WSSS Charts

45
JEPPESEN JeppView 3.7.5.0 WSSS (Changi) Airport Information General Info Singapore, SGP N 01° 21.6' E103° 59.4' Mag Var: 0.0°W Elevation: 22' Public, IFR, Control Tower, Rotating Beacon, Low Level Wind Shear Alert System, Customs Fuel: Jet A-1 Repairs: Major Airframe, Major Engine Time Zone Info: GMT+8:00 no DST Runway Info Runway 02C-20C 13123' x 197' bitu Runway 02L-20R 13123' x 197' bitu Runway 02C (23.0°M) TDZE 15' Lights: Edge, ALS, Centerline, REIL Stopway Distance 197' Runway 02L (23.0°M) TDZE 22' Lights: Edge, ALS, Centerline, REIL, TDZ Stopway Distance 197' Runway 20C (203.0°M) TDZE 15' Lights: Edge, ALS, Centerline, REIL, TDZ Stopway Distance 197' Runway 20R (203.0°M) TDZE 15' Lights: Edge, ALS, Centerline, REIL Displaced Threshold Distance 2428' Stopway Distance 197' Communications Info 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 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 JEPPESEN JeppView 3.7.5.0 WSSS (Changi) Airport Information Notebook Info

Transcript of WSSS Charts

Page 1: WSSS Charts

JEPPESENJeppView 3.7.5.0WSSS (Changi)

Airport Information

General InfoSingapore, SGPN 01° 21.6' E103° 59.4' Mag Var: 0.0°WElevation: 22'

Public, IFR, Control Tower, Rotating Beacon,Low Level Wind Shear Alert System, CustomsFuel: Jet A-1Repairs: Major Airframe, Major Engine

Time Zone Info: GMT+8:00 no DST

Runway InfoRunway 02C-20C 13123' x 197' bituRunway 02L-20R 13123' x 197' bitu

Runway 02C (23.0°M) TDZE 15' Lights: Edge, ALS, Centerline, REIL Stopway Distance 197'Runway 02L (23.0°M) TDZE 22' Lights: Edge, ALS, Centerline, REIL, TDZ Stopway Distance 197'Runway 20C (203.0°M) TDZE 15' Lights: Edge, ALS, Centerline, REIL, TDZ Stopway Distance 197'Runway 20R (203.0°M) TDZE 15' Lights: Edge, ALS, Centerline, REIL Displaced Threshold Distance 2428' Stopway Distance 197'

Communications InfoATIS 128.6Singapore Tower 118.25Singapore Tower 118.6Singapore Ground Control 124.3Singapore Ground Control 121.725Singapore Ground Control 121.85Singapore Clearance Delivery 121.65Singapore Pre-Taxi Clearance 121.65Singapore Approach Control 124.6 SecondarySingapore Approach Control 120.3Singapore Arrival Control 119.3Singapore Radar 124.05 Arrival Service

JEPPESENJeppView 3.7.5.0WSSS (Changi)

Airport Information

Notebook Info

Page 2: WSSS Charts

Licensed to QANTAS. Printed on 30 Dec 2011.Notice: After 13 Jan 2012 0901Z, this chart may no longer be valid. Disc 26-2011

JEPPESENJeppView 3.7.5.0

JEPPESENWSSS/SIN10-1PCHANGI

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:

New chart. | JEPPESEN, 2011. ALL RIGHTS RESERVED.

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.

2.2 DEPARTURES2.2.1 When instructed to enter runway, pilots are required to commence the

maneuver without delay.2.2.2 Pilots are required to commence take-off roll as soon as take-off

clearance is issued by ATC.

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

CHANGES:

.AIRPORT.BRIEFING.30 SEP 11

Licensed to QANTAS. Printed on 30 Dec 2011.Notice: After 13 Jan 2012 0901Z, this chart may no longer be valid. Disc 26-2011

JEPPESENJeppView 3.7.5.0

JEPPESENWSSS/SIN10-1P1CHANGI

SINGAPORE, SINGAPORE

New chart. | JEPPESEN, 2011. ALL RIGHTS RESERVED.

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

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

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

2.4 ARRIVALS2.4.1 Upon landing, pilots are reminded that it is imperative to vacate the

runway as quickly as practicable to enable ATC to apply minimum spacingon final approach to maximize runway utilization and minimize theoccurrence of "go-arounds".

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)

CHANGES:

.AIRPORT.BRIEFING.30 SEP 11

Page 3: WSSS Charts

Licensed to QANTAS. Printed on 30 Dec 2011.Notice: After 13 Jan 2012 0901Z, this chart may no longer be valid. Disc 26-2011

JEPPESENJeppView 3.7.5.0

JEPPESEN

244^

252^

235^243^

220^

D57.3

D43.6

D38

.6 D24.0

D11.

6COMMSLOST COMMSLOST COMMSLOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS LOSTCOMMS LOSTLOST

17 N

M

CHANGES:

WSSS/SINCHANGI

SINGAPORE, SINGAPORE

TEKONG

116.5

VTK

VTK

N01

24.9

E104

01.3

D

A

Apt Elev

22'1

1RO

UT

IN

G

and p

roceed o

n B

OBAG 1

A t

o S

AMKO.

10-2 .RNAV.STAR.

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

4. RADAR required.

Fro

m A

RAMA t

rack 1

47^

to B

OBAG.

Fro

m R

EKOP t

rack 1

41^

to B

OBAG.

2. W

hen c

leare

d v

ia B

OBAG 1

A b

y S

ingapore

ATC:

MA

IN

TA

IN

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

50 K

T

ARAMA

REKOP

41

39

20

14

9

SINJO

N11

3.5

SJS

J

N01

13.4

E103

51.3

D

1. Set

transponder

to M

ode A

/C c

ode 7

600.

last

assig

ned f

light

level or

altitude

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

a.

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:

Refe

r to

Sin

gapore

Specia

l Pro

cedure

s f

or

radio

communic

ations f

ailure

pro

cedure

.

ARA

MA

(SJ

R-29

8/D

50.0

)(V

TK R

-282

/D55

.5)

Cha

ngi

Apt

Dir

ect

dist

ance

fro

m S

AM

KO

to:

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

A

(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

MA

X 2

50 K

T

10000'

090^

180^ 360^

3400

'

2500

'21

00'

090^

180^ 360^

3400

'

2100

'19

00'

MSA

VTK

VO

RM

SA S

J VO

R

(RWYS 02L/C)

1T

RA

NSIT

IO

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,

N01

36.9

E103

07.2

.A464.

.A576.

.R469.

25 NOV 11

At

or a

bove

6000'

ARA

MA

(A

-464)

REK

OP

(A

-576)

D-ATIS

128.6

| JEPPESEN, 2006, 2011. ALL RIGHTS RESERVED.

shall remain under the control of WMKK ATC.

Procedure note added.

(BOBAG1A) [BOBA1A]BOBAG ONE ALPHA ARRIVAL

1. For RNAV operations, aircraft shall be GNSS-equipped and meet RNP-1/P-RNAV standard of accuracy. 2. Non-RNP-1/P-RNAV approved aircraftshall fly this as a basic RNAV (B-RNAV) procedure or EXPECT RADARvectors from ATC. 3. All SOUTHBOUND flights from the WEST landing at

on 133.25 or 135.8 when Rwy 20 is in use and within 120 DME SJ. FlightSingapore Changi Apt are to request the STAR only from Singapore ATC

NO

T TO

SCA

LE

Licensed to QANTAS. Printed on 30 Dec 2011.Notice: After 13 Jan 2012 0901Z, this chart may no longer be valid. Disc 26-2011

JEPPESENJeppView 3.7.5.0

JEPPESEN

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

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0

D26.

2

D30.0

COMMSLOST COMMSLOST COMMSLOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS LOSTCOMMS LOSTCOMMS LOST

15 N

M

CHANGES:

WSSS/SINCHANGI

SINGAPORE, SINGAPORE

TEKONG

116.5

VTK

VTK

N01

24.9

E104

01.3

D

A

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

A

.RNAV.STAR.

2. W

hen c

leare

d v

ia B

OBAG 1

B b

y S

ingapore

ATC:

MA

IN

TA

IN

1RO

UT

IN

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

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(VTK

R-2

78/D

56.6

)

147^

141^

083^

083^

080^

023^

348^

ASUNA

N00

59.8

E103

09.9

BO

BA

GN01

02.5

E103

29.9

BO

KIP

(VTK

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21/D

27.0

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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

50 K

T

203^

ARAMA

REKOP

41

39

20

14

9

15

1212

SINJO

N

113.5

SJS

J

N01

13.4

E103

51.3

D

BATA

M

*116

.0 B

TMB

TM

N01

08.2

E104

08.0

D

1. Set

transponder

to M

ode A

/C c

ode 7

600.

last

assig

ned f

light

level or

altitude

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

a.

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:

Refe

r to

Sin

gapore

Specia

l Pro

cedure

s f

or

radio

communic

ations f

ailure

pro

cedure

.

ARA

MA

(SJ

R-29

8/D

50.0

)(V

TK R

-282

/D55

.5)

N01

36.9

E103

07.2

Cha

ngi

Apt

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.

10-2A

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)

1T

RA

NSIT

IO

NS

At

BOBAG t

rack 0

83^

to B

OKIP

then t

o S

AMKO. Turn

LEFT, tr

ack 0

80^

to

.R469.

.A576.

.A464.

25 NOV 11

At

or a

bove

10000'

At

or a

bove

MA

X 2

50 K

T7000'

or a

s di

rect

ed b

y A

TC

At

or a

bove

4000'

ARA

MA

(A

-464)

REK

OP (

A-576)

| JEPPESEN, 2006, 2011. ALL RIGHTS RESERVED.

128.6D-ATIS Apt Elev

22'

shall remain under the control of WMKK ATC.on 133.25 or 135.8 when Rwy 20 is in use and within 120 DME SJ. Flightat Singapore Changi Apt are to request the STAR only from Singapore ATC

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

1

4. RADAR required.

Procedure note added.

[BOBA1B](BOBAG1B)ARRIVAL

BOBAG ONE BRAVO

1. For RNAV operations, aircraft shall be GNSS-equipped and meet RNP-1/P-RNAV standard of accuracy. 2. Non-RNP-1/P-RNAV approved aircraftshall fly this as a basic RNAV (B-RNAV) procedure or EXPECT RADARvectors from ATC. 3. All SOUTHBOUND flights from the WEST landing at

NO

T TO

SCA

LE

Page 4: WSSS Charts

Licensed to QANTAS. Printed on 30 Dec 2011.Notice: After 13 Jan 2012 0901Z, this chart may no longer be valid. Disc 26-2011

JEPPESENJeppView 3.7.5.0

COMMSLOST COMMSLOST COMMSLOSTCOMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS LOSTCOMMS LOSTCOMMS LOST

096^

D36.2

120^

D30

.0

D8.0168^

14 N

M

CHANGES:

JEPPESENWSSS/SINCHANGI

SINGAPORE, SINGAPORE

TEKONG

116.5

VTK

VTK

N01

24.9

E104

01.3

D

A

Apt Elev

22'1

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

A

.RNAV.STAR.Alt Set: hPa Trans level: FL130 Trans alt: 11000'

D-ATIS

128.6

3. RADAR required.

2. W

hen c

leare

d v

ia L

AVAX 1

A b

y S

ingapore

ATC:

MA

IN

TA

IN

1RO

UT

IN

G

1. Set

transponder

to M

ode A

/C c

ode 7

600.

last

assig

ned f

light

level or

altitude

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

a.

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:

Refe

r to

Sin

gapore

Specia

l Pro

cedure

s f

or

radio

communic

ations f

ailure

pro

cedure

.

Cha

ngi

Apt

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

AM

KO.

10-2B

GO

BIK

TO

MA

N

Tra

ck 3

16^

from A

KTOD t

o I

KIM

A, th

en t

rack 2

91^

to I

BULA.

Then t

rack 3

35^

to L

AVAX.

Tra

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.

283^

297^

316^

291^

335^

233^

269^

195

21

20

17

46

21

90

94

TOMAN

GO

BIK

ATV

IX

AKT

OD

090^

180^ 360^

3400

'

2500

'21

00'

090^

180^ 360^

3400

'

2100

'19

00'

MSA

VTK

VO

R

MSA

SJ

VO

R

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

(VTK

R-1

35/D

48.7

)

IBULA

(SJ

R-11

7/D

50.2

)

IKIM

A(S

J R-

115/

D70

.5)

(VTK

R-1

28/D

67.9

)N00

43.2

E104

55.0

AKTO

D(S

J R-

127/

D16

1)

S00

24.8 E10

5 59

.6(V

TK R

-133

/D16

1)

GO

BIK

(SJ

R-10

6/D

266)

(VTK

R-1

09/D

259)

N00

00.0

E108

06.1

ATVIX

(SJ

R-11

6/D

160)

(VTK

R-1

22/D

157)

N00

02.4

E106

14.9

089^

089^

111^

FL1

50 -

FL2

50

MA

X 2

50 K

T

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)

SINJO

N11

3.5

SJS

J

N01

13.4

E103

51.3

D

168^

348^

4000'

- FL1

40

220 K

TM

AX

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

(RWYS 02L/C)

1TRA

NSITIO

NS

Tra

ck 2

97^

from A

TVIX

to I

KIM

A, th

en t

rack 2

91^

to I

BULA.

Then t

rack 3

35^

to L

AVAX.

Tra

ck 2

83^

from G

OBIK

to I

KIM

A, th

en t

rack 2

91^

to I

BULA.

Then t

rack 3

35^

to L

AVAX.

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

.A464.

.A576.

FL2

60 -

FL3

10

MA

X 2

80 K

T7000'

- FL1

40

MA

X 2

20 K

T

At

or b

elow

FL1

60

EXPE

CT

RAD

AR

vect

ors

for

ILS

appr

oach

Rw

y 02

1. For RNAV operations, aircraft shall be GNSS-equipped and meet RNP-1/P-RNAV standard of accuracy.

LAVAX ONE ALPHA(LAVAX1A) ARRIVAL

or EXPECT RADAR vectors from ATC.

26 JAN 07

MA

X 2

50 K

T

At

or a

bove

7000'

MA

X 2

20 K

T

AK

TO

D(A

-576)

ATV

IX

(A

-464)

At

or b

elow

FL1

80

Note 2. | JEPPESEN SANDERSON, INC., 2006, 2007. ALL RIGHTS RESERVED.

(B-RNAV) procedure2. Non-RNP-1/P-RNAV approved aircraft shall fly this as a basic RNAV

NO

T TO

SCA

LE

Licensed to QANTAS. Printed on 30 Dec 2011.Notice: After 13 Jan 2012 0901Z, this chart may no longer be valid. Disc 26-2011

JEPPESENJeppView 3.7.5.0

074^

055^

033^

D22.5

D11.0

D30.0

COMMSLOST COMMSLOST COMMSLOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS LOSTCOMMS LOSTCOMMS LOST

096^

087^

D36.2

D28.6

15 N

M

CHANGES:

JEPPESENWSSS/SINCHANGI

SINGAPORE, SINGAPORE

TEKONG

116.5

VTK

VTK

N01

24.9

E104

01.3

D

A

Apt Elev

22'1

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

A

.RNAV.STAR.Alt Set: hPa Trans level: FL130 Trans alt: 11000'

D-ATIS

128.6

3. RADAR required.

2. W

hen c

leare

d v

ia L

AVAX 1

B b

y S

ingapore

ATC:

MA

IN

TA

IN

1RO

UT

IN

G

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.

last

assig

ned f

light

level or

altitude

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

a.

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:

Refe

r to

Sin

gapore

Specia

l Pro

cedure

s f

or

radio

communic

ations f

ailure

pro

cedure

.

Cha

ngi

Apt

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.

10-2C

GO

BIK

TO

MA

N

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.

Tra

ck 3

16^

from A

KTOD t

o I

KIM

A, th

en t

rack 2

91^

to I

BULA.

Then t

rack 3

35^

to L

AVAX.

Tra

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.

304^

9

8

090^

180^ 360^

3400

'

2500

'21

00'

090^

180^ 360^

3400

'

2100

'19

00'

MSA

VTK

VO

RM

SA S

J VO

R

N01

14.9

E104

19.8

RUTO

T(V

TK R

-118

/D21

.0)

N01

09.8

E104

27.2

LAVA

X(V

TK R

-120

/D30

.0)

3000'

- FL1

40

MA

X 2

20 K

T

089^

SINJO

N11

3.5

SJS

J

N01

13.4

E103

51.3

D

(RWYS 20C/R)

Tra

ck 2

97^

from A

TVIX

to I

KIM

A, th

en t

rack 2

91^

to I

BULA.

Tra

ck 2

83^

from G

OBIK

to I

KIM

A, th

en t

rack 2

91^

to I

BULA.

Then t

rack 3

35^

to L

AVAX.

Then t

rack 3

35^

to L

AVAX.

EXPE

CT

RAD

AR

vect

ors

for

ILS

appr

oach

Rw

y 20

(SJ

R-04

7/D

26.2

)

21

335^

21

N00

50.6

E104

36.0

(VTK

R-1

35/D

48.7

)

IBULA

(SJ

R-11

7/D

50.2

)

7000'

- FL1

40

MA

X 2

20 K

T

N01

10.3

E104

48.3

(VTK

R-1

07/D

49.2

)

KEXA

S(S

J R-

093/

D57

.2)

269^

46

233^

17TO

MAN

089^

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)

283^

297^

316^

195

90

GO

BIK

ATV

IX

GO

BIK

(SJ

R-10

6/D

266)

(VTK

R-1

09/D

259)

N00

00.0

E108

06.1

ATVIX

(SJ

R-11

6/D

160)

(VTK

R-1

22/D

157)

N00

02.4

E106

14.9

FL1

50 -

FL2

50

MA

X 2

50 K

T .A464.

FL2

60 -

FL3

10

MA

X 2

80 K

T

291^

20

94AKT

OD

IKIM

A(S

J R-

115/

D70

.5)

(VTK

R-1

28/D

67.9

)N00

43.2

E104

55.0

AKTO

D(S

J R-

127/

D16

1)

S00

24.8 E10

5 59

.6(V

TK R

-133

/D16

1)

111^

291^

.A576.

At

or b

elow

FL1

60

N01

19.6

E104

12.8

(VTK

R-1

15/D

12.7

)

1T

RA

NSIT

IO

NS

1. For RNAV operations, aircraft shall be GNSS-equipped and meet RNP-1/P-RNAV standard of accuracy.

LAVAX ONE BRAVO(LAVAX1B) ARRIVAL

or EXPECT RADAR vectors from ATC.

26 JAN 07

MA

X 2

50 K

T

At

or a

bove

8000'

4000'

At

or a

bove

At

or a

bove

MA

X 2

20 K

T

3000'

AK

TO

D(A

-576)

AT

VIX

(A

-464)

At

or b

elow

FL1

80

Note 2. | JEPPESEN SANDERSON, INC., 2006, 2007. ALL RIGHTS RESERVED.

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

NO

T TO

SCA

LE

Page 5: WSSS Charts

Licensed to QANTAS. Printed on 30 Dec 2011.Notice: After 13 Jan 2012 0901Z, this chart may no longer be valid. Disc 26-2011

JEPPESENJeppView 3.7.5.0

JEPPESEN

COMMSLOST COMMSLOST COMMSLOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS LOSTCOMMS LOSTCOMMS 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

14 N

M

CHANGES:

WSSS/SINCHANGI

SINGAPORE, SINGAPORE

TEKONG

116.5

VTK

VTK

N01

24.9

E104

01.3

D

A

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

A

.RNAV.STAR.

2. W

hen c

leare

d v

ia L

ELIB

2B b

y S

ingapore

ATC:

MA

IN

TA

IN

1RO

UT

IN

G

023^

NYLO

NN01

37.0

E104

06.4

203^

1. Set

transponder

to M

ode A

/C c

ode 7

600.

last

assig

ned f

light

level or

altitude

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

a.

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:

Refe

r to

Sin

gapore

Specia

l Pro

cedure

s f

or

radio

communic

ations f

ailure

pro

cedure

.

ARA

MA

(SJ

R-29

8/D

50.0

)

Cha

ngi

Apt

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.

10-2D

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)

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 t

urn

LEFT a

nd t

rack 0

57^

to B

IDUS. Fro

m B

IDUS, EXPECT R

ADAR v

ecto

rs f

or

ILS

appro

ach R

wy 2

0.

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

N

113.5

SJS

J

N01

13.4

E103

51.3

D

JAYBE

E

400

JBJ

B

N01

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

E103

07.2

LELIB TWO BRAVO

25 NOV 11

At

or a

bove

10000'

At

or a

bove

250 K

TM

AX 7000'

At

or a

bove

220 K

TM

AX 3000'

3000'

- FL1

40

MA

X 2

20 K

T

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

1

at Singapore Changi Apt are to request the STAR only from Singapore ATCon 133.25 or 135.8 when Rwy 20 is in use and within 120 DME SJ. Flight

4. RADAR required.shall remain under the control of WMKK ATC.

Apt Elev

22'D-ATIS

128.6

| JEPPESEN, 2006, 2011. ALL RIGHTS RESERVED.Procedure note added.

[LELI2B]ARRIVAL

(LELIB2B)

1. For RNAV operations, aircraft shall be GNSS-equipped and meet RNP-1/P-RNAV standard of accuracy. 2. Non-RNP-1/P-RNAV approved aircraftshall fly this as a basic RNAV (B-RNAV) procedure or EXPECT RADARvectors from ATC. 3. All SOUTHBOUND flights from the WEST landing

NO

T TO

SCA

LE

Licensed to QANTAS. Printed on 30 Dec 2011.Notice: After 13 Jan 2012 0901Z, this chart may no longer be valid. Disc 26-2011

JEPPESENJeppView 3.7.5.0

JEPPESEN

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

COMMSLOST COMMSLOST COMMSLOST COMMSLOST

14 NM

CHANGES:

WSSS/SINCHANGI

SINGAPORE, SINGAPORE

TEKONG116.5 VTKVTK

N01 24.9 E104 01.3

D

A

Apt Elev

22'1

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

Air Force (RSAF) Aircraft

A

.RNAV.STAR.

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

3. RADAR required.

MAINTAIN

1ROUTING

023^

NYLON

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

a.

3. No clearance or instruction received from Singapore ATC:

Changi AptDirect distance from SANAT to:

10-2E

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 SJSJ

N01 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 40.4PIBAP

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/D104)

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

last assigned flight level or 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

Refer to Singapore Special Procedures for radio communications failure procedure.

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^

1. For RNAV operations, aircraft shall be GNSS-equipped and meet RNP-1/P-RNAV standard of accuracy.

or EXPECT RADAR vectors from ATC.

