minimum net climb gradient of 5.0% until

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

Rwy 20C: Departures shall be on a

.B.470.

At DOSNO turn LEFT and track 150^ to ANITO and join ATS route B-470.

SINJON113.5 SJSJ

N01 13.4 E103 51.3

D

DTEKONG

116.5 VTKN01 24.9 E104 01.3VTK

090^

180^

360^

3400'

2500'2100'090^

180^

360^

3400'

2100'1900'



Climb straight ahead to TOKIM, turn RIGHT and track 115^ to DOKTA.Turn RIGHT and track 173^ to DOBLU. Then track 177^ to DOSNO.

Climb straight ahead to SUDPO, turn LEFT and track 180^ to SUSIN.Turn LEFT and track 120^ to DOBLU. Turn RIGHT and track 177^ to DOSNO.

RWY

02C

20C

ANI5A

ANI4B

Apt Elev

22'



A

(Rwy 02C) to: TOKIM 9 NM(Rwy 20C) to: SUDPO 4 NM



5.0% V/V(fpm) 380 506 760 1013 1266 1519

Thereafter refer to 10-1P pages

Lost comms.

Thereafter refer to 10-1P pages for

procedure.radio communications failure

for radio communications failureprocedure.

Trans level: FL130 Trans alt: 11000'

12

1. RADAR required.

instructions by ATC shall also cross VTK 8 DME at or above 2000' between 2301-1100 UTC. If the altitude restriction cannot be complied with, the pilot-in-commandof an aircraft departing on Runway 20C shall inform ATC during the time when theaircraft commences taxiing to the holding point for departure. 4. All SIDs includenoise preferential routes. 5. Cruising levels will be issued after take-off by Singapore RADAR. 6. On initial contact when requesting ATC, inform ATC of the FLcan cross at ANITO.

2. Non-RNP-1/P-RNAV approved aircraft shall fly this as a basic RNAV (B-RNAV) procedure3.

or EXPECT RADAR vectors from ATC. The restriction to cross SUDPO at or above 2000' is applicable between

2301-1100 UTC. All departure aircraft on Runway 20C issued with heading

SPEED:

023^

NOT TO SCALE

083^

057^

053^

097^

195^

150^161^138^

D9.4

D23.2

D24.2

D39.0D34.1

D7.6

D6.9

D12.8



COMMS

COMMS

LOST

COMMS

LOST

LOST

CHANGES:

WSSS/SINCHANGI

SINGAPORE, SINGAPORE10-3E

A

115^173^

120^

203^

172^

177^

9

22

16

17

5

(VTK R-013/D5.1)

TOPOM

N01 17.9E103 57.4

(VTK R-210/D8.0)SUNVA

N01 12.5E103 58.1

SUSIN

At or above4000'

N01 26.1E104 10.7

DOKTA


.RNAV.SID.

1 ROUTING

Rwy 02L: Proceed straight ahead to Nylon Holding Area (NHA) climbing

Rwy 20R: Proceed straight ahead to Samko Holding Area (SHA) climbing

DOSNON00 48.0 E104 14.2


ANIT

O F

IVE E

CHO

(ANI5E)

(ANI4F)

2At or above

2000'

(SJ R-034/D20.0)

DOSNON00 48.0 E104 14.2

75

150^




N01 03.8 E104 13.3


6000'

ANITO FOUR

FOXTROT

ANITO(SJ R-146/D109)

S00 17.0 E104 52.0(VTK R-153/D113)

22 NOV 13

JEPPESEN

N01 29.9 E104 02.5


2000'At or above

SINJON113.5 SJSJ

N01 13.4 E103 51.3

D

DTEKONG

116.5 VTKN01 24.9 E104 01.3VTK

75 100 150 200 250 300Gnd speed-KT




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

Rwy 20R: Departures shall be on a

.B.470.

At DOSNO turn LEFT and track 150^ to ANITO and join ATS route B-470.

4000'At or above

090^

180^

360^

3400'

2500'2100'090^

180^

360^

3400'

2100'1900'


(RWYS 02L, 20R)ANITO FOUR FOXTROT (ANI4F) DEPARTURES

ANITO FIVE ECHO (ANI5E),


SID 1 INITIAL CLIMBRWY

02L

20R

ANI5E

ANI4F

Turn RIGHT and track 173^ to DOBLU. Then track 177^ to DOSNO.Climb straight ahead to TOPOM, turn RIGHT and track 115^ to DOKTA.

Turn LEFT and track 120^ to DOBLU. Turn RIGHT and track 177^ to DOSNO.Climb straight ahead to SUNVA, turn LEFT and track 172^ to SUSIN.

Apt Elev

22'



A

(Rwy 02L) to: TOPOM 9 NM(Rwy 20R) to: SUNVA 4 NM


5.0% V/V(fpm) 380 506 760 1013 1266 1519


Thereafter refer to 10-1P pages


Lost comms.

procedure.

procedure.

radio communications failure

for radio communications failure

12

1. RADAR required.

instructions by ATC shall also cross VTK 8 DME at or above 2000' between 2301-1100 UTC. If the altitude restriction cannot be complied with, the pilot-in-commandof an aircraft departing on Runway 20R shall inform ATC during the time when theaircraft commences taxiing to the holding point for departure. 4. All SIDs includenoise preferential routes. 5. Cruising levels will be issued after take-off by Singapore RADAR. 6. On initial contact when requesting ATC, inform ATC of the FLcan cross at ANITO.


or EXPECT RADAR vectors from ATC. The restriction to cross SUNVA at or above 2000' is applicable between

2301-1100 UTC. All departure aircraft on Runway 20R issued with heading


SPEED:

023^

NOT TO SCALE


COMMS

LOST

COMMS

LOST

COMMS

LOST


LOST COMMS

COMMSLOST

LOST

CHANGES:

WSSS/SINCHANGI

SINGAPORE, SINGAPORE10-3F .RNAV.SID.


JEPPESEN

22 NOV 13

090^

180^

360^

3400'

2500'2100'

090^

180^

360^

3400'

2100'1900'

MSA VTK VOR

MSA SJ VOR

A

203^

180^5

N01 17.5E103 58.1

SUDPO

SUSIN

TOKIMN01 29.6E104 03.3

342^

342^

332^10

17

(ARO1A

)

SULUG

AKOMAN01 45.4E103 54.7

21

(ARO

1B)

(RWYS 02C, 20C)

ARO

SO 1

BARO

SO 1

A

097^

026^

14 308^

24

AROSON02 08.8E103 24.4

AKMETN01 53.9E103 43.7

11000'At or above

N01 15.6E104 04.4

SAKINN01 12.0E104 02.65

To TOKIM on course 023^, then to AKOMA.

ROUTING

INITIAL CLIMB

7000'At or above

AROSO 1A

75 100 150 200 250 300Gnd speed-KT



A



minimum net climb gradient of 5.0% untilRwy 20C: Departures shall be on a

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







4

1. RADAR required. 12.

SINJON113.5 SJSJ

N01 13.4 E103 51.3

D

DTEKONG

116.5 VTKN01 24.9 E104 01.3VTK

7000'At or above

AROSO 1B1

To SUDPO on course 203^, then to SUSIN, SAKIN, SULUG, VTK, AKOMA.

At AKOMA to AKMET, AROSO.

RWY

20C

02C

SID

AROSO 1A

AROSO 1B

AROSO 1A (ARO1A), AROSO 1B (ARO1B) DEPARTURES

RWY 02C ARO 1A: MAX 220 KT UNTIL 4000'AND 250 KT UNTIL PASSING 10000'RWY 20C ARO 1B: MAX 220 KT UNTIL SAKINAND 250 KT UNTIL PASSING 10000'

4000'At or above

220 KTMAXN01 12.5 E103 58.1

220 KTMAX

2000'At or above

220 KTMAX

2000'At or above




5.0% V/V(fpm) 380 506 760 1013 1266 1519





radio communications failureprocedure.


The restriction to cross SUDPO at or above 2000' isapplicable between 2301-1100 UTC. All departure aircraft on Runway 20C issuedwith heading instructions by ATC shall also cross VTK 8 DME at or above 2000'between 2301-1100 UTC. If the altitude restriction cannot be complied with, the pilot-in-command of an aircraft departing on Runway 20C shall inform ATC during the

Apt Elev

22'time when the aircraft commences taxiing to the holding point for departure. 3. All SIDs include noise preferential routes. 4. Cruising levels will be issued after take-off by Singapore RADAR.

SPEED:

023^

NOT TO SCALE


COMMS

LOST

COMMS

LOST

COMMS

LOST


LOST COMMS

COMMSLOST

LOST

CHANGES:

WSSS/SINCHANGI

SINGAPORE, SINGAPORE10-3G .RNAV.SID.


JEPPESEN

22 NOV 13

090^

180^

360^

3400'

2500'2100'

090^

180^

360^

3400'

2100'1900'

MSA VTK VOR

MSA SJ VOR

A 342^

342^

333^10

17

(ARO1E)

SULUG

AKOMAN01 45.4E103 54.7

21

(ARO

1F)

(RWYS 02L, 20R)

ARO

SO 1

FARO

SO 1

E

097^ 026^

14 308^

24

AROSON02 08.8E103 24.4

AKMETN01 53.9E103 43.7

11000'At or above

N01 15.6E104 04.4

5

4

To TOPOM on course 023^, then to AKOMA.

ROUTING

INITIAL CLIMB

203^

172^5

N01 29.9E104 02.5

TOPOM

7000'At or above

7000'At or above

AROSO 1E


75 100 150 200 250 300Gnd speed-KT



A


minimum net climb gradient of 5.0% untilRwy 20R: Departures shall be on a

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

N01 17.9E103 57.4

SUNVA

1. RADAR required. 12.

SINJON

113.5 SJSJN01 13.4 E103 51.3

D

DTEKONG

116.5 VTKN01 24.9 E104 01.3VTK







To SUNVA on course 203^, then to SUSIN, SAKIN, SULUG, VTK, AKOMA.

At AKOMA to AKMET, AROSO.

RWYSID

AROSO 1E

AROSO 1F

02L

20R

AROSO 1E (ARO1E), AROSO 1F (ARO1F) DEPARTURES

RWY 20R ARO 1F: MAX 220 KT UNTIL SAKINAND 250 KT UNTIL PASSING 10000'

RWY 02L ARO 1E: MAX 220 KT UNTIL 4000'AND 250 KT UNTIL PASSING 10000'

1

2000'At or above

220 KTMAX

SUSINN01 12.5 E103 58.1

220 KTMAX 4000'At or above

220 KTMAX

SAKINN01 12.0E104 02.6

2000'At or above




5.0% V/V(fpm) 380 506 760 1013 1266 1519







The restriction to cross SUNVA at or above 2000' is applicable between 2301-1100 UTC. All departure aircraft on Runway 20R issued withheading instructions by ATC shall also cross VTK 8 DME at or above 2000' between2301-1100 UTC. If the altitude restriction cannot be complied with, the pilot-in-command of an aircraft departing on Runway 20R shall inform ATC during the time whenthe aircraft commences taxiing to the holding point for departure. 3. All SIDs includenoise preferential routes. 4. Cruising levels will be issued after take-off by SingaporeRADAR.

Apt Elev

22'

SPEED:

023^

NOT TO SCALE

083^

057^

059^

097^

195^

150^

D9.4

D23.2

D24.2

D8.0

D6.9

D12.8

113^

188^

D24.0

D23.4D

13.5

149^



COMMS

COMMS

LOST

COMMS

LOST

LOST

COMMS

COMMS

75 100 150 200 250 300

CHANGES:

WSSS/SINCHANGI

SINGAPORE, SINGAPORE10-3H

Gnd speed-KT

A

115^

173^

203^

180^9

225

N01 17.5E103 58.1


N01 12.5E103 58.1

SUSIN

N01 26.1E104 10.7

DOKTA

N01 03.8E104 13.3

DOBLU

2At or above

2000'

.RNAV.SID.

4000'At or above



A

BO

BA

G O

NE A

LPHA

(BOG1A)

TOKIM(SJ R-037/D20.1)(VTK R-023/D5.0)

BOBAG ONE ALPHA (BOG1A),

At or above4000'

N01 01.6E103 58.1

DUNAL

11

BO

BA

G O

NE

(BOG1B)

BRA

VO

262^

272^

1528

BOBAG(SJ R-243/D24.0)

N01 02.5 E103 29.9(VTK R-235/D38.6)




At or below6000'


10000'At or above

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

(RWYS 02C, 20C)

22 NOV 13

JEPPESEN

Apt Elev

22'


BOBAG ONE BRAVO (BOG1B) DEPARTURES

N01 29.6 E104 03.3

2000'At or above



SINJON113.5 SJSJ

N01 13.4 E103 51.3

D

DTEKONG

116.5 VTKN01 24.9 E104 01.3VTK

.R.469.

090^

180^

360^

3400'

2500'2100'090^

180^

360^

3400'

2100'1900'


MAX 220 KT UNTIL PASSING 4000' AND250 KT UNTIL PASSING 10000'

SID 1 INITIAL CLIMB

Climb straight ahead to TOKIM, turn RIGHT and track 115^ to DOKTA.

Climb straight ahead to SUDPO, turn LEFT and track 180^ to SUSIN.

RWY

02C

20C

BOG1A

BOG1B

turn RIGHT and track 173^ to DOBLU. Turn RIGHT and track 262^ to DUNAL,then track 272^ to BOBAG and join ATS route R-469.

Then track 180^ to DUNAL, turn RIGHT and track 272^ to BOBAG and joinATS route R-469.



5.0% V/V(fpm) 380 506 760 1013 1266 1519


Rwy 02C: Proceed straight ahead to NylonHolding Area (NHA) climbing to the last

Rwy 20C: Proceed straight ahead to SamkoHolding Area (SHA) climbing to the last

assigned altitude. Thereafter refer to10-1P pages for radio communications



failure procedure.

failure procedure.


12

1. RADAR required.

instructions by ATC shall also cross VTK 8 DME at or above 2000' between 2301-1100 UTC. If the altitude restriction cannot be complied with, the pilot-in-commandof an aircraft departing on Runway 20C shall inform ATC during the time when theaircraft commences taxiing to the holding point for departure. 4. All SIDs includenoise preferential routes. 5. Cruising levels will be issued after take-off by




Singapore RADAR.

SPEED:

023^

NOT TO SCALE

083^

057^

097^

195^

150^

D9.4

D23.2

D24.2

D6.9

D12.8

113^

188^

D24.0

D23.4D

13.5

149^

053^

D7.6



COMMS

COMMS

LOST

COMMS

LOST

LOST

COMMS

COMMS

75 100 150 200 250 300

CHANGES:

WSSS/SINCHANGI

SINGAPORE, SINGAPORE10-3J

Gnd speed-KT

A

173^22

N01 12.5E103 58.1

SUSIN

N01 26.1E104 10.7

DOKTA

.RNAV.SID.

