flight crew b737-300 simulator assessment briefing
Post on 04-Nov-2021
42 Views
Preview:
TRANSCRIPT
FC_B737-300_ Simulator_ Briefing_REV00Applicant
Rev. No. 00 / April 04, 2017
Flight Crew B737-300
Simulator Assessment Briefing
SunExpress Deutschland GmbH
SIMULATOR ASSESSMENT BRIEFING Page 2 of 13
Flight Crew Boeing 737-300 Simulator Assessment Briefing SunExpress Deutschland GmbH
Rev. No. 00 / April 04, 2017
Table of Contents
0 General Information 1 SXD Simulator Assessment Objectives 2 Detailed Information 3 SXD Simulator Assessment Part 1 4 SXD Simulator Assessment Part 2 5 Limitations / Pitch and Power Tables / Bug Settings 6 Cockpit Layouts and Charts
SIMULATOR ASSESSMENT BRIEFING Page 3 of 13
Flight Crew Boeing 737-300 Simulator Assessment Briefing SunExpress Deutschland GmbH
Rev. No. 00 / April 04, 2017
0 General Information
After a positive result of the SXD Psychometric Assessment you are invited to participate in a SXD Simulator Assessment. This assessment will be conducted in a B737 Full Flight Simulator.
Prior the simulator session you will receive a detailed briefing in German language (30 min). You are welcome to ask questions during the briefing at any time.
The simulator will be operated by a SXD Training Captain. Another SXD Training Captain will perform the duties of the Pilot Monitoring (PM). You may choose the right or left hand seat.
The purpose of the attached navigation charts is to familiarize yourself with the LIDO chart layout. Different German airports may be used at the discretion of the SXD Training Captain.
Please read and study the following information in preparation for this event.
1 SXD Simulator Assessment Objectives
Evaluation of the applicants Basic Performance/Competence
Technical
Manual Aircraft Control: Applicants are able to control the aircraft during all manoeuvers. They endeavor to make the flight as accurate and smooth as possible.
Basic Knowledge of Systems: Applicants know the given limits of the screening aircraft well.
Procedural
Knowledge and Adherence: Applicants are thoroughly familiar with the given procedures (e.g. call outs, Flap Retraction/ Extension Schedule) and with basic IFR procedures (e.g. radial interceptions, holding entry).
Interpersonal
Communication: Applicants share information, and assure reception and understanding. Ambiguities and uncertainties are announced.
Leadership and Teamwork: Applicants shows high level of social interaction skills and are acting as a constructive part of the team.
Workload Management: Applicants are able to plan ahead and to minimize negative effects of stress.
Situational Awareness and Decision Making: Applicants recognize and anticipate factors affecting the flight. After these factors are evaluated, they choose the appropriate course of action. To achieve a favorable outcome, the applicants monitor execution and development of the situation.
SIMULATOR ASSESSMENT BRIEFING Page 4 of 13
Flight Crew Boeing 737-300 Simulator Assessment Briefing SunExpress Deutschland GmbH
Rev. No. 00 / April 04, 2017
2 Detailed Information
Your simulator assessment consists of two parts:
Raw Data T/O, SID, Airwork, Navigation Exercises and Raw Data ILS Approach (optional G/A if unstable)
Line Orientated Flight Scenario (LOFT)
As Pilot Flying (PF) it is expected to initiate all checklists, briefings and communications.
It is expected to be familiar with the given procedures. Beyond that use your own procedures.
The PM will not call out parameter deviations and will not initiate any actions unless instructed to do so (e.g. “Set HDG xyz”, “SPEED xyz”, “ALT xyz”,…). Even if your PM is acting passive, keep your PM in the loop (see Interpersonal-Communication). The PM is able to take over controls for a short period of time (e.g. chart preparation, approach setup and approach briefing).