25 NOV 11

MAX 250 KT

MAX 220 KT

BIKTA(M-751/B-469)

MABAL(N-892)

VEPLI(L-642)

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

At or belowFL270

| JEPPESEN, 2006, 2011. ALL RIGHTS RESERVED.

D-ATIS

128.6

(PASPU1A) [PASP1A]

Navdata ident added.

PASPU ONE ALPHA ARRIVAL

NOT TO SCALE

Page 6: WSSS Charts

Licensed to QANTAS. Printed on 30 Dec 2011.Notice: After 13 Jan 2012 0901Z, this chart may no longer be valid. Disc 26-2011

JEPPESENJeppView 3.7.5.0

COMMS

COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMSLOST COMMSLOST COMMSLOST COMMSLOST

COMMSLOST COMMSLOST COMMSLOST COMMSLOST

D90.2

D80.4

347^

355^

17 NM

CHANGES:

JEPPESENWSSS/SINCHANGI

SINGAPORE, SINGAPORE

TEKONG116.5 VTKVTK

N01 24.9 E104 01.3

D

A

Apt Elev

22'1

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

Air Force (RSAF) Aircraft

A

.RNAV.STAR.

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

D-ATIS

128.6

3. RADAR required.

MAINTAIN

1ROUTING

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

a.

3. No clearance or instruction received from Singapore ATC:

Changi AptDirect distance from NYLON to:

10-2F

090^

180^

360^

3400'

2500'2100'090^

180^

360^

3400'

2100'1900'

MSA VTK VOR MSA SJ VOR

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.

last assigned flight level or 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

Refer to Singapore Special Procedures for radio communications failure procedure.

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

Singapore Special Procedures for missed approach procedure.

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/D104)

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

3000' - FL140MAX 220 KT

023^

22

1 TRANSITIONS

EXPECT RADARvectors for ILS

approach Rwy 20

1. For RNAV operations, aircraft shall be GNSS-equipped and meet RNP-1/P-RNAV standard of accuracy.

180^

PASPU ONE BRAVO(PASPU1B) ARRIVAL

or EXPECT RADAR vectors from ATC.

26 JAN 07

MAX 250 KT

At or above3000' 220 KTMAX

or as directed by ATC

At or belowFL250

BIKTA(M-751/B-469)

MABAL(N-892)

VEPLI(L-642)

Note 2. | JEPPESEN SANDERSON, INC., 2006, 2007. ALL RIGHTS RESERVED.

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

NOT TO SCALE

Licensed to QANTAS. Printed on 30 Dec 2011.Notice: After 13 Jan 2012 0901Z, this chart may no longer be valid. Disc 26-2011

JEPPESENJeppView 3.7.5.0

COMMSLOST COMMSLOST COMMSLOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS LOSTCOMMS LOSTCOMMS LOST

278^

273^

293^

296^

355^

326^

007^

033^

023^

D56.6

D41.3

D33.9

D12.9

D17.2

D22.6

D13.2

D30.0

D13.0

VTK

116.5

14 N

M

CHANGES:

JEPPESENWSSS/SINCHANGI

SINGAPORE, SINGAPORE

TEKONG

116.5

VTK

VTK

N01

24.9

E104

01.3

D

A

Apt Elev

22'1

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

A

.RNAV.STAR.

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

D-ATIS

128.6

3. RADAR required.

2. W

hen c

leare

d v

ia P

IMOK 2

B b

y S

ingapore

ATC:

MA

IN

TA

IN

1RO

UTIN

G

023^

NYLO

NN01

37.0

E104

06.4

203^

1. Set

transponder

to M

ode A

/C c

ode 7

600.

last

assig

ned f

light

level or

altitude

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

a.

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:

Refe

r to

Sin

gapore

Specia

l Pro

cedure

s f

or

radio

communic

ations f

ailure

pro

cedure

.

REKO

P(S

J R-

293/

D50

.0)

Cha

ngi

Apt

Dir

ect

dist

ance

fro

m B

IDUS

to:

and p

roceed o

n P

IMOK 2

B t

o B

IDUS, th

en d

irect

to N

YLON.

10-2G

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)

At

PIM

OK, tu

rn L

EFT a

nd t

rack 0

82^

to J

B. Then t

rack 0

86^

to A

LFA, th

en t

urn

LEFT a

nd t

rack 0

57^

to B

IDUS. Fro

m B

IDUS, EXPECT R

ADAR v

ecto

rs f

or

ILS

appro

ach R

wy 2

0.

113^

082^

086^

057^

16

23

7

10

PIM

OK

N01

26.8

E103

20.1

N01

30.6

E103

49.7

ALF

A

At

or a

bove

6000'

N01

35.9

E103

57.9

BID

US

3000'

- FL1

40

MA

X 2

20 K

T

SINJO

N11

3.5

SJS

J

N01

13.4

E103

51.3

D

JAYBE

E40

0 JB

JB

N01

30.0

E103

42.7

(SJ

R-33

3/D

18.6

)(V

TK R

-285

/D19

.3)

N01

33.1

E103

05.4

EXPE

CT

RAD

AR

vect

ors

for

ILS

appr

oach

Rw

y 20

.A576.

1. For RNAV operations, aircraft shall be GNSS-equipped and meet RNP-1/P-RNAV standard of accuracy.

PIMOK TWO BRAVO(PIMOK2B) ARRIVAL

or EXPECT RADAR vectors from ATC.

26 JAN 07

At

or a

bove

10000'

At

or a

bove

250 K

TM

AX7000'

At

or a

bove

220 K

TM

AX3000'

Note 2. | JEPPESEN SANDERSON, INC., 2006, 2007. ALL RIGHTS RESERVED.

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

NO

T TO

SCA

LE

Page 7: WSSS Charts

Licensed to QANTAS. Printed on 30 Dec 2011.Notice: After 13 Jan 2012 0901Z, this chart may no longer be valid. Disc 26-2011

JEPPESENJeppView 3.7.5.0

179^

185^

D41.2

D68.2

204^

D21.1

COMMSLOST COMMSLOST COMMSLOST COMMSLOST COMMSLOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS COMMSLOST COMMSLOST COMMSLOST COMMSLOST 17 NM

CHANGES:

JEPPESENWSSS/SINCHANGI

SINGAPORE, SINGAPORE

TEKONG116.5 VTKVTK

N01 24.9 E104 01.3

D

A

Apt Elev

22'1

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

Air Force (RSAF) Aircraft

A

.RNAV.STAR.

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

D-ATIS

128.6

3. RADAR required.

1ROUTING

Changi AptDirect distance from SAMKO to:

10-2H

090^

180^

360^

3400'

2500'2100'090^

180^

360^

3400'

2100'1900'

MSA VTK VOR MSA SJ VOR

(RWYS 02L/C)

SINJON113.5 SJSJ

N01 13.4 E103 51.3

D

FRO

M P

ARDI

.G579.348^

51

28

REPOV(SJ R-168/D57.9)

REMESN00 43.7E103 57.6

348^

2. When cleared via REMES 5A by Singapore ATC:MAINTAIN

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

last assigned flight level or altitude

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

Special Procedures for missed approach procedure.

b. From SAMKO commence descent and carry out

a.

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

3. No clearance or instruction received from Singapore ATC:Refer to Singapore Special Procedures for radio communications failure procedure.

and proceed on REMES 5A to SAMKO.

6000' - FL140MAX 220 KT

168^168^

At or belowFL250

22

168^

(SJ R-168/D30.2)

4000' - FL140MAX 220 KT

EXPECT RADARvectors for ILS

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

1. For RNAV operations, aircraft shall be GNSS-equipped and meet RNP-1/P-RNAV standard of accuracy.

or EXPECT RADAR vectors from ATC.

REMES FIVE ALPHA(REMES5A) ARRIVAL

10 AUG 07

6000'

MAX 250 KT

At or above

At or above4000'

MAX 220 KT

| JEPPESEN SANDERSON, INC., 2006, 2007. ALL RIGHTS RESERVED.

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

None.

NOT TO SCALE

Licensed to QANTAS. Printed on 30 Dec 2011.Notice: After 13 Jan 2012 0901Z, this chart may no longer be valid. Disc 26-2011

JEPPESENJeppView 3.7.5.0

COMMSLOST COMMSLOST COMMSLOST COMMSLOST COMMSLOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

1 79^

185^168^

115^

074^

047^

055^

D26.

2D11.0

D12.7

D22.5

D41.2

D30.2

D68.2

COMMSLOST COMMSLOST COMMSLOST COMMSLOST COMMSLOST

15 NM

CHANGES:

JEPPESENWSSS/SINCHANGI

SINGAPORE, SINGAPORE

TEKONG116.5 VTKVTK

N01 24.9 E104 01.3

D

A

Apt Elev

22'1

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

Air Force (RSAF) Aircraft

A

.RNAV.STAR.

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

D-ATIS

128.6

3. RADAR required.

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

1ROUTING

023^

203^

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

last assigned flight level or altitude

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

Special Procedures for missed approach procedure.

b. From NYLON commence descent and carry out

a.

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

3. No clearance or instruction received from Singapore ATC:Refer to Singapore Special Procedures for radio communications failure procedure.

Changi AptDirect distance from BIPOP to:

10-2J

090^

180^

360^

3400'

2500'2100'090^

180^

360^

3400'

2100'1900'

MSA VTK VOR MSA SJ VOR

(RWYS 20C/R)

SINJON113.5 SJSJ

N01 13.4 E103 51.3

DFROM

PARDI

.G579.348^

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.

EXPECT RADARvectors for ILS

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,

1. For RNAV operations, aircraft shall be GNSS-equipped and meet RNP-1/P-RNAV standard of accuracy.

REMES SIX BRAVO(REMES6B) ARRIVAL

or EXPECT RADAR vectors from ATC.

10 AUG 07

At or belowFL270

N00 43.7 E103 57.6

At or above

MAX 250 KT7000'

or as directedby ATC

At or above4000'

At or above3000'

MAX 220 KT

| JEPPESEN SANDERSON, INC., 2006, 2007. ALL RIGHTS RESERVED.

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

REPOV crossing altitude.

NOT TO SCALE

Page 8: WSSS Charts

Licensed to QANTAS. Printed on 30 Dec 2011.Notice: After 13 Jan 2012 0901Z, this chart may no longer be valid. Disc 26-2011

JEPPESENJeppView 3.7.5.0

JEPPESEN

1. Introduction

CHANGES:

WSSS/SINCHANGI

SINGAPORE, SINGAPORE.RNAV.STAR.10-2K-111 NOV 11 .Eff.17.Nov.

CONTINUOUS DESCENT OPERATION (CDO) FOR ARRIVALS

| JEPPESEN, 2011. ALL RIGHTS RESERVED.

FLIGHT CREW INSTRUCTIONS

2. Conditions for conducting a CDO

a) Changi Runway 02L/20R is open for landing; b) ILS for the intended runway of landing into Changi is in operation;

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

3. Requirements for individual flights

-LNAV and VNAV;

4. Preparations for CDO

Table 15. CDO Execution

C-D-O" "Request

-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

New temporary chart.

be met;

radio telephony phraseologies to execute the CDO procedures.

conditions for ILS procedures into Changi. In addition, the following conditions must

1.1 This flight crew instruction outlines the conditions, requirements and the associated

2.1 Pilots shall adhere to the instructions as depicted on the CDO RNAV STARs and the

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

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:

-flying Changi RNAV STARS and to abide by all speed and altitude restrictions depicted on the charts; -continuing on planned vertical path from RNAV STAR onto ILS of intended

and inform you accordingly.

c) Visibility is greater than or equal to 800 m; d) RVR is greater than or equal to 550 m for runway-in-use; and

GOBIK

IGARI (N891)

IPRIX (M753)

ESPOB (L642)

MELAS (N892)

TEGID (M767)

KAMIN (B348)

AGOBA (G580)

KIKOR (M774/A464)

SANOS (A576)

PARDI (G579)

TAROS (R469)

b) RNAV-equipped aircraft with FMC capable of:

FIR entry point RWY STAR Transition

02L

20R

PASPU 1K

PASPU 1LVEPLI

MELAS02L

20R

PASPU 1K

PASPU 1LMABAL

20R

02L LAVAX 1K

LAVAX 1LTOMAN

KIKOR02L

20R LAVAX 1L

LAVAX 1KATVIX

SANOS02L LAVAX 1K

20R LAVAX 1LAKTOD

GOBIK02L LAVAX 1K

GOBIKLAVAX 1L20R

PARDI02L REMES 1K

REMES 1L20R

TAROSBOBAG 1K02L

20R BOBAG 1L

ESPOB, IPRIX,

IGARI

TEGID, KAMIN,

AGOBA

runway of landing.

CDO flight will not reap any operational benefit, ATC shall disapprove your request

(a) Check if conditions for conducting the CDO are met; (b) Check if flight meets requirement for executing a CDO; and

4.1 To ensure that the CDO procedures can be effectively carried out, pilots are advised to abide by the following;

(c) Plan the lateral route in your FMC as shown in Table 1 based on FIR entry point and landing runway-in-use. The landing runway-in-use is available from D-ATIS.

Licensed to QANTAS. Printed on 30 Dec 2011.Notice: After 13 Jan 2012 0901Z, this chart may no longer be valid. Disc 26-2011

JEPPESENJeppView 3.7.5.0

JEPPESEN

CHANGES:

WSSS/SINCHANGI

SINGAPORE, SINGAPORE.RNAV.STAR.10-2K-211 NOV 11 .Eff.17.Nov.

| JEPPESEN, 2011. ALL RIGHTS RESERVED.

6. CDO Flight procedures

New temporary chart.

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

FLIGHT CREW INSTRUCTIONS (CONTD)

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

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

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

Once cleared for descent: -Start descent at the calculated FMC TOD based on the planned lateral and vertical

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

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

report ready for descent"

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

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

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

-If CDO flight has commenced and in the course of the CDO execution, Changi changes

5.6 Deviation from lateral or vertical path - At times, it may be necesary for ATC to take

6.1 The CDO flight shall track along the CDO RNAV STARs up to the intermediate segment

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

pilot and ATC.

traffic situation. When instructed, pilot shall comply with ATC instructions until such

terminate the CDO flight. In doing so, ATC shall use the following phrase to terminate the CDO flight:

and ILS procedure for the final and missed approaches for the respective runways. The

to aid pilot in landing into Changi.

[transition, if any] transition, Runway [runway-in-use].

such, please refrain from requesting for a change in landing runway (i.e 02C or 20C).

you off track temporarily or stop descent at an intermediate level due to a change in

5.7 Termination of a CDO - In the event that traffic complexity reaches a stage where

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.

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

"Request descent"

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

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

Runway [runway-in-use]"

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

6.2 In the event that airborne RNAV equipment fails, pilot shall inform ATC as soon as

path;

-With this clearance, pilot may proceed on remaining route of CDO flight procedure to

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

direction of its runway-in-use , i.e Rwy 02 to Rwy 20 or vice versa, ATC shall advise if the CDO flight can resume and issue the necessary re-clearance. Pilot shall then re-plan arrival route to the revised landing runway and advice ATC if the flight would still be able to meet all the required speed/altitude restrictions.

a time when informed that the CDO flight can resume.

cancellation of the CDO flight becomes necessary, ATC shall issue a clearance to

practicable. ATC shall then terminate CDO operation and resume with RADAR vectors

reaching 3000' from last assigned altitude so as to prevent leveling off. ATC shall endeavour to issue further descent clearance prior to the CDO flight

intercept on the appropriate ILS.

Page 9: WSSS Charts

Licensed to QANTAS. Printed on 30 Dec 2011.Notice: After 13 Jan 2012 0901Z, this chart may no longer be valid. Disc 26-2011

JEPPESENJeppView 3.7.5.0

JEPPESEN

COMMSLOST COMMSLOST COMMSLOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS LOSTCOMMS LOSTLOST

CHANGES:

WSSS/SINCHANGI

SINGAPORE, SINGAPORE

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:

MA

IN

TA

IN

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

SJS

J

N01

13.4

E103

51.3

D

1. Set

transponder

to M

ode A

/C c

ode 7

600.

last

assig

ned f

light

level or

altitude

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

a.

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:

Refe

r to

Sin

gapore

Specia

l Pro

cedure

s f

or

radio

communic

ations f

ailure

pro

cedure

.

090^

180^ 360^

3400

'

2500

'

2100

'

MSA

SJ

VO

R

11 NOV 11 10-2L-1

| JEPPESEN, 2011. ALL RIGHTS RESERVED.

Fro

m A

SUNA t

o B

OBAG, to

BOKIP

, to

SAMKO, to

SADET,

RO

UT

IN

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

New temporary procedure.

.Eff.17.Nov.

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'

FROM 0000 UTC 17 NOV 2011 TO 2359 UTC 16 FEB 2012FOR USE DURING CONTINUOUS DESCENT OPERATION (CDO) TRIAL

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

2. RNAV 1.3. RADAR required.

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

Licensed to QANTAS. Printed on 30 Dec 2011.Notice: After 13 Jan 2012 0901Z, this chart may no longer be valid. Disc 26-2011

JEPPESENJeppView 3.7.5.0

JEPPESEN

COMMSLOST COMMSLOST LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMSCOMMS LOSTCOMMS LOST

CHANGES:

WSSS/SINCHANGI

SINGAPORE, SINGAPORE

TEKONG

116.5

VTK

VTK

N01

24.9

E104

01.3

D

1

.RNAV.STAR.

2. W

hen c

leare

d v

ia B

OBAG 1

L b

y S

ingapore

ATC:

MA

IN

TA

IN

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*1

16.0 B

TMB

TM

N01

08.2

E104

08.0

D

1. Set

transponder

to M

ode A

/C c

ode 7

600.

last

assig

ned f

light

level or

altitude

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

a.

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:

Refe

r to

Sin

gapore

Specia

l Pro

cedure

s f

or

radio

communic

ations f

ailure

pro

cedure

.

090^

180^ 360^

3400

'

2100

'

1900

'

MSA

VTK

VO

R

11 NOV 11

At

or a

bove

4000'

RO

UT

IN

G

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

10-2M-1

BIP

AL

N01

33.1

E104

03.9

IDURO

N01

26.7

E104

01.1

285^

203^

| JEPPESEN, 2011. ALL RIGHTS RESERVED.New temporary procedure.

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

.Eff.17.Nov.

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,

FROM 0000 UTC 17 NOV 2011 TO 2359 UTC 16 FEB 2012FOR USE DURING CONTINUOUS DESCENT OPERATION (CDO) TRIAL

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

3. RADAR required.2. RNAV 1.

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

- 4

2.2

NM

IDURO -

4.5

NM

Page 10: WSSS Charts

Licensed to QANTAS. Printed on 30 Dec 2011.Notice: After 13 Jan 2012 0901Z, this chart may no longer be valid. Disc 26-2011

JEPPESENJeppView 3.7.5.0

JEPPESEN

COMMSLOST COMMSLOST LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMSCOMMS LOSTCOMMS LOST

CHANGES:

WSSS/SINCHANGI

SINGAPORE, SINGAPORE

1

.RNAV.STAR.2. W

hen c

leare

d v

ia L

AVAX 1

K b

y S

ingapore

ATC:

MA

IN

TA

IN

1. Set

transponder

to M

ode A

/C c

ode 7

600.

last

assig

ned f

light

level or

altitude

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

a.

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:

Refe

r to

Sin

gapore

Specia

l Pro

cedure

s f

or

radio

communic

ations f

ailure

pro

cedure

.

GO

BIK

TO

MA

N

283^

297^

316^

291^

335^

233^

269^

195

21

20

17

46

21

90

94

TOMAN

GO

BIK

ATV

IX

AKT

OD

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

AKTO

D

GO

BIK

ATVIX

KA

RTO

TO

MA

N

SINJO

N11

3.5

SJS

J

N01

13.4

E103

51.3

D

IGNO

NN01

08.8

E104

13.0

SA

NA

T

266^

14

14

11 NOV 11

[LAVA1K](RWY 02L)

LAVAX ONE KILO (LAVAX1K) ARRIVALM

SA S

J VO

R

Fro

m A

KTOD t

o I

KIM

A, to

IBULA, to

LAVAX.

Fro

m T

OMAN t

o K

ARTO, to

KEXAS, to

LAVAX.

AK

TO

D

ATV

IX

TRA

NSIT

IO

NS

RO

UT

IN

G

S00

24.8

E105

59.6

N00

02.4

E106

14.9

N00

43.2

E104

55.0

N00

00.0

E108

06.1

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

| JEPPESEN, 2011. ALL RIGHTS RESERVED.New temporary procedure.

10-2N-1

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

.

.Eff.17.Nov.

Fro

m A

TVIX

to I

KIM

A, to

IBULA, to

LAVAX.

Fro

m G

OBIK

to I

KIM

A, to

IBULA, to

LAVAX.

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

FROM 0000 UTC 17 NOV 2011 TO 2359 UTC 16 FEB 2012FOR USE DURING CONTINUOUS DESCENT OPERATION (CDO) TRIAL

3. RADAR required.2. RNAV 1.1. RNAV (GNSS) CDO.Alt Set: hPa Trans level: FL130 Trans alt: 11000'

NO

T TO

SCA

LE

WA

YPO

IN

T T

O T

HRESH

OLD

DISTA

NC

E

AKTOD -

182.2

NM

ATVIX

- 1

78.2

NM

GOBIK

- 2

83.2

NM

IBULA -

68.2

NM

IGNON -

31.5

NM

IKIM

A -

88.2

NM

ADNIK

- 4

.5 N

MKARTO -

114.2

NM

KEXAS -

68.2

NM

LAVAX -

47.2

NM

SADET -

11.7

NM

SANAT -

17.6

NM

TOM

AN -

131.2

NM

Licensed to QANTAS. Printed on 30 Dec 2011.Notice: After 13 Jan 2012 0901Z, this chart may no longer be valid. Disc 26-2011

JEPPESENJeppView 3.7.5.0

JEPPESEN

COMMSLOST COMMSLOST COMMSLOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMS LOSTCOMMS LOSTLOST

CHANGES:

WSSS/SINCHANGI

SINGAPORE, SINGAPORE

TEKONG

116.5

VTK

VTK

N01

24.9

E104

01.3

D

1

.RNAV.STAR.

2. W

hen c

leare

d v

ia L

AVAX 1

L b

y S

ingapore

ATC:

MA

IN

TA

IN

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.

last

assig

ned f

light

level or

altitude

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

a.

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:

Refe

r to

Sin

gapore

Specia

l Pro

cedure

s f

or

radio

communic

ations f

ailure

pro

cedure

.