4000'At or above



A

(BOG1E)

At or above4000'

11

BO

BA

G O

NE

(BOG1F)

262^

272^

1528


N01 02.5 E103 29.9(VTK R-235/D38.6)

TOPOM

(VTK R-013/D5.1)(SJ R-034/D20.0)

SUNVA(VTK R-210/D8.0)

203^

172^5

115^

9

BO

BA

G O

NE E

CHO

FO

XTRO

T

At or below6000'


N01 03.8E104 13.3

DOBLU




180^

At or above10000'

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

22 NOV 13

2At or above

2000'

2000'At or above

JEPPESEN

N01 01.6E103 58.1

DUNAL




(RWYS 02L, 20R)MAX 220 KT UNTIL PASSING 4000' AND250 KT UNTIL PASSING 10000'

BOBAG ONE FOXTROT (BOG1F) DEPARTURESBOBAG ONE ECHO (BOG1E),

SINJON

113.5 SJSJN01 13.4 E103 51.3

D

DTEKONG

116.5 VTKN01 24.9 E104 01.3VTK

.R.469.

090^

180^

360^

3400'

2500'2100'090^

180^

360^

3400'

2100'1900'



02L

20R

BOG1E

BOG1F



5.0% V/V(fpm) 380 506 760 1013 1266 1519


Rwy 02L: Proceed straight ahead to NylonHolding Area (NHA) climbing to the last

Rwy 20R: Proceed straight ahead to SamkoHolding Area (SHA) climbing to the lastassigned altitude. Thereafter refer to


10-1P pages for radio communications


failure procedure.

failure procedure.

N01 29.9 E104 02.5

N01 17.9 E103 57.4

12

2. Non-RNP-1/P-RNAV approved aircraft shall fly this as


instructions by ATC shall also cross VTK 8 DME at or above 2000' between 2301-2301-1100 UTC. All departure aircraft on Runway 20R issued with heading

1100 UTC. If the altitude restriction cannot be complied with, the pilot-in-commandof an aircraft departing on Runway 20R shall inform ATC during the time when theaircraft commences taxiing to the holding point for departure. 4. All SIDs includenoise preferential routes. 5. Cruising levels will be issued after take-off by

a basic RNAV (B-RNAV) procedure3.

1. RADAR required.Trans level: FL130 Trans alt: 11000'

Singapore RADAR.

Apt Elev

22'

Climb straight ahead to TOPOM, turn RIGHT and track 115^ to DOKTA.Turn RIGHT and track 173^ to DOBLU. Turn RIGHT and track 262^ toDUNAL, then track 272^ to BOBAG and join ATS route R-469.

Climb straight ahead to SUNVA, turn LEFT and track 172^ to SUSIN. Then track 180^ to DUNAL, then turn RIGHT and track 272^ to BOBAG andjoin ATS route R-469.

SPEED:

023^

NOT TO SCALE

097D6.9

188^

D23.4

D13.5

149^

D7.

6

053^


COMMS

COMMS

LOST

COMMSLOST COMMSLOST COMMSLOST COMMSLOST LOST

293^

D50.0

CHANGES:

WSSS/SINCHANGI


A

203^

180^5

N01 17.5E103 58.1

(VTK R-203/D8.0)

SUDPO

N01 12.5E103 58.1

SUSIN

.RNAV.SID.



A

N01 01.6E103 58.1

DUNAL

11

272^

28


N01 02.5 E103 29.9(VTK R-235/D38.6)

FL140At or above

22 NOV 13

SUNVA(VTK R-210/D8.0)

N01 17.9E103 57.4

203^

172^5

(SJ R-059/D8.0)

(VTK R-195/D12.8)

(BOG1V

)

BOBAG O

NE

VIC

TOR

(BOG1X

)

2At or above

2000'

2At or above

2000'

At or above4000'

Climb straight ahead to SUDPO, turn LEFT and track 180^ to SUSIN.

Climb straight ahead to SUNVA, turn LEFT and track 172^ to SUSIN.

ROUTING

At SUSIN track 180^ to DUNAL, then turn RIGHT and track 272^ to BOBAG. From BOBAGfollow the appropriate transition route to join the ATS route.

321^327^

41

39

ARAM

AREK

OP

ARAMA

REKOP

N01 33.1E103 05.4


75 100 150 200 250 300Gnd speed-KT

minimum net climb gradient of 5.0% untilRwys 20C/R: Departures shall be on a


2. Communications failure occurs immediatelyafter departure on:Rwys 20C/R: Proceed straight ahead toSamko Holding Area (SHA) climbing to thelast assigned altitude. Thereafter refer to

(SJ R-298/D50.0)

N01 36.9 E103 07.2

1

1

BO

BA

G O

NE

X-R

AY

180^

JEPPESEN

10-3K


(VTK R-282/D55.5)

(VTK R-278/D56.6)

SINJON

113.5 SJSJN01 13.4 E103 51.3

D

DTEKONG

116.5 VTKN01 24.9 E104 01.3VTK

090^

180^

360^

3400'

2500'2100'090^

180^

360^

3400'

2100'1900'



BOBAG ONE X-RAY (BOG1X) DEPARTURESBOBAG ONE VICTOR (BOG1V),

(RWYS 20C/R)

SID INITIAL CLIMBRWY

BOG1V

BOG1X 20C

20R

(Rwy 20C) to: SUDPO 4 NM(Rwy 20R) to: SUNVA 4 NM


5.0% V/V(fpm) 380 506 760 1013 1266 1519


10-1P pages for radio communications


failure procedure.


1 2

1. RADAR required. 2. These SIDs will be assigned during air defense exercises.

RADAR.preferential routes. 6. Cruising levels will be issued after take-off by Singapore.

3. Non-RNP-1/P-RNAV approved aircraft shall fly this as a basic RNAV (B-RNAV)procedure or EXPECT RADAR vectors from ATC. 4. The restriction to crossSUDPO or SUNVA at or above 2000' is applicable between 2301-1100 UTC. Alldeparture aircraft on Runways 20C/R issued with heading instructions by ATC

altitude restriction cannot be complied with, the pilot-in-command of an aircraftdeparting on Runways 20C/R shall inform ATC during the time when the aircraftcommences taxiing to the holding point for departure. 5. All SIDs include noise

Apt Elev

22' shall also cross VTK 8 DME at or above 2000' between 2301-1100 UTC. If the

SPEED:

NOT TO SCALE

023^

D13

332^

285^

343^D7

D19D19 00

1^

TEKONG116.5 VTKVTK

N01 24.9 E104 01.3

D



A

A

KONG KONG

286 KKKKN01 31.3 E103 59.4

JAYBEE

400 JBJBN01 30.0 E103 42.7

LELIBN01 27.5E103 24.8

NYLONN01 37.0E104 06.4

to LELIB

MAINTAINFL140

At FL140

Passing10000'

090^

180^

360^

3400'

2100'

1900'

MSA VTK VOR

WSSS/SINCHANGI



10-3L .SID.

2. All SIDs include noise preferential routes.3. Cruising levels will be issued after take-off by Singapore

RADAR.

(RWYS 02L/C)

CHANGES:

ROUTING

22 NOV 13

LELIB ONE CHARLIE (LLB1C) DEPARTURE


RWY

02L Climb straight ahead.

INITIAL CLIMB

02C Climb straight ahead to VTK.

Rwys 02L/C- See 10-3 and 10-3A.

Direct distance from Changi Apt to:

turn RIGHT and proceed direct to KK. Track 266^ bearing from KK to JB. Track 262^ bearing

1. This SID will be assigned during air defense exercises.


SINJON

113.5 SJSJN01 13.4 E103 51.3

D

JEPPESEN


Apt Elev

22'

(Rwy 02C) to: VTK 4 NM


Intercept and proceed on VTK R-001. After passing 10000', turn RIGHT to NYLON. At NYLON,

from JB to LELIB and join airway A-464. MAINTAIN FL140 from NYLON to LELIB

Airport elevation.

SPEED:

266^

262^17

18FL140

FL140

NOT TO SCALE

.A.464.


COMMS

LOST

COMMS

LOST

COMMS

LOST


LOST COMMS

COMMSLOST

CHANGES:

WSSS/SINCHANGI

SINGAPORE, SINGAPORE10-3M .RNAV.SID.


JEPPESEN

22 NOV 13

090^

180^

360^

3400'

2500'2100'

090^

180^

360^

3400'

2100'1900'

MSA VTK VOR

MSA SJ VOR

A

180^5

TOKIMN01 29.6E104 03.3

342^

342^

332^10

17

(MAS1A

)

SULUG

AKOMAN01 45.4E103 54.7

21

(MAS1B)

(RWYS 02C, 20C)

MASBO 1

BM

ASB

O 1

A

026^

13278^

MASBON02 02.8E102 52.9 AGVAR

N01 47.3E103 41.8

N01 15.6E104 04.4

4


ROUTING

75 100 150 200 250 300Gnd speed-KT



A




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







1

25

27 296^11000'

At or above

SABKAN01 50.9E103 17.2

7000'At or above

MASBO 1A

203^

097^5

N01 17.5E103 58.1

SUDPO

1. RADAR required.


At AKOMA to AGVAR, SABKA, MASBO.

SINJON

113.5 SJSJN01 13.4 E103 51.3

D

DTEKONG

116.5 VTKN01 24.9 E104 01.3VTK

At or above7000'

MASBO 1B

INITIAL CLIMBSID RWY

02C

20C

MASBO 1A

MASBO 1B

MASBO 1A (MAS1A), MASBO 1B (MAS1B) DEPARTURES

RWY 02C MAS 1A: MAX 220 KT UNTIL 4000'AND 250 KT UNTIL PASSING 10000'RWY 20C MAS 1B: MAX 220 KT UNTIL SAKINAND 250 KT UNTIL PASSING 10000'

SAKINN01 12.0E104 02.6

At or above

MAX

4000'

220 KTSUSIN

1

N01 12.5 E103 58.1

220 KTMAX

2000'At or above

220 KTMAX

2000'At or above




5.0% V/V(fpm) 380 506 760 1013 1266 1519

Initial climb clearance 3000' or as depicted by ATC






2. The restriction to cross SUDPO at or above 2000' isapplicable between 2301-1100 UTC. All departure aircraft on Runway 20C issued withheading instructions by ATC shall also cross VTK 8 DME at or above 2000' between2301-1100 UTC. If the altitude restriction cannot be complied with, the pilot-in-

command of an aircraft departing on Runway 20C shall inform ATC during the timewhen the aircraft commences taxiing to the holding point for departure. 3. All SIDsinclude noise preferential routes. 4. Cruising levels will be issued after take-off bySingapore RADAR.

Apt Elev

22'

SPEED:

023^

NOT TO SCALE


COMMS

LOST

COMMS

LOST

COMMS

LOST


LOST COMMS

COMMSLOST

CHANGES:

WSSS/SINCHANGI

SINGAPORE, SINGAPORE10-3N .RNAV.SID.

JEPPESEN

22 NOV 13

090^

180^

360^

3400'

2500'2100'

090^

180^

360^

3400'

2100'1900'

MSA VTK VOR

MSA SJ VOR

TEKONG116.5 VTKVTK

N01 24.9 E104 01.3

D

A 342^

342^

333^

10

17

(MAS1E)

SULUG

AKOMAN01 45.4E103 54.7

21

(MAS1F)

(RWYS 02L, 20R)

MASBO 1

FM

ASB

O 1

E

097^ 026^

N01 15.6E104 04.4

5

4


ROUTING

203^

172^5

N01 29.9E104 02.5

TOPOM

7000'At or above

7000'At or above

MASBO 1E


75 100 150 200 250 300Gnd speed-KT



A



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

N01 17.9E103 57.4

SUNVA

13278^

MASBON02 02.8E102 52.9 AGVAR

N01 47.3E103 41.8

25

27 296^11000'

At or above

SABKAN01 50.9E103 17.2

SINJON113.5 SJSJ

N01 13.4 E103 51.3

D








At AKOMA to AGVAR, SABKA, MASBO.


02L

20R

MASBO 1E

MASBO 1F

MASBO 1E (MAS1E), MASBO 1F (MAS1F) DEPARTURES

RWY 02L MAS 1E: MAX 220 KT UNTIL 4000'AND 250 KT UNTIL PASSING 10000'RWY 20R MAS 1F: MAX 220 KT UNTIL SAKINAND 250 KT UNTIL PASSING 10000'

4000'At or above

220 KTMAXN01 12.5 E103 58.1

220 KTMAX

SUSIN

SAKINN01 12.0E104 02.6

220 KT

1

2000'At or above

MAX

2000'At or above



5.0% V/V(fpm) 380 506 760 1013 1266 1519






radio communications failure procedure.



11. RADAR required. 2. The restriction to cross SUNVA at or above 2000' isapplicable between 2301-1100 UTC. All departure aircraft on Runway 20R issued withheading instructions by ATC shall also cross VTK 8 DME at or above 2000' between2301-1100 UTC. If the altitude restriction cannot be complied with, the pilot-in-

command of an aircraft departing on Runway 20R shall inform ATC during the timewhen the aircraft commences taxiing to the holding point for departure. 3. All SIDsinclude noise preferential routes. 4. Cruising levels will be issued after take-off bySingapore RADAR.

Apt Elev

22'

SPEED:

023^

NOT TO SCALE


COMMS

LOST

COMMS

LOST

COMMS

LOST


LOST COMMS

COMMSLOST

75 100 150 200 250 300

CHANGES:

WSSS/SINCHANGI


TEKONG116.5 VTKVTK

N01 24.9 E104 01.3

D

10-3P


Gnd speed-KT



A

180^5

Rwy 20C: Departures shall be on a

.RNAV.SID.



A

342^

332^

21

17

(VMR4A

)

356^38





7600.


(RWYS 02C, 20C)

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

22 NOV 13

JEPPESEN

203^

342^10

SULUG

026^

N01 15.6E104 04.4

4

097^5

MER

SING 4

A

MERSIN

G 5

B

(VMR5B)

SINJON113.5 SJSJ

N01 13.4 E103 51.3

D



ROUTING

At AKOMA to VMR.