Simulator Setup
Autopilot, Flight Director, Autothrottle and Flight Management Computer are not available
NAV Display in VOR CTR / APP CTR Mode (=Full Rose Mode) or Expanded VOR/APP Mode (=ARC Mode)
Aircraft is parked on the runway; engines running and Flaps 5 set
PF performs COM Setup / NAV Setup / Speed Bug Setting (refer to Section 5)
PF performs Departure Briefing (Emergency Briefing not required)
All checklists on ground are considered to be completed
ATIS is not required
WX
Wind 50° off RWY HDG with 10 kts, VIS 5000, BKN 005 00/-05 QNH 999
Performance Data
TOW 48.00 tons
T/O Flaps 5,T/O N1 90%, CLB N1 85%,V1/VR/V2=125/127/136
Acceleration Altitude 1500ft AAL
Engine Failure Procedure ( EFP ) depending on airport is given by SXD Training Captain
LDG Vref Flaps 30 =131
SIMULATOR ASSESSMENT BRIEFING Page 5 of 13
Flight Crew Boeing 737-300 Simulator Assessment Briefing SunExpress Deutschland GmbH
Rev. No. 00 / April 04, 2017
3 SXD Simulator Assessment Part 1
T/O
PM sets T/O Thrust (90% N1), CPT ( left hand seat) keeps hands on Thrust Levers until V1
Rotation Rate 2-3°/sec
Target Pitch Attitude 17.5°, Speed V2+15-25 kts
At Acceleration Altitude (1500 ft AAL) PF takes over Thrust Levers and sets CLB Thrust (85% N1) and simultaneously lower Pitch Attitude to 10°
Acceleration to Flaps UP Maneuvering Speed (“Speed 210”) Retract flaps according Flap Retraction Schedule
Follow SID / ATC instructions
Flight Patterns Takeoff (All Engines)
PM manually sets T/O
PM calls “80”
PF calls “CHECKED”
80 kts V1 VR
PM calls “V1”
PM calls “ROTATE”
Positive rate of climb
PF calls “GEAR UP”
Pitch 17.5°
Initial climb speed
V2+15 – 25 kts
Pitch 10°
Set Climb Thrust
ACC. ALT
PF calls “SPEED 210”
Passing V2+15 kts
PF calls “FLAPS 1”
Passing 190 kts
PF calls “FLAPS UP”
Follow SID / ATC Instructions
PF calls “AFTER TAKEOFF CHECKLIST”
SIMULATOR ASSESSMENT BRIEFING Page 6 of 13
Flight Crew Boeing 737-300 Simulator Assessment Briefing SunExpress Deutschland GmbH
Rev. No. 00 / April 04, 2017
Airwork
Steep Turns
Climbing and Descending Turns
Navigation Exercises
Position Report
Terrain Awareness
Radial Interceptions
Holding (published or non-published)
Approach
Radar Vectored ILS Approach
Configure according Flaps Extension Schedule
Intercept Localizer with Flaps 5 / Speed 170
At 1 dot below GS Gear Down/ Flaps 15/ Speed 150
Just prior GS intercept Flaps 30 / Speed Vref+5
Flight Patterns ILS Approach (All Engines)
On Radar Vectors for intercept
PF calls “FLAPS 1, SPEED 190”
PF calls “FLAPS 5, SPEED 170”
Localizer capture
PF calls “FINAL HEADING”
One dot below GS
PF calls “GEAR DOWN, FLAPS 15, SPEED 150”
Prior GS intercept
PF calls “FLAPS 30, SPEED Vref+5”
On GLIDE SLOPE
PF calls “MISSED APPROACH ALTITUDE”
PF calls “LANDING CHECKLIST”
SIMULATOR ASSESSMENT BRIEFING Page 7 of 13
Flight Crew Boeing 737-300 Simulator Assessment Briefing SunExpress Deutschland GmbH
Rev. No. 00 / April 04, 2017
Go Around (if unstable)
Command “GO AROUND, FLAPS 15” G/A pitch attitude 15° and simultaneously set G/A Thrust 90% N1
Command “GEAR UP” at positive rate of climb
At Acceleration Altitude (1500 AAL) set CLB Thrust 85% N1 and simultaneously lower pitch attitude to 10°.
Acceleration to Flaps UP maneuvering speed and flap retraction according schedule.
Follow published missed approach procedure
4 SXD Simulator Assessment Part 2
After completion of part 1 the aircraft is repositioned in T/O position with engines running and Flaps 5. All checklists are considered to be completed. Perform your NAV Setup for the cleared SID.
After V1 an Engine Failure will occur
Single Engine Traffic Pattern
Single Engine Radar Vectored ILS APP
Flight Patterns Takeoff (One Engine Inop.)