GO

BIK

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

N01

10.3

E104

48.3

KEXA

S

269^

46

233^

17

TOMAN

KA

RTO

TO

MA

N

283^

297^

316^

195

90

GO

BIK

ATV

IX

GO

BIK

ATVIX

291^

20

94AKT

OD

IKIM

A

AKTO

D

11 NOV 11

At

or a

bove

8000'

4000'

At

or a

bove

(RWY 20R)

[LAVA1L]

N01

11.4

E105

33.7

N01

21.8

E105

47.3

N00

43.2

E104

55.0

S00

24.8

E105

59.6

286^

203^

7

7

BIP

AL

N01

33.1

E104

03.9

AK

TO

D

AT

VIX

Fro

m A

KTOD t

o I

KIM

A, to

IBULA, to

LAVAX.

Fro

m G

OBIK

to I

KIM

A, to

IBULA, to

LAVAX.

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

NSIT

IO

NS

RO

UT

IN

G

N00

02.4

E106

14.9

N00

00.0

E108

06.1

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

| JEPPESEN, 2011. ALL RIGHTS RESERVED.New temporary procedure.

10-2P-1 .Eff.17.Nov.

Fro

m A

TVIX

to I

KIM

A, to

IBULA, to

LAVAX.

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'

FROM 0000 UTC 17 NOV 2011 TO 2359 UTC 16 FEB 2012FOR USE DURING CONTINUOUS DESCENT OPERATION (CDO) TRIAL

3. RADAR required.

Alt Set: hPa Trans level: FL130 Trans alt: 11000'1. RNAV (GNSS) CDO.2. RNAV 1.

NO

T TO

SCA

LE

WA

YPO

IN

T T

O T

HRESH

OLD

DIST

AN

CE

AKTOD -

182.2

NM

ATVIX

- 1

78.2

NM

BIP

AL -

11.5

NM

BIP

OP -

18.2

NM

DOVAN -

30.2

NM

GOBIK

- 2

83.2

NM

IBULA -

68.2

NM

TOM

AN -

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

Page 11: WSSS Charts

Licensed to QANTAS. Printed on 30 Dec 2011.Notice: After 13 Jan 2012 0901Z, this chart may no longer be valid. Disc 26-2011

JEPPESENJeppView 3.7.5.0

JEPPESEN

COMMS

COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMSLOST COMMSLOST COMMSLOST COMMSLOST

COMMSLOST COMMSLOST COMMSLOST COMMSLOST

CHANGES:

WSSS/SINCHANGI

SINGAPORE, SINGAPORE

1

.RNAV.STAR.

MAINTAIN

NYLON

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

a.

3. No clearance or instruction received from Singapore ATC:

090^

180^

360^

3400'

2500'

2100'

MSA SJ VOR

VEPLI

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^

last assigned flight level or 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

Refer to Singapore Special Procedures for radio communications failure procedure.

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

Singapore Special Procedures for missed approach procedure.

11 NOV 11

At or belowFL270

10-2Q-1

[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

| JEPPESEN, 2011. ALL RIGHTS RESERVED.

PASPU ONE KILO (PASPU1K) ARRIVAL

.Eff.17.Nov.

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

Air Force (RSAF) Aircraft

1

Apt Elev

22'D-ATIS

128.6

MAX 250 KT

At or above6000'

MAX 220 KT

At or above4000'

172^10

New temporary procedure.

FROM 0000 UTC 17 NOV 2011 TO 2359 UTC 16 FEB 2012FOR USE DURING CONTINUOUS DESCENT OPERATON (CDO) TRIAL

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.

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

Licensed to QANTAS. Printed on 30 Dec 2011.Notice: After 13 Jan 2012 0901Z, this chart may no longer be valid. Disc 26-2011

JEPPESENJeppView 3.7.5.0

JEPPESEN

COMMS

COMMS

LOST

COMMS

LOST

COMMS

LOST

COMMSLOST COMMSLOST COMMSLOST COMMSLOST

COMMSLOST COMMSLOST COMMSLOST COMMSLOST

CHANGES:

WSSS/SINCHANGI

SINGAPORE, SINGAPORE

TEKONG116.5 VTKVTK

N01 24.9 E104 01.3

D

1

.RNAV.STAR.

MAINTAIN

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

a.

3. No clearance or instruction received from Singapore ATC:

090^

180^

360^

3400'

2100'

1900'

MSA VTK VOR

last assigned flight level or 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

Refer to Singapore Special Procedures for radio communications failure procedure.

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

11 NOV 11

At or belowFL250

10-2S-1

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

| JEPPESEN, 2011. ALL RIGHTS RESERVED.New temporary procedure.

.Eff.17.Nov.

Singapore Special Procedures for missedapproach procedure.

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

Air Force (RSAF) Aircraft

1

Apt Elev

22'D-ATIS

128.6

MAX 250 KT

At or above6000'

FROM 0000 UTC 17 NOV 2011 TO 2359 UTC 16 FEB 2012FOR USE DURING CONTINUOUS DESCENT OPERATION (CDO) TRIAL

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.

NOT TO SCALE

THRESHOLD DISTANCEWAYPOINT TO

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

Page 12: WSSS Charts

Licensed to QANTAS. Printed on 30 Dec 2011.Notice: After 13 Jan 2012 0901Z, this chart may no longer be valid. Disc 26-2011

JEPPESENJeppView 3.7.5.0

JEPPESEN

COMMSLOST COMMSLOST COMMSLOST COMMSLOST COMMSLOST

COMMS

LOST

COMMS

LOST

LOSTC

OMMS

COMMS

LOST

COMMS

LOST

CHANGES:

WSSS/SINCHANGI

SINGAPORE, SINGAPORE.RNAV.STAR.

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:MAINTAIN

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

last assigned flight level or altitude

close as possible to EAT or ETA.

Special Procedures for missed approach procedure.

b. From ADNIK commence descent and carry out

a.

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

3. No clearance or instruction received from Singapore ATC:Refer to Singapore Special Procedures for radio communications failure procedure.

and proceed on REMES 1K to ADNIK.

22

N01 05.5E103 52.9

SAMKO

N00 16.4E104 03.0

11 NOV 11 10-2T-1

[REME1K](RWY 02L)

SADETN01 10.1E103 54.2

ADNIKN01 16.9E103 56.9

015^

023^

5

7

ROUTING

| JEPPESEN 2011. ALL RIGHTS RESERVED.New temporary procedure.

appropriate landing procedure for Rwy 02L as

.Eff.17.Nov.

REMES ONE KILO (REMES1K) ARRIVAL

MAX 220 KT

At or above4000'

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

1

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

Air Force (RSAF) Aircraft

1

Apt Elev

22'D-ATIS

128.6

FROM 0000 UTC 17 NOV 2011 TO 2359 UTC 16 FEB 2012FOR USE DURING CONTINUOUS DESCENT OPERATION (CDO) TRIAL

3. RNAV (GNSS) CDO.

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

At or belowFL250

MAX 250 KT

At or above6000'

1. RADAR required. 2. RNAV 1.

NOT TO SCALE

WAYPOINT TO THRESHOLD DISTANCE

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

ADNIK - 4.5 NM

Licensed to QANTAS. Printed on 30 Dec 2011.Notice: After 13 Jan 2012 0901Z, this chart may no longer be valid. Disc 26-2011

JEPPESENJeppView 3.7.5.0

JEPPESEN

COMMSLOST COMMSLOST COMMSLOST COMMSLOST COMMSLOST

COMMS

COMMS

LOST

COMMS

LOST

COMMSLOST COMMSLOST COMMSLOST COMMSLOST COMMSLOST

CHANGES:

WSSS/SINCHANGI

SINGAPORE, SINGAPORE

TEKONG116.5 VTKVTK

N01 24.9 E104 01.3

D

1

.RNAV.STAR.

2. When cleared via REMES 1L by Singapore ATC:MAINTAIN

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

last assigned flight level or altitude

close as possible to EAT or ETA.

Special Procedures for missed approach procedure.

b. From IDURO commence descent and carry out

a.

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

3. No clearance or instruction received from Singapore ATC:Refer to Singapore Special Procedures for radio communications failure procedure.

090^

180^

360^

3400'

2100'

1900'

MSA VTK VOR

023^

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

11 NOV 11

At or above4000'

New temporary procedure.

10-2U-1

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

MAX 220 KTAt or above

3000'

MAX 250 KTAt or above

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.

| JEPPESEN, 2011. ALL RIGHTS RESERVED.

.Eff.17.Nov.

Apt Elev

22'D-ATIS

128.6

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

Air Force (RSAF) Aircraft

1

FROM 0000 UTC 17 NOV 2011 TO 2359 UTC 16 FEB 2012FOR USE DURING CONTINUOUS DESCENT OPERATION (CDO) TRIAL

3. RNAV (GNSS) CDO.

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

NOT TO SCALE

THRESHOLD DISTANCEWAYPOINT TO

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

Page 13: WSSS Charts

Licensed to QANTAS. Printed on 30 Dec 2011.Notice: After 13 Jan 2012 0901Z, this chart may no longer be valid. Disc 26-2011

JEPPESENJeppView 3.7.5.0

| 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

Licensed to QANTAS. Printed on 30 Dec 2011.Notice: After 13 Jan 2012 0901Z, this chart may no longer be valid. Disc 26-2011

JEPPESENJeppView 3.7.5.0

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

SINGAPORE, SINGAPORECHANGI

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 1020m02C 2360m

20C 5945m

20R 8370m

10-3A26 JAN 07

Page 14: WSSS Charts

Licensed to QANTAS. Printed on 30 Dec 2011.Notice: After 13 Jan 2012 0901Z, this chart may no longer be valid. Disc 26-2011

JEPPESENJeppView 3.7.5.0

JEPPESEN

COMMSLOST COMMSLOST COMMSLOST COMMSLOSTLOST

COMMSLOST COMMSLOST COMMSLOST COMMSLOST LOST

333^

D19.3

D18.6

285^

COMMS

COMMS

LOST

CHANGES:

WSSS/SINCHANGI

SINGAPORE, SINGAPORE

SID

10-3A1

Apt Elev

22'

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

| JEPPESEN, 2009. ALL RIGHTS RESERVED.

ROUTING

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

2. Communications failure occurs immediately

communications failure.

INITIAL CLIMB

022^

023^

001^

001 ^

266^297^

VIDAX

NUGSI

TOREKN01 43.3 E104 01.6

ADPAXN01 44.0 E103 15.6

216

24

30

FL140

FL140

MAA FL240

MAA FL240ADPAX 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 assignedaltitude. Thereafter refer to SingaporeSpecial Procedures on radio

1. These SIDs will be assigned during air defense exercises.

090^

180^

360^

3400'

2100'1900'

MSA VTK VOR

090^

180^

360^

3400'

2500'2100'

MSA SJ VOR

2. RNAV 1 (GNSS, DME/DME). 3. For RNAV operations, aircraft shallbe GNSS-equipped and meet RNP-1/P-RNAV standard of accuracy.4. RADAR required. 5. All SIDs include noise preferential routes.6. Initial departure climb altitude is 3000' or as directed by ATC.7. Cruising levels will be issued after take-off by Singapore RADAR.8. Aircraft unable to fly SID profile shall inform ATC prior todeparture and to EXPECT RADAR vectoring, if necessary.

DEPARTURES

ADPAX 1UADPAX 1W

(RWY 02L),

(RWY 02C)

To VIDAX on course 022^.

To VTK on course 023^.

To TOREK. Climb on track 001^, at or above 6000'

ADPAX 1U (RWY 02L)

ADPAX 1W (RWY 02C)

JB (JAYBEE), to ADPAX. turn RIGHT direct to NUGSI. Then to

At or aboveFL140

6 NMDirect distance from Changi Apt

(Rwy 02L) to: VIDAX 4 NM(Rwy 02C) to: VTK

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

SINJON113.5 SJSJ

N01 13.4 E103 51.3

D

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

Air Force (RSAF) Aircraft

JAYBEE

400 JBJB

N01 30.0 E103 42.7

11 DEC 09

None.

NOT TO SCALE

Licensed to QANTAS. Printed on 30 Dec 2011.Notice: After 13 Jan 2012 0901Z, this chart may no longer be valid. Disc 26-2011

JEPPESENJeppView 3.7.5.0

JEPPESEN

COMMSLOST COMMSLOST COMMSLOST COMMSLOSTLOST

COMMS

COMMS

LOST

COMMSLOST COMMSLOST COMMSLOST COMMSLOST LOST

097D6.9

188^

D23.4

D13.5

149^

D7.

6

053^

CHANGES:

WSSS/SINCHANGI

SINGAPORE, SINGAPORE

SID

10-3A2

Apt Elev

22'

.RNAV.SID.

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

Air Force (RSAF) Aircraft

A

Trans level: FL130 Trans alt: 11000'

| JEPPESEN, 2009. ALL RIGHTS RESERVED.

ROUTING

090^

180^

360^

3400'

2500'2100'090^

180^

360^

3400'

2100'1900'

MSA VTK VOR MSA SJ VOR

4 NMDirect distance from Changi Apt

(Rwy 20C) to: SUDPO

75 100 150 200 250 300Gnd speed-KT

1519126610137605063805.0% V/V (fpm)

3.3% V/V (fpm) 251 334 501 668 835 1003

, then 3.3%. 400'minimum net climb gradient of 5.0% untilreaching or passing

Rwys 20C/R: Departures shall be on a

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

2. Communications failure occurs immediately

communications failure.

(Rwy 20R) to: SUNVA 4 NM

INITIAL CLIMB

A

203^

180^5

N01 17.5E103 58.1

(VTK R-203/D8.0)

SUDPO

SUSIN

DUNAL

11

271^

28

BOBAG(SJ R-243/D24.0)

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

FL140At or above

SUNVA(VTK R-210/D8.0)

N01 17.9E103 57.4 20

3^

171^5

(SJ R-059/D8.0)

(VTK R-195/D12.8)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 FL240

FL140

DEPARTURES

ADPAX 1VADPAX 1X

(RWY 20R),

(RWY 20C)ADPAXN01 44.0E103 15.6

BASIXN01 10.0E103 24.9

N01 12.5 E103 58.1

1. These SIDs will be assigned during air defense exercises.

ADPAX 1V (RWY 20R)

ADPAX 1X (RWY 20C)

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

Special Procedures on radioaltitude. Thereafter refer to Singapore

To SUNVA on course 203^, then to SUSIN.

To SUDPO on course 203^, then to SUSIN.

2. RNAV 1 (GNSS, DME/DME). 3. For RNAV operations, aircraft shall beGNSS-equipped and meet RNP-1/P-RNAV standard of accuracy. 4. RADAR required.5. 1 The restriction to cross SUDPO or SUNVA at or above 2000' is applicablebetween 2301-1100 UTC. All departure aircraft on Runways 20C/R issued with headinginstructions by ATC shall also cross VTK 8 DME at or above 2000' between 2301-1100UTC. If the altitude restriction cannot be complied with, the pilot-in-command of anaircraft departing on Runways 20C/R shall inform ATC during the time when theaircraft commences taxiing to the holding point for departure. 6. All SIDs includenoise preferential routes. 7. Initial departure climb altitude is 3000' or as directed byATC. 8. Cruising levels will be issued after take-off by Singapore RADAR.

1At or above

2000' 1At or above

2000'

9. Aircraft unable to fly SID profile shall inform ATC prior to departure and toEXPECT RADAR vectoring, if necessary.

At SUSIN to DUNAL, BOBAG, BASIX, ADPAX.

11 DEC 09

Lost comm note.

NOT TO SCALE

Page 15: WSSS Charts

Licensed to QANTAS. Printed on 30 Dec 2011.Notice: After 13 Jan 2012 0901Z, this chart may no longer be valid. Disc 26-2011

JEPPESENJeppView 3.7.5.0

083^

057^

059^

097^

195^

150^161^138^

D9.4

D23.2

D24.2

D39.0D34.1

D8.0

D6.9

D12.8

COMMSLOST COMMSLOST COMMSLOST LOSTCOMMS

LOST

COMMS

LOST

COMMS

LOST

LOST

COMMSLOST COMMSLOST COMMSLOST LOST

75 100 150 200 250 300

9 NM 4 NM

CHANGES:

JEPPESENWSSS/SINCHANGI

SINGAPORE, SINGAPORE

SID

SINJON

113.5 SJSJ

N01 13.4 E103 51.3

D

TEKONG116.5 VTKVTK

N01 24.9 E104 01.3

D

Trans level: FL130 Trans alt: 11000'

10-3B

Direct distance from Changi Apt

Gnd speed-KT

, then 3.3%. 400'

1519126610137605063805.0% V/V(fpm)

3.3% V/V(fpm) 251 334 501 668 835 1003

For minimum climb gradient criteria:

minimum net climb gradient of 5.0% untilreaching or passing

A

Apt Elev

22'

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

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

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

1 2

2At or above

2000'

.RNAV.SID.

1 INITIAL CLIMB

1ROUTING

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

Air Force (RSAF) Aircraft

A

ANITO FIVE ALPHA (ANI5A),

ANI 5A(RWY 02C)

ANI 4B(RWY 20C)

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

(Rwy 02C) to: TOKIM(Rwy 20C) to: SUDPO

TOKIM(SJ R-037/D20.1)

N01 29.6E104 03.3

(VTK R-023/D5.0)

2000'At or above

(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.

to the last assigned altitude.

7600.1. Set transponder to Mode A/C code

2. Communications failure occurs immediately after departure on:

Thereafter refer to Singapore Special Procedures on radio communications failure.

Thereafter refer to Singapore Special Procedures on radio communications failure.

177^

.B470.

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

and track 173^ to DOBLU. Then track 177^ to DOSNO.

track 120^ to DOBLU. Turn RIGHT and track 177^ to DOSNO.

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

090^

180^

360^

3400'

2500'2100'090^

180^

360^

3400'

2100'1900'

MSA VTK VOR MSA SJ VOR(RWYS 02C, 20C)

ANITO FOUR BRAVO (ANI4B)

1. For RNAV operations, aircraft shall be GNSS-equipped and meet RNP-1/P-RNAV

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

DEPARTURES

18 MAY 07

or EXPECT RADAR vectors from ATC. 3.

| JEPPESEN SANDERSON, INC., 2006, 2007. ALL RIGHTS RESERVED.Note 3.

standard of accuracy. 2. Non-RNP-1/P-RNAV approved aircraft shall fly this as a basic RNAV (B-RNAV) procedure The restriction to cross SUDPO at or above 2000' is applicable between 2301-1100 UTC.

6. On initial contact when requesting ATC, inform ATC of the flight level aircraft can

8. RADAR required.cross ANITO. 7. Cruising levels will be issued after take-off by Singapore RADAR.

4000'At or above

All departure aircraft on Runway 20C issued with heading instructions by ATC shallalso 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 departingon Runway 20C shall inform ATC during the time when the aircraft commences taxiingto the holding point for departure. 4. All SIDs include noise preferential routes.5. Initial departure climb altitude is 3000' or as directed by ATC.

Rwy 20C-Departures shall be on a

023^

NOT TO SCALE

Licensed to QANTAS. Printed on 30 Dec 2011.Notice: After 13 Jan 2012 0901Z, this chart may no longer be valid. Disc 26-2011

JEPPESENJeppView 3.7.5.0

083^

057^

053^

097^

195^

150^161^138^

D9.4

D23.2

D24.2

D39.0D34.1

D7.6

D6.9

D12.8

COMMSLOST COMMSLOST COMMSLOST LOST

COMMSLOST COMMSLOST COMMSLOST LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

LOST

083^

057^

053^

097^

195^

150^161^138^

D9.4

D23.2

D24.2

D39.0D34.1

D7.6

D6.9

D12.8

COMMSLOST COMMSLOST COMMSLOST LOST

COMMSLOST COMMSLOST COMMSLOST LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

LOST

75 100 150 200 250 300

CHANGES:

JEPPESENWSSS/SINCHANGI

SINGAPORE, SINGAPORE

SID

SINJON

113.5 SJSJ

N01 13.4 E103 51.3

D

TEKONG116.5 VTKVTK

N01 24.9 E104 01.3

D

10-3C

Gnd speed-KT

, then 3.3%. 400'

1519126610137605063805.0% V/V(fpm)

3.3% V/V(fpm) 251 334 501 668 835 1003

For minimum climb gradient criteria:

minimum net climb gradient of 5.0% untilreaching or passing

A

Apt Elev

22'

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

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

115^

173^

120^

203^

172^

177^

9

22

16

17

5

N01 29.9E104 02.5

(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

(SJ R-113/D24.0)DOBLU

.RNAV.SID.

1 INITIAL CLIMB

1ROUTING

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

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

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

Air Force (RSAF) Aircraft

A

ANI 5E(RWY 02L)

ANI 4F(RWY 20R)

DOSNON00 48.0 E104 14.2

to the last assigned altitude.

ANIT

O F

IVE E

CHO

(ANI5E)

(ANI4F)

ANITO FIVE ECHO (ANI5E),

9 NM 4 NM

Direct distance from Changi Apt(Rwy 02L) to: TOPOM(Rwy 20R) to: SUNVA

2At or above

2000'

(SJ R-034/D20.0)

DOSNON00 48.0 E104 14.2

75

.B470.

150^

(RWYS 02L, 20R)

ANITO FOUR FOXTROT (ANI4F)

2000'At or above

4000'At or above

to the last assigned altitude.

7600.1. Set transponder to Mode A/C code

2. Communications failure occurs immediately after departure on:

Thereafter refer to Singapore Special Procedures on radio communications failure.

Thereafter refer to Singapore Special Procedures on radio communications failure.

N01 03.8 E104 13.3

At or belowor as directed by ATC

6000'

and track 173^ to DOBLU. Then track 177^ to DOSNO.

track 120^ to DOBLU. Turn RIGHT and track 177^ to DOSNO.

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

ANITO FOUR

FOXTROT

090^

180^

360^

3400'

2500'2100'090^

180^

360^

3400'

2100'1900'

MSA VTK VOR MSA SJ VOR

Trans level: FL130 Trans alt: 11000'

ANITO(SJ R-146/D109)

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

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

DEPARTURES

18 MAY 07

standard of accuracy. 2. Non-RNP-1/P-RNAV approved aircraft shall fly this as a 1. For RNAV operations, aircraft shall be GNSS-equipped and meet RNP-1/P-RNAV

or EXPECT RADAR vectors from ATC. 3. restriction to cross SUNVA at or above 2000' is applicable between 2301-1100 UTC.

cross ANITO. 7. Cruising levels will be issued after take-off by Singapore RADAR.

The 21basic RNAV (B-RNAV) procedure

8. RADAR required.

6. On initial contact when requesting ATC, inform ATC of the flight level aircraft can

Note 3. | JEPPESEN SANDERSON, INC., 2006, 2007. ALL RIGHTS RESERVED.