090^

180^

360^

3400'

2500'2100'

090^

180^

360^

3400'

2100'1900'

MSA VTK VOR

MSA SJ VOR

7000'

MERSING 5B

At or above


MERSING116.8 VMRVMR

N02 23.3 E103 52.3

D


02C

20C

VMR4A

VMR5B

7000'At or above

MERSING 4A

MERSING 4A (VMR4A), MERSING 5B (VMR5B) DEPARTURES

RWY 02C VMR 4A: MAX 220 KT UNTIL 4000'AND 250 KT UNTIL PASSING 10000'RWY 20C VMR 5B: MAX 220 KT UNTIL SAKINAND 250 KT UNTIL PASSING 10000'

1

2000'At or above

220 KTMAX

SAKINN01 12.0E104 02.6SUSIN

N01 12.5 E103 58.1

220 KTMAX

4000'At or above

220 KTMAX

2000'At or above



5.0% V/V(fpm) 380 506 760 1013 1266 1519







1. Set transponder to Mode A/C code


11. RADAR required. 2. The restriction to cross SUDPO at or above 2000' isapplicable between 2301-1100 UTC. All departure aircraft on Runway 20C issued withheading instructions by ATC shall also cross VTK 8 DME at or above 2000' between2301-1100 UTC. If the altitude restriction cannot be complied with, the pilot-in-command of an aircraft departing on Runway 20C shall inform ATC during the timewhen the aircraft commences taxiing to the holding point for departure. 3. All SIDsinclude noise preferential routes. 4. Cruising levels will be issued after take-off bySingapore RADAR. 5. MERSING 4A will also be assigned during air defense exercises.

Apt Elev

22'

AKOMAN01 45.4E103 54.7

TOKIMN01 29.6E104 03.3

SUDPON01 17.5E103 58.1

SPEED:

023^

NOT TO SCALE


COMMS

LOST

COMMS

LOST

COMMS

LOST


LOST COMMS

LOST COMMS

75 100 150 200 250 300

CHANGES:

WSSS/SINCHANGI


TEKONG116.5 VTKVTK

N01 24.9 E104 01.3

D

10-3Q


Gnd speed-KT



A

Rwy 20R: Departures shall be on a

.RNAV.SID.



A

342^333^

21 17

(VMR4E)

MER

SING

4E

AKOMAN01 45.4E103 54.7

N01 29.9E104 02.5

TOPOM

203^

N01 17.9E103 57.4

SUNVA

At or above7000'

356^38







(RWYS 02L, 20R)

090^

180^

360^

3400'

2500'2100'

090^

180^

360^

3400'

2100'1900'

MSA VTK VOR

MSA SJ VOR

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

22 NOV 13

JEPPESEN


342^10

SULUGN01 15.6E104 04.4

4026^

5

172^5

097^


ROUTING


At AKOMA to VMR.

MERSIN

G 5

F

(VMR5F)



02L

20R

VMR4E

VMR5F

7000'At or above

MERSING 4E

MERSING 4E (VMR4E), MERSING 5F (VMR5F) DEPARTURES

MERSING116.8 VMRVMR

N02 23.3 E103 52.3

D

RWY 02L VMR 4E: MAX 220 KT UNTIL 4000'AND 250 KT UNTIL PASSING 10000'RWY 20R VMR 5F: MAX 220 KT UNTIL SAKINAND 250 KT UNTIL PASSING 10000'

SUSINN01 12.5 E103 58.1

220 KTMAX

SAKINN01 12.0E104 02.6

4000'At or above

220 KTMAX

SINJON

113.5 SJSJN01 13.4 E103 51.3

D

1

2000'At or above

220 KTMAX

2000'At or above



5.0% V/V(fpm) 380 506 760 1013 1266 1519







11. RADAR required. 2. The restriction to cross SUNVA at or above 2000' isapplicable between 2301-1100 UTC. All departure aircraft on Runway 20R issued withheading instructions by ATC shall also cross VTK 8 DME at or above 2000' between2301-1100 UTC. If the altitude restriction cannot be complied with, the pilot-in-command of an aircraft departing on Runway 20R shall inform ATC during the timewhen the aircraft commences taxiing to the holding point for departure. 3. All SIDsinclude noise preferential routes. 4. Cruising levels will be issued after take-off bySingapore RADAR. 5. MERSING 4E will also be assigned during air defense exercises.

Apt Elev

22'

SPEED:

023^

NOT TO SCALE

023^

D13

332^

285^

343^D7

D19D19

001^

090^

180^

360^

3400'

2100'

1900'

CHANGES:

MSA VTK VOR

WSSS/SINCHANGI


TEKONG

116.5 VTKVTKN01 24.9 E104 01.3

D

10-3S .SID.



A

A

KONG KONG

286 KKKKN01 31.3 E103 59.4

JAYBEE

400 JBJBN01 30.0 E103 42.7

NYLONN01 36.9E104 06.4

to PIMOK

MAINTAINFL140

At FL140

Passing10000'

22 NOV 13


Apt Elev

22'


2. All SIDs include noise preferential routes.3. Cruising levels will be issued after take-off by Singapore

RADAR.

(RWYS 02L/C)

1. This SID will be assigned during air defense exercises.

PIMOK ONE CHARLIE (PMK1C) DEPARTURE

SINJON

113.5 SJSJN01 13.4 E103 51.3

D

ROUTING

RWY

02L Climb straight ahead.

INITIAL CLIMB

02C Climb straight ahead to VTK.

turn RIGHT and proceed direct to KK. Track 266^ bearing from KK to JB. Track 262^ bearing

JEPPESEN

MAX 220 KT UNTIL PASSING 4000'AND 250 KT UNTIL PASSING 10000'

For minimum climb gradient criteria:Rwys 02L/C- See 10-3 and 10-3A.

Direct distance from Changi Apt to:(Rwy 02C) to: VTK 4 NM


Intercept and proceed on VTK R-001. After passing 10000', turn RIGHT to NYLON. At NYLON,

from JB to PIMOK and join airway A-576. MAINTAIN FL140 from NYLON to PIMOK.

Airport elevation.

SPEED:

266^

262^17

FL140

NOT TO SCALE

.A.576.

PIMOKN01 26.8E103 20.1

23

FL140

083^

057^

059^

097^

195^

150^

D9.4

D23.2

D24.2

D8.0

D6.9

D12.8

103^

079^

D23.6

D33.7



COMMS

COMMS

LOST

COMMS

LOST

LOST

CHANGES:

WSSS/SINCHANGI


SINJON113.5 SJSJ

N01 13.4 E103 51.3

D

TEKONG116.5 VTKVTK

N01 24.9 E104 01.3

D

10-3T

A

115^

120^

203^

180^

9

15

17

5

N01 17.5E103 58.1


N01 12.5E103 58.1

SUSIN

At or above4000'

N01 26.1E104 10.7

DOKTA

2At or above

2000'

.RNAV.SID.



A

(TOM1A)

TOKIM(SJ R-037/D20.1)(VTK R-023/D5.0)


N01 03.8 E104 13.3

4000'At or above

TOMAN ONE ALPHA

035^

089^20

83

N01 19.8E104 24.3

HOSBA

At or above7000'

TOMAN(SJ R-086/D117)

(VTK R-092/D106)N01 21.8 E105 47.3

22 NOV 13

TOMAN ONE ALPHA (TOM1A),

(RWYS 02C, 20C)


JEPPESEN

TOMAN ONE BRAVO (TOM1B) DEPARTURES


6000'

N01 29.6 E104 03.3

2000'At or above

090^

360^

3400'

2500'2100'090^

360^

3400'

2100'1900'


180^

180^

TOMAN O

NE

BRAVO

(TOM

1B)

75 100 150 200 250 300


Gnd speed-KT



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


SID 1 INITIAL CLIMB

Climb straight ahead to TOKIM, turn RIGHT and track 115^ to DOKTA,

RWY

02C

20C

then track 115^ to HOSBA. Turn LEFT and track 089^ to TOMAN.

Climb straight ahead to SUDPO, turn LEFT and track 180^ to SUSIN.Turn LEFT and track 120^ to DOBLU. Turn LEFT and track 035^ to HOSBA,then turn RIGHT and track 089^ to TOMAN.

TOM1A

TOM1B



5.0% V/V(fpm) 380 506 760 1013 1266 1519














12

1. RADAR required.





Singapore RADAR.

Apt Elev

22'

SPEED:

023^

NOT TO SCALE

097^

195^

D6.9

D12.8

083^

057^

150^

D9.4

D23.2

D24.2

103^

079^

D23.6

D33.7

053^D7.

6

COMMS COMMSLOST COMMSLOST LOST


COMMS

LOST

COMMS

LOST

LOST

COMMS

LOST

CHANGES:

WSSS/SINCHANGI

SINGAPORE, SINGAPORE10-3U .RNAV.SID.

SINJON

113.5 SJSJN01 13.4 E103 51.3

D

D

A

120^

N01 12.5E103 58.1

SUSIN

At or above4000'



A

TEKONG116.5 VTKVTK

N01 24.9 E104 01.3

15

17

(TOM1E)


N01 03.8 E104 13.3

4000'At or above

035^

20

N01 26.1E104 10.7

DOKTA

N01 19.8E104 24.3

HOSBA

At or above7000'

089^83

TOMAN(SJ R-086/D117)

(VTK R-092/D106)

203^2

At or above2000'

N01 17.9E103 57.4


172^5

115^

9

TOMAN ONE ECHO

N01 21.8 E105 47.3

JEPPESEN


22 NOV 13

TOMAN ONE ECHO (TOM1E),

(RWYS 02L, 20R)

TOPOM

(VTK R-013/D5.1)(SJ R-034/D20.0)

N01 29.9 E104 02.5

2000'At or above


6000'

TOMAN ONE FOXTROT (TOM1F) DEPARTURES090^

180^

360^

3400'

2500'2100'090^

180^

360^

3400'

2100'1900'


TOMAN O

NE

FOXTR

OT

(TOM

1F)

75 100 150 200 250 300Gnd speed-KT




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



02L

20R

TOM1E

TOM1F

Climb straight ahead to TOPOM, turn RIGHT and track 115^ to DOKTA,then track 115^ to HOSBA. Turn LEFT and track 089^ to TOMAN.

Climb straight ahead to SUNVA, turn LEFT and track 172^ to SUSIN.

then turn RIGHT and track 089^ to TOMAN.Turn LEFT and track 120^ to DOBLU. Turn LEFT and track 035^ to HOSBA,



5.0% V/V(fpm) 380 506 760 1013 1266 1519














12

1. RADAR required.

instructions by ATC shall also cross VTK 8 DME at or above 2000' between 2301-1100 UTC. If the altitude restriction cannot be complied with, the pilot-in-commandof an aircraft departing on Runway 20R shall inform ATC during the time when theaircraft commences taxiing to the holding point for departure. 4. All SIDs includenoise preferential routes. 5. Cruising levels will be issued after take-off by




Singapore RADAR.

Apt Elev

22'

SPEED:

023^

NOT TO SCALE

COMMS

LOST

COMMS

LOST

LOST

COMMS COMMSLOST COMMSLOST LOST COMMS


083^

057^

059^

097^

195^

150^D9.4

D23.2

D24.2

D8.0

D6.9

D12.8

LOST

75 100 150 200 250 300

CHANGES:

WSSS/SINCHANGI

SINGAPORE, SINGAPORE10-3V


Gnd speed-KT



126^

16

44

Rwy 20C- Departures shall be on a

.RNAV.SID.

1 ROUTING



A

DOSNO

VENPA

N00 48.0 E104 14.2

N00 21.7 E104 49.9


N01 03.8 E104 13.3







177^

(SJ R-131/D78.1)

join the ATS route.

(SJ R-138/D34.1)

KADAR

SURGA

097^

105^120^

(VTK R-161/D39.0)

(RWYS 02C, 20C)

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

JEPPESEN

[VENP1A]

[VENP1B]

VENPA1A

VENPA1B

(VTK R-142/D79.6)

131

30

87

BAVUS092^

46VENIX

S00 21.9 E106 05.4

(SJ R-125/D164)

SURGA

S00 37.0 E106 31.3

(SJ R-124/D194)

KADAR

ATKAX

N00 05.2 E106 59.8

(SJ R-110/D201)(VTK R-114/D196)

(VTK R-131/D164)

(VTK R-129/D193)

3

At or below6000'


S00 06.8E107 43.7


Turn RIGHT and track 173^ to DOBLU, then track 177^ to DOSNO.

N00 00.0 E109 00.0 TO BAVUS1213

VENPA ONE ALPHA (VENPA1A),

22 NOV 13

VENPA ONE BRAVO (VENPA1B) DEPARTURES

(SJ R-037/D20.1)TOKIM

SINJON113.5 SJSJ

N01 13.4 E103 51.3

D

TEKONG116.5 VTKVTK

N01 24.9 E104 01.3

D

A

115^173^

120^

203^

180^

922

17

5

N01 17.5E103 58.1


N01 12.5E103 58.1

SUSIN

At or above4000'

VENPA

ONE A

LPHAVENPA ONE BRAVO

(VTK R-023/D5.0)

(VEN

PA1A)

(VENPA1B)

N01 26.1E104 10.7

DOKTA

4000'At or above

2000'At or above

N01 29.6 E104 03.3

2At or above

2000'

090^

180^

360^

3400'

2500'2100'090^

180^

360^

3400'

2100'1900'


At DOSNO turn LEFT and track 126^ to VENPA and follow the appropriate transition route to




02C

20C

Climb straight ahead to TOKIM, turn RIGHT and track 115^ to DOKTA.

Climb straight ahead to SUDPO, turn LEFT and track 180^ to SUSIN. TurnLEFT and track 120^ to DOBLU, then turn RIGHT and track 177^ to DOSNO.



5.0% V/V(fpm) 380 506 760 1013 1266 1519







12

1. RADAR required.





Singapore RADAR.

Apt Elev

22'

SPEED:02

3^

NOT TO SCALE

083^

057^

097^

195^

150^D9.4

D23.2

D24.2

D6.9

D12.8

053^D7.

6

COMMS

COMMS

LOST

COMMS

LOST

LOST

COMMS COMMSLOST COMMSLOST LOST COMMS


75 100 150 200 250 300

CHANGES:

WSSS/SINCHANGI


SID

SINJON

113.5 SJSJN01 13.4 E103 51.3

D

TEKONG116.5 VTKVTK

N01 24.9 E104 01.3

D

10-3W

Gnd speed-KT

A

173^

120^

22

16

17N01 12.5E103 58.1

SUSIN

At or above4000'

N01 26.1E104 10.7

DOKTA

.RNAV.SID.

1 INITIAL CLIMB

1 ROUTING



A

177^

join the ATS route.

From DOSNO turn LEFT and track 126^ to VENPA and follow the appropriate transition route to

(VTK R-013/D5.1)

TOPOM(SJ R-034/D20.0)

N01 17.9E103 57.4


172^5

203^

115^ 9




VENPA

ONE E

CHOVENPA ONE FOXTROT

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

JEPPESEN


[VENP1E]VENPA1E

[VENP1F]VENPA1F

Turn RIGHT and track 173^ to DOBLU, then track 177^ to DOSNO.