During the LOFT part the primary concerns are:
A/C Handling during One Engine Inoperative
Procedural / Interpersonal according applicants experience
Workflow Management (Sequence of events, Decision Making Model (e.g. FORDEC), Communication/ Information to ATC/ Cabin Crew/Passengers (e.g. NITS)
PM manually sets T/O
PM calls “80”
PF calls “CHECKED”
80 kts V1 VR
PM calls “V1”
PM calls “ROTATE”
Positive rate of climb
PF calls “GEAR UP”
Pitch ~12.5°
Initial climb speed
V2 - V2+20kts
Pitch ~7.5°
ACC. ALT
PF calls “SPEED 210” Passing V2+15 kts
PF calls “FLAPS 1”
Passing 190 kts
PF calls “FLAPS UP”
Follow Engine Failure Procedure (EFP) / ATC Instructions
PF calls “AFTER TAKEOFF CHECKLIST”
PM calls “ENGINE FAILURE”
SIMULATOR ASSESSMENT BRIEFING Page 8 of 13
Flight Crew Boeing 737-300 Simulator Assessment Briefing SunExpress Deutschland GmbH
Rev. No. 00 / April 04, 2017
Flight Patterns ILS Approach (One Engine Inop.)
Please remember that only the given information is expected to be known and used. Beyond that use your own procedures.
On Radar Vectors for intercept
PF calls “FLAPS 1, SPEED 190”
PF calls “FLAPS 5, SPEED 170”
Localizer capture
PF calls “FINAL HEADING” Prior GS intercept
PF calls “GEAR DOWN, FLAPS 15, SPEED Vref+5”
On GLIDE SLOPE
PF calls “MISSED APPROACH ALTITUDE”
PF calls “LANDING CHECKLIST”
SIMULATOR ASSESSMENT BRIEFING Page 9 of 13
Flight Crew Boeing 737-300 Simulator Assessment Briefing SunExpress Deutschland GmbH
Rev. No. 00 / April 04, 2017
5 Limitations / Pitch and Power Tables / Bug Settings
VLO ( EXT ) 270 kts
FLAP PLACARD SPEEDS
Flap Position VFE – KNOTS IAS
1 230
5 225
15 195
30 185
Pitch and Power all Engine Operative
Speed kts Pitch ° N1 %
Flaps Up
Level Flight
210 ~ 6° 59%
Flaps 1
Level Flight
190 ~ 6,5° 61%
Flaps 5
Level Flight
170 ~6° 59%
Gear Down, Flaps 15
Level Flight /
on Glide
150 ~6° / ~ 4,5° 67 % / 51%
Gear Down. Flaps 30
On Glide
136 ~ 3° 56 %
Note: For reference only
SIMULATOR ASSESSMENT BRIEFING Page 10 of 13
Flight Crew Boeing 737-300 Simulator Assessment Briefing SunExpress Deutschland GmbH
Rev. No. 00 / April 04, 2017
Bug Settings
T/O
LDG
ASI
80 kts
V1
VR
V2 +15 kts 210 kts
ASI
80 kts
Vref
Vref +15 kts 210 kts
Bug One: 80 kts
Bug Two: V1
Bug Three: VR
Bug Four: V2+15 kts
Bug Five: 210 kts
Bug One: 80 kts
Bug Two: Vref
Bug Three: Vref
Bug Four: Vref+15 kts
Bug Five: 210 kts
SIMULATOR ASSESSMENT BRIEFING Page 11 of 13
Flight Crew Boeing 737-300 Simulator Assessment Briefing SunExpress Deutschland GmbH
Rev. No. 00 / April 04, 2017
6 Cockpit Layouts and Charts
Full Rose VOR Mode
1 - Reference VOR DME 2 - Current Heading 3 - Selected Heading Mode 4 - Lateral deviation indication 5 - TO / FROM indication 6 - Wind direction and speed 9 - Drift angle pointer 10 - Selected course pointer 12 - TO / FROM indication 13 - Reference VOR freq.