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

on Runway 20R shall inform ATC during the time when the aircraft commences taxiing

5. Initial departure climb altitude is 3000' or as directed by ATC. to the holding point for departure. 4. All SIDs include noise preferential routes.

All departure aircraft on Runway 20R issued with heading instructions by ATC shall

restriction cannot be complied with, the pilot-in-command of an aircraft departing

Rwy 20R-Departures shall be on a

75 100 150 200 250 300

CHANGES:

JEPPESENWSSS/SINCHANGI

SINGAPORE, SINGAPORE

SID

SINJON

113.5 SJSJ

N01 13.4 E103 51.3

D

TEKONG116.5 VTKVTK

N01 24.9 E104 01.3

D

10-3C

Gnd speed-KT

, then 3.3%. 400'

1519126610137605063805.0% V/V(fpm)

3.3% V/V(fpm) 251 334 501 668 835 1003

For minimum climb gradient criteria:

minimum net climb gradient of 5.0% untilreaching or passing

A

Apt Elev

22'

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

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

115^

173^

120^

203^

172^

177^

9

22

16

17

5

N01 29.9E104 02.5

(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

(SJ R-113/D24.0)DOBLU

.RNAV.SID.

1 INITIAL CLIMB

1ROUTING

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

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

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

Air Force (RSAF) Aircraft

A

ANI 5E(RWY 02L)

ANI 4F(RWY 20R)

DOSNON00 48.0 E104 14.2

to the last assigned altitude.

ANIT

O F

IVE E

CHO

(ANI5E)

(ANI4F)

ANITO FIVE ECHO (ANI5E),

9 NM 4 NM

Direct distance from Changi Apt(Rwy 02L) to: TOPOM(Rwy 20R) to: SUNVA

2At or above

2000'

(SJ R-034/D20.0)

DOSNON00 48.0 E104 14.2

75

.B470.

150^

(RWYS 02L, 20R)

ANITO FOUR FOXTROT (ANI4F)

2000'At or above

4000'At or above

to the last assigned altitude.

7600.1. Set transponder to Mode A/C code

2. Communications failure occurs immediately after departure on:

Thereafter refer to Singapore Special Procedures on radio communications failure.

Thereafter refer to Singapore Special Procedures on radio communications failure.

N01 03.8 E104 13.3

At or belowor as directed by ATC

6000'

and track 173^ to DOBLU. Then track 177^ to DOSNO.

track 120^ to DOBLU. Turn RIGHT and track 177^ to DOSNO.

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

ANITO FOUR

FOXTROT

090^

180^

360^

3400'

2500'2100'090^

180^

360^

3400'

2100'1900'

MSA VTK VOR MSA SJ VOR

Trans level: FL130 Trans alt: 11000'

ANITO(SJ R-146/D109)

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

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

DEPARTURES

18 MAY 07

standard of accuracy. 2. Non-RNP-1/P-RNAV approved aircraft shall fly this as a 1. For RNAV operations, aircraft shall be GNSS-equipped and meet RNP-1/P-RNAV

or EXPECT RADAR vectors from ATC. 3. restriction to cross SUNVA at or above 2000' is applicable between 2301-1100 UTC.

cross ANITO. 7. Cruising levels will be issued after take-off by Singapore RADAR.

The 21basic RNAV (B-RNAV) procedure

8. RADAR required.

6. On initial contact when requesting ATC, inform ATC of the flight level aircraft can

Note 3. | JEPPESEN SANDERSON, INC., 2006, 2007. ALL RIGHTS RESERVED.

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

on Runway 20R shall inform ATC during the time when the aircraft commences taxiing

5. Initial departure climb altitude is 3000' or as directed by ATC. to the holding point for departure. 4. All SIDs include noise preferential routes.

All departure aircraft on Runway 20R issued with heading instructions by ATC shall

restriction cannot be complied with, the pilot-in-command of an aircraft departing

Rwy 20R-Departures shall be on a

023^

023^

NOT TO SCALENOT TO SCALE

Page 16: WSSS Charts

Licensed to QANTAS. Printed on 30 Dec 2011.Notice: After 13 Jan 2012 0901Z, this chart may no longer be valid. Disc 26-2011

JEPPESENJeppView 3.7.5.0

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^

COMMSLOST COMMSLOST COMMSLOST LOST

COMMSLOST COMMSLOST COMMSLOST LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

LOST

75 100 150 200 250 300

090^

180^

360^

3400'

2500'2100'

CHANGES:

JEPPESENWSSS/SINCHANGI

SINGAPORE, SINGAPORE

SID

SINJON113.5 SJSJ

N01 13.4 E103 51.3

D

TEKONG116.5 VTKVTK

N01 24.9 E104 01.3

D

10-3D

Gnd speed-KT

1519126610137605063805.0% V/V(fpm)

3.3% V/V(fpm) 251 334 501 668 835 1003

A

Apt Elev

22'

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

115^

173^

203^

180^

9

225

N01 17.5E103 58.1

(VTK R-203/D8.0)SUDPO

N01 12.5E103 58.1

SUSIN

N01 26.1E104 10.7

DOKTA

N01 03.8E104 13.3

DOBLU

2At or above

2000'

.RNAV.SID.

1 INITIAL CLIMB

4000'At or above

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

Air Force (RSAF) Aircraft

A

BOG 1A(RWY 02C)

BOG 1B(RWY 20C)

BO

BA

G O

NE A

LPHA

(BOG1A

)

TOKIM(SJ R-037/D20.1)

N01 29.6E104 03.3

(VTK R-023/D5.0)

BOBAG ONE ALPHA (BOG1A),

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

At or above4000'

N01 01.6E103 58.1

DUNAL

11

BO

BA

G O

NE

(BOG1B)

BRA

VO

262^

272^.R469.15

28

BOBAG(SJ R-243/D24.0)

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

9 NM 4 NM

Direct distance from Changi Apt

, then 3.3%. 400'

For minimum climb gradient criteria:

minimum net climb gradient of 5.0% untilreaching or passing

Rwy 20C- Departures shall be on a

(Rwy 02C) to: TOKIM(Rwy 20C) to: SUDPO

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.

to the last assigned altitude.

7600.1. Set transponder to Mode A/C code

2. Communications failure occurs immediately after departure on:

Thereafter refer to Singapore Special Procedures on radio communications failure.

Thereafter refer to Singapore Special Procedures on radio communications failure.

At or below6000'

or as directedby ATC

10000'At or above

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

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

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

(RWYS 02C, 20C)

BOBAG ONE BRAVO (BOG1B)090^

180^

360^

3400'

2100'1900'

MSA VTK VOR MSA SJ VOR

Trans level: FL130 Trans alt: 11000'1. For RNAV operations, aircraft shall be GNSS-equipped and meet RNP-1/P-RNAV

DEPARTURES

standard of accuracy. 2. Non-RNP-1/P-RNAV approved aircraft shall fly this as a

18 MAY 07

Note 3. | JEPPESEN SANDERSON, INC., 2006, 2007. ALL RIGHTS RESERVED.

1basic RNAV (B-RNAV) procedurerestriction to cross SUDPO at or above 2000' is applicable between 2301-1100 UTC.

7. RADAR required.6. Cruising levels will be issued after take-off by Singapore RADAR.

or EXPECT RADAR vectors from ATC. 3. The2

2000'At or above

All departure aircraft on Runway 20C issued with heading instructions by ATC shallalso 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 departingon Runway 20C shall inform ATC during the time when the aircraft commences taxiing

5. Initial departure climb altitude is 3000' or as directed by ATC. to the holding point for departure. 4. All SIDs include noise preferential routes.

023^

NOT TO SCALE

Licensed to QANTAS. Printed on 30 Dec 2011.Notice: After 13 Jan 2012 0901Z, this chart may no longer be valid. Disc 26-2011

JEPPESENJeppView 3.7.5.0

097D6.9

188^

D23.4

D13.5

149^

D7.

6

053^

COMMSLOST COMMSLOST COMMSLOST COMMSLOSTLOST

COMMS

COMMS

LOST

COMMSLOST COMMSLOST COMMSLOST COMMSLOST LOST

282^

278^

293^

D55.5

D56.6

D50.0

CHANGES:

JEPPESENWSSS/SINCHANGI

SINGAPORE, SINGAPORE

SID

10-3D1

A

Apt Elev

22'

203^

180^5

N01 17.5E103 58.1

(VTK R-203/D8.0)

SUDPO

N01 12.5E103 58.1

SUSIN

.RNAV.SID.

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

Air Force (RSAF) Aircraft

AN01 01.6E103 58.1

DUNAL

11

272^

28

BOBAG(SJ R-243/D24.0)

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

FL140At or above

Trans level: FL130 Trans alt: 11000'

18 APR 08 .Eff.1.May.

| JEPPESEN, 2008. ALL RIGHTS RESERVED.

TEKONG116.5 VTKVTK

N01 24.9 E104 01.3

D

SUNVA(VTK R-210/D8.0)

N01 17.9E103 57.4

203^

172^5

(SJ R-059/D8.0)

(VTK R-195/D12.8)

(BOG1

V)

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.BOG 1V (RWY 20R)

BOG 1X (RWY 20C)

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.

090^

180^

360^

3400'

2500'2100'090^

180^

360^

3400'

2100'1900'

MSA VTK VOR MSA SJ VOR

321^327^

41

39

ARAM

AREK

OP

ARAMA

REKOPN01 33.1E103 05.4

SINJON113.5 SJSJ

N01 13.4 E103 51.3

D

New procedures at this airport.

4 NMDirect distance from Changi Apt

(Rwy 20C) to: SUDPO

75 100 150 200 250 300Gnd speed-KT

1519126610137605063805.0% V/V(fpm)

3.3% V/V(fpm) 251 334 501 668 835 1003

, then 3.3%. 400'minimum net climb gradient of 5.0% untilreaching or passing

Rwys 20C/R- Departures shall be on a

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

2. Communications failure occurs immediatelyafter departure on:

Rwys 20C/R: Proceed straight ahead toSamko Holding Area (SHA) climbing to thelast assigned altitude. Thereafter refer toSingapore Special Procedures on radiocommunications failure.

(SJ R-298/D50.0)N01 36.9 E103 07.2

(Rwy 20R) to: SUNVA 4 NM

1 INITIAL CLIMB

1

1 2

1. These SIDs will be assigned during air defense exercises. 2. For RNAV operations,

procedure or EXPECT RADAR vectors from ATC. 4. 3. Non-RNP-1/P-RNAV approved aircraft shall fly this as a basic RNAV (B-RNAV)

The restriction to cross SUDPO 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 also cross VTK 8 DME at or above 2000' between 2301-1100 UTC. If the altituderestriction cannot be complied with, the pilot-in-command of an aircraft departing on Runways 20C/R shall inform ATC during the time when the aircraft commencestaxiing to the holding point for departure. 5. All SIDs include noise preferential

levels will be issued after take-off by Singapore RADAR. 8. RADAR required.routes. 6. Initial departure climb altitude is 3000' or as directed by ATC. 7. Cruising

DEPARTURES

BOBAG ONE VICTOR (BOG1V),

(RWYS 20C/R)

BOBAG ONE X-RAY (BOG1X)

BO

BA

G O

NE

X-R

AY

aircraft shall be GNSS-equipped and meet RNP-1/P-RNAV standard of accuracy.

180^

NOT TO SCALE

Page 17: WSSS Charts

Licensed to QANTAS. Printed on 30 Dec 2011.Notice: After 13 Jan 2012 0901Z, this chart may no longer be valid. Disc 26-2011

JEPPESENJeppView 3.7.5.0

083^

057^

097^

195^

150^

D9.4

D23.2

D24.2

D6.9

D12.8

113^

188^

D24.0D23.4D

13.5

149^

053^

D7.6

COMMSLOST COMMSLOST COMMSLOST LOST

COMMSLOST COMMSLOST COMMSLOST LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

LOST

75 100 150 200 250 300

CHANGES:

JEPPESENWSSS/SINCHANGI

SINGAPORE, SINGAPORE

SID

SINJON113.5 SJSJ

N01 13.4 E103 51.3

D

TEKONG116.5 VTKVTK

N01 24.9 E104 01.3

D

10-3E

Gnd speed-KT

1519126610137605063805.0% V/V(fpm)

3.3% V/V(fpm) 251 334 501 668 835 1003

A

Apt Elev

22'

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

22

N01 12.5E103 58.1

SUSIN

N01 26.1E104 10.7

DOKTA

.RNAV.SID.

1 INITIAL CLIMB

4000'At or above

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

Air Force (RSAF) Aircraft

A

BOG 1E(RWY 02L)

BOG 1F(RWY 20R)

(BOG1E)

BOBAG ONE ECHO (BOG1E),

At or above4000'

11

BO

BA

G O

NE

(BOG1F)

262^

272^.R469.15

28

BOBAG(SJ R-243/D24.0)

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

TOPOM

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

N01 29.9E104 02.5

SUNVA(VTK R-210/D8.0)

N01 17.9E103 57.4

203^

172^5

115^9

BO

BA

G O

NE E

CHO

FO

XTRO

T

N01 01.6E103 58.1

DUNAL

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

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

to the last assigned altitude.

to the last assigned altitude.

7600.1. Set transponder to Mode A/C code

2. Communications failure occurs immediately after departure on:

Thereafter refer to Singapore Special Procedures on radio communications failure.

Thereafter refer to Singapore Special Procedures on radio communications failure.

At or below6000'

or as directedby ATC

N01 03.8E104 13.3

DOBLU

, then 3.3%. 400'

For minimum climb gradient criteria:

minimum net climb gradient of 5.0% untilreaching or passing

Rwy 20R- Departures shall be on a

9 NM 4 NM

Direct distance from Changi Apt(Rwy 02L) to: TOPOM(Rwy 20R) to: SUNVA

BOBAG ONE FOXTROT (BOG1F)

(RWYS 02L, 20R)

180^

At or above10000'

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

to DUNAL, then turn RIGHT and 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^

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

090^

180^

360^

3400'

2500'2100'090^

180^

360^

3400'

2100'1900'

MSA VTK VOR MSA SJ VOR

DEPARTURES

Trans level: FL130 Trans alt: 11000'1. For RNAV operations, aircraft shall be GNSS-equipped and meet RNP-1/P-RNAV standard of accuracy. 2. Non-RNP-1/P-RNAV approved aircraft shall fly this as a

restriction to cross SUNVA at or above 2000' is applicable between 2301-1100 UTC. basic RNAV (B-RNAV) procedure 1 or EXPECT RADAR vectors from ATC. 3. 2The

6. Cruising levels will be issued after take-off by Singapore RADAR.7. RADAR required.

18 MAY 07

Note 3. | JEPPESEN SANDERSON, INC., 2006, 2007. ALL RIGHTS RESERVED.

2At or above

2000'

2000'At or above

All departure aircraft on Runway 20R issued with heading instructions by ATC shall

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

5. Initial departure climb altitude is 3000' or as directed by ATC. to the holding point for departure. 4. All SIDs include noise preferential routes.

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

023^

NOT TO SCALE

Licensed to QANTAS. Printed on 30 Dec 2011.Notice: After 13 Jan 2012 0901Z, this chart may no longer be valid. Disc 26-2011

JEPPESENJeppView 3.7.5.0

059^

097^

195^

D8.0

D6.9

D12.8

078^

D12.2

D32.0

006^

COMMSLOST COMMSLOST COMMSLOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

LOST

COMMSLOST COMMSLOST COMMSLOST

LOST COMMS

COMMSLOST

75 100 150 200 250 300

CHANGES:

JEPPESENWSSS/SINCHANGI

SINGAPORE, SINGAPORE

SID

SINJON113.5 SJSJ

N01 13.4 E103 51.3

D

TEKONG116.5 VTKVTK

N01 24.9 E104 01.3

D

10-3F

Gnd speed-KT

1519126610137605063805.0% V/V(fpm)

3.3% V/V(fpm) 251 334 501 668 835 1003

A203^

180^5

N01 17.5E103 58.1

(VTK R-203/D8.0)SUDPO

N01 12.5E103 58.1

SUSIN

2At or above

2000'

.RNAV.SID.

1 INITIAL CLIMB

1ROUTING

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

Air Force (RSAF) Aircraft

A

VJR 4A(RWY 02C)

VJR 8B(RWY 20C)

TOKIM(SJ R-037/D20.1)

N01 29.6E104 03.3

(VTK R-023/D5.0)

JOHOR BAHRU FOUR ALPHA (VJR4A),

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

At AKOMA, turn LEFT and track 265^ to VJR.

Climb straight ahead to TOKIM, turn LEFT and track 332^ to AKOMA.

SABUG, then track 348^ to VTK. Then track 342^ to AKOMA.

348^

342^

332^

265^

9

21

17

18

(VJR8B)

(VJR4A

)

JOHO

R B

AHRU

JOHOR B

AHRU

FOUR A

LPHA

SABUG(VTK R-168/D9.2)

AKOMA

N01 45.4E103 54.7

(VTK R-342/D21.4)

.A457.

.B466.

.R325.

112.7 VJRVJR

N01 43.8 E103 37.3

DJOHOR BAHRU

At or above11000'

9 NM 4 NM

Direct distance from Changi Apt

, then 3.3%. 400'

For minimum climb gradient criteria:

minimum net climb gradient of 5.0% untilreaching or passing

Rwy 20C- Departures shall be on a

(Rwy 02C) to: TOKIM(Rwy 20C) to: SUDPO

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.

to the last assigned altitude.

7600.1. Set transponder to Mode A/C code

2. Communications failure occurs immediately after departure on:

Thereafter refer to Singapore Special Procedures on radio communications failure.

Thereafter refer to Singapore Special Procedures on radio communications failure.

(RWYS 02C, 20C)

JOHOR BAHRU EIGHT BRAVO (VJR8B)

7000'At or above

VJR 8B

EIG

HT B

RA

VO

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

090^

180^

360^

3400'

2500'2100'

090^

180^

360^

3400'

2100'1900'

MSA VTK VOR

MSA SJ VOR(SJ R-335/D33.4)(VTK R-308/D30.5)

DEPARTURES

N01 15.9E104 03.2

At or above4000'

Apt Elev

22'

Trans level: FL130 Trans alt: 11000'1. For RNAV operations, aircraft shall be GNSS-equipped and meet RNP-1/P-RNAV

basic RNAV (B-RNAV) procedurerestriction to cross SUDPO at or above 2000' is applicable between 2301-1100 UTC.

or EXPECT RADAR vectors from ATC. 3. standard of accuracy. 2. Non-RNP-1/P-RNAV approved aircraft shall fly this as a

2The1

6. Cruising levels will be issued after take-off by Singapore RADAR.7. RADAR required.

2000'At or above

Note 3. | JEPPESEN SANDERSON, INC., 2006, 2007. ALL RIGHTS RESERVED.

18 MAY 07

7000'At or above

VJR 4A

All departure aircraft on Runway 20C issued with heading instructions by ATC shallalso cross VTK 8 DME at or above 2000' between 2301-1100 UTC. If the altituderestriction cannot be complied with, the pilot-in-command of an aircraft departingon Runway 20C shall inform ATC during the time when the aircraft commences taxiing

5. Initial departure climb altitude is 3000' or as directed by ATC. to the holding point for departure. 4. All SIDs include noise preferential routes.

023^

NOT TO SCALE

Page 18: WSSS Charts

Licensed to QANTAS. Printed on 30 Dec 2011.Notice: After 13 Jan 2012 0901Z, this chart may no longer be valid. Disc 26-2011

JEPPESENJeppView 3.7.5.0

097^

195^

D6.9

D12.8

078^

D12.2

D32.0

006^

053^

D7.6

COMMSLOST COMMSLOST COMMSLOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

LOST

COMMSLOST COMMSLOST COMMSLOST

LOST COMMS

LOST COMMS

75 100 150 200 250 300

9 NM 4 NM

CHANGES:

JEPPESENWSSS/SINCHANGI

SINGAPORE, SINGAPORE

SID

SINJON

113.5 SJSJ

N01 13.4 E103 51.3

D

TEKONG116.5 VTKVTK

N01 24.9 E104 01.3

D

10-3G

Direct distance from Changi Apt

Gnd speed-KT

, then 3.3%. 400'

1519126610137605063805.0% V/V(fpm)

3.3% V/V(fpm) 251 334 501 668 835 1003

For minimum climb gradient criteria:

minimum net climb gradient of 5.0% untilreaching or passing

A

Rwy 20R- Departures shall be on a

.RNAV.SID.

1 INITIAL CLIMB

1ROUTING

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

Air Force (RSAF) Aircraft

A

VJR 4E(RWY 02L)

VJR 8F(RWY 20R)

(Rwy 02L) to: TOPOM(Rwy 20R) to: SUNVA

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

At AKOMA, turn LEFT and track 265^ to VJR.

Climb straight ahead to TOPOM, turn LEFT and track 333^ to AKOMA.

SABUG, then track 348^ to VTK. Then track 342^ to AKOMA.

348^

342^333^

265^

9

21

17

18

(VJR8F)

(VJR4E)

JOHO

R B

AHRU

JOHOR B

AHRU

FOUR EC

HO

AKOMA

N01 45.4E103 54.7

(VTK R-342/D21.4)

.A457.

.B466.

.R325.

112.7 VJRVJR

N01 43.8 E103 37.3

DJOHOR BAHRU

At or above11000'

JOHOR BAHRU FOUR ECHO (VJR4E),

N01 29.9E104 02.5

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

203^2

At or above2000'

N01 17.9E103 57.4

(VTK R-210/D8.0)SUNVA

172^5

7000'At or above

VJR 4E

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

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

to the last assigned altitude.

to the last assigned altitude.

7600.1. Set transponder to Mode A/C code

2. Communications failure occurs immediately after departure on:

Thereafter refer to Singapore Special Procedures on radio communications failure.

Thereafter refer to Singapore Special Procedures on radio communications failure.

(RWYS 02L, 20R)

JOHOR BAHRU EIGHT FOXTROT (VJR8F)

EIG

HT F

OXTRO

T

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

090^

180^

360^

3400'

2500'2100'

090^

180^

360^

3400'

2100'1900'

MSA VTK VOR

MSA SJ VOR

At or above7000'

(SJ R-335/D33.4)(VTK R-308/D30.5)

DEPARTURES

SABUG(VTK R-168/D9.2)N01 15.9E104 03.2

At or above4000'

N01 12.5E103 58.1

SUSIN

Apt Elev

22'

Trans level: FL130 Trans alt: 11000'1. For RNAV operations, aircraft shall be GNSS-equipped and meet RNP-1/P-RNAV standard of accuracy. 2. Non-RNP-1/P-RNAV approved aircraft shall fly this as a

restriction to cross SUNVA at or above 2000' is applicable between 2301-1100 UTC. basic RNAV (B-RNAV) procedure 1 or EXPECT RADAR vectors from ATC. 3. 2The

6. Cruising levels will be issued after take-off by Singapore RADAR.7. RADAR required.

18 MAY 07

Note 3. | JEPPESEN SANDERSON, INC., 2006, 2007. ALL RIGHTS RESERVED.