126^44

DOSNO

VENPA

N00 48.0 E104 14.2

N00 21.7 E104 49.9

(SJ R-131/D78.1)

(SJ R-138/D34.1)

KADAR

SURGA

097^

105^120^

(VTK R-161/D39.0)

(VTK R-142/D79.6)

131

30

87

BAVUS092^

46VENIX

S00 21.9 E106 05.4

(SJ R-125/D164)

KADAR

ATKAX

N00 05.2 E106 59.8

(SJ R-110/D201)(VTK R-114/D196)

(VTK R-131/D164)

3

S00 06.8E107 43.7

At or below6000'



N01 03.8 E104 13.3

N00 00.0 E109 00.0 TO BAVUS1213

(VEN

PA1E)

(VENPA1F)

22 NOV 13

SURGA

S00 37.0 E106 31.3

(SJ R-124/D194)(VTK R-129/D193)

2000'At or above

N01 29.9 E104 02.5

2At or above

2000'

4000'At or above

090^

180^

360^

3400'

2500'2100'090^

180^

360^

3400'

2100'1900'


(RWYS 02L, 20R)

VENPA ONE ECHO (VENPA1E),VENPA ONE FOXTROT (VENPA1F) DEPARTURES


RWY

02L

20RClimb straight ahead to SUNVA, turn LEFT and track 172^ to SUSIN. Turn LEFT and track 120^ to DOBLU, then turn RIGHT and track 177^ to DOSNO.

Climb straight ahead to TOPOM, turn RIGHT and track 115^ to DOKTA.



5.0% V/V(fpm) 380 506 760 1013 1266 1519














12

1. RADAR required.

instructions by ATC shall also cross VTK 8 DME at or above 2000' between 2301-1100 UTC. If the altitude restriction cannot be complied with, the pilot-in-commandof an aircraft departing on Runway 20R shall inform ATC during the time when theaircraft commences taxiing to the holding point for departure. 4. All SIDs includenoise preferential routes. 5. Cruising levels will be issued after take-off by




Singapore RADAR.

Apt Elev

22'

SPEED:

023^

NOT TO SCALE

Apt Elev

the direction of Twy A7.

104-00103-59

Elev 14'

FOR PARKING POSITIONS

from Twy EP to Twy A7 only. No-entry signs have

Taxiway centerline lights along Twy A2 have beenshielded to provide guidance only from Twy EP in

Twy A2 is a one-way taxiway for aircraft taxiing

been mounted on either side of Twy A2 along Twy A7.

01-20 01-20

01-21

01-22

01-23stands 506, 507 and 508 diverted

Rw

y 0

2R/20LT2

SO

UTH A

PRO

N

Twy WC centerline behind aircraft

SERVICEAPRON

NORTH

SOUTH-EASTREMOTE APRON

APRON

BUDGETTERMINAL

L8

L5

L6

L7

L4

Taxiway centerline along Twy EP

Pilots are advised to applyminimum thrust when turning

T3 SOUTH APRON


1

1

JEPPESEN

SEE 10-9B & 10-9C1

aircraft stands E7 and F36.

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

between Twys B1 and B3 offseteastward by 8'

Twy N1 (behind aircraft standsC16 to C19 and between Twy NC2and Twy NC3), Twy N2 and Twy N3 (behind aircraft standsD35 to D38 and between Twy NC2and Twy NC3) can only be usedby aircraft with maximum wingspan of 213' (65m).

eastward by 8' (2.5m) away from

wingspan of 118' (36m).

into Twy WA from Taxilane V6.

Twy NC3 (between Twy WA and Twy A6)is a twy with reduced minimum separationdistances between the twy centerline andobject. Due to the reduced minimum separation distances, pilots are advised to adhere strictly to the twy centerline and to slow down the taxispeed accordingly. Twy NC3 (betweenTwy WA and Twy A6) can only be used by aircraft with a maximum wingspan of 213' (65m).

105' (32m) westward. Pilots to followthe twy centerline while taxiing alongTwy WC.

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 applyspeed limit of 20 Kts when 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.

5 JUL 13

L9

L10

Twy L5 can only be used byaircraft with maximum

Twys L8, L9, and L10 can onlybe used by aircraft withmaximum wingspan 213' (65m).Pilots are advised to exercise

L5, L8, L9 and L10.caution when taxiing near Twys

VAR 0^

Ramp area added.

oversteering may be required when

Pilots operating aircraft with wheel

shall take note that judgemental

NO

RTH

APR

ON

maneuvering around taxiway turns.

base longer than B747 or 85' (26m)

Bldg Area

N01 21.6 E103 59.4 CHANGI10-922'SINGAPORE, SINGAPORE

CHANGES:

WSSS/SIN

02L

177'

EP

Bldg Area

Elev 17'

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

C1

C2

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

20RElev 13'

243'

164'

WP

EA

EASTCARGOAPRON

WCW3

W2

W1

APRONCARGOWEST

WP

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

N1N2 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

118.252

D-ATIS

128.6

ACARS:D-ATIS

SINGAPORE Delivery (Cpt)

121.65West of Terminal 2

124.3

Ground*East of Terminal 2

121.72 0001Z-1600Z

Tower

118.6

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.

None.

5 JUL 13

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^.

11,998' 197'

197'

3657m

2930m 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


any RVR out, Adequate Vis Ref

250m (200m)

200m (150m) 250m

300m

Low-level wind shear alert system.

3662m

3662m12,014'12,014'

other two required

2

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

3260m 9613'

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

175m175m

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

D47

D48 D

49

400

401402

404

403

W4

NC2

NC2

NC1

NC1

NC3

NC3

N1

N3

NC3

NC1

NC2

EAWC

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 N

ORTH

APRO

N

T3 S

OUTH

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

25 OCT 13

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

202L and 202R added.

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

1

1 For Parking Positions see 10-9C1.

25 OCT 13

202L and 202R added.

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 59.3N01 20.5 E103 59.2103, 104

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 59.5N01 21.6 E103 59.5E27, E28

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

F34 thru F36

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 59.8N01 21.9 E103 59.8

N01 21.7 E103 59.6D41, D42, D44D46

D47, D48

N01 21.6 E103 59.5

D49

D40

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 59.5

T3 North Apron

N01 22.0 E103 59.4C24C25

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 South 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

509 N01 22.7 E103 59.6

505

506

504

503

502

507

508

509

604

603

602

601

606 607

609

JEPPESEN


103 104

12

3456

789

10

E8

L9

L5

L7

L6

L4

SC2 SC2

EP

EP

E7

E6

SC1

E9

EPC7C6

SC1

EA

EA

NC1NC1NC1

NC2 NC2N1 N3

WP

WP

W3

W4

V3

V4

WC

WC

WA

5 JUL 13

EC

611

612

14

131211

L8

L10

101R

101 102

102L

102R

101L

South-East Remote Apron revised, parking spots added.

RWY 0

2L-2

0R

RWY 0

2C-2

0C

CHANGISINGAPORE, SINGAPORE

CHANGES:

WSSS/SIN

West Cargo Apron

503, 504505, 506507, 508

N01 22.4 E103 59.6N01 22.5 E103 59.6N01 22.6 E103 59.6

N01 22.4 E103 59.5502

East Service Apron

606607609

N01 22.2 E103 59.9N01 22.1 E103 59.9N01 22.2 E103 59.9

603601, 602

604

N01 22.3 E103 59.8N01 22.4 E103 59.8N01 22.4 E103 59.9

East Cargo Apron

SERVICEAPRON

EASTCARGOAPRON

APRONCARGOWEST

NORTH

SERVICEAPRON

EAST

10-9C1


COORDINATESBAY No. BAY No. COORDINATES

TERMINALAPRON

BUDGET


BAY No.

Budget Terminal Apron

31, 2

N01 20.6 E103 59.1

COORDINATES

N01 20.4 E103 59.24 thru 67 thru 11

N01 20.5 E103 59.2

N01 20.4 E103 59.1N01 20.3 E103 59.1

South-East Remote Apron

N01 22.4 E104 00.0611, 612

N01 20.2 E103 59.1N01 20.2 E103 59.0

12, 1314

N01 20.6 E103 59.1N01 20.5 E103 59.2103, 104

101, 101L, 101R102, 102L, 102R

JEPPESEN


5 JUL 13

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 ChangiControl Tower using the Taxiway Lighting Control Panel (TLCP).

Route Selection and Priority

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

centerline lights on the maneuvering area are switched on automatically. When two or

more 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.

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

holding positions where, by default, red stopbar lights remain on unless deselected bythe runway controller. When deselected, these stopbar lights will re-activate automatically after 50 seconds.

When following the directional guidance provided by the green taxiway centerlinelights 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: None.

Information and Mandatory Signs/Markings

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

CHANGISINGAPORE, SINGAPOREWSSS/SIN

10-9C2



WSSS/SIN JEPPESEN+

ADVANCED- SURFACE MOVEMENT GUIDANCE AND CONTROL SYSTEM

(A-SMGCS)- MULTILATERATION SYSTEM DEPLOYMENT AT SINGAPORE CHANGI AIRPORT

1 Introduction

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

2 Carriage of Mode-S SSR Transponder

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

3 Multilateration System Outline

3.1 The Multilateration System uses multiple receivers to pick up ‘‘squitters’’ transmitted by aircraft or vehicle Mode S transponders. It calculates the position of an aircraft or a vehicle by comparing the time its ‘‘squitter’’ arrives at each receiver.

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

4 Aircraft Requirements

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

4.2 For the Multilateration System to work effectively, all aircraft Mode S transponders need to transmit Mode S squitters at all times when moving on the airfield, starting immediately prior to pushback, and for arrival aircraft until they are stationary at the aircraft stands. The Mode S transponders should not respond to All-Call interrogations, but should respond to addressed interrogations.

10-9C330 APR 10



WSSS/SIN JEPPESEN+

5 Procedures / Actions Required By Pilots

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

5.2 Pre-Push back / Taxi

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

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

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

5.3 After Landing

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

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

10-9C430 APR 10

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

Note removed.

22 NOV 13

WSSS/SINJEPPESEN

10-9ESINGAPORE, SINGAPORE

CHANGI

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

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 clearance

even though the 5 minutes grace period would have been exceeded.

DELAY DUE TO OVERFLIGHTS

These are flights operating through Singapore FIR without landing at 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 frequencyor to monitor Singapore Ground Control (frequencies 124.3 or 121.72). It should be noted that when instructed to monitor Singapore Ground frequencies, pilots shall not establish contact with the Singapore Ground Control, rather, pilots shall maintain a

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

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

22 NOV 13

None.

JEPPESEN

WSSS/SIN 10-9E1SINGAPORE, SINGAPORE

CHANGI

CHANGES:

6 JUL 12

GROUND MOVEMENT CONTROL ON 124.3

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 listen out on the Ground Movement Control frequency on 124.3.

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.

2. Change from Ground Movement Control frequency to the Runway Control frequency (118.6) when nearing the taxiway holding position.

3. Request for take-off clearance on 118.6.

d. The pilot-in-command stopping for a pre-flight check at the taxiway holding position shall change over from 124.3 to 118.6 and request for further clearance before recommencing taxiing.

e. Departing aircraft will be instructed when to change from 118.6 to Singapore Approach frequency of 120.3.

f. In the case of the aircraft having landed, the pilot-in-command shall change from 118.6to 124.3 immediately after clearing the runway. He shall maintain watch on 124.3 for

taxiing and parking instructions until he arrives at his aircraft stand.

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.

| JEPPESEN, 2012. ALL RIGHTS RESERVED.

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

Text.


WSSS/SIN JEPPESEN+

PROCEDURES FOR START-UP AND PUSHBACK OF AIRCRAFT1. Ground crew must ensure that the area behind an aircraft is clear of vehicles, equip-

ment and other obstructions before the start-up or pushback of aircraft commences.

2. When the pilot is ready for start-up and pushback, he/she shall seek confirmationfrom the ground crew that there is no hazard to the aircraft starting up. The pilotshall then notify the Ground Movement Controller (Callsign: Singapore Ground) thatthe aircraft is ready for pushback. On being informed by Singapore Ground that push-back is approved, the pilot shall coordinate with the ground crew for the start-up andpushback of the aircraft.

3. The following table describes the procedures for the pushback of aircraft from thevarious aircraft stands. When it becomes necessary to vary a procedure to expediteaircraft movements, Singapore Ground will issue specific instructions to the pilot.

APRON/ACFT STANDS PUSHBACK PROCEDURES

PHRASEOLOGY USED BY SINGAPORE

GROUND

T3 WEST

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

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

Standard pushback approved.

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

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


A3 The aircraft (on idle thrust) shall be pushed back onto TWY WA until its nosewheel is at the intersection of the aircraft stand lead-in line and TWY WA centerline. The aircraft may breakaway from there.

Pushback approved, to face North (or South).

A4 The aircraft (on idle thrust) shall be pushed back onto TWY WA to face North (or South) such that the pushback line is always kept midway between the aircraft main gear until its nosewheel is at TWY WA centerline. The aircraft may breakaway from there.


10-9F


12 JUN 09

JEPPESEN

WSSS/SIN SINGAPORE, SINGAPORECHANGI

CHANGES:

10-9F-0

GATE HOLD PROCEDURES

1. Whenever there are about five to seven departing aircraft at the runwayholding point, subsequent push-backs of departures will be regulated such thatthe Ground Movement Planner (GMP) on VHF frequency 121.65 will start toissue pilots with Expected Pushback Time (EPT). The determination of EPT will take into account an aircraft's parking bay as well as taxi time to the runway-in-use holding point.

2. When an Expected Pushback Time (EPT) is issued, pilots will be instructedto either remain on Ground Movement Planner (GMP) frequency or to monitor

Singapore Ground Control (frequencies 124.3 or 121.72). It should be notedthat when instructed to monitor Singapore Ground frequencies, pilots shall not establish contact with the Singapore Ground Control, rather, pilots shall maintain a listening watch on the assigned Signapore Ground Control

frequency congestion.

3. A flight issued with an Expected Pushback Time (EPT) but chooses tocommence 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.

MAXIMIZING GATE AND RUNWAY UTILIZATION

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

assigned to an arriving aircraft, the departing aircraft will be instructed bythe Ground Movement Planner (GMP) to contact Signapore Ground for pushback for the purpose of better gate utilization.

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


frequency and await for pushback instruction. This is to prevent unnecessary

8 JUN 12

Introduction paragraph removed.

GATE HOLD PROCEDURES FOR DEPARTING AIRCRAFT


WSSS/SIN JEPPESEN+

A5, A9 The aircraft (on idle thrust) shall be pushed back onto TWY U2 to face North such that the pushback line is always kept midway between the aircraft main gear until the nose of the aircraft is behind the stopbar behind aircraft stand A11. The aircraft may breakaway from there. ORThe aircraft (on idle thrust) shall be pushed back onto TWY WA to face South until nose of the aircraft is behind the stopbar behind aircraft stand A4. The aircraft may breakaway from there.