Green needle = ADF pointer
SIMULATOR ASSESSMENT BRIEFING Page 12 of 13
Flight Crew Boeing 737-300 Simulator Assessment Briefing SunExpress Deutschland GmbH
Rev. No. 00 / April 04, 2017
Expanded Rose VOR Mode Full Rose VOR Mode
EADI
SIMULATOR ASSESSMENT BRIEFING Page 13 of 13
Flight Crew Boeing 737-300 Simulator Assessment Briefing SunExpress Deutschland GmbH
Rev. No. 00 / April 04, 2017
Main Instrument Panel
02-MAR-2017
AFCGermany Stuttgart
© L
ido
2017
STR-EDDS AFC2-10
AFC
AFC
Stuttgart Germany¡AGC¯ ¡AGC¯
h
h
h
h
h
h
h
h
g
g
g
g
e
d
Y
V
A
AA
A
A
A
V
V
V
E
E
E
E
E
E
E
E
U
U
U
U
U
U
U
U
US
S
S
S
S
S
S
S
S
B
B
BB
B
B
B
B
B
B
D
D
D
D
D
D
D
D
6
b
b
b
b
a
a
a
a
a
a
a
a
a
a
a
a
a
a
a
a
ALTs in brackets are operational
MINO
SBU
MI
DENEL
MI
SUL
MI
IBIRU
MI
TAGIK
MIGEBNO
MIBABEG
MIDITBA
MILUPOL
MIKUNOD
MILB
U
MI
KRH
MIARSUT
Clearance Limit
Clearance Limit
Clearance Limit
ILS Cat 3bD 109.9 ISTW
D8.8 M ISTW M 4000 D3.9 M ISTW M 2 410
ISTW d 115.45 SGD SGD
ILS Cat 3bD 109.5 ISTE
d 115.45 SGD D8.6 M ISTE M 4000 D3.9 ISTE M 2 500
ISTE
SGD
252 ° - 3.00 °
072 ° - 3.00 ° BA07
BA25
2353
43
53
64
84
24
44
93
04
43
3 3
4 3
2 4 6 4
9 3
1 5
S T G
2 5
S T G
165
°
22
5
°
3 0 0 °
0
6
5
°
R131
R132A
R132B
R133
R307R207A
R38
R39
R40
MTA ADEXA SOUTH A
MTA ADEXA SOUTH BMTA ADEXA SOUTH C
MTA ADEXA SOUTH DMTA ADEXA SOUTH E
MTA LANIA 3
R307 N
R307R207B
R207C
R207D
R307
R150 KF2-KE1
R150 JE1-KE1
R150 GE1-JE1
R150 JE1-JD1
R150 JD1-JD2
R150 JD2-JD3
R150 JD2-HD1E
R150 JD2-KD2
R150 JD1-KD2
R150 KD2-KD3
R150 KD3-KD1
R150 KD3-KC1
R150 KD3-KD6
R150 LE1-KE1
R150 LD1-KD6
AARA GRETCHEN
AARA GRETCHEN LOW
4500-CLASS D-FL100
5
5
0
0
-
C
L
A
S
S
D
-
F
L
1
0
0
3
5
0
0
-
C
L
A
S
S
C
-
5
5
0
0
5
5
0
0
-
C
L
A
S
S
D
-
F
L
1
0
0
F
L
7
5
-
C
L
A
S
S
D
-
F
L
1
0
0
FL75-CLASS D-FL100
CLASS D-3500
L
A
N
G
E
N
F
I
R
E
D
G
G
M
U
N
I
C
H
F
I
R
E
D
M
M
1
0
S
T
G
4 0
S
T
G
3
0
S
T
G
5 0
S T G
MITEDGO
MIGEB
NO
MIVESID
MIKRH
MI
OKIB
A
MIETASA
MIROTWE
MISUL
MF
TAGIK
MFABTAL
MFDKB
MIREUTL
MITEKSI
MFBADSO
E
§
4100
8000
12
=
T125
§
MAA
FL2
20
4800
6000
£
O
23
£
T7
24=
MAA
FL25
0
£
E/E
§
32005000
27 Z76=
/=T726
§
MAA FL200/...
4800800029
=T126 §
4800
6000
£
O
10
£
T7
24=
MAA
FL25
0
3400
5000
10
£
T7
26=
46006000
11
£
Y126= MAA FL220
34005000
20
£
T726=
004?
215?
168?
090?
207?
253?
248?
1276AD ELEV
MAG UP VAR 2 ° E
NIKUT
ARSUTEMKIL
TUBL
O
268?6000088?
174?7000354?