2000'At or above

All departure aircraft on Runway 20R issued with heading instructions by ATC shallalso cross VTK 8 DME at or above 2000' between 2301-1100 UTC. If the altituderestriction cannot be complied with, the pilot-in-command of an aircraft departingon Runway 20R shall inform ATC during the time when the aircraft commences taxiing

5. Initial departure climb altitude is 3000' or as directed by ATC. to the holding point for departure. 4. All SIDs include noise preferential routes.

023^

NOT TO SCALE

Licensed to QANTAS. Printed on 30 Dec 2011.Notice: After 13 Jan 2012 0901Z, this chart may no longer be valid. Disc 26-2011

JEPPESENJeppView 3.7.5.0

343^

023^

285^

332^

274^

033^

025^

298^

D36.6

D30.0

D19.3D18.6

D6.6

D19.6

D13.0D30.0

001 ^

TEKONG116.5 VTKVTK

N01 24.9 E104 01.3

D

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

Air Force (RSAF) Aircraft

A

A

KONG KONG

286 KKKK

N01 31.3 E103 59.4

JAYBEE400 JBJB

N01 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

Apt Elev

22'

JEPPESENWSSS/SINCHANGI

SINGAPORE, SINGAPORE

Trans level: FL130 Trans alt: 11000'

10-3H .SID.

2. All SIDs include noise preferential routes.

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

(RWYS 02L/C)

3. Initial departure climb altitude is 3000' or as directed by ATC.

.Eff.1.May.

CHANGES:

ROUTING

18 APR 08

LELIB ONE CHARLIE (LLB1C) DEPARTURE

10000',

4 NM

For minimum climb gradient criteria:

RWY

02L Climb straight ahead.

INITIAL CLIMB

02C Climb straight ahead to VTK.

Intercept and proceed on VTK R-001. After passing

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

MAINTAIN FL140

Direct distance from Changi Apt to:

turn RIGHT to NYLON. At NYLON,turn RIGHT and proceed direct to KK. Track 266^ bearing from KK to JB. Track 262^ bearingfrom JB to LELIB and join airway A-464. from NYLON to LELIB.

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

LELIB ONE DELTA SID cancelled. | JEPPESEN, 2004, 2008. ALL RIGHTS RESERVED.

SINJON113.5 SJSJ

N01 13.4 E103 51.3

D

(Rwy 02L/C) to: VTK

266^

262^17

18FL140

FL140

NOT TO SCALE

.A.464.

Page 19: WSSS Charts

Licensed to QANTAS. Printed on 30 Dec 2011.Notice: After 13 Jan 2012 0901Z, this chart may no longer be valid. Disc 26-2011

JEPPESENJeppView 3.7.5.0

097D6.9

078^

D12.2

D32.0

006^

053^

D7.6

029^

D22.2

COMMSLOST COMMSLOST COMMSLOST COMMSLOST

COMMS

LOST

COMMS

LOST

COMMSLOST COMMSLOST COMMSLOST COMMSLOST

75 100 150 200 250 300

4 NM

CHANGES:

JEPPESENWSSS/SINCHANGI

SINGAPORE, SINGAPORE

SID

SINJON113.5 SJSJ

N01 13.4 E103 51.3

D

TEKONG116.5 VTKVTK

N01 24.9 E104 01.3

D

10-3J

Direct distance from Changi Apt

Gnd speed-KT

, then 3.3%. 400'

1519126610137605063805.0% V/V(fpm)

3.3% V/V(fpm) 251 334 501 668 835 1003

minimum net climb gradient of 5.0% untilreaching or passing

A

203^

180^ 5

N01 17.5E103 58.1

(SJ R-059/D8.0)SUDPO

N01 12.5E103 58.1

SUSIN

.RNAV.SID.

1 INITIAL CLIMB

1ROUTING

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

Air Force (RSAF) Aircraft

A

VMR 1X(RWY 20C)

VMR 1V(RWY 20R)

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

348^9

AKOMA(VTK R-342/D21.4)

MERSING ONE X-RAY (VMR1X)

Rwys 20C/R- Departures shall be on a

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

At SUSIN turn LEFT to SABUG, then track 348^ to VTK. From VTK track 004^ to NITAD, then turn LEFT and track 330^ to AKOMA. Turn RIGHT and track 356^ to VMR.

N01 17.9E103 57.4

(VTK R-210/D8.0)SUNVA

172^5

2At or above

2000'

2At or above

2000'

(VTK R-203/D8.0)

(VTK R-195/D12.8)

7000'At or above

NITAD(VTK R-004/D8.0)N01 33.0 E104 01.9

N01 45.4 E103 54.7

004^

330^

356^

8

14

38

MERSING116.8 VMRVMR

N02 23.3 E103 52.3

D

090^

180^

360^

3400'

2500'2100'090^

180^

360^

3400'

2100'1900'

MSA VTK VOR MSA SJ VOR

to the last assigned altitude.

7600.1. Set transponder to Mode A/C code

2. Communications failure occurs immediately after departure on:

Thereafter refer to Singapore Special Procedures on radio communications failure.

Rwys 20C/R: Proceed straight ahead to Samko Holding Area (SHA) climbing

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

CB

(VTK R-351/D58.8)(SJ R-001/D69.6)

DEPARTURES

SABUG(VTK R-168/D9.2)N01 15.9E104 03.2

At or above4000'

Apt Elev

22'

Trans level: FL130 Trans alt: 11000'

1 2

1. For RNAV operations, aircraft shall be GNSS-equipped and meet RNP-1/P-RNAV

or EXPECT RADAR vectors from ATC. 3. standard of accuracy. 2. Non-RNP-1/P-RNAV approved aircraft shall fly this as a basic RNAV (B-RNAV) procedure The restriction to cross SUDPO or SUNVA at or above 2000' is applicable between

2301-1100 UTC. If the altitude restriction cannot be complied with, the pilot-in-command of an aircraft departing on Runway 20C/R shall inform ATC during the time when the aircraft commences taxiing to the holding point for departure. 4. All SIDs include noise preferential routes. 5. Initial departure climb altitude is

Singapore RADAR. 7. RADAR required. 8. These SIDs will be assigned during airdefense exercises.

3000' or as directed by ATC. 6. Cruising levels will be issued after take-of by

2301-1100 UTC. All departure aircraft on Runways 20C/R issued with headinginstructions by ATC shall also cross VTK 8 DME at or above 2000' between

B

(VMR1X)

C

(VMR1V)MERSING ONE VICTOR

MERSING ONE X-RAY

MERSING ONE VICTOR (VMR1V),

18 APR 08 .Eff.1.May.

None. | JEPPESEN, 2006, 2008. ALL RIGHTS RESERVED.

(RWYS 20C/R)

NOT TO SCALE

Licensed to QANTAS. Printed on 30 Dec 2011.Notice: After 13 Jan 2012 0901Z, this chart may no longer be valid. Disc 26-2011

JEPPESENJeppView 3.7.5.0

059^

097^

195^

D8.0

D6.9

D12.8

078^

D12.2

D32.0

006^

COMMSLOST COMMSLOST COMMSLOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

LOST

COMMSLOST COMMSLOST COMMSLOST

LOST COMMS

COMMSLOST

75 100 150 200 250 300

9 NM 4 NM

CHANGES:

JEPPESENWSSS/SINCHANGI

SINGAPORE, SINGAPORE

SID

SINJON113.5 SJSJ

N01 13.4 E103 51.3

D

TEKONG116.5 VTKVTK

N01 24.9 E104 01.3

D

10-3K

Direct distance from Changi Apt

Gnd speed-KT

, then 3.3%. 400'

1519126610137605063805.0% V/V(fpm)

3.3% V/V(fpm) 251 334 501 668 835 1003

For minimum climb gradient criteria:

minimum net climb gradient of 5.0% untilreaching or passing

A

Apt Elev

22'

203^

180^5

N01 17.5E103 58.1

(VTK R-203/D8.0)SUDPO

2At or above

2000'

Rwy 20C- Departures shall be on a

.RNAV.SID.

1 INITIAL CLIMB

1ROUTING

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

Air Force (RSAF) Aircraft

A

VMR 3A(RWY 02C)

VMR 4B(RWY 20C)

(Rwy 02C) to: TOKIM(Rwy 20C) to: SUDPO

TOKIM(SJ R-037/D20.1)

N01 29.6E104 03.3

(VTK R-023/D5.0)

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

At AKOMA turn RIGHT and track 356^ to VMR.

Climb straight ahead to TOKIM, turn LEFT and track 332^ to AKOMA.

SABUG, then track 348^ to VTK. Then track 342^ to AKOMA.

348^

342^

332^9

21

17

(VMR4B)

(VMR3A

)

FO

UR B

RA

VO

2000'At or above

AKOMA

N01 45.4E103 54.7

(VTK R-342/D21.4)

MERSING THREE ALPHA (VMR3A),MERSING FOUR BRAVO (VMR4B)

356^38

MERSIN

G

MER

SING

THREE A

LPHA

7000'At or above

VMR 4B

7000'At or above

VMR 3A

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.

to the last assigned altitude.

7600.1. Set transponder to Mode A/C code

2. Communications failure occurs immediately after departure on:

Thereafter refer to Singapore Special Procedures on radio communications failure.

Thereafter refer to Singapore Special Procedures on radio communications failure.

(RWYS 02C, 20C)

090^

180^

360^

3400'

2500'2100'090^

180^

360^

3400'

2100'1900'

MSA VTK VOR MSA SJ VORMERSING116.8 VMRVMR

N02 23.3 E103 52.3

D

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

(VTK R-351/D58.8)(SJ R-001/D69.6)

Trans level: FL130 Trans alt: 11000'1. For RNAV operations, aircraft shall be GNSS-equipped and meet RNP-1/P-RNAV

1 2

DEPARTURES

standard of accuracy. 2. Non-RNP-1/P-RNAV approved aircraft shall fly this as a or EXPECT RADAR vectors from ATC. 3.

SABUG

At or above4000'

(VTK R-168/D9.2)N01 15.9E104 03.2

At or above4000'4000'

At or aboveSUSIN

N01 12.5E103 58.1

18 MAY 07

basic RNAV (B-RNAV) procedure Therestriction to cross SUDPO at or above 2000' is applicable between 2301-1100 UTC.

Note 3. | JEPPESEN SANDERSON, INC., 2006, 2007. ALL RIGHTS RESERVED.

All departure aircraft on Runway 20C issued with heading instructions by ATC shallalso cross VTK 8 DME at or above 2000' between 2301-1100 UTC. If the altituderestriction cannot be complied with, the pilot-in-command of an aircraft departingon Runway 20C shall inform ATC during the time when the aircraft commences taxiingto the holding point for departure. 4. All SIDs include noise preferential routes.5. Initial departure climb altitude is 3000' or as directed by ATC. 6. RADAR required.7. Cruising levels will be issued after take-off by Singapore RADAR.8. Mersing Three Alpha will also be assigned during air defense exercises.

023^

NOT TO SCALE

Page 20: WSSS Charts

Licensed to QANTAS. Printed on 30 Dec 2011.Notice: After 13 Jan 2012 0901Z, this chart may no longer be valid. Disc 26-2011

JEPPESENJeppView 3.7.5.0

195^

D12.8

078^

D12.2

D32.0

006^

053^

D7.6

COMMSLOST COMMSLOST COMMSLOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

LOST

COMMSLOST COMMSLOST COMMSLOST

LOST COMMS

LOST COMMS

097D6.9

097D6.9

75 100 150 200 250 300

9 NM 4 NM

CHANGES:

JEPPESENWSSS/SINCHANGI

SINGAPORE, SINGAPORE

SID

TEKONG116.5 VTKVTK

N01 24.9 E104 01.3

D

10-3L

Direct distance from Changi Apt

Gnd speed-KT

, then 3.3%. 400'

1519126610137605063805.0% V/V(fpm)

3.3% V/V(fpm) 251 334 501 668 835 1003

For minimum climb gradient criteria:

minimum net climb gradient of 5.0% untilreaching or passing

A

Apt Elev

22'

Rwy 20R- Departures shall be on a

.RNAV.SID.

1 INITIAL CLIMB

1ROUTING

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

Air Force (RSAF) Aircraft

A

VMR 3E(RWY 02L)

VMR 4F(RWY 20R)

(Rwy 02L) to: TOPOM(Rwy 20R) to: SUNVA

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

At AKOMA turn RIGHT and track 356^ to VMR.

Climb straight ahead to TOPOM, turn LEFT and track 333^ to AKOMA.

SABUG, then track 348^ to VTK. Then track 342^ to AKOMA.

348^

342^333^

9

21

17

(VMR4F)

(VMR3E)

THREE EC

HO

AKOMA

N01 45.4E103 54.7

(VTK R-342/D21.4)

N01 29.9E104 02.5

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

203^2At or above

2000'

N01 17.9E103 57.4

(VTK R-210/D8.0)SUNVA

172^5

2000'At or above

At or above7000'F

OUR F

OXTRO

T

MERSING THREE ECHO (VMR3E),MERSING FOUR FOXTROT (VMR4F)

SINJON

113.5 SJSJ

N01 13.4 E103 51.3

D

356^38

MERSIN

G

MER

SING

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

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

to the last assigned altitude.

to the last assigned altitude.

7600.1. Set transponder to Mode A/C code

2. Communications failure occurs immediately after departure on:

Thereafter refer to Singapore Special Procedures on radio communications failure.

Thereafter refer to Singapore Special Procedures on radio communications failure.

(RWYS 02L, 20R)

090^

180^

360^

3400'

2500'2100'090^

180^

360^

3400'

2100'1900'

MSA VTK VOR MSA SJ VORMERSING116.8 VMRVMR

N02 23.3 E103 52.3

D

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

(VTK R-351/D58.8)(SJ R-001/D69.6)

DEPARTURES

SUSINN01 12.5E103 58.1

(VTK R-168/D9.2)

SUSINN01 12.5E103 58.1

N01 15.9E104 03.2

At or above4000'

SABUG

18 MAY 07

Note 3. | JEPPESEN SANDERSON, INC., 2006, 2007. ALL RIGHTS RESERVED.

Trans level: FL130 Trans alt: 11000'1. For RNAV operations, aircraft shall be GNSS-equipped and meet RNP-1/P-RNAV standard of accuracy. 2. Non-RNP-1/P-RNAV approved aircraft shall fly this as a

1basic RNAV (B-RNAV) procedure or EXPECT RADAR vectors from ATC. 3. restriction to cross SUNVA at or above 2000' is applicable between 2301-1100 UTC.

2 The

7000'At or above

VMR 3E

All departure aircraft on Runway 20R issued with heading instructions by ATC shall

restriction cannot be complied with, the pilot-in-command of an aircraft departingon Runway 20R shall inform ATC during the time when the aircraft commences taxiingto the holding point for departure. 4. All SIDs include noise preferential routes.5. Initial departure climb altitude is 3000' or as directed by ATC. 6. RADAR required.7. Cruising levels will be issued after take-off by Singapore RADAR.8. Mersing Three Echo will also be assigned during air defense exercises.

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

023^

NOT TO SCALE

Licensed to QANTAS. Printed on 30 Dec 2011.Notice: After 13 Jan 2012 0901Z, this chart may no longer be valid. Disc 26-2011

JEPPESENJeppView 3.7.5.0

343^285^273^

033^

025^

D33.9

293^

D41.3

D19.3

332^

D18.6

D6.6

D19.6

D30.0

D13.0

023^

001 ^

090^

180^

360^

3400'

2100'

1900'

CHANGES:

MSA VTK VOR

JEPPESENWSSS/SINCHANGI

SINGAPORE, SINGAPORE

TEKONG116.5 VTKVTK

N01 24.9 E104 01.3

D

10-3M .SID.

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

Air Force (RSAF) Aircraft

A

A

KONG KONG

286 KKKK

N01 31.3 E103 59.4

JAYBEE400 JBJB

N01 30.0 E103 42.7

NYLONN01 37.0E104 06.4

to PIMOK

MAINTAINFL140

At FL140

Passing10000'

18 APR 08 .Eff.1.May.

| JEPPESEN, 2004, 2008. ALL RIGHTS RESERVED.

Apt Elev

22'

Trans level: FL130 Trans alt: 11000'

2. All SIDs include noise preferential routes.

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

(RWYS 02L/C)

3. Initial departure climb altitude is 3000' or as directed by ATC.

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

PIMOK ONE CHARLIE (PMK1C) DEPARTURE

SINJON113.5 SJSJ

N01 13.4 E103 51.3

D

4 NM

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

Direct distance from Changi Apt to:

ROUTING

10000',

RWY

02L Climb straight ahead.

INITIAL CLIMB

02C Climb straight ahead to VTK.

Intercept and proceed on VTK R-001. After passing

MAINTAIN FL140

turn RIGHT to NYLON. At NYLON,turn RIGHT and proceed direct to KK. Track 266^ bearing from KK to JB. Track 262^ bearingfrom JB to PIMOK and join airway A-576. from NYLON to PIMOK.

PIMOK ONE DELTA SID cancelled.

(Rwy 02L/C) to: VTK

266^

262^17

FL140

NOT TO SCALE

.A.576.PIMOK

N01 26.8E103 20.1

23FL140

Page 21: WSSS Charts

Licensed to QANTAS. Printed on 30 Dec 2011.Notice: After 13 Jan 2012 0901Z, this chart may no longer be valid. Disc 26-2011

JEPPESENJeppView 3.7.5.0

083^

057^

059^

097^

195^

150^

D9.4

D23.2

D24.2

D8.0

D6.9

D12.8

COMMSLOST COMMSLOST COMMSLOST LOST

COMMSLOST COMMSLOST COMMSLOST LOST

103^

079^

D23.6

D33.7

COMMS

LOST

COMMS

LOST

COMMS

LOST

LOST

75 100 150 200 250 300

9 NM 4 NM

CHANGES:

JEPPESENWSSS/SINCHANGI

SINGAPORE, SINGAPORE

SID

SINJON

113.5 SJSJ

N01 13.4 E103 51.3

D

TEKONG116.5 VTKVTK

N01 24.9 E104 01.3

D

10-3N

Direct distance from Changi Apt

Gnd speed-KT

, then 3.3%. 400'

1519126610137605063805.0% V/V(fpm)

3.3% V/V(fpm) 251 334 501 668 835 1003

For minimum climb gradient criteria:

minimum net climb gradient of 5.0% untilreaching or passing

A

Apt Elev

22'

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

115^

120^

203^

180^

9

15

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

2At or above

2000'

Rwy 20C- Departures shall be on a

.RNAV.SID.

1 INITIAL CLIMB

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

Air Force (RSAF) Aircraft

A

TOM 1A(RWY 02C)

TOM 1B(RWY 20C)

(TOM1A)

(TOM1B)

TOMAN ONE BRAVO

(Rwy 02C) to: TOKIM(Rwy 20C) to: SUDPO

TOKIM(SJ R-037/D20.1)

N01 29.6E104 03.3

(VTK R-023/D5.0)

(SJ R-113/D24.0)DOBLU

N01 03.8 E104 13.3

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.

to the last assigned altitude.

7600.1. Set transponder to Mode A/C code

2. Communications failure occurs immediately after departure on:

Thereafter refer to Singapore Special Procedures on radio communications failure.

Thereafter refer to Singapore Special Procedures on radio communications failure.

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

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

4000'At or above

TOMAN ONE ALPHA

At or belowor as directed by ATC

6000'

2000'At or above

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

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

Trans level: FL130 Trans alt: 11000'1. For RNAV operations, aircraft shall be GNSS-equipped and meet RNP-1/P-RNAV

1 2

18 APR 08

standard of accuracy. 2. Non-RNP-1/P-RNAV approved aircraft shall fly this as a or EXPECT RADAR vectors from ATC. 3.basic RNAV (B-RNAV) procedure The

restriction to cross SUDPO at or above 2000' is applicable between 2301-1100 UTC.

6. Cruising levels will be issued after take-off by Singapore RADAR. 7. RADAR required.

TOMAN ONE ALPHA (TOM1A),TOMAN ONE BRAVO (TOM1B)

DEPARTURES(RWYS 02C, 20C)

090^

360^

3400'

2500'2100'090^

360^

3400'

2100'1900'

MSA VTK VOR MSA SJ VOR

180^

180^

All departure aircraft on Runway 20C issued with heading instructions by ATC shallalso cross VTK 8 DME at or above 2000' between 2301-1100 UTC. If the altituderestriction cannot be complied with, the pilot-in-command of an aircraft departingon Runway 20C shall inform ATC during the time when the aircraft commences taxiing

5. Initial departure climb altitude is 3000' or as directed by ATC. to the holding point for departure. 4. All SIDs include noise preferential routes.

.Eff.1.May.

None. | JEPPESEN, 2006, 2008. ALL RIGHTS RESERVED.

023^

NOT TO SCALE

Licensed to QANTAS. Printed on 30 Dec 2011.Notice: After 13 Jan 2012 0901Z, this chart may no longer be valid. Disc 26-2011

JEPPESENJeppView 3.7.5.0

097^

195^

D6.9

D12.8

083^

057^

150^

D9.4

D23.2

D24.2

103^

079^

D23.6

D33.7

COMMSLOST COMMSLOST COMMSLOST LOST

COMMSLOST COMMSLOST COMMSLOST LOST

053^

D7.6

COMMS

LOST

COMMS

LOST

COMMS

LOST

LOST

75 100 150 200 250 300

CHANGES:

JEPPESENWSSS/SINCHANGI

SINGAPORE, SINGAPORE10-3P

Gnd speed-KT

, then 3.3%. 400'

1519126610137605063805.0% V/V(fpm)

3.3% V/V(fpm) 251 334 501 668 835 1003

For minimum climb gradient criteria:

minimum net climb gradient of 5.0% untilreaching or passing

Rwy 20R- Departures shall be on a

.RNAV.SID.

TOMAN ONE ECHO (TOM1E),

9 NM 4 NM

Direct distance from Changi Apt(Rwy 02L) to: TOPOM(Rwy 20R) to: SUNVA

(RWYS 02L, 20R)

SINJON

113.5 SJSJ

N01 13.4 E103 51.3

D

D

A

120^

N01 12.5E103 58.1

SUSIN

At or above4000'

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

Air Force (RSAF) Aircraft

A

TEKONG116.5 VTKVTK

N01 24.9 E104 01.3

15

17

(TOM1E)

(TOM1F)

(SJ R-113/D24.0)DOBLU

N01 03.8 E104 13.3

4000'At or above

At or belowor as directed by ATC

6000'

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)

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

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

to the last assigned altitude.

to the last assigned altitude.