Pushback approved, to face North.

Pushback approved, to face South.

A10 The aircraft (on idle thrust) shall be pushed back onto TWY U2 to face North until the nose of the aircraft is behind the stopbar behind aircraft stand A11. The aircraft may breakaway from there. ORThe aircraft (on idle thrust) shall be pushed back onto TWY WA to face South until the nose of the aircraft is behind the stopbar behind aircraft stand A4. The aircraft may breakaway from there.



A11 The aircraft (on idle thrust) shall be pushed back onto TWY U2 to face North until the nose of the aircraft is at the intersection of the aircraft stand lead-in line and TWY U2 centerline. The aircraft shall then be towed forward until the nose of the aircraft is behind the stopbar behind aircraft stand A11. The aircraft may breakaway from there. ORThe aircraft (on idle thrust) shall be pushed back onto TWY U2 to face South until the nose of the aircraft is at the intersection of the aircraft stand lead-in line and TWY U2 centerline. The aircraft shall then be towed forward until its nosewheel is behind the stopbar behind aircraft stand A12. The aircraft may breakaway from there.



A12 The aircraft (on idle thrust) shall be pushed back onto TWY U2 to face North until the nose of the aircraft is at the intersection of the aircraft stand lead-in line and TWY U2 centerline. The aircraft shall then be towed forward until its nosewheel is behind the stopbar behind aircraft stand 11. The aircraft may breakaway from there. ORThe aircraft (on idle thrust) shall be pushed back onto TWY U2 to face South until its nosewheel is at the intersection of the aircraft stand lead-in line and TWY U2 centerline. The aircraft may breakaway from there.



A13, A14, A15

The aircraft (on idle thrust) shall be pushed back onto TWY WA to face North until the nose of the aircraft is behind the stopbar behind aircraft stand A16. The aircraft may breakaway from there. ORThe aircraft (on idle thrust) shall be pushed back onto TWY U2 to face South until the nose of the aircraft is behind the stopbar behind aircraft stand A12. The aircraft may breakaway from there.

Pushback approved to face North.


A16 The aircraft (on idle thrust) shall be pushed back onto TWY WA until its nosewheel is at the intersection of the aircraft stand lead-in line and TWY WA centerline. The aircraft may breakaway from there.

Pushback approved to face North(or South).



GROUND

10-9G


12 JUN 09


WSSS/SIN JEPPESEN+

A17 Pushback facing WestThe aircraft (on idle thrust) shall be pushed back onto Taxiway V8 to face West until its nosewheel is at the "END OF PUSH" position behind aircraft stand A17. The aircraft may breakaway from there.Pushback facing SouthThe aircraft (on idle thrust) shall be pushed back onto TWY WA to face South until the nose of the aircraft is behind the stopbar behind aircraft stand A16. The aircraft may breakaway from there.

Pushback approved to face West.

Pushback approved to face South.

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


A19 The aircraft (on idle thrust) shall be pushed back onto Taxiway U4 to face West such that the pushback line is always kept midway between the aircraft main gear until its main gear is aligned with the centerline of Taxiway U4 and the nose of the aircraft is behind the stopbar behind the "END OF PUSH" line. The aircraft may breakaway from there. Pushback to face East is not permitted.


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


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


B1 The aircraft shall be pushed back onto Taxilane V6 to face West such that the pushback line is always kept midway between the aircraft main gear until its nosewheel is at the "END OF PUSH (for B1 nose gear)" position. The aircraft shall then be towed forward along the pushback line until its nosewheel is at the "END OF TOW (for A1, A2, B1, B2)" position. The aircraft may breakaway from there. Engine startup is not permitted during standard pushback.Alternate PushbackThe aircraft (on idle thrust) shall be pushed back onto Taxilane V6 to face East, followed by TWY WA, such that the alternate pushback line is always kept midway between the aircraft main gear until the nose of the aircraft is behind the stopbar behind aircraft stand A3 or B2. The aircraft may breakaway from there. This alternate pushback procedure can only be exercised if the auxiliary power unit of aircraft is unserviceable.


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



GROUND

10-9H


12 JUN 09


WSSS/SIN JEPPESEN+

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


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


B4 The aircraft (on idle thrust) shall be pushed back onto TWY WA to face North (or South) such that the pushback line is always kept midway between the aircraft main gear until its nosewheel is at TWY WA centerline. The aircraft may breakaway from there.


B5, B6 The aircraft (on idle thrust) shall be pushed back onto TWY WA to face North until the nose of the aircraft is behind the stopbar behind aircraft stand B4. The aircraft may breakaway from there. ORThe aircraft (on idle thrust) shall be pushed back onto TWY U1 to face South such that the pushback line is always kept midway between the aircraft main gear until the nose of the aircraft is behind the stopbar behind aircraft stand B7. The aircraft may breakaway from there.



B7 The aircraft (on idle thrust) shall be pushed back onto TWY U1 to face South until the nose of the aircraft is behind the stopbar behind aircraft stand B7. The aircraft may breakaway from there. ORThe aircraft (on idle thrust) shall be pushed back onto TWY WA to face North until the nose of the aircraft is behind the stopbar behind aircraft stand B4. The aircraft may breakaway from there.



B8 The aircraft (on idle thrust) shall be pushed back onto TWY U1 to face South until its nosewheel is at the intersection of the aircraft stand lead-in line and TWY U1 centerline. The aircraft may breakaway from there. ORThe aircraft (on idle thrust) shall be pushed back onto TWY U1 to face North until its nosewheel is at the intersection of the lead-in line and TWY U1 centerline. The aircraft shall then be towed forward until its nosewheel is at the intersection of the aircraft stand B9 lead-in line and Twy U1 centerline. The aircraft may breakaway from there.



B9, B10 The aircraft (on idle thrust) shall be pushed back onto TWY U1 until its nosewheel is at the intersection of the aircraft stand lead-in line and TWY U1 centerline. The aircraft may breakaway from there.

Pushback approved to face North (or South).



GROUND

10-9J


12 JUN 09


JEPPESEN

200, 201, The aircraft (on idle thrust) shall be pushed back onto Twy C6 to face North (or South).

Pushback approved,to face North (orSouth).

The aircraft (on idle thrust) shall be pushed back

205, 206,207, 208

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



103, 104

209face North (or South) until its nose wheel is at the intersection of the lead-in line and Twy C7 centerline.


301, 304,

300, 303facing West until its nose wheel is at the intersection of the lead-in line and taxiway centerline.

The aircraft (on idle thrust) shall be pushed back facing East until its nose wheel is at the intersection of the lead-in line and taxiway centerline.

OR

Pushback approved,to face West.

Pushback approved,to face East.

305The aircraft (on idle thrust) shall be pushed back toface East (or West) until its nose wheel is at the

centerline.intersection of the lead-in line and the taxiway

Pushback approved,to face East (orWest).

302, 306

of the lead-in line and taxiway centerline.

OR

Pushback approved,to face East.


The aircraft (on idle thrust) shall be pushed back toface East until its nose wheel is at the intersection

The aircraft (on idle thrust) shall be pushed back toface West until its nose wheel is at the intersection of the lead-in line and Twy A6 centerline.

307, 308, The aircraft (on idle thrust) shall be pushed back toface East (or West) until its nose wheel is at the

centerline.

Pushback approved,to face East (orWest).

309, 310

intersection of the lead-in line and Twy NC2

503, 504,

400, 401

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

402, 403404

The aircraft (on idle thrust) shall be pushed back toface North (or South) until its nose wheel is at theintersection of the lead-in line and Twy A6 centerline.


The aircraft (on idle thrust) shall be pushed back to Pushback approved,to face North (orSouth).

502face North (or South). The aircraft may breakaway from here. There shall be no simultaneous pushbackof aircraft unless with two aircraft stands separation.

505, 506 face North (or South).Pushback approved,to face North (orSouth).


The aircraft (on idle thrust) shall be pushed back 200Lonto Twy C6 centerline to face North until its

200L. The acft may breakaway from there.nosewheel is on the end of push behind acft stand

Pushback approved,to face North.

ORThe aircraft (on idle thrust) shall be pushed back Pushback approved,

to face South.onto Twy C6 centerline to face South.

The aircraft (on idle thrust) shall be pushed back Pushback approved,to face North (orSouth).

onto Twy C6 centerline to face North (or South).

202, 203

200R, 202L202R

onto Twy L4 centerline to face East until the aircraft

3 JAN 14

The aircraft may break away from there.

Standard pushback approved

nose is behind the stopbar behind aircraft stand 102.


10-9KWSSS/SIN

APRON/ACFTSTANDS

PUSHBACK PROCEDURESPHRASEOLOGY USED

BY SINGAPOREGROUND

EAST REMOTE

SOUTH-EAST REMOTE

NORTH REMOTE

NORTH-EAST REMOTE

WEST CARGO


JEPPESEN

509 Standard pushbackapproved.

face South until its nose wheel is at the intersectionStandard pushbackapproved.

603face South until its nose wheel is at the intersection

Standard pushbackapproved.



face South until its nose wheel is at the intersectionThe aircraft (on idle thrust) shall be pushed back to

of the pushback line and Twy WC centerline.

601, 602

aircraft shall then be towed forward along the

"END OF TOW" marking behind aircraft stand 602.

604 Standard pushbackapproved.

The aircraft (on idle thrust) shall be pushed back to face South until its nose wheel is at the positionof "END OF PUSH". The aircraft shall then be towed

nose wheel is on the "END OF TOW" marking behind aircraft stand 602.


C1, C20,C22, C23,C24, C25

The aircraft (on idle thrust) shall be pushed backonto Twy U1 to face North (or South).

C26

ORThe aircraft (on idle thrust) shall be pushed back Pushback approved,

to face South.

The aircraft (on idle thrust) shall be pushed back onto Twy WA to face North. The aircraft may breakaway from there.

onto Twy WA to face South until its nose wheel is at the intersection of the aircraft stand lead-in line

The aircraft (on idle thrust) shall be pushed backC11such that the pushback line is always kept midway between the aircraft main gear until the nose wheel of the aircraft is at the "EOP 21" position. The aircraft shall then be towed forward until its nose wheel is at the "EOT 22A" position.


of the lead-in line and taxilane EA centerline.

of the lead-in line and taxilane EA centerline. The

centerline of taxilane EA until its nose wheel is on the

forward along the centerline of taxilane EA until its



611, 612

towed forward along the centerline of the taxilane EC and turn left onto the centerline of taxilane EA until its nose wheel is at the "END OF TOW" marking behind aircraft stand 602.

The aircraft shall be pushed back to face North untilits nosewheel is at the "END OF PUSH" position.The aircraft shall then be towed forward along thecenterline of taxilane EC and turn Left onto thecenterline of taxilane EA until its nosewheel is onthe "END OF TOW" marking behind stand 602. Theaircraft may breakaway from there. Engine start upis not permitted during standard push back.

ORThe aircraft shall be pushed back to face North untilits nosewheel is at the "END OF PUSH" position.Engine start up is permitted only on the port engine.The aircraft shall then be towed forward along thecenterline of taxilane EC and turn Left onto thecenterline of taxilane EA until its nosewheel is on the"END OF TOW" marking behind stand 602. Theaircraft may breakaway from there. This alternatepushback 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 to Standard pushbackapproved.

507, 508face South.

3 JAN 14 CHANGISINGAPORE, SINGAPORE

10-9LWSSS/SIN

APRON/ACFTSTANDS


BY SINGAPOREGROUND

EAST CARGO

T1 WEST

T1 CENTRAL

JEPPESEN


8 JUN 12

C13

OR

The aircraft (on idle thrust) shall be pushed back to face North such that the pushback line is always kept midway between the aircraft main gear until its nose wheel is at the "END OF PUSH (Stopbar 22)" position. The aircraft shall be towed forward until its nose wheel is at the "END OF TOW (Stopbar 22A)" position.


Alternate Pushback ProcedureThe aircraft (on idle thrust) shall be pushed back

ORAlternate Pushback Procedure

onto Twy N2 to face South followed by Twy N3 until the nose of the aircraft is behind the stopbar line

The aircraft (on idle thrust) shall be pushed back onto Twy N2 to face South followed by Twy N1 until the nose of the aircraft is behind the stopbar line

Pushback approved,onto Twy N3 toface South.


behind the aircraft stand D35. The aircraft may break away from there.

behind the aircraft stand C16. The aircraft may break away from there.

D32

OR

The aircraft (on idle thrust) shall be pushed back to face North such that the pushback line is always kept midway between the aircraft main gear until its nose wheel is at the "END OF PUSH (Stopbar 22)" position. The aircraft shall be towed forward until its nose wheel is at the "END OF TOW (Stopbar 22A)" position.










OR

The aircraft (on idle thrust) shall be pushed back Standard pushbackapproved.









facing North until its nose wheel is at the intersection of the lead-in line and Twy N2 centerline.

C15, D34

C16, C17face North (or South) until its nose wheel is at the




C18to face North until its nose wheel is at the intersection of the lead-in line and Twy N1 centerline.



C19to face North along Twy N1 until the "END OF PUSHBACK" position.


intersection of the lead-in line and Twy N1 centerline.


10-9L1WSSS/SIN

APRON/ACFTSTANDS


BY SINGAPOREGROUND

JEPPESEN


8 JUN 12

The aircraft (on idle thrust) shall be pushed back to D40, D41,D42, D44,D46, D47,D48, D49

face North (or South) until its nose wheel is at the

centerline.intersection of the lead-in line and Twy A6


E1 The aircraft (on idle thrust) shall be pushed back such that the pushback line is always kept midway between the aircraft main gear until its nose wheel is at Stopbar 12. This is marked as "END OF PUSHBACK" on the ground. The aircraft shall then be towed forward to Stopbar 9. this is marked as "END OF TOW" on the ground.


The aircraft (on idle thrust) shall be pushed back such that the pushback line is always kept midway between the aircraft main gear until its nose wheel


D30

of the aircraft is at the "END OF PUSH (Stopbar 20)"position. the aircraft shall then be towed forwarduntil its nose wheel is at the "END OF TOW (Stopbar 22A)" position.

D35, D36 The aircraft (on idle thrust) shall be pushed backto face North (or South) until its nose wheel is atthe intersection of the lead-in line and Twy N3centerline.


D37face North until its nose wheel is at the intersectionof the lead-in line and Twy N3 centerline.



D38face North along Twy N3 until the "END OF PUSHBACK" position.

E2 The aircraft (on idle thrust) shall be pushed back Standard pushbackapproved.until its nose wheel is at the intersection of the

lead-in line and Twy B2 centerline. The aircraft shall then be towed forward to Stopbar 9. This is marked as "END OF TOW" on the ground.

E3 The aircraft (on idle thrust) shall be pushed back Standard pushbackapproved.until its nose wheel is at Stopbar 9. This is marked

as "END OF TOW" on the ground.

E4 The aircraft (on idle thrust) shall be pushed back Standard pushbackapproved.

OR

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


Pushback approved,to pushback ontoTwy B3.



E7 The aircraft (on idle thrust) shall be pushed back Standard pushbackapproved.until its nose wheel is at Stopbar 13. This is marked

as "END OF TOW" on the ground.

E5, E6until its nose wheel is at the intersection of the lead-in line and Twy B1 centerline. The aircraft shall then be towed forward to Stopbar 13. This is marked as "END OF TOW" on the ground.

until its nose wheel is at "END OF PUSHBACK" 8 position.

onto Twy B1 until its nose wheel is at "END OFPUSHBACK" 13A position.

onto Twy B3 until its nose wheel is at "END OF

PUSHBACK" 7A position.


10-9L2WSSS/SIN

APRON/ACFTSTANDS


BY SINGAPOREGROUND

T1 EAST

T2 CENTRAL


JEPPESEN

F30 Standard pushbackapproved.




1 FEB 13

The aircraft (on idle thrust) shall be pushed back such that the pushback line is always kept midway in between the aircraft main gear until its nose wheel is at Stopbar 11. This is marked as "END OF PUSHBACK" on the ground. The aircraft shall then betowed forward to Stopbar 9. This is marked as "END OF TOW" on the ground.

The aircraft (on idle thrust) shall be pushed back until its nose wheel is at Stopbar 10. This is marked as "END OF PUSHBACK" on the ground. The aircraft shall then be towed forward to Stopbar 9. This is marked as "END OF TOW" on the ground.


The aircraft (on idle thrust) shall be pushed back until its nose wheel is at Stopbar 9. This is marked

The aircraft (on idle thrust) shall be pushed back Standard pushbackapproved.until its nose wheel is at Stopbar 8. This is marked

ORThe aircraft (on idle thrust) shall be pushed back

ORThe aircraft (on idle thrust) shall be pushed back



F33

as "END OF PUSHBACK" on the ground.

as "END OF PUSHBACK" on the ground.

onto Twy B1 until its nose wheel is at Stopbar 13A.

onto Twy B3 until its nose wheel is at Stopbar 7A.

F34, F35 The aircraft (on idle thrust) shall be pushed backuntil its nose wheel is at the intersection of the lead-in line and Twy B3 centerline. The aircraft shall then be towed forward to Stopbar 7. This is marked as "END OF TOW" on the ground.

The aircraft (on idle thrust) shall be pushed back until its nose wheel is at Stopbar 7. This is marked as "END OF PUSHBACK" on the ground.

The aircraft (on idle thrust) shall be pushed back until its nose wheel is at Stopbar 14. This is marked as "END OF PUSHBACK" on the ground. The aircraft

marked as "END OF TOW" on the ground.


E8

shall then be towed forward to Stopbar 15. This is


E10

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

OR

OR

E11- with the main gear mid-point following the main gear pushback line onto Twy A6 centerline. The aircraft shall then be towed forward to Stopbar 16 on Twy A5. This is marked as "END OF TOW" on theground.

- with the main gear mid-point following the main gear pushback line until its body is aligned with Twy A6 centerline.

Pushback approved,onto Twy A6.

Alternate Pushback Procedure for aircraft wingspanof more than 213ft (65M):The aircraft (on idle thrust) shall be pushed backwith the main gear mid-point following the main gear pushback line until its nose wheel is at the "END OF PUSH 19A" position behind aircraft Stand E24. The aircraft shall then be towed forward to"END OF TOW 18B" behind aircraft Stand E26.

Pushback approved,onto Twy A6.

with the main gear mid-point following the pushbackline until its nose wheel is at position EOP 19.


10-9L3WSSS/SIN

APRON/ACFTSTANDS


BY SINGAPOREGROUND

T2 NORTH


JEPPESEN


1 FEB 13

E12

OR

The aircraft (on idle thrust) shall be pushed back:- until its nose wheel is at the intersection of the lead-in line and Twy A5 centerline. The aircraft shallthen be towed forward to Stopbar 16. This is marked as "END OF TOW" on the ground.

- onto Twy A6 until its nose wheel is at the intersection of Twy A5 and A6 centerline.

Pushback approved,to pushback ontoTwy A6.

E20 Standard pushbackapproved.

The aircraft (on idle thrust) shall be pushed backwith the main gear mid-point following the main gear pushback line until its nose wheel is at Stopbar 17. The aircraft shall then be towed forward to "END OF TOW" Stopbar 18A. Aircraft may breakaway from here.

E22 Standard pushbackapproved.

The aircraft (on idle thrust) shall be pushed backwith the main gear mid-point following the main gear pushback line until its nose wheel is at Stopbar 19. This is marked as "END OF PUSHBACK" on the ground. The aircraft shall then be towed forward to

ground.Stopbar 18. This is marked as "END OF TOW" on the


E26 The aircraft (on idle thrust) shall be pushed back to face North until its body is aligned with Twy A6 centerline.


E27, E28face North (or South) until its body is aligned with Twy A6 centerline.



OR

F37 The aircraft (on idle thrust) shall be pushed backwith the main gear following the main gear pushback

"END OF TOW (EOP)" Stopbar 4 behind aircraft Stand F42.

The aircraft (on idle thrust) shall be pushed backwith the main gear following the main gear pushback

gear pushback line, until its nose wheel is on the

gear pushback line, until its nose wheel is on the"END OF TOW (EOP)" Stopbar 5 on Twy C1.

Pushback approved,to face East onTwy C1

The aircraft (on idle thrust) shall be pushed back until its nose wheel is at Stopbar 2. This is marked as "END OF PUSHBACK" on the ground. The aircraft shall then be towed forward to Stopbar 3. This is marked as "END OF TOW" on the ground.

F40, F52 Standard pushbackapproved.

OR

lead-in line and Twy C2 centerline. The aircraft shallthen be towed forward to Stopbar 4. This is marked

Pushback approved,to pushback ontoTwy C6.


F41, F42 The aircraft (on idle thrust) shall be pushed backuntil its nose wheel is at the intersection of the

as "END OF TOW 4" on the ground.

The aircraft (on idle thrust) shall be pushed backonto Twy C6 until its nose wheel is at the intersection of Twy C2 and Twy C6 centerline.

ORAlternate Pushback Procedure for aircraft wingspanof more than 213ft (65M):The aircraft (on idle thrust) shall be pushed back

F42 Pushback approved,to pushback ontoTwy C6.

until its nose wheel is at the "END OF PUSH 4A" position. The aircraft shall then be towed forward towith its nose wheel following the towed forward line until its nose wheel is on the "END OF TOW 4B" position behind aircraft Stand F59.

E24, E24L/Rfacing North until its body is aligned with Twy A6centerline. Aircraft may breakaway from there.


10-9L4WSSS/SIN

APRON/ACFTSTANDS


BY SINGAPOREGROUND

T2 SOUTH


JEPPESEN

F50 The aircraft shall be pushed back with the main gearfollowing the main gear pushback line, facing Southuntil its nosewheel is on the "END OF PUSH" Stopbar1 marking painted on the ground behind aircraft standF50. The aircraft shall then be towed forward withthe nosewheel following the tow-forward line untilits nosewheel is on the "END OF TOW" Stopbar 3marking painted on the ground behind aircraft stand F52.


F52Lface South until its nosewheel is at the intersectionof the aircraft push back line and Taxilane C6.


F52Rface South until its nosewheel is at the intersectionof the aircraft push back line and Taxilane C6. The

nosewheel is on the "END OF TOW" position.


F54 The aircraft (on idle thrust) shall be pushed backuntil its nosewheel is at a point on Twy C6 inline with the mid-point of aircraft stands F52 andF54. It shall breakaway from this position.




1, 2 The aircraft (on idle thrust) shall be pushed back to face West onto Twy L7 until its nosewheel is at thestopbar marked "END OF PUSH" behind aircraft stand2. The aircraft may breakaway from there.

ORThe aircraft (on idle thrust) shall be pushed backonto Twy L5 to face North until its nosewheel isbehind the stopbar behind aircraft stand 3. The

Pushback from aircraft stands 1 and 2 to face Southis not permitted.



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

The aircraft (on idle thrust) shall be pushed backonto Twy L5 to face North or South until itsnosewheel is at the intersection of the aircraft standlead-in line and the centerline of Twy L5. Theaircraft may breakaway from there. There shall beno simultaneous pushback of aircraft unless thereis at least one aircraft stand separation.



face North (or South), on Twy C6 centerline.


aircraft shall then be towed forward until its

11,12,13 The aircraft (on idle thrust) shall be pushed backonto Twy L5 to face North or South until itsnosewheel is at the "END OF PUSH (EOP)" positionand the centerline of Twy L5. The aircraft maybreakaway from there. There shall be no simultaneouspushback of aircraft unless there is at least one

Pushback approved,to face North or South.

aircraft stand separation.

14 The aircraft (on idle thrust) shall be pushed back Pushback approved,to face North.

unless there is at least one aircraft stand separation.

onto Twy L5 to face North until its nosewheel is atthe "END OF PUSH (EOP)" position and the centerlineof Twy L5. The aircraft may breakaway from there.There shall be no simultaneous pushback of aircraft

Pushback approved,to face North (or South).

Simultaneous pushback is not permitted for aircraft stands 1, 2 and 3.

aircraft may breakaway from there. Simultaneouspushback is not permitted for aircraft stands1, 2 and 3.

Simultaneous pushback is not permitted for aircraftstands 1, 2 and 3.

15 FEB 13


F56, F56L,F56R to face South until its nosewheel is at the

OR

The aircraft (on idle thrust) shall be pushed back Pushback approved,to face South.

nosewheel is abeam stand F56.

F58, F60

F59, F59L,

F59R

intersection of the aircraft pushback line and taxilane C6. The aircraft shall then be towed forward until its

face North on taxilane C6 centerline until its nosewheel is abeam Bay F60.

to face South on taxilane C6 centerline.

Pushback procedures for F56 and F59 aircraft stands.


10-9L5

CHANGES:

WSSS/SIN

APRON/ACFTSTANDS

PUSHBACK PROCEDURES PHRASEOLOGY USEDBY SINGAPORE

GROUND

BUDGET TERMINAL

Apt ElevJEPPESEN

AERO

DRO

ME A

DVIS

ORY C

HA

RT

Adv

isor

y

Air

craf

t ta

xiin

g on

Tw

y W

A a

re n

otcl

ear

of a

ircr

aft

push

back

fro

m a

ircr

aft

stan

ds A

9, A

10,

A13

, A

14,

A15

, A

16 &

A17

unti

l at

end

of

push

back

.

Adv

isor

y

Air

craf

t ta

xiin

g on

Tw

y W

A a

re n

otcl

ear

of a

ircr

aft

push

back

fro

m a

ircr

aft

unti

l at

end

of

push

back

.

Adv

isor

y

Air

craf

t ta

xiin

g on

Tw

y W

A a

re n

otcl

ear

of a

ircr

aft

push

back

fro

m a

ircr

aft

Adv

isor

y

clea

r of

air

craf

t pu

shba

ck f

rom

air

craf

tA

dvis

ory

Air

craf

t ta

xiin

g on

Tw

y EP

are

not

clea

r of

air

craf

t pu

shba

ck f

rom

air

craf

t

unti

l at

end

of

push

back

.

Adv

isor

y

Air

craf

t ta

xiin

g on

Tw

y C1

are

not

clea

r of

air

craf

t pu

shba

ck f

rom

air

craf

t

Adv

isor

y

clea

r of

air

craf

t pu

shba

ck f

rom

air

craf

tst

ands

A2,

A3,

A4,

A5,

B2,

B4,

B5

& B

6

of p

ushb

ack.

stan

ds C

24,

C25

& C

26 u

ntil

at

end

Air

craf

t ta

xiin

g on

Tw

y N

C3

are

not

stan

d C26

unt

il a

t en

d of

pus

hbac

k.

stan

ds F

37 &

F42

unt

il a

t en

d of

pus

hbac

k.st

ands

E6/

F35

(Cod

e E)

& E

7/F3

6

Air

craf

t ta

xiin

g on

Tw

y N

C3

are

not

Rwy

02L/

20R

Rwy

02C/2

0C

stan

d D

49 u

ntil

at

end

of p

ushb

ack.

None. | JEPPESEN, 2009, 2013. ALL RIGHTS RESERVED.

15 FEB 13N01 21.6 E103 59.4 CHANGI22'


CHANGES:

WSSS/SIN10-9L6

JEPPESEN

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

F32F31

F30

E1 E2 E3

E4

11

10

9 8

7

5

4

32

1

12

3A

7A

T2 C

ENTR

AL

APR

ON

T2 S

OUTH

APR

ON

C2

13A

F52L

F52R

8 JUN 12

SOUT

H E

AST

PIE

R

TERM

INA

L 2

CHANGES:


10-9L7

PUSHBACK PROCEDURES

WSSS/SIN

| JEPPESEN, 2008, 2012. ALL RIGHTS RESERVED.Pushback and tow forward lines behind F33 and E4 revised.

JEPPESEN

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

APRO

N

EP

7A

B1

B3

B2

E4

A5

A4

A3 E3

13

13A

8 JUN 12

NO

RTH

EAST

PIE

R

TERM

INA

L 2

CHANGES:


10-9L8

PUSHBACK PROCEDURES

WSSS/SIN

| JEPPESEN, 2008, 2012. ALL RIGHTS RESERVED.Pushback and tow forward lines behind F33 and E4 revised.

JEPPESEN

WSSS/SIN 10-9M SINGAPORE, SINGAPORECHANGI

.PARKING.


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 recognize 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

B7673. DOCKING PROCEDURES

3.2 Follow the lead-in line.

B767

B7679M

automatic aircraft docking guidance system installed at the fixed gates in

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

CHANGES: Text, graphic.

23 DEC 11

Terminals 1, 2, and 3 of Singapore Changi Airport. There are two types of

ADGS in Singapore Changi Airport, Safedock Type 1 (T1) ADGS and

Safedock Type 2 (T2) ADGS.

B7679 M

LED DISPLAY AND LASER SCANNING UNIT

Safedock Type 1 (T1) Safedock Type 2 (T2)

LED Closing Rate Field

Azimuth Guidance

Digital Countdown

B767

3.3 When the solid yellow closing rate field appears, the aircraft has been caught by the scanning unit. The scanning unit now checks that the aircraft is the correct type and the display provides azimuth guidanceinformation (see figure 2).

B767

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

System tracking

for aircraft.

( depicts flashing red arrow.)