7600.1. Set transponder to Mode A/C code

2. Communications failure occurs immediately after departure on:

Thereafter refer to Singapore Special Procedures on radio communications failure.

Thereafter refer to Singapore Special Procedures on radio communications failure.

SID

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

1 INITIAL CLIMB

TOM 1E(RWY 02L)

TOM 1F(RWY 20R)

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

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

TOPOM

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

N01 29.9E104 02.5

203^2

At or above2000'

N01 17.9E103 57.4

(VTK R-210/D8.0)SUNVA

172^5

115^

9

TOMAN ONE FOXTROT (TOM1F)

TOMAN ONE ECHO

TOMAN ONE

FOXTROT

090^

180^

360^

3400'

2500'2100'090^

180^

360^

3400'

2100'1900'

MSA VTK VOR MSA SJ VOR

N01 21.8 E105 47.3

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

18 MAY 07

DEPARTURES

| JEPPESEN SANDERSON, INC., 2006, 2007. ALL RIGHTS RESERVED.Note 3.

Apt Elev

22'

Trans level: FL130 Trans alt: 11000'

standard of accuracy. 2. Non-RNP-1/P-RNAV approved aircraft shall fly this as a1. For RNAV operations, aircraft shall be GNSS-equipped and meet RNP-1/P-RNAV

basic RNAV (B-RNAV) procedurerestriction to cross SUNVA at or above 2000' is applicable between 2301-1100 UTC.

1 or EXPECT RADAR vectors from ATC. 3. The2

6. Cruising levels will be issued after take-off by Singapore RADAR. 7. RADAR required.

2000'At or above

All departure aircraft on Runway 20R issued with heading instructions by ATC shallalso cross VTK 8 DME at or above 2000' between 2301-1100 UTC. If the altituderestriction cannot be complied with, the pilot-in-command of an aircraft departingon Runway 20R shall inform ATC during the time when the aircraft commences taxiing

5. Initial departure climb altitude is 3000' or as directed by ATC. to the holding point for departure. 4. All SIDs include noise preferential routes.

023^

NOT TO SCALE

Page 22: WSSS Charts

Licensed to QANTAS. Printed on 30 Dec 2011.Notice: After 13 Jan 2012 0901Z, this chart may no longer be valid. Disc 26-2011

JEPPESENJeppView 3.7.5.0

083^

057^

059^

097^

195^

150^

D9.4

D23.2

D24.2

D8.0

D6.9

D12.8

COMMSLOST COMMSLOST COMMSLOST LOST

COMMSLOST COMMSLOST COMMSLOST LOST

COMMS

LOST

COMMS

LOST

COMMS

LOST

LOST

75 100 150 200 250 300

9 NM 4 NM

CHANGES:

JEPPESENWSSS/SINCHANGI

SINGAPORE, SINGAPORE

SID

SINJON

113.5 SJSJ

N01 13.4 E103 51.3

D

TEKONG116.5 VTKVTK

N01 24.9 E104 01.3

D

10-3Q

Direct distance from Changi Apt

Gnd speed-KT

, then 3.3%. 400'

1519126610137605063805.0% V/V(fpm)

3.3% V/V(fpm) 251 334 501 668 835 1003

For minimum climb gradient criteria:

minimum net climb gradient of 5.0% untilreaching or passing

A

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

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

115^

173^

120^

203^

180^

128^

9

22

16

67

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

2At or above

2000'

Rwy 20C- Departures shall be on a

.RNAV.SID.

1 INITIAL CLIMB

1ROUTING

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

Air Force (RSAF) Aircraft

A

VEN 1A(RWY 02C)

VEN 1B(RWY 20C)

DOSNO

VENTU

N00 48.0 E104 14.2

N00 05.8 E105 06.8

VENTU O

NE A

LPHA

(VEN

1A)

(VEN1B)

VENTU ONE BRAVO

(Rwy 02C) to: TOKIM(Rwy 20C) to: SUDPO

TOKIM(SJ R-037/D20.1)

N01 29.6E104 03.3

(VTK R-023/D5.0)

2000'At or above

(SJ R-113/D24.0)DOBLU

N01 03.8 E104 13.3

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.

to the last assigned altitude.

7600.1. Set transponder to Mode A/C code

2. Communications failure occurs immediately after departure on:

Thereafter refer to Singapore Special Procedures on radio communications failure.

Thereafter refer to Singapore Special Procedures on radio communications failure.

177^

(SJ R-132/D101)

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

VENTU ONE ALPHA (VEN1A),

join the ATS route.

(SJ R-138/D34.1)

N00 00.0 E108 06.1

S00 22.7 E107 05.4S00 42.1 E106 19.0

GOBIKKIKOR

SANOS

122 TO KIKOR87 TO SANOS

179 TO GOBIK092^

104^124^

(VTK R-161/D39.0)

(VTK R-140/D103)

From DOSNO turn LEFT and track 128^ to VENTU and follow the appropriate transition route to

At or belowor as directed by ATC

6000'

090^

180^

360^

3400'

2500'2100'090^

180^

360^

3400'

2100'1900'

MSA VTK VOR MSA SJ VOR(RWYS 02C, 20C)

VENTU ONE BRAVO (VEN1B)

4000'At or above

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

track 120^ to DOBLU, then turn RIGHT and track 177^ to DOSNO.

18 MAY 07

DEPARTURES

| JEPPESEN SANDERSON, INC., 2006, 2007. ALL RIGHTS RESERVED.Note 3.

Apt Elev

22'

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

Trans level: FL130 Trans alt: 11000'1. For RNAV operations, aircraft shall be GNSS-equipped and meet RNP-1/P-RNAV

or EXPECT RADAR vectors from ATC. 3.1 2 Therestriction to cross SUDPO at or above 2000' is applicable between 2301-1100 UTC.

6. Cruising levels will be issued after take-off by Singapore RADAR. 7. RADAR required.

All departure aircraft on Runway 20C issued with heading instructions by ATC shallalso cross VTK 8 DME at or above 2000' between 2301-1100 UTC. If the altituderestriction cannot be complied with, the pilot-in-command of an aircraft departingon Runway 20C shall inform ATC during the time when the aircraft commences taxiing

5. Initial departure climb altitude is 3000' or as directed by ATC. to the holding point for departure. 4. All SIDs include noise preferential routes.

023^

NOT TO SCALE

Licensed to QANTAS. Printed on 30 Dec 2011.Notice: After 13 Jan 2012 0901Z, this chart may no longer be valid. Disc 26-2011

JEPPESENJeppView 3.7.5.0

083^

057^

097^

195^

150^

D9.4

D23.2

D24.2

D6.9

D12.8

COMMSLOST COMMSLOST COMMSLOST LOST

COMMSLOST COMMSLOST COMMSLOST LOST

053^

D7.6

COMMS

LOST

COMMS

LOST

COMMS

LOST

LOST

75 100 150 200 250 300

CHANGES:

JEPPESENWSSS/SINCHANGI

SINGAPORE, SINGAPORE

SID

SINJON113.5 SJSJ

N01 13.4 E103 51.3

D

TEKONG116.5 VTKVTK

N01 24.9 E104 01.3

D

10-3S

Gnd speed-KT

1519126610137605063805.0% V/V(fpm)

3.3% V/V(fpm) 251 334 501 668 835 1003

A

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

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

173^

120^

128^

22

16

67

17N01 12.5E103 58.1

SUSIN

At or above4000'

N01 26.1E104 10.7

DOKTA

.RNAV.SID.

1 INITIAL CLIMB

1ROUTING

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

Air Force (RSAF) Aircraft

A

VEN 1E(RWY 02L)

VEN 1F(RWY 20R)

DOSNO

VENTU

N00 48.0 E104 14.2

N00 05.8 E105 06.8

(VEN

1E)

(VEN1F)

(SJ R-113/D24.0)DOBLU

N01 03.8 E104 13.3

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

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

to the last assigned altitude.

to the last assigned altitude.

7600.1. Set transponder to Mode A/C code

2. Communications failure occurs immediately after departure on:

Thereafter refer to Singapore Special Procedures on radio communications failure.

Thereafter refer to Singapore Special Procedures on radio communications failure.

177^

(SJ R-132/D101)

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

VENTU ONE ECHO (VEN1E),

join the ATS route.

(SJ R-138/D34.1)

N00 00.0 E108 06.1

S00 22.7 E107 05.4S00 42.1 E106 19.0

GOBIKKIKOR

SANOS

122 TO KIKOR87 TO SANOS

179 TO GOBIK092^

104^124^

(VTK R-161/D39.0)

(VTK R-140/D103)

From DOSNO turn LEFT and track 128^ to VENTU and follow the appropriate transition route to

At or belowor as directed by ATC

6000'

(RWYS 02L, 20R)

VENTU ONE FOXTROT (VEN1F)

4000'At or above

N01 29.9E104 02.5

(VTK R-013/D5.1)

TOPOM(SJ R-034/D20.0)

2000'At or above

N01 17.9E103 57.4

(VTK R-210/D8.0)SUNVA

2At or above

2000'

172^5

203^

115^ 9

For minimum climb gradient criteria:

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

9 NM 4 NM

Direct distance from Changi Apt(Rwy 02L) to: TOPOM(Rwy 20R) to: SUNVA

, then 3.3%. 400'reaching or passing

090^

180^

360^

3400'

2500'2100'090^

180^

360^

3400'

2100'1900'

MSA VTK VOR MSA SJ VORVENTU O

NE E

CHO

VENTU ONE FOXTROT

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

track 120^ to DOBLU, then turn RIGHT and track 177^ to DOSNO.

DEPARTURES

Note 3. | JEPPESEN SANDERSON, INC., 2006, 2007. ALL RIGHTS RESERVED.

18 MAY 07

Trans level: FL130 Trans alt: 11000'1. For RNAV operations, aircraft shall be GNSS-equipped and meet RNP-1/P-RNAV standard of accuracy. 2. Non-RNP-1/P-RNAV approved aircraft shall fly this as a

1 or EXPECT RADAR vectors from ATC. 3. 2 Thebasic RNAV (B-RNAV) procedurerestriction to cross SUNVA at or above 2000' is applicable between 2301-1100 UTC.

6. Cruising levels will be issued after take-off by Singapore RADAR. 7. RADAR required.

Apt Elev

22'All departure aircraft on Runway 20R issued with heading instructions by ATC shallalso cross VTK 8 DME at or above 2000' between 2301-1100 UTC. If the altituderestriction cannot be complied with, the pilot-in-command of an aircraft departingon Runway 20R shall inform ATC during the time when the aircraft commences taxiing

5. Initial departure climb altitude is 3000' or as directed by ATC. to the holding point for departure. 4. All SIDs include noise preferential routes.

023^

NOT TO SCALE

Page 23: WSSS Charts

Licensed to QANTAS. Printed on 30 Dec 2011.Notice: After 13 Jan 2012 0901Z, this chart may no longer be valid. Disc 26-2011

JEPPESENJeppView 3.7.5.0

JEPPESEN

Apt Elev

the direction of Twy A7.

104-00103-59

Elev 14'

FOR PARKING POSITIONS

D48 and D49. A mandatory instruction sign with the

Pilots are advised to apply minimum thrust when turninginto Twy A1 while taxiing either northwards or southwards

This is in view of apron activities of aircraft stands D47,

inscription "APPLY MNM THRUST" has been installed along

from the north as well as from the south.

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 01-22

01-23stands 506, 507 and 508 diverted

Rw

y 0

2R/20LT2

SO

UTH A

PRO

N

Twy WC centerline behind aircraft

SERVICEAPRON

NORTH 01^E

SOUTH-EASTREMOTE APRON

oversteering may be required when

Pilots operating aircraft with wheel

shall take note that judgemental

APRON

BUDGETTERMINAL

L8

L5

L6

L7

L4

Taxiway centerline along Twy EP

Pilots are advised to applyminimum thrust when turning

T3 SOUTH APRON

| JEPPESEN, 1998, 2011. ALL RIGHTS RESERVED.

1

1

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 offset

maneuvering around taxiway turns.

eastward by 8'

base longer than B747 or 85' (26m)

by aircraft with maximum

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 200' (61m).

wingspan of 118' (36m).

Twys L5 and L8 can only be used

on Taxilane A6, and thereafter when taxiing along Twy A1up to and including the Twy A7 - A1 junction.

the eastern side of Taxilane A6 before the turn into Twy A1

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

Taxilane U4 can only be usedby aircraft with maximum

30 SEP 11

Airport briefing note added.

NO

RTH

APR

ON

Bldg Area

N01 21.6 E103 59.4 CHANGI10-922'SINGAPORE, SINGAPORE

CHANGES:

WSSS/SIN

02L

177'

EP

Bldg Area

Elev 22'

E11

E10

E9

E8

E7

197' Stopway

60m

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

023^

13,123

'40

00m

197'60mStopway

023^

02C

T2 CENTRAL APRON

T2 NORTH APRON

REMOTE APRON

CHANGI EAST(MILITARY ONLY)

138'

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

E1

E2

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

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

For AIPORT BRIEFINGrefer to 10-1P pages.

Licensed to QANTAS. Printed on 30 Dec 2011.Notice: After 13 Jan 2012 0901Z, this chart may no longer be valid. Disc 26-2011

JEPPESENJeppView 3.7.5.0

JEPPESEN

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, 1998, 2011. ALL RIGHTS RESERVED.

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

None.

30 SEP 11

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

SINGAPORE, SINGAPORE

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

Page 24: WSSS Charts

Licensed to QANTAS. Printed on 30 Dec 2011.Notice: After 13 Jan 2012 0901Z, this chart may no longer be valid. Disc 26-2011

JEPPESENJeppView 3.7.5.0

JEPPESEN

| JEPPESEN, 1998, 2009. ALL RIGHTS RESERVED.Chart revised.

205

206207 2

082

09

200

201

202

203

F60

F59

F58

F56

F54

F52

F50

F42

F41

F40

F37

F30

F31

F32

E1

E2

E3

B2

SC1

SC1

E6

EP

E5

C7

C3

C1

F33

F34

F35

F36

E4

E5

E6

E7

B3

B1

B2

EP

E4

A21

A20

A19

A18

A17 A

16A

15 A14

U4

U4

SC2

W10

W9

W8

WP

WA

V8

SC1

A13

A12

A11

A9

A10

A5

A4

A3

A2 A1

V6

V6

W6

W7

WP

WP

WA

WA

V7

B1

B2

B3

B4

B5

B6

B7

B8

B9

B10

C1

C20

WA

WA

W5

VY

VZ

VZ

U1

U1

C22

C23

C24

C25

C26

C11

C13

C15

D30

D32

D34

N2

D35

D36 D37 D

38

C16C

17C

18C

19

300

301

302

303

304

305

306

307

308

309

310N

1

N3

D41

D42

D40

E28

E27

E26

E24

E22

E20

E10

E11

E12

E8

D44

D46

D47D48 D

49

400

401402

404

403

W4

NC2

NC2

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

UTH-E

AST

REM

OTE A

PRO

N

C7

T2 S

OUTH

APRO

N

T2 N

ORTH

APRO

NT1 E

AST

APRO

N

NO

RTH-E

AST

REM

OTE A

PRO

N

T1 W

EST A

PRO

N

T3 N

ORTH

APRO

NT3 S

OUTH

APRO

NNO

RTH

REM

OTE

APRO

N

T1 C

ENTRA

LA

PRO

N

30 OCT 09

T2 C

ENTRA

LA

PRO

N

SC2

EA

ST R

EM

OTE

APRO

N

U2

U3

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:

Licensed to QANTAS. Printed on 30 Dec 2011.Notice: After 13 Jan 2012 0901Z, this chart may no longer be valid. Disc 26-2011

JEPPESENJeppView 3.7.5.0

JEPPESEN

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, 1998, 2009. ALL RIGHTS RESERVED.

30 OCT 09

304305, 306

307 thru 309

310

N01 22.0 E103 59.7N01 22.1 E103 59.7

N01 22.0 E103 59.8

Parking Bays.

1

1 For Parking Positions see 10-9C1

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 21.1 E103 59.3

N01 21.0 E103 59.3

F52, F54, F56F50

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 59.5E24, E26N01 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

200, 201202, 203 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

B5 , B6N01 21.6 E103 59.2B7

T1 West Apron

F58, F59N01 21.0 E103 59.3F60

North Remote Apron

302, 303300, 301 N01 22.1 E103 59.5

N01 22.1 E103 59.6

N01 22.0 E103 59.9

Page 25: WSSS Charts

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JEPPESENJeppView 3.7.5.0

JEPPESEN

509 N01 22.7 E103 59.6

505

506

504

503

502

507

508

509

604

603

602

601

606 607

609

| JEPPESEN, 2006, 2009. ALL RIGHTS RESERVED.

30 OCT 09

103 104

12

3456

78

9

10

E8

L8

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

Chart depiction.

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

PARKING BAY COORDINATES

COORDINATESBAY No. BAY No. COORDINATES

TERMINALAPRON

BUDGET

103, 104

PARKING BAY COORDINATES

BAY No.

Budget Terminal Apron

31, 2

N01 20.5 E103 59.2

COORDINATES

N01 20.4 E103 59.24 thru 67 thru 10

N01 20.5 E103 59.2

N01 20.4 E103 59.1N01 20.3 E103 59.1

South-East Remote Apron

Licensed to QANTAS. Printed on 30 Dec 2011.Notice: After 13 Jan 2012 0901Z, this chart may no longer be valid. Disc 26-2011

JEPPESENJeppView 3.7.5.0

SINGAPORE, SINGAPORECHANGI

WSSS/SIN JEPPESEN+

TAXIING GUIDANCE SYSTEM AT SINGAPORE CHANGI AIRPORT

The taxiing guidance system at Singapore Changi Airport consists of stop bars andselectable segments of green taxiway centerline lights. The system is designed to pro-vide pilots with visual guidance while taxiing during night operations and during periods of low visibility. It is controlled by the Ground Movement Controller (GMC) atChangi Control 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 cen-terline lights on the maneuvering area are switched on automatically. When two ormore routes are selected, the system will give priority to the first route and activatered stopbar lights across conflicting routes, as necessary. A segment of the centerlinelights of the conflicting routes that cut across the first route will also be suppressed.The GMC has the option of overriding the taxiing route priority by selecting or dese-lecting the appropriate stopbar lights.

All taxiing guidance lights on taxiways leading to the runways terminate at the runwayholding positions where, by default, red stopbar lights remain on unless deselected bythe runway controller. When deselected, these stopbar lights will re-activate auto-matically after 50 seconds.

Information and Mandatory Signs / Markings

When following the directional guidance provided by the green taxiway centerlinelights and red stop bar lights, pilots are advised to also navigate their taxi route withreference to information and mandatory sign / markings provided at the airport so asto maintain situational awareness of their whereabouts at all times.

10-9C230 OCT 09

| JEPPESEN, 2007, 2009. ALL RIGHTS RESERVED.

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| JEPPESEN, 2008, 2010. ALL RIGHTS RESERVED.

SINGAPORE, SINGAPORECHANGI

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

Licensed to QANTAS. Printed on 30 Dec 2011.Notice: After 13 Jan 2012 0901Z, this chart may no longer be valid. Disc 26-2011

JEPPESENJeppView 3.7.5.0

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SINGAPORE, SINGAPORECHANGI

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

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

WSSS/SIN 23 DEC 11 10-9D SINGAPORE, SINGAPORECHANGI

FLIGHT LEVELS TO DEPARTING AIRCRAFT

GENERAL

a. 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.

b. Departing flights from Singapore requesting FL 280 or FL 320 on L759, M770, N571,

1. Aircraft departing Singapore will be cleared to FL 280.

2. Succeeding aircraft on the same route will be cleared to FL 280 with 10 min longitudinal

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.

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

PROCEDURES paragraph a. when ready for push back.

d. A Multilateration Surveillance System (MSS) is operational at Changi airport. The Mode S

transponder equipped vehicles on the airport surface. Procedures/Actions required by pilotspre-push back/taxi:

1. The pilot will be requested to enter a Mode A code at start-up (i.e. assigned Mode A code). This code will be either a discrete or non-discrete code (A conspicuous code, e.g.

according to specific installation, auto if available, not OFF or SDBY) and the assignedMode A code is selected from the request for push back or taxi, whichever is earlier.

2. Whenever the aricraft is capable of reporting aircraft identification (i.e. the ICAO callsign

used in flight inserted in the FMS (Flight Management System) or transponder control

panel) the aircraft's identification should also be entered from the request for push backor taxi whichever is earlier, through the FMS (Flight Management System) or the transponder control panel. Flight crew must use the 3-letter ICAO designator of the

landing, pilots shall ensure that the transponder is operating (i.e. XPNDER or the

equivalent according to specific installation, auto if available, not OFF or SDBY) afterlanding, continuously until the aircraft is fully parked on the stand.

PROCEDURES

a. The pilot shall notify ATC whene the aircraft is ready to push back within 5 min usingthe 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 canceled upon expiration of the 5 minute grace period.

MSS will provide the controller with surveillance and identification of all aircraft and

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.

1000). Pilots shall ensure that the transponder is operating (i.e. XPNDR or the equivalent

operator, followed by the Flight Identification number (i.e. BAW123, SIA002). After

- persons on board

Procedure text.

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JEPPESENJeppView 3.7.5.0

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WSSS/SIN 23 DEC 11 10-9E SINGAPORE, SINGAPORECHANGI

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

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

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.

CANCELLATION OF ATC CLEARANCE

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)'.

OBTAINING A FRESH CLEARANCE

Pilots who are ready to depart following the cancellation of an ATC clearance will adopt the normal procedures as if it is the first time they are ready to depart.

REGULATING OF AIR TRAFFIC MOVEMENTS AFTER CLOSURE OF SINGAPORE CHANGIAIRPORT'S RUNWAYS/CONTROL ZONE

a. in order to prevent unncessary air traffic congestion which normally occurs followingthe resumption of air traffic operations after the closure of the Singapore Changi Airport'sRunways/Control Zone, due to VIP Movement or Major Air Exercise, slot-times will beintroduced to regulate the flow of aircraft which are scheduled to depart for a period of at

traffic conditions all such departures will be spaced at intervals of 5 minutes or more to

b. During the one hour period, pilots will be required to give ATC 5 minutes notice prior to starting engines.

c. Slot time is defined as the time during which take-off clearance may be expected.

paragraph c., it is until 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:

least one hour after the commencement of operations. Thus, depending on the prevailing

minimize unnecessary delays on the ground, which may be caused by arriving aircraft.