Acft tracked andsystem identifying

( or depictssolid yellow arrow.)

B767LED closing ratefield starts diminishing whenthe acft is 15m from stopbar at onerow for every 0.5mthat the acft movesforward.

terminal or pole in front of the aircraft stand.

acft.

9M

3.1 Check that the correct aircraft type is displayed. The scrollingarrows indicate that the system isactivated (see figure 1).

Figure A

Figure 1

Figure 2

Figure 3

Safedock Type 1 (T1)

Safedock Type 2 (T2)

JEPPESEN

WSSS/SIN 10-9N SINGAPORE, SINGAPORECHANGI

.PARKING.

Figure 4B767

Figure 5STOP

Figure 6

Figure 7

Figure 8

Figure 9

SLOW

LED closingrate field

moves nearer

pilot thateverything

Indicates thatthe acft hasgone beyondthe stopbar.Pilot tocheck withgroundengineer on

move.the next

Pilot to holdacft and waitfor otherinstructionsfrom thedisplay.

Figure 10

'STOP' mayappearsuddenly inthe processof docking.Pilot to stopimmediatelyand wait forfurtherinstructions.

Figure 11

speed is toofast. Pilot toslow downthe speed.

4. SAFETY MEASURES

1.8M

OK

WAIT

DOWN


Informs thepilot that theacft traveling

SAFEDOCK-Continued.

CHANGES: Text, graphic.

23 DEC 11

gettingshorteras acft

to stopbar.

B7671.8M

STOP Pilot to stopacft when "STOP" is displayed.

OKInforms the

is in orderand he can shutdownengine.

(see figure 6).

TOO FAR

TOO FAR

3.8 If the aircraft has gone past the correct stopposition, the display will show "TOO FAR"(see figure 7).

3.10 The aircraft must be identified at least 12m

WAIT

STOPSTOP

ID

IDFAIL

STOP

4.3 To avoid overshooting, pilots are advised to

failed to

Indicates the system

identify the acft.

FAIL

SLOW1.8M

3.5 When the aircraft is 15m from the stop

"Distance to go" is indicated by turning off one row of LEDs (Laser Electronic Displays) for every half meter that the aircraftadvances towards the stop position. From 15m to the stop position, a digital displaywill indicate the distance from the stop

will be off, the word "STOP" will appear in the display. For Safedock TI ADGS, the word "STOP" will be displayed in red with red border. For Safedock T2 ADGS, the word

red, rectangular fields will light in the azimuth guidance area of the display(see figure 5).

"OK" will be displayed after a few seconds3.7 If the aircraft stops in the correct position,

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

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

4.1 Pilot should not turn an aircraft into theparking stand if the docking system is not

displayed on the system.activated or on seeing a wrong aircraft type

4.2 When using the docking system, pilots are to taxi into the aircraft stand at minimum speed. The system will display "SLOW

taxiing speed is too fast (see figure 11).DOWN: to inform the pilot if the aircraft's

approach the stop position slowly and observe the closing rate information displayed. Pilots should stop the aircraft

aircraft marshaller.display or when given the stop sign by the

4.4 Pilot should stop the aircraft immediately if the display goes black during the docking

the stand manually. process. The aircraft is to be marshalled into

"STOP" will be displayed in yellow and two

"ID FAIL" (see figures 8, 9 and 10).

immediately when seeing the "STOP"

all of the LEDs for the closing rate field 3.6 When the correct stop position is reached,

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

distance from the stop position for every

position, closing rate information is given.

position, the display will indicate the

0.2m (see figures 3 and 4).

SafedockType 1 (T1)

SafedockType 2 (T2)

WSSS/SIN 10-9P SINGAPORE, SINGAPORECHANGI

.PARKING.JEPPESEN


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

23 NOV 12

B788 aircraft stands C18 and C24 revised.

B757

B74S

B747

B737

B717

B707

A380

A346

A345

A343

A342

A333

A321

A319

B763

B762

A332

AircraftType C11 C13 C15 C16 C17 C18 C19 C20 C22 C23 C24 C25 C26

B772

MD80

MD11

L101

IL96

IL62

F100

DC9

DC10

B773

MD88

MD82

C1

TERMINAL 1 AIRCRAFT STANDS

A300

A310

A320

B727

B773ER

BA146

IL86

B788

WSSS/SIN 10-9Q SINGAPORE, SINGAPORECHANGI

.PARKING.JEPPESEN



23 NOV 12

B788 stand D47 revised.

B757

B74S

B747

B737

B717

B707

A380

A346

A345

A343

A342

A333

A321

A319

B763

B762

A332

AircraftType D30 D32 D34 D35 D36 D37 D38 D40 D41 D42 D44 D46 D47 D48 D49

YK42

MD88

MD82

L101

IL96

IL86

IL62

F100

DC9

DC10

B773

TERMINAL 1 AIRCRAFT STANDS (contd)

A300

A310

A320

B727

B772

B773ER

BA146

MD11

MD80

B788

WSSS/SIN 10-9R SINGAPORE, SINGAPORECHANGI

.PARKING.JEPPESEN



15 MAR 13

B788 added.

MD88

MD87

MD82

MD80

MD11

L101

IL96

IL86

IL62

F100

F70

DC9

DC10

B773ER

B773

B772

B763

B762

B757

B74S

B747

B737

B727

B707

A380

A346

A345

A343

A342

A333

A332

A321

A320

A319

A310

A300

AircraftType

E1 E2 E3 E4 E5 E6 E7 E8 E10 E11 E12 E20 E22 E24 E26 E27 E28

TERMINAL 2 AIRCRAFT STANDS

F30E24LE24R

B788

WSSS/SIN 10-9R1 SINGAPORE, SINGAPORECHANGI

.PARKING.JEPPESEN


DC8


B788

15 MAR 13

B788 parking stand revised.

MD87

MD11

L101

F70

DC9

DC10

B773ER

B773

B772

B763

B762

B757

B74S

B747

B737

B727

B707

A380

A346

A345

A343

A342

A333

A332

A320

A319

A310

A300

AircraftType F40 F41 F42 F50 F52 F54 F56 F58 F59F31 F32 F33 F34 F35 F36 F37 F60

TERMINAL 2 AIRCRAFT STANDS (contd)

F52L/R

A321

F59L/RF56L/R


.PARKING.JEPPESEN



14 MAR 14

B788 added.

B772

B744

B737

A380

A346

A345

A1

A300, A310, A319, A320, A321

B757, B767

B773, B773ER

A2 A3 A4 A5 A9 A10 A11 A12

B737

A380

A346

A345

A300, A310, A319, A320, A321

A332

A333, A343

B757, B767

B772

B773, B773ER

A13 A14 A15 A16 A17 A18 A19 A20 A21

A332, A333, A343

B744

B737

B707

A300, A310, A319, A320, A321

B773, B773ER

B1

A332, A333, A343, A345

A346, A380

B772

B2 B3 B4 B5 B6 B7 B8 B9 B10

B757, B767

B744

TERMINAL 3 Aircraft Type / Stands

TERMINAL 3 (contd) AircraftType / Stands

TERMINAL 3 (contd) AircraftType / Stands

B74S

B74S

B74S

B788

B788

B788


.PARKING.JEPPESEN


REMOTE STANDS - Aircraft types that can be parked at stands (o) are as follows:

REMOTE STANDS - Aircraft types that can be parked at stands (o) are as follows:

14 MAR 14

BUDGET TERMINAL - Aircraft types that can be parked at stands (o) are as follows:

Budget stands added.

1 2 3 4 5 6 7 8 9 10

A319, A320, AT72, B737, DHC7

11 12 13 14

L101

F70

DC8

DC10

B747

B737

B727

MD11

L101

IL62

F70

DHC7

DC10

DC8

B757

A380

103 104 200 201 202 203 205 206 207 208 209

AT72

MD11

B773ER

B707

A343, A345

A319, A320

A300, A310

300 301 302 303 304 305 306 307 308 309 310 400 401 402 403 404

AT72

Aircraft Type / Stands

Acft TypeStands

B74S, B788

B767, B772, B773, B773ER

B737

B707, B727

A300, A310

A319, A320

A321

A330, A342, A343, A345

B747, B74S, B788

B748

202L/R200L/R

A330, A342

B757, B767

B772, B773

A321



.PARKING.JEPPESEN


MARS STANDS - Aircraft types that can be parked at stands (o) are as follows:

22 NOV 13

None.

B773

B757

B748

B747

B737

A342

A320

101 101L 101R 102 102L 102R

A321


A300

A310

A319

A332

A333

A343

A380

B772

B763

B762

B773ER

B787-8

A345


.PARKING.JEPPESEN

CHANGES:



22 NOV 13

A330 cargo stands.

B757

B74S

B747

B737

B707

A380

A346

A345

A343

A342

A333

B767

A332

AircraftType 502 503 504 505 506 507 508 509 601 602 603 604 611 612

L101

IL86

IL62

DC10

B773

A300

A310

B727

B772

B773ER

MD11

CARGO STANDS

B748

DC8

A306

A330

B744

B753

B752

B763

B762

B772LR

B777F

JEPPESEN

MALAYSIA

INDONESIA

168^

INDONESIASINGAPORE356^

356^PU

115.1

WS(P)-3

WS(P)-24

WS(P)-36

WM(P)-228

WS(R)-2

WS(R)-31

WS(R)-38

WS(D)-4

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

WS(D)-5Seletar

Paya Lebar

Hang Nadim

SINGA-PORE

MALAYSIA

WS(D)-33WS(D)-1

637'

942'

500'

DSINJON

113.5 SJS J

SAMKO

ILS DME

023^ 110.9 ICWI C WANUMA

1 D16.6 ICW

023^

4000

3500023^

D8/14

1

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^

FMS required forholding during SJ VOR

01-10

103-50 104-00 104-10

ALTITUDE

outage.


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

RVR 550mVIS 800m

RVR 720mVIS 800m

or CL outTDZDA(H) 222'(200') MDA(H) 420'(398')

RVR 720mVIS 800m

1200m

RVR 1500mVIS 1600m

RVR 1800mVIS 2000m

APCH FIXMISSED

360^

090^

3400'

2100'

180^

1900'

MSA VTK VOR

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 02L 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

25 NOV 11


372 478 531 637 743 849

Tower frequency.

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 02L 22'22'Apt Elev

WS(P)-49

535'

620'

436'

656'

680'

630'

440'

550'

611'

602'

437'

1017'

CHANGES:

523'

JEPPESEN

MALAYSIA

INDONESIA

168^

INDONESIASINGAPORE356^

356^PU

115.1

WS(P)-3

WS(P)-24

WS(P)-36

WM(P)-228

WS(R)-2

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

WS(D)-4

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

WS(D)-5Seletar

Paya Lebar

Hang Nadim

SINGA-PORE

MALAYSIA

WS(D)-33WS(D)-1

ILS DME Rwy 02L CAT II

CAT II ILS

637'

942'

500'

DSINJON

113.5 SJS J

SAMKO

ILS DME

023^ 110.9 ICWI C WANUMA

1 D16.6 ICW

023^

4000

3500023^

D8/14

1


MISSED APCH:

CHANGI

LOC

110.9ICW

FinalApch Crs023^

GS

(3478')3500'

PA

NS O

PS


WSSS/SIN

348^

168^

FMS required forholding during SJ VOR

01-10

103-50 104-00 104-10outage.



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


335^hdg

AKOMA

356^

176^

D20.0 PU

4000

BRIE

FIN

G S

TRIP

TM

hdg

335^1000'

LT

4000'

APCH FIXMISSED

360^

090^

3400'

2100'

180^

1900'

MSA VTK VOR

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 02L 22'

ANUMAD11.1 ICW

023^


11-1A

DA(H) 122'(100')

STRAIGHT-IN LANDING RWY

DA(H) 127'(105')

350m

02L

4.9

via

3500

D8.0 SJ/R-168

25 NOV 11

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.


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

Tower frequency.


WS(P)-49

535'

620'

436'

656'

680'

630'

440'550'

611'

602'

437'

1017'

CHANGES:

523'

RA 112'CAT II ILS

RA 131'

RVRRVR

JEPPESEN

SINGAPORE

INDONESIA

MALAYSIA

168^SJ

113.5

023^

VTK

116.

5

WS(D)-34

WS(R)-38

Paya Lebar

Seletar

WS(P)-36

Hang Nadim

LOC(GS out)

348^

168^

023^1.8

023^

SAMKO

4000

4500 436'

440'

D8/14

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'(4485')

ILSDA(H)

215'(200')

Apt Elev 22'Rwy 02C 15'

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

D13

/19

25 NOV 11

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'

Rwy 02C 15'

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'(405') MDA(H) 660'(645')

LAGUSLUXOL

05

510

BRIE

FIN

G S

TRIP

TM

hdg

023^

MSA VTK VOR

3400'

090^

180^

360^

1900'

2100'

RVR

VIS 800m

720mRVRVIS 800m

720m RVR 1500mVIS 1600m 800mVIS

RVR 720m RVR 1500mVIS 1600m

1800m2000mVIS

RVR

DA(H) 215'(200')

2000mRVR 1800mVIS

STRAIGHT-IN LANDING RWY02C

FMS required for holdingduring SJ VOR outage.

4500

01-10

*118.25

of Rwy.

Tower frequency, notes. | JEPPESEN, 1998, 2011. ALL RIGHTS RESERVED.

372 478 531 637 743 8493.00^

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

CHANGES:

523'

1500'

JEPPESEN

SINGAPO

RE

MALA

YSIA

INDONESIA

SIN

GAPORE

MALA

YSIA

158^VTK

116.5

023^

VTK

116.

5

Seletar

Paya Lebar

WS(P)-36

WS(R)-38

WS(D)-34

158^VTK116.5

627'

440'

611'

602'

203^

PA

NS O

PS

920'

D 116.5 VTKTEKONG

V T K

I C C ILS DME

203^ 109.7 ICC

680'

573'

MISSED APCH:

SINGAPORE, SINGAPORECHANGI ILS DME Rwy 20C11-3

LOC

109.7ICC

FinalApch Crs203^

GS

4500'(4485')

ILSDA(H)

215'(200')

ESLUX (1000' or above) turn LEFT heading 130^ to intercept VTK R-158


01-20

01-30

WSSS/SIN

500'



22 JUL 11

ELALU

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

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

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^

3000

D13

/19

203^

ELALUD14.2 ICC

EGORAD16.0 ICC

05

510

BRIE

FIN

G S

TRIP

TM

RWY 20C 15'22'Apt Elev

(GS out)LOC

ALTITUDEICC DME

650'2.0

970'3.0

1290'4.0

MISSEDAPCH FIX

104-10

EXOMOD22.0 VTK

338^

4000158^

104-00

PAPIREIL

ELALUD14.2 ICCELBEB

D7.8 ICC

6.43.23.9

TCH 58'

15'1500'

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

B

C

D

ILS

FULL ALS out

1200m

LOC (GS out)

ALS out


CIRCLE-TO-LAND

NA

A

B

C

D

4000'

R-203

VTK

116.5via ESLUX

ALSF-II


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

1200m RVR 1800mVIS 2000m

RVR 720mVIS 800m

RVR 1500mVIS 1600m

090^

180^

360^

1900'

2100'

3400'

MSA VTK VOR

NOT TOSCALE

130^hdg

RWY 20C

ESLUXD6.7 VTK

VIS 800mRVR 720m

TDZ or CL out

RVR 550mVIS 800m

4500

D4.6 ICC

D4.6 ICC

Ground


119.3120.3SINGAPORE Tower

118.6D-ATIS

*118.25128.6

Tower communications, aircraft speed restriction note removed.

of Rwy.