None.

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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 confirmation

from 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.

Standard pushback approved.

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

Pushback approved, to face North (or South).

10-9F

| JEPPESEN, 1999, 2009. ALL RIGHTS RESERVED.

12 JUN 09

Licensed to QANTAS. Printed on 30 Dec 2011.Notice: After 13 Jan 2012 0901Z, this chart may no longer be valid. Disc 26-2011

JEPPESENJeppView 3.7.5.0

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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.

Pushback approved, to face North.

Pushback approved, to face South.

A11 The aircraft (on idle thrust) shall be pushed back onto TWY U2 to face North until the nose of the aircraft is at the intersection of the aircraft stand lead-in line and TWY U2 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.

Pushback approved, to face North.

Pushback approved, to face South.

A12 The aircraft (on idle thrust) shall be pushed back onto TWY U2 to face North until the nose of the aircraft is at the intersection of the aircraft stand lead-in line and TWY U2 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.

Pushback approved, to face North.

Pushback approved, to face South.

A13, A14, A15

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

Pushback approved, to face South.

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

Pushback approved to face North(or South).

APRON/ACFT STANDS PUSHBACK PROCEDURES

PHRASEOLOGY USED BY SINGAPORE

GROUND

10-9G

| JEPPESEN, 1999, 2009. ALL RIGHTS RESERVED.

12 JUN 09

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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.

Standard pushback approved.

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.

Standard pushback approved.

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.

Standard pushback approved.

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

Standard pushback approved.

B1 The aircraft shall be pushed back onto 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.

Standard pushback approved.

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

APRON/ACFT STANDS PUSHBACK PROCEDURES

PHRASEOLOGY USED BY SINGAPORE

GROUND

10-9H

| JEPPESEN, 1999, 2009. ALL RIGHTS RESERVED.

12 JUN 09

Licensed to QANTAS. Printed on 30 Dec 2011.Notice: After 13 Jan 2012 0901Z, this chart may no longer be valid. Disc 26-2011

JEPPESENJeppView 3.7.5.0

SINGAPORE, SINGAPORECHANGI

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.

Standard pushback approved.

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

Pushback approved, to face North (or South).

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

Pushback approved, to face North (or South).

B5, B6 The aircraft (on idle thrust) shall be pushed back onto TWY WA to face North until the nose of the aircraft is behind the stopbar behind aircraft stand B4. The aircraft may breakaway from there. 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.

Pushback approved, to face North.

Pushback approved, to face South.

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

Pushback approved, to face South.

Pushback approved, to face North.

B8 The aircraft (on idle thrust) shall be pushed back onto TWY U1 to face South until its nosewheel is at the intersection of the aircraft stand lead-in line and TWY U1 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.

Pushback approved, to face South.

Pushback approved, to face North.

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

Pushback approved to face North (or South).

APRON/ACFT STANDS PUSHBACK PROCEDURES

PHRASEOLOGY USED BY SINGAPORE

GROUND

10-9J

| JEPPESEN, 1999, 2009. ALL RIGHTS RESERVED.

12 JUN 09

Page 30: WSSS Charts

Licensed to QANTAS. Printed on 30 Dec 2011.Notice: After 13 Jan 2012 0901Z, this chart may no longer be valid. Disc 26-2011

JEPPESENJeppView 3.7.5.0

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WSSS/SIN JEPPESEN+

EAST REMOTE200, 201, 202, 203

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

Pushback approved, to face North (or South).

SOUTH-EAST REMOTE

103, 104 The aircraft (on idle thrust) shall be pushed back onto Twy SC2 to face East (or West) until the nose of the aircraft is behind the stopbar on Twy SC2. The aircraft may breakaway from there.

Pushback approved, onto SC2 to face East (or West).

205, 206, 207, 208

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

Pushback approved, to face North (or South).

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

Pushback approved, to face North (or South).

NORTH REMOTE

300, 303 The aircraft (on idle thrust) shall be pushed back facing West until its nosewheel is at the intersection of the lead-in line and taxiway centerline. ORThe aircraft (on idle thrust) shall be pushed back facing East until its nosewheel is at the intersection of the lead-in line and taxiway centerline.

Pushback approved, to face West.

Pushback approved, to face East.

301, 304, 305

The aircraft (on idle thrust) shall be pushed back to face East (or West) until its nosewheel is at the intersection of the lead-in line and the taxiway centerline.

Pushback approved, to face East (or West).

302, 306 The aircraft (on idle thrust) shall be pushed back to face East until its nosewheel is at the intersection of the lead-in line and the taxiway centerline.

ORThe aircraft (on idle thrust) shall be pushed back to face West until its nosewheel is at the intersection of the lead-in line and TWY A6 centerline.

Pushback approved, to face East.

Pushback approved, to face West.

307, 308, 309, 310

The aircraft (on idle thrust) shall be pushed back to face East (or West) until its nosewheel is at the intersection of the lead-in line and TWY NC2 centerline.

Pushback approved, to face East (or West).

NORTH-EAST REMOTE

400, 401, 402, 403, 404

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

Pushback approved, to face North (or South).

WEST CARGO502 The aircraft (on idle thrust) shall be pushed back to

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

Pushback approved, to face North (or South)

503, 504, 505, 506

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

Pushback approved, to face North (or South).

507, 508 The aircraft (on idle thrust) shall be pushed back to face South.

Standard pushback approved.

APRON/ACFT STANDS PUSHBACK PROCEDURES

PHRASEOLOGY USED BY SINGAPORE

GROUND

10-9K

| JEPPESEN, 1999, 2010. ALL RIGHTS RESERVED.

29 OCT 10

Licensed to QANTAS. Printed on 30 Dec 2011.Notice: After 13 Jan 2012 0901Z, this chart may no longer be valid. Disc 26-2011

JEPPESENJeppView 3.7.5.0

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WSSS/SIN JEPPESEN+

509 The aircraft (on idle thrust) shall be pushed back to face South until its nosewheel is at the intersection of the pushback line and TWY WC centerline.

Standard pushback approved.

EAST CARGO601, 602 The aircraft (on idle thrust) shall be pushed back to

face South until its nosewheel is at the intersection of the lead-in line and TWY EA centerline.

Standard pushback approved.

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

Standard pushback approved.

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

Standard pushback approved.

T1 WEST

C1, C20, C22, C23, C24, C25

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

Pushback approved, to face North (or South).

C26 The aircraft (on idle thrust) shall be pushed back onto TWY WA to face North. The aircraft may breakaway from there. ORThe aircraft (on idle thrust) shall be pushed back onto TWY WA to face South until its nosewheel is at the intersection of the aircraft stand lead-in line and TWY WA centerline. The aircraft shall then be towed forward until its nosewheel is on the "END OF TOW" position. This is marked as "EOT" on the ground. The aircraft may breakaway from there.

Pushback approved, to face North.

Pushback approved, to face South.

T1 CENTRALC11 The aircraft (on idle thrust) shall be pushed back such

that the pushback line is always kept midway between the aircraft main gear until the nosewheel of the aircraft is at the "EOP 21" position. The aircraft shall then be towed forward until its nosewheel is at the "EOT 22A" position.

Standard pushback approved.

APRON/ACFT STANDS PUSHBACK PROCEDURES

PHRASEOLOGY USED BY SINGAPORE

GROUND

10-9L

| JEPPESEN, 1999, 2010. ALL RIGHTS RESERVED.

29 OCT 10

Page 31: WSSS Charts

Licensed to QANTAS. Printed on 30 Dec 2011.Notice: After 13 Jan 2012 0901Z, this chart may no longer be valid. Disc 26-2011

JEPPESENJeppView 3.7.5.0

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WSSS/SIN JEPPESEN+

C13 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 nosewheel is at the ’’END OF PUSH (Stopbar 22)’’ position. The aircraft shall be towed forward until its nosewheel is at the ’’END OF TOW (Stopbar 22A)’’ position.

ORAlternate Pushback ProcedureThe aircraft (on idle thrust) shall be pushed back onto Taxiway N2 to face South followed by Taxiway N3 until the nose of the aircraft is behind the stopbar line behind the aircraft stand D35. The aircraft may break away from there.

ORAlternate Pushback ProcedureThe aircraft (on idle thrust) shall be pushed back onto Taxiway N2 to face South followed by Taxiway N1 until the nose of the aircraft is behind the stopbar line behind aircraft stand C16. The aircraft may break away from there.

Standard pushback approved.

Pushback approved, onto Twy N3 to face South.

Pushback approved, onto Taxiway N1 to face South.

D32 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 nosewheel is at the ’’END OF PUSH (Stopbar 22)’’ position. The aircraft shall then be towed forward until its nosewheel is at the ’’END OF TOW (Stopbar 22A)’’ position.

ORAlternate Pushback Procedure The aircraft (on idle thrust) shall be pushed back onto Taxiway N2 to face South followed by Taxiway N3 until the nose of the aircraft is behind the stopbar line behind the aircraft stand D35. The aircraft may break away from there.

ORAlternate Pushback ProcedureThe aircraft (on idle thrust) shall be pushed back onto Taxiway N2 to face South followed by Taxiway N1 until the nose of the aircraft is behind the stopbar line behind aircraft stand C16. The aircraft may break away from there.

Standard pushback approved.

Pushback approved, onto Twy N3 to face South.

Pushback approved, onto Taxiway N1 to face South.

C15, D34 The aircraft (on idle thrust) shall be pushed back facing North until its nosewheel is at the intersection of the lead-in line and TWY N2 centerline.

ORAlternate Pushback Procedure The aircraft (on idle thrust) shall be pushed back onto Taxiway N2 to face South followed by Taxiway N3 until the nose of the aircraft is behind the stopbar line behind the aircraft stand D35. The aircraft may break away from there.

ORAlternate Pushback ProcedureThe aircraft (on idle thrust) shall be pushed back onto Taxiway N2 to face South followed by Taxiway N1 until the nose of the aircraft is behind the stopbar line behind aircraft stand C16. The aircraft may break away from there.

Standard pushback approved.

Pushback approved, onto Taxiway N3 to face South.

Pushback approved, onto Taxiway N1 to face South.

C16, C17 The aircraft (on idle thrust) shall be pushed back to face North (or South) until its nosewheel is at the intersection of the lead-in line and TWY N1 centerline.

Pushback approved, to face North (or South).

C18 The aircraft (on idle thrust) shall be pushed back to face North until its nosewheel is at the intersection of the lead-in line and TWY N1 centerline.

Standard pushback approved.

C19 The aircraft (on idle thrust) shall be pushed back to face North along TWY N1 until the "END OF PUSHBACK" position.

Standard pushback approved.

APRON/ACFT STANDS PUSHBACK PROCEDURES

PHRASEOLOGY USED BY SINGAPORE

GROUND

10-9L1

| JEPPESEN, 2007, 2010. ALL RIGHTS RESERVED.

12 NOV 10

Licensed to QANTAS. Printed on 30 Dec 2011.Notice: After 13 Jan 2012 0901Z, this chart may no longer be valid. Disc 26-2011

JEPPESENJeppView 3.7.5.0

SINGAPORE, SINGAPORECHANGI

WSSS/SIN JEPPESEN+

D30 The aircraft (on idle thrust) shall be pushed back such that the pushback line is always kept midway between the aircraft main gear until the nosewheel of the aircraft is at the "END OF PUSH (Stopbar 20)" position. The aircraft shall then be towed forward until its nosewheel is at the "END OF TOW (Stopbar 22A)" position.

Standard pushback approved.

D35, D36 The aircraft (on idle thrust) shall be pushed back to face North (or South) until its nosewheel is at the intersection of the lead-in line and TWY N3 centerline.

Pushback approved, to face North (or South).

D37 The aircraft (on idle thrust) shall be pushed back to face North until its nosewheel is at the intersection of the lead-in line and TWY N3 centerline.

Standard pushback approved.

D38 The aircraft (on idle thrust) shall be pushed back to face North along TWY N3 until the "END OF PUSHBACK" position.

Standard pushback approved.

T1 EASTD40, D41, D42, D44, D46, D47, D48, D49

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

Pushback approved, to face North (or South).

T2 CENTRALE1 The aircraft (on idle thrust) shall be pushed back such

that the pushback line is always kept midway between the aircraft main gear until its nosewheel is at Stopbar 12. This is marked as "END OF PUSHBACK" on the ground. The aircraft shall then be towed forward to Stopbar 9. This is marked as "END OF TOW"on the ground.

Standard pushback approved.

E2 The aircraft (on idle thrust) shall be pushed back until its nosewheel is at the intersection of the lead-in line and TWY B2 centerline. The aircraft shall then be towed forward to Stopbar 9. This is marked as "END OF TOW" on the ground.

Standard pushback approved.

E3 The aircraft (on idle thrust) shall be pushed back until its nosewheel is at Stopbar 9. This is marked as "END OF TOW" on the ground.

Standard pushback approved.

E4 The aircraft (on idle thrust) shall be pushed back until its nosewheel is at Stopbar 8. This is marked as "END OF PUSHBACK" on the ground.

OR

Standard pushback approved.

The aircraft (on idle thrust) shall be pushed back onto TWY B3 until its nosewheel is at Stopbar 7A.

OR

Pushback approved, to pushback onto TWY B3.

The aircraft (on idle thrust) shall be pushed back onto TWY B1 until its nosewheel is at Stopbar 13A.

Pushback approved to pushback onto TWY B1.

E5, E6 The aircraft (on idle thrust) shall be pushed back until its nosewheel is at the intersection of the lead-in line and TWY B1 centerline. The aircraft shall then be towed forward to Stopbar 13. This is marked as "END OF TOW" on the ground.

Standard pushback approved.

E7 The aircraft (on idle thrust) shall be pushed back until its nosewheel is at Stopbar 13. This is marked as "END OF TOW" on the ground.

Standard pushback approved.

APRON/ACFT STANDS PUSHBACK PROCEDURES

PHRASEOLOGY USED BY SINGAPORE

GROUND

| JEPPESEN, 2007, 2010. ALL RIGHTS RESERVED.

10-9L212 NOV 10

Page 32: WSSS Charts

Licensed to QANTAS. Printed on 30 Dec 2011.Notice: After 13 Jan 2012 0901Z, this chart may no longer be valid. Disc 26-2011

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WSSS/SIN JEPPESEN+

F30 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 nosewheel is at Stopbar 11. 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.

Standard pushback approved.

F31 The aircraft (on idle thrust) shall be pushed back until its nosewheel is at Stopbar 10. This is marked as "END OF PUSHBACK" on the ground. The aircraft shall then be towed forward to Stopbar 9. This is marked as "END OF TOW" on the ground.

Standard pushback approved.

F32 The aircraft (on idle thrust) shall be pushed back until its nosewheel is at Stopbar 9. This is marked as "END OF TOW" on the ground.

Standard pushback approved.

F33 The aircraft (on idle thrust) shall be pushed back until its nosewheel is at Stopbar 8. This is marked as "END OF PUSHBACK" on the ground.

OR

Standard pushback approved.

The aircraft (on idle thrust) shall be pushed back onto TWY B1 until its nosewheel is at Stopbar 13A.

OR

Pushback approved to pushback onto TWY B1.

The aircraft (on idle thrust) shall be pushed back onto TWY B3 until its nosewheel is at Stopbar 7A.

Pushback approved, to pushback onto TWY B3.

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

Standard pushback approved.

F36 The aircraft (on idle thrust) shall be pushed back until its nosewheel is at Stopbar 7. This is marked as '’END OF TOW" on the ground.

Standard pushback approved.

T2 NORTH

E8 The aircraft (on idle thrust) shall be pushed back until its nosewheel is at Stopbar 14. This is marked as "END OF PUSHBACK" on the ground. The aircraft shall then be towed forward to Stopbar 15. This is marked as "END OF TOW" on the ground.

Standard pushback approved.

E10 The aircraft (on idle thrust) shall be pushed back with the main gear mid-point following the main gear pushback line until its nosewheel is at Stopbar 19. This is marked as "END OF PUSHBACK" on the ground. The aircraft shall then be towed forward to Stopbar 18. This is marked as "END OF TOW" on the ground.

Standard pushback approved.

E11 The aircraft (on idle thrust) shall be pushed back:- 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 the ground.

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

ORAlternate Pushback Procedure for aircraft wingspan of more than 213ft (65m):The aircraft (on idle thrust) shall be pushed back with main gear mid-point following the main gear pushback line until its nosewheel 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.

Standard pushback approved.

Pushback approved, onto TWY A6.

Pushback approved, onto TWY A6.

APRON/ACFT STANDS PUSHBACK PROCEDURES

PHRASEOLOGY USED BY SINGAPORE

GROUND

10-9L3

| JEPPESEN, 2007, 2011. ALL RIGHTS RESERVED.

21 JAN 11

Licensed to QANTAS. Printed on 30 Dec 2011.Notice: After 13 Jan 2012 0901Z, this chart may no longer be valid. Disc 26-2011

JEPPESENJeppView 3.7.5.0

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WSSS/SIN JEPPESEN+

E12 The aircraft (on idle thrust) shall be pushed back:- until its nosewheel is at the intersection of the lead-in line and Twy A5 centerline. The aircraft shall then be towed forward to Stopbar 16. This is marked as "END OF TOW" on the ground.

OR

Standard pushback approved.

- onto Twy A6 until its nosewheel is at the intersection of Twy A5 and A6 centerlines.

Pushback approved, to pushback onto TWY A6.

E20 The aircraft (on idle thrust) shall be pushed back with the main gear mid-point following the main gear pushback line until its nosewheel is at Stopbar 17. The aircraft shall then be towed forward to "END OF TOW" Stopbar 18A. Aircraft may breakaway from here.

Standard pushback approved.

E22 The aircraft (on idle thrust) shall be pushed back with the main gear mid-point following the main gear pushback line until its nosewheel is at Stopbar 19. This is marked as "END OF PUSHBACK" on the ground. The aircraft shall then be towed forward to Stopbar 18. This is marked as "END OF TOW" on the ground.

Standard pushback approved.

E24 The aircraft (on idle thrust) shall be pushed back facing North with the main gear mid-point following the main gear pushback line until its body is aligned with TWY A6 centerline. Aircraft may breakaway from there.

Standard pushback approved.

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

Standard pushback approved.

E27, E28 The aircraft (on idle thrust) shall be pushed back to face North (or South) until its body is aligned with TWY A6 centerline.

Pushback approved, to face North (or South).

T2 SOUTHF37 The aircraft (on idle thrust) shall be pushed back with the

main gear following the main gear pushback line, until its nosewheel is on the "END OF PUSH (EOP)" Stopbar 4 behind aircraft stand F42.

ORThe aircraft (on idle thrust) shall be pushed back with the main gear following the main gear pushback line, until its nosewheel is on the "END OF PUSH (EOP)" Stopbar 5 on TWY C1.

Standard pushback approved

Pushback approved, to face East on TWY C1.

F40, F52 The aircraft (on idle thrust) shall be pushed back until its nosewheel is at Stopbar 2. This is marked as "END OF PUSH" on the ground. The aircraft shall then be towed forward to Stopbar 3. This is marked as "END OF TOW" on the ground.

Standard pushback approved.

F41, F42 The aircraft (on idle thrust) shall be pushed back until its nosewheel is at the intersection of the lead-in line and the TWY C2 centerline. The aircraft shall then be towed forward to Stopbar 4. This is marked as "END OF TOW 4" on the ground.

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

Standard pushback approved.

Pushback approved, to pushback onto TWY C6.

F42 ORAlternate Pushback Procedure for aircraft wingspan of more than 213ft (65m):The aircraft (on idle thrust) shall be pushed back until its nosewheel is at the "END OF PUSH 4A" position. The aircraft shall then be towed forward with its nosewheel following the towed forward line until its nosewheel is on the "END OF TOW 4B" position behind aircraft Stand F59.

Pushback approved, to push onto TWY C6.

APRON/ACFT STANDS PUSHBACK PROCEDURES

PHRASEOLOGY USED BY SINGAPORE

GROUND

10-9L421 JAN 11

| JEPPESEN, 2009, 2011. ALL RIGHTS RESERVED.

Page 33: WSSS Charts

Licensed to QANTAS. Printed on 30 Dec 2011.Notice: After 13 Jan 2012 0901Z, this chart may no longer be valid. Disc 26-2011

JEPPESENJeppView 3.7.5.0

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WSSS/SIN JEPPESEN+

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

Standard pushback approved.

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

Standard pushback approved.

F56 The aircraft (on idle thrust) shall be pushed back until its nosewheel is at position mid-point between aircraft stands F52 and F56 on TWY C6 centerline.

Standard pushback approved.

F58, F59, F60

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

Pushback approved, to face North (or South).

BUDGET TERMINAL1, 2 The aircraft (on idle thrust) shall be pushed back to

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

OR

Pushback approved, to face West.

The aircraft (on idle thrust) shall be pushed back onto TWY L5 to face North until its nosewheel is behind the stopbar behind aircraft stand 3. The aircraft may breakaway from there. Simultaneous pushback is not permitted for aircraft stands 1, 2, and 3.

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

Pushback approved, to face North.

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

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

Pushback approved, to face North or South.

APRON/ACFT STANDS PUSHBACK PROCEDURES

PHRASEOLOGY USED BY SINGAPORE

GROUND

10-9L512 JUN 09

| JEPPESEN, 2009. ALL RIGHTS RESERVED.

Licensed to QANTAS. Printed on 30 Dec 2011.Notice: After 13 Jan 2012 0901Z, this chart may no longer be valid. Disc 26-2011

JEPPESENJeppView 3.7.5.0

JEPPESEN

Apt Elev

| JEPPESEN, 2009. ALL RIGHTS RESERVED.

AERO

DRO

ME A

DVIS

ORY C

HA

RT

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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.

12 JUN 09

Chart reindexed.

N01 21.6 E103 59.4 CHANGI22'SINGAPORE, SINGAPORE

CHANGES:

WSSS/SIN10-9L6

Page 34: WSSS Charts

Licensed to QANTAS. Printed on 30 Dec 2011.Notice: After 13 Jan 2012 0901Z, this chart may no longer be valid. Disc 26-2011

JEPPESENJeppView 3.7.5.0

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

F32

F31

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

12 JUN 09

SOUT

H EA

ST P

IER

TERM

INA

L 2

CHANGES:

SINGAPORE, SINGAPORECHANGI

10-9L7

PUSHBACK PROCEDURES

WSSS/SIN

Chart reindexed. | JEPPESEN, 2008, 2009. ALL RIGHTS RESERVED.

Licensed to QANTAS. Printed on 30 Dec 2011.Notice: After 13 Jan 2012 0901Z, this chart may no longer be valid. Disc 26-2011

JEPPESENJeppView 3.7.5.0

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

APR

ON

EP

7A

B1

B3

B2

E4

A5

A4

A3 E3

13

13A

12 JUN 09

NO

RTH

EAST

PIE

R

TERM

INA

L 2

CHANGES:

SINGAPORE, SINGAPORECHANGI

10-9L8

PUSHBACK PROCEDURES

WSSS/SIN

Chart reindexed. | JEPPESEN, 2008, 2009. ALL RIGHTS RESERVED.

Page 35: WSSS Charts

Licensed to QANTAS. Printed on 30 Dec 2011.Notice: After 13 Jan 2012 0901Z, this chart may no longer be valid. Disc 26-2011

JEPPESENJeppView 3.7.5.0

JEPPESEN

WSSS/SIN 10-9M SINGAPORE, SINGAPORECHANGI

.PARKING.

| JEPPESEN, 1998, 2011. ALL RIGHTS RESERVED.

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 ofADGS 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)

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JEPPESENJeppView 3.7.5.0

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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

| JEPPESEN, 1998, 2011. ALL RIGHTS RESERVED.

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)

Page 36: WSSS Charts

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JEPPESENJeppView 3.7.5.0

JEPPESEN

WSSS/SIN 10-9N1SINGAPORE, SINGAPORE

CHANGI

.PARKING.

| JEPPESEN, 1998, 2010. ALL RIGHTS RESERVED.CHANGES:

22 JAN 10

RLG VISUAL DOCKING GUIDANCE SYSTEM

b. The system is aligned for interpretation by the pilot in the left hand seat.

INTRODUCTION

DOCKING PROCEDURES

A pilot, while taxiing his/her aircraft into a fixed gate, shall STOP the aircraftimmediately if he/she sees that the docking system is not switched on or is un-serviceable, or when it shows a different aircraft type.

a. Aircraft Type Indication

1. Confirm that your aircraft type is displayed prior to turning into stand.2. Discontinue docking when wrong aircraft type is illuminated. (Aircraft

b. Center Line Guidance

1. Look at the bottom half of the housing and interpret vertical neon lights asshown below:

RED REDGREENGREEN GREEN

Aircraft on

centerline- steer towards GREEN

Aircraft right of centerline

- steer towards GREEN

Aircraft left of centerline

2. Discontinue docking when lights go off. (Aircraft Marshaller shall marshalaircraft into bay.)

c. Stopping Guidance

Marshaller shall recheck system or marshal aircraft into stand.)

SteadyGreen

SteadyAmber

SteadyRed

- STOP

- Slow Down4.5m to stop

- Ramp Clear

at right:housing and interpret as shownlamps on the top half of the

1. Look at the round incandescent

marshal aircraft into bay.)(Aircraft Marshaller shall thenshould the lights go off.

2. Discontinue docking immediately

Chart re-indexed.

a. The RLG visual docking guidance system is installed at all the fixed gatesin Terminal 2 of Singapore Changi Airport.

Licensed to QANTAS. Printed on 30 Dec 2011.Notice: After 13 Jan 2012 0901Z, this chart may no longer be valid. Disc 26-2011

JEPPESENJeppView 3.7.5.0

JEPPESEN

WSSS/SIN 10-9N2SINGAPORE, SINGAPORE

CHANGI

.PARKING.

| JEPPESEN, 1998, 2010. ALL RIGHTS RESERVED.CHANGES:

22 JAN 10

d. Stopping Guidance at the North East and South East Piers at Terminal 2

SteadyGreen

SteadyAmber

- Ramp Clear

on the top half of the housing and

TO AVOID OVER SHOOTING

a. When using the RLG system, pilotsare to taxi into the stand at minimumspeed.

Look at the round incandescent lamps

interpret as illustrated:

b. On seeing the round incandescentamber lights, slow down and prepareto stop.

c. The round incandescent amber andred lights are activated manually bythe RLG system operator as theaircraft approaches the stopbar. Pilotsshould stop the aircraft immeadiatelywhen the red lights come on suddenlyor when given the stop sign by theAircraft Marshaller.

Chart re-indexed

SteadyAmber

SteadyRed

- STOP

- Slow Down

SteadyAmber

- Slow Down

- Slow Down

Page 37: WSSS Charts

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JEPPESENJeppView 3.7.5.0

JEPPESEN

WSSS/SIN 10-9P SINGAPORE, SINGAPORECHANGI

.PARKING.

| JEPPESEN, 2004, 2011. ALL RIGHTS RESERVED.CHANGES:

23 DEC 11

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

Aircraft stand C11 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

Licensed to QANTAS. Printed on 30 Dec 2011.Notice: After 13 Jan 2012 0901Z, this chart may no longer be valid. Disc 26-2011

JEPPESENJeppView 3.7.5.0

JEPPESEN

WSSS/SIN 10-9Q SINGAPORE, SINGAPORECHANGI

.PARKING.

| JEPPESEN, 2004, 2011. ALL RIGHTS RESERVED.CHANGES:

23 DEC 11

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

Aircraft stand D30 revised.

B757

B47S

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

Page 38: WSSS Charts

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JEPPESENJeppView 3.7.5.0

JEPPESEN

WSSS/SIN 10-9R SINGAPORE, SINGAPORECHANGI

.PARKING.

| JEPPESEN, 2004, 2011. ALL RIGHTS RESERVED.CHANGES:

16 SEP 11

A321 parking stands.

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

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

Licensed to QANTAS. Printed on 30 Dec 2011.Notice: After 13 Jan 2012 0901Z, this chart may no longer be valid. Disc 26-2011

JEPPESENJeppView 3.7.5.0

JEPPESEN

WSSS/SIN 10-9R1 SINGAPORE, SINGAPORECHANGI

.PARKING.

| JEPPESEN, 2004, 2011. ALL RIGHTS RESERVED.CHANGES:

16 SEP 11

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

None.

MD87

MD11

L101

F70

DC9

DC8

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 F59F30 F31 F32 F33 F34 F35 F36 F37 F60

TERMINAL 2 AIRCRAFT STANDS (contd)

Page 39: WSSS Charts

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JEPPESENJeppView 3.7.5.0

JEPPESEN

WSSS/SIN 10-9R2 SINGAPORE, SINGAPORECHANGI

.PARKING.

| JEPPESEN, 2004, 2011. ALL RIGHTS RESERVED.CHANGES:

25 NOV 11

TERMINAL 3 - Aircraft types that can be parked at stands (o) are as follows:

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

TERMINAL 3 - Aircraft types that can be parked at stands (o) are as follows:(contd)

TERMINAL 3 - Aircraft types that can be parked at stands (o) are as follows:(contd)

B74S gates removed.

B772

B744

B737

A380

A346

A345

A1

A300, A310, A319, A320, A321

B757, B767

B773, B773ER

A2 A3 A4 A5 A9 A10 A11 A12Stands

B737

A380

A346

A345

A300, A310, A319, A320, A321

Stands

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

Stands B1

A332, A333, A343, A345

A346, A380

B772

B2 B3 B4 B5 B6 B7 B8 B9 B10

Stands 1 2 3 4 5 6 7 8 9 10

A319, A320, AT72, B737, DHC7

B757, B767

B744

Licensed to QANTAS. Printed on 30 Dec 2011.Notice: After 13 Jan 2012 0901Z, this chart may no longer be valid. Disc 26-2011

JEPPESENJeppView 3.7.5.0

JEPPESEN

WSSS/SIN 10-9R3 SINGAPORE, SINGAPORECHANGI

.PARKING.

| JEPPESEN, 2004, 2011. ALL RIGHTS RESERVED.CHANGES:

25 NOV 11

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

B748.

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

L101

F70

DC8

DC10

B773

B772

B767

B757

B74S

B747

B737

B727

A345

A330

MD11

L101

IL62

F70

DHC7

DC10

DC8

B757

A380

A330

AircraftType 103 104 200 201 202 203 205 206 207 208 209

REMOTE STANDS

AT72

MD11

A300, A310, A319, A320

A342, A343, A345

B707, B727, B737

B747, B74S

B767, B772, B773, B773ER

B773ER

B707

A342, A343

A319, A320

A300, A310

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

REMOTE STANDS (contd)

B748

Page 40: WSSS Charts

Licensed to QANTAS. Printed on 30 Dec 2011.Notice: After 13 Jan 2012 0901Z, this chart may no longer be valid. Disc 26-2011

JEPPESENJeppView 3.7.5.0

SINGAPORE, SINGAPORECHANGI

WSSS/SIN JEPPESEN+.PARKING.

Aircraft CARGO STANDS

Type 502 503 504 505 506 507 508 509 601 602 603 604

A300 ^ ^ ^ ^ ^ ^ ^ ^ ^ ^ ^ ^

A310 ^ ^ ^ ^ ^ ^ ^ ^ ^ ^ ^ ^

A332 ^ ^ ^ ^ ^ ^ ^ ^ ^ ^ ^ ^

A333 ^ ^ ^ ^ ^ ^ ^ ^ ^ ^ ^ ^

A342 ^ ^ ^ ^ ^ ^ ^ ^ ^ ^ ^ ^

A343 ^ ^ ^ ^ ^ ^ ^ ^ ^ ^ ^ ^

A345 ^ ^

A346 ^ ^

A380 ^ ^

B707 ^ ^ ^ ^ ^ ^ ^ ^ ^ ^ ^ ^

B727 ^ ^ ^ ^ ^ ^ ^ ^ ^ ^ ^ ^

B737 ^ ^ ^ ^ ^ ^ ^ ^ ^ ^ ^ ^

B747 ^ ^ ^ ^ ^ ^ ^ ^ ^ ^ ^ ^

B748 ^ ^ ^ ^ ^

B74S ^ ^ ^ ^ ^ ^ ^ ^ ^ ^ ^ ^

B757 ^ ^ ^ ^ ^ ^ ^ ^ ^ ^ ^ ^

B767 ^ ^ ^ ^ ^ ^ ^ ^ ^ ^ ^ ^

B772 ^ ^ ^ ^ ^ ^ ^ ^ ^ ^ ^ ^

B773 ^ ^ ^ ^ ^ ^ ^ ^ ^ ^ ^ ^

B773ER ^ ^ ^ ^ ^ ^ ^ ^ ^ ^ ^ ^

DC8 ^ ^ ^ ^ ^ ^ ^ ^ ^ ^ ^ ^

DC10 ^ ^ ^ ^ ^ ^ ^ ^ ^ ^ ^ ^

IL62 ^ ^ ^ ^ ^ ^ ^ ^ ^ ^ ^ ^

IL86 ^ ^ ^ ^ ^ ^ ^ ^ ^ ^ ^ ^

L101 ^ ^ ^ ^ ^ ^ ^ ^ ^ ^ ^ ^

MD11 ^ ^ ^ ^ ^ ^ ^ ^ ^ ^ ^ ^

10-9R41 APR 11

| JEPPESEN, 2004, 2011. ALL RIGHTS RESERVED.

Licensed to QANTAS. Printed on 30 Dec 2011.Notice: After 13 Jan 2012 0901Z, this chart may no longer be valid. Disc 26-2011

JEPPESENJeppView 3.7.5.0

JEPPESEN

MALAYSIA

INDONESIA

168^INDONESIASINGAPORE

356^

356^P U

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 W

ANUMA

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.

Air Force (RSAF) Aircraft

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^hdgAKOMA

356^

176^

D20.0 PU

4000

BRIE

FIN

G S

TRIP

TM

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 PUPU

D

4.9

via

3500

D8.0 SJ/R-168

25 NOV 11

| JEPPESEN, 1998, 2011. ALL RIGHTS RESERVED.

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'

Page 41: WSSS Charts

Licensed to QANTAS. Printed on 30 Dec 2011.Notice: After 13 Jan 2012 0901Z, this chart may no longer be valid. Disc 26-2011

JEPPESENJeppView 3.7.5.0

JEPPESEN

MALAYSIA

INDONESIA

168^

INDONESIASINGAPORE

356^

356^P U

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 W

ANUMA

1 D16.6 ICW

023^

4000

3500023^

D8/14

1

SINGAPORE, SINGAPORE

MISSED APCH:

CHANGI

LOC

110.9ICW

FinalApch Crs023^

GS

(3478')3500'

PA

NS O

PS

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

WSSS/SIN

348^

168^

FMS required forholding during SJ VOR

01-10

103-50 104-00 104-10outage.

Air Force (RSAF) Aircraft

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

D116.5 VTKTEKONG

V T K

D11.1 ICW

D16.0 ICWAPIPA

Gnd speed-Kts

REILPAPI PAPI

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

ANUMA

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

335^hdg

AKOMA

356^

176^

D20.0 PU

4000

BRIE

FIN

G S

TRIP

TM

hdg

335^1000'

LT

4000'

APCH FIXMISSED

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^

PAPA UNIFORM115.1 PUPU

D

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.

| JEPPESEN, 1998, 2011. ALL RIGHTS RESERVED.

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.

Rwy 02L 22'22'Apt Elev

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

Licensed to QANTAS. Printed on 30 Dec 2011.Notice: After 13 Jan 2012 0901Z, this chart may no longer be valid. Disc 26-2011

JEPPESENJeppView 3.7.5.0

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 VTK

V T K

D

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

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

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'

1 Timing not authorized when GS inop.

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

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'

Page 42: WSSS Charts

Licensed to QANTAS. Printed on 30 Dec 2011.Notice: After 13 Jan 2012 0901Z, this chart may no longer be valid. Disc 26-2011

JEPPESENJeppView 3.7.5.0

JEPPESEN

SINGAPORE

MALAYSIA

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

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

01-20

01-30

WSSS/SIN

500'

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

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

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

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

1 Timing not authorized when GS inop.

CIRCLE-TO-LAND

NA

A

B

C

D

4000'

R-203

VTK

116.5via ESLUX

ALSF-II

STRAIGHT-IN LANDING RWY20C

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

124.3SINGAPORE Approach (R) SINGAPORE Arrival (R)

119.3120.3SINGAPORE Tower

118.6D-ATIS

*118.25128.6

Tower communications, aircraft speed restriction note removed.

of Rwy.

| JEPPESEN, 1998, 2011. ALL RIGHTS RESERVED.

372 478 531 637 743 849

CHANGES:

Licensed to QANTAS. Printed on 30 Dec 2011.Notice: After 13 Jan 2012 0901Z, this chart may no longer be valid. Disc 26-2011

JEPPESENJeppView 3.7.5.0

JEPPESEN

SINGAPO

RE

MALAYSIA

INDONESIA

SINGAPORE

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:

SINGAPORE, SINGAPORECHANGI

LOC

109.7ICC

FinalApch Crs203^

GS

4500'(4485')

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

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

01-20

01-30

WSSS/SIN

500'

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

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

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

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'

Gnd speed-KtsGS 3.00^

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)

STRAIGHT-IN LANDING RWY20C

115'DA(H) (100')

350m

4500

| JEPPESEN, 1998, 2011. ALL RIGHTS RESERVED.

Ground

124.3SINGAPORE Approach (R) SINGAPORE Arrival (R)

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

Page 43: WSSS Charts

Licensed to QANTAS. Printed on 30 Dec 2011.Notice: After 13 Jan 2012 0901Z, this chart may no longer be valid. Disc 26-2011

JEPPESENJeppView 3.7.5.0

SINGAPO

RE

MALAYSIA

MA

LAYSIA

SIN

GA

PO

RE

Seletar

Paya Lebar

WM(D)-230

WS(R)-38

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

VTK

023^

116.

5

JS

168^SJ113.5

146^

113.5SJJS

203^

602'

611'

761'

440'

TEKONG

116.5 VTKD

V T K

680'

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'(3486')

ILSDA(H)

214'(200')

Apt Elev 22'RWY 20R 14'

MSA VTK VOR

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

128.6 120.3 119.3 118.6 124.3

FMS required for holdingduring SJ VOR outage.

1

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

01-20

01-30

104-00

104-10

WSSS/SIN

D-ATIS

| JEPPESEN SANDERSON, INC., 1998, 2005. ALL RIGHTS RESERVED.

500'

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

573'

29 JUL 05 .Eff.4.Aug.

Procedure.

Alt Set: hPa1. RADAR required. 2. Simultaneous approaches authorized with Rwy 20L or 20C. 3. ILS DMEco-located with glide slope. 4. Maritime vessels of variable heights in water north and southof Rwy. 5. For acft speed restrictions refer to ATC Singapore-1 or Singapore Area 10-1.

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

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

Gnd speed-KtsGS 3.00^

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

70 90 100 120 140 160377 484 538 646 753 8613:21 2:36 2:20 1:57 1:40 1:28

1 Timing not authorized when GS inop.

CIRCLE-TO-LAND

NARVR

VIS 800m

720mRVRVIS 800m

720m RVR 1500mVIS 1600m

ABCD 2000m

RVR 1800mVIS

ABCD

5000'PAPIREIL

PAPI

R-146

SJ

113.5 SAMKODALSF-I

oncrossing

MDA(H) 420'(406')DA(H) 214'(200')

3500'

3.33.2

2500'

0.6

203^

3.8

TCH 57'

RWY 20R 14'

IDUNAD0.8 ICH

IDUROD4.6 ICH

IGULAD11.1 ICHIDVAS

D7.8 ICH

STRAIGHT-IN LANDING RWY20R

4.9

3500

D8/14

CHANGES:

JEPPESEN

1500'

Licensed to QANTAS. Printed on 30 Dec 2011.Notice: After 13 Jan 2012 0901Z, this chart may no longer be valid. Disc 26-2011

JEPPESENJeppView 3.7.5.0

MALAYSIA

INDONESIA

168^INDONESIASINGAPORE

356^

356^P U

115. 1

SINGA-PORE

MALAYSIA

WS(P)-3

WS(P)-24

WS(P)-36

WM(P)-228

WS(R)-2

WS(R)-31

WS(R)-38

WS(D)-1

WS(D)-4

WS(D)-33

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

WS(D)-5Seletar

Paya Lebar

Hang Nadim

[TCH 50']

[3.00^]

0.4 NMto SAPAX

637'

942'

500'

DSINJON

113.5 SJS J

SAMKO

023^

4000

SINGAPORE, SINGAPORE

Ground

124.3

MISSED APCH:

CHANGI 12-1SINGAPORE Approach (R) SINGAPORE Arrival (R)

128.6 119.3

RNAVFinal

Apch Crs023^ (2478')

DA(H)530'2500'

120.3SINGAPORE Tower

118.6

(508')

PA

NS O

PS

D-ATIS

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

WSSS/SIN

348^

168^

01-10

104-00 104-10

Air Force (RSAF) Aircraft

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

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

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

335^hdg

AKOMA

356^

176^

D20.0 PU

4000

01-20

4.4 2.6 5.0 RWY 02L 22'

SAPAXC~2LF

C~2LSRW~2L

1000'

023^

PAPA UNIFORM115.1 PUPU

D

via

STRAIGHT-IN LANDING RWY02L

Rwy 02L 22'22'Apt Elev

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'(508') MDA(H) 580'(558')

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

TM

hdg

335^1000'

LT

4000'

APCH FIXMISSED

360^

090^

3400'

2100'

180^

1900'

MSA VTK VOR

4 NM

660'2000'

4000'SANATSAMKO

13 JUN 08

C~2LS altitude. | JEPPESEN, 2007, 2008. ALL RIGHTS RESERVED.

1670'

WS(P)-49

535'

620'

436'

656'

680'

630'

440'550'

611'

602'

437'

1017'

CHANGES:

523'

JEPPESEN

Page 44: WSSS Charts

Licensed to QANTAS. Printed on 30 Dec 2011.Notice: After 13 Jan 2012 0901Z, this chart may no longer be valid. Disc 26-2011

JEPPESENJeppView 3.7.5.0

MALAYSIA

168^

146^

SJ

SJ

113.5

113.5

SJ

SJ

INDONESIA

MALAYSIA

Paya Lebar

WM(R)-229

WM(D)-230

WM(D)-231

WS(R)-31

WS(D)-34

SINGAPORE

[TCH 50'][3.00^]

4.5 NMto C2~RF3.2 NM

to C2~RF

500'

SINGAPORE, SINGAPORE

Ground

124.3

MISSED APCH:

CHANGI 12-2SINGAPORE Approach (R) SINGAPORE Arrival (R)

128.6 119.3

RNAVFinal

Apch Crs203^ (1986')

DA(H)530'2000'

120.3

SINGAPORE Tower

118.6

(516')

PA

NS O

PS

D-ATIS

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

WSSS/SIN

Air Force (RSAF) Aircraft

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

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 14'

NOMAKC2~RF

RW2~R

1500'

203^

STRAIGHT-IN LANDING RWY20R

Rwy 20R 14'22'Apt Elev

RNAV (GNSS) Rwy 20R

LNAV/VNAV

LNAV/VNAV LNAV

DA(H) 530'(516') MDA(H) 580'(566')

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 VTKVTK

D

RW2~R

C2~RF

NOMAK BIPOP

BIDUS

NYLON(IAF)

(IAF)

(IAF)(IF)

203^

023^

D19.0VTK

3000

SAMKO

348^

168^

D14.0SJ

MISSEDAPCH FIX

203^

110^

290^

216^6.5 4.

1

6.7

3000

3000

3400

5000

D8.0 SJ

1

1

1

1Max 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

TM

360^

090^

3400'

2100'

180^

1900'

MSA VTK VOR

ALSF-I

468'

573'

BIDUS

BIPOPNYLON2000'

Gnd speed-Kts 70 90 100 120 140 160

13 JUN 08

None. | JEPPESEN, 2007, 2008. ALL RIGHTS RESERVED.

680'

440'

611'

602'

CHANGES:

611'

425'

627'

611'

630'

JEPPESEN

Licensed to QANTAS. Printed on 30 Dec 2011.Notice: After 13 Jan 2012 0901Z, this chart may no longer be valid. Disc 26-2011

JEPPESENJeppView 3.7.5.0

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

D113.5 SJS J

SINJON

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 RWY02C

With D8.0 VTK Without D8.0 VTK

RVR

VIS 1600m1500m

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 Crs023^

Minimum Alt

2500'(2485')

MDA(H)

410'(395')

Apt Elev 22'Rwy 02C 15'

(CONDITIONAL)

090^

180^

360^

2100'

3400'

1900'

MSA VTK VOR

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

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

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

FMS required for holdingduring SJ VOR outage.

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'

Page 45: WSSS Charts

Licensed to QANTAS. Printed on 30 Dec 2011.Notice: After 13 Jan 2012 0901Z, this chart may no longer be valid. Disc 26-2011

JEPPESENJeppView 3.7.5.0

JEPPESEN

MALAYSIA

SINGAPO

RE

INDONESIA

SIN

GAPO

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

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

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'

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

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