372 478 531 637 743 849

CHANGES:

JEPPESEN

SINGAPO

RE

MALA

YSIA

INDONESIA

SING

APORE

MALA

YSIA

158^VTK

116.5

023^

VTK

116.

5

Seletar

Paya Lebar

WS(P)-36

WS(R)-38

WS(D)-34

158^VTK116.5

CAT II ILSRA 102'

ILS DME Rwy 20C CAT II

4500'

14.0

203^

627'

440'

611'

602'

203^

PA

NS O

PS

920'

D 116.5 VTKTEKONG

V T K

I C C ILS DME

203^ 109.7 ICC

680'

573'

MISSED APCH:


LOC

109.7ICC

FinalApch Crs203^

GS

4500'(4485')

ESLUX (1000' or above) turn LEFT heading 130^ to intercept VTK R-158


01-20

01-30

WSSS/SIN

500'



22 JUL 11

ELALU

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

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

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

NYLOND16.7 ICCD13.0 VTK

1.8

4500203^ 023^

3000

D13

/19

203^

ELALUD14.2 ICC

EGORAD16.0 ICC

05

510

BRIE

FIN

G S

TRIP

TM

RWY 20C 15'22'Apt Elev

MISSEDAPCH FIX

104-10

EXOMOD22.0 VTK

338^

4000158^

104-00

PAPIREIL

ELALUD14.2 ICC

TCH 58'

15'


70 90 100 120 140 160 4000'

R-203

VTK

116.5via ESLUX

ALSF-II

090^

180^

360^

1900'

2100'

3400'

MSA VTK VOR

NOT TOSCALE

130^hdg

RWY 20C

ESLUXD6.7 VTK

11-3A

115'(100')DA(H)


115'DA(H) (100')

350m

4500


Ground


128.6 119.3120.3SINGAPORE Tower

118.6D-ATIS

*118.25

of Rwy.

Twr comms, acft speed restriction note removed, profile, minimums.

372 478 531 637 743 849

CHANGES:

CAT II ILS

RA 102'

RVR

JEPPESEN

Seletar

VTK

023^

116.

5

JS168^SJ113.5

146^

113.5SJJSWS(P)-36

WS(R)-38

WS(D)-34

WM(D)-230

MALA

YSIA

Paya Lebar Aero

SINGAPORE

MALAYSIA

SINGAPORE

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')

ILSDA(H)

213'(200')

Apt Elev 17'Rwy 20R 13'

MSA VTK VOR


128.6 120.3 119.3 118.6 124.3


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

D13

/19

D16.0 ICHIPNAK

203^

3500

NOT TO SCALE

348^

SAMKOD8.0 SJ1

5000168^

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

NARVR

VIS 800m

720mRVRVIS 800m

720m RVR 1500mVIS 1600m

ABCD 2000m

RVR 1800mVIS

ABCD

5000'PAPIREIL

PAPIR-146

SJ

113.5 SAMKODoncrossing

DA(H) 213'(200')

3500'

3.33.2

2500'

0.6

203^

3.8

TCH 57'

Rwy 20R 13'

IDUNAD0.8 ICH

IDUROD4.6 ICH

IGULAD11.1 ICHIDVAS

D7.8 ICH

STRAIGHT-IN LANDING RWY20R

4.9

3500

D8/14

8 JUN 12


HIALS

MDA(H) 420'(407')

680'

440'

761'

611'

500'

621'

*118.25

of rwy.

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

Communications, rwy and apt elevation, notes, lighting.CHANGES:

1500'

JEPPESEN

168^

356^

356^PU

115.1

Seletar

Hang Nadim

SINGAPORE

INDONESIA

MALAYSIA

WS(P)-3

WS(P)-24

WS(P)-36

WM(P)-228

WS(R)-2

WS(R)-38

WS(D)-4

WS(D)-35

WS(D)-5

INDONESIASIN

GAPORE

WS(R)-31

Paya Lebar Aero

MALAYSIA

[TCH 50']

[3.00^]

0.4 NMto SAPAX

DSINJON

113.5 SJS J

SAMKO

023^

4000


Ground

124.3

MISSED APCH:


128.6 119.3

RNAVFinal

Apch Crs023^ (2483')

DA(H)530'2500'

120.3SINGAPORE Tower

118.6

(513')

PA

NS O

PS

D-ATIS


WSSS/SIN

348^

168^

01-10

104-00 104-10



D116.5 VTKTEKONG

V T K

Gnd speed-Kts

REILPAPI PAPI

70 90 100 120 140 160

A

B

C

D

ALS out

2800m

ALS out

ALSF-II

CIRCLE-TO-LAND

NA

A

B

C

D

C~2LF


335^hdg

AKOMA

356^

176^

D20.0 PU

4000

01-20

4.4 2.6 5.0 Rwy 02L 17'

SAPAXC~2LF

C~2LSRW~2L

1000'

023^


via

STRAIGHT-IN LANDING RWY02L


RNAV (GNSS) Rwy 02L

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

LNAV/VNAV

LNAV/VNAV LNAVDA(H) 530'(513') MDA(H) 580'(563')

MAP at RW~2L7.6 6:31 5:04 4:34 3:48 3:15 2:51

SAPAX(IAF)

(IAF)

(IF)

SANAT

C~2LF

C~2LS

Descent angle [3.00^] 372 478 531 637 743 849

05.07.612.0

RW~2L

2. Maritime vessels of variable heights in water north and south of runway.1. Minimum temperature for which Baro-VNAV operations are authorized: 15^C.

D14.0SJ

1

11 Max IAS 220 Kts.

Procedure Alt

2500'3900'

MDA

290^

013^

C~2LF to MAP

RVR 1500mVIS 1600m

2800m

2400m

RVR 720mVIS 800m

RVRVIS 1600m

1500m

RVRVIS 2000m

1800m

3900

3900

5.9

4.5

2000m

01-00

4000

4000

BRIE

FIN

G S

TRIP

TM0

55

1015

20

hdg

335^1000'

LT

4000'

APCH FIXMISSED

360^

090^

3400'

2100'

180^

1900'

MSA VTK VOR

660'2000'

4000'SANATSAMKO


1670'

*118.25

31 AUG 12

Hold designation revised.

436'

620'

637'920'

538'

942'

656'

500' 621'

611'

WS(P)-49

WS(D)-34

CHANGES:

535'

620'

JEPPESEN

MALAYSIA

168^

146^

SJ

SJ

113.5

113.5

SJ

SJINDONESIA

MALAYSIA

Paya Lebar

WM(R)-229

WM(D)-230

WM(D)-231

WS(R)-31

WS(D)-34

SINGAPORE

Aero

WM(D)-8

[TCH 50'][3.00^]

4.5 NMto C2~RF3.2 NM

to C2~RF


Ground

124.3

MISSED APCH:


128.6 119.3

RNAVFinal

Apch Crs203^ (1987')

DA(H)530'2000'

120.3

SINGAPORE Tower

118.6

(517')

PA

NS O

PS

D-ATIS


WSSS/SIN



REILPAPI PAPI

A

B

C

D

ALS out

2800m

ALS out

CIRCLE-TO-LAND

NA

A

B

C

D

C2~RF

6.06.0Rwy 20R 13'

NOMAKC2~RF

RW2~R

1500'

203^

STRAIGHT-IN LANDING RWY20R

Rwy 20R 13'17'Apt Elev

RNAV (GNSS) Rwy 20R

LNAV/VNAV

LNAV/VNAV LNAV

DA(H) 530'(517') MDA(H) 580'(567')

MAP at RW2~R

Descent angle [3.00^] 372 478 531 637 743 849

0 6.0 12.0

2. Maritime vessels of variable heights in water north and south of runway.1. Minimum temperature for which Baro-VNAV operations are authorized: 15^C.

Procedure Alt

2000'

MDA

C2~RF to MAP

RVR 1500mVIS 1600m

2800m

2400m

RVR 720mVIS 800m

RVRVIS 1600m

1500m

RVRVIS 2000m

1800m

2000m

Climb STRAIGHT AHEAD to 5000'. On crossing SJ VORR-146, proceed direct to SAMKO holding area and hold or as directedby ATC.

5000'cross

SJ

113.5R-146

SAMKO6.0 5:09 4:00 3:36 3:00 2:34 2:15

TO DISPLACED THR

3400'

3000'

TEKONG116.5 VTKVTKD

RW2~R

C2~RF

NOMAK BIPOP

BIDUS

NYLON(IAF)

(IAF)

(IAF)(IF)

203^

023^

D19.0VTK

3000

SAMKO348^

168^

D14.0SJ

MISSEDAPCH FIX

203^

110^

290^216^6.5 4.

16.7

300030

00

3400

5000D8.0 SJ

1

1

1

1 Max IAS 220 Kts.

3400

3000

3000

01-20

01-30

01-40

103-50

104-00 104-10 104-20

BRIE

FIN

G S

TRIP

TM0

55

1015

20

360^

090^

3400'

2100'

180^

1900'

MSA VTK VOR

BIDUS

BIPOPNYLON2000'

Gnd speed-Kts 70 90 100 120 140 160


*118.25

HIALS

31 AUG 12

None.

620'

611'

468'

573'

500'

627'

621'

CHANGES:

JEPPESEN

SINGAPORE

INDONESIA

MALAYSIA

Paya Lebar

168^

Seletar

WS(D)-34WS(P)-36

WS(R)-38

D8

SJ

113.5

Hang Nadim

023^

VTK

116.

5

348^

023^

023^

(IF)

168^

2500

4000D

8/14

436'

440'

611'

D116.5 VTKTEKONG

V T K

D 113.5 SJS JSINJON

680'

10.0 9.0 8.011.0VTK DME

1470' 1150' 830'1790'

SAMKO

70 90 100 120 140 160

A

B

C

D

PA

NS O

PS

STRAIGHT-IN LANDING RWY 02C

With D8.0 VTK Without D8.0 VTK

RVRVIS 1600m

1500m

VIS 1600mRVR 1500m

MDA(H) 410'

ALS out ALS out

MDA(H)

1500m1600mVIS

RVRRVR 720m

800mVIS

RVR 720m800mVIS

(395')

RVRVIS

660'

2800m

3200m

1800m2000m

MAP at D6.0 VTK

(645')

RVRVIS

1800m2000m 2400m

Gnd speed-Kts

VTKD16.6

D6.0VTK

NOT TOSCALE

VTKD13.3

MISSED APCH:

SINGAPORE, SINGAPORECHANGI VOR DME Rwy 02C13-1

VOR

116.5VTK

FinalApch Crs

023^

Minimum Alt

2500'(2485')

MDA(H)

410'(395')

Apt Elev 22'Rwy 02C 15'

(CONDITIONAL)

090^

180^

360^

2100'

3400'

1900'

MSA VTK VOR


128.6 120.3 119.3 118.6 124.3

2500'

2.0

2500'023^

0.4 15'Rwy 02C3.3 5.3660'

D16.6 VTK D13.3 VTKD8.0VTK D6.0

VTK

1

1

1017'

D13.3 VTK

01-10

01-20

104-00 104-10

WSSS/SIN

D-ATIS

ALTITUDE

05

510

BRIE

FIN

G S

TRIP

TM

203^

023^

3000

D13

/19

NYLOND13.0 VTK

MISSEDAPCH FIX

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

D8.0VTK

Descent Gradient 5.2% 369 474 527 632 737 843

FAF to MAP 7.3 6:15 4:52 4:23 3:39 3:08 2:44

12.02100'

13.02420'

NYLONPAPIREIL

ALSF-I

PAPI

VTK

R-023116.5via and

3000'

hdg

023^

25 NOV 11

4.4


023

hdg

VTKVOR

VTK R-203D21.0 VTK

Air Force (RSAF) Aircraftthe Republic of Singapore 02R/20L is solely for use byCAUTION: Changi East Rwy

*118.25

1. Maritime vessels of variable heights in water north and south of Rwy. Alt Set: hPa Rwy Elev: 1 hPa Trans level: FL 130 Trans alt: 11000'

| JEPPESEN, 1998, 2011. ALL RIGHTS RESERVED.Tower frequency.CHANGES:

523'

JEPPESEN

MALA

YSIA

SINGAPO

RE

INDONESIA

SIN

GA

PO

RE

MALA

YSIA

Seletar

WS(D)-34

WS(R)-38

WS(P)-36

158^VTK116.5

116.5VTK

158^

Paya Lebar

V T K

203^

(IF)

627'

440'

611'

602'

920'

3000

023^

203^

2000

D13

/19

203^

NYLOND13.0 VTK

680'

VTKD9.1

VTKD2.62

03^

D3.0VTK

MISSED APCH:

SINGAPORE, SINGAPORECHANGI VOR DME Rwy 20C13-2


128.6 120.3 119.3 118.6 124.3VOR

116.5 VTK

FinalApch Crs203^

Minimum Alt

2000'(1985')

MDA(H)

580'(565')Apt Elev 22'Rwy 20C 15'

D2.6 VTK

090^

180^

360^

1900'

2100'

3400'

MSA VTK VOR

MAP at D3.0 VTK

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

Gnd speed-Kts 70 90 100 120 140 160

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^

4000158^

104-10

ESLUX130^hdg

1180'VTK D1.0 BEFORE VTK

1500'

Descent Gradient 5.2% 369 474 527 632 737 843

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

4000'

R-203

VTK

116.5via ESLUX

25 NOV 11

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

Rwy 20C 15' 3.0 2.6

2000'

6.5

203^ 2000'203^

0.5

1180'

VTKD3.0 VTK

D2.6VTK

D9.1

Air Force (RSAF) Aircraftthe Republic of Singapore 02R/20L is solely for use byCAUTION: Changi East Rwy

VTK R-023

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

D6.7 VTK

*118.25

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

Tower frequency, notes. | JEPPESEN, 1998, 2011. ALL RIGHTS RESERVED.CHANGES:

VOR

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