0
2
4
6
8
10 NM
E009 ° 00' E009 ° 30' E010 ° 00'
N4
8
°
40'
N4
9
°
00'
Stuttgart
EDTYSchwabisch Hall
feN48 41.3 E009 13.4SGD? 115.45 SGD
lkN48 24.3 E010 06.0LPH
? 111.6 LPHLEIPHEIM
lkN48 13.1 E009 54.7LUP
407 LUPLAUPHEIM
lkN49 20.2 E008 44.0NKR
292 NKRNECKAR
lkN49 08.6 E010 14.3DKB
D 117.8 DKBDINKELSBUHL
lkN48 59.6 E008 35.1KRH
D 115.95 KRHKARLSRUHE
lkN48 22.9 E008 38.7SUL
116.1 SULSULZ
feN48 41.8 E009 15.4
WH
STGD 116.85 STG
lkN48 54.8 E009 20.4
WH
LBUD 109.2 LBU
LUBURG
SOLGO E009 37.1N48 20.3KUNOD
E008 36.3 N48 49.2
R257/D29.7 LBU R174/D10.4 KRH
BADSO
E009 07.7N49 11.4ETASA E009 19.0
N49 12.9OKIBA
E008 57.0N49 11.7TAGIK
E008 47.6N49 10.0VESID
E010 04.1N48 41.4R088/D32.5 STGTEKSI
E008 40.5N48 30.8ROTWE
E010 06.4N48 51.3ABTAL
E009 21.7N48 22.1R166/D20.1 STGREUTL
E009 55.9N49 10.0GEBNO
E009 27.3N49 03.1NOSBU
E009 15.6N48 37.1TEDGO
E009 38.7N48 31.2DITBA
E009 39.9N48 40.3BABEG
E009 54.7N48 13.1LUPOL
E009 16.8N48 37.4IBIRU
2588
2500 ?
3500 ?
3760
MM
2718
2692
2858
2740
2783
2844
2648
28032297
3563
3760
2635
2825
1726
2663
2780
2763
26782953
3191
TA 5000TRL ATC
33 x 28 mm
d 346
°
6000
166?
AB
HP REUTL Clearance Limit REUTL R166/D20 STG N48 22.1 E009 21.7
24 x 33 mm
d 357
° 5000 (6000) 177
°
WH
HP LBU
US
lkN48 54.8 E009 20.4LBU
D 109.2 LBULUBURG
24 x 33 mm
d 346
°
5000
166?
WHHP STG
US
feSTG
D 116.85 STGN48 41.8 E009 15.4
24 x 28 mmde 270 °
d 346
°
5000
166?
1000
090 °
Clearance Limit
MAX 230KT NOO OO.O E000 00.0
5000
AB
ED
vr
st
su
sD
RNAV waypoint fly-by (compulsory)
RNAV waypoint fly-by (non-compulsory)
waypoint fly by (compulsory)
waypoint fly by (non-compulsory)
RNAV waypoint fly-over (compulsory)
RNAV waypoint fly-over (non-compulsory)
waypoint fly over(compulsory)
waypoint fly over (non-compulsory)
A
A
C
vq
WH
HP IBIRU
US
lkN44 44.4 E005 55.5nam
D 123.45 NAMNAME
US
feN44 44.4 E005 55.5ema
D 123.45 EMA
R270
R166
STG
OLLIP
IBIRU N48 37.4 E009 16.8
WAYPOINT
D 13
5.7
ABC
D 116.85 STGD12
D8 RUE
D-ATIS 126.125Langen RAD 125.050
119.200DIR 119.850 0500-2100‡
TWR 118.800119.050
GND 118.600DLV 121.900DCL
07
HL-P2F -0.8%
3.0 °
THR 1267 (45hPa) / TDZ --- (-0.8%)
3045 x 45 15 H60 H
300
25
HL-P2F+0.8%
3.0 ° TDZ --- (+0.8%) / THR 1181 (42hPa)
45 x 334515 H60 H
Landing RWY system:
Changes: Nil
SunExpress (SunExpress)
Effective_18-AUG-201611-AUG-2016 SI
DGermany Stuttgart
© L
ido
2016
STR-EDDS SIDs RWY 25 (RNAV Overlay)4-20
SID
SIDs RWY 25 (RNAV Overlay)
Stuttgart Germany
33
34
42
46
39
225°
300°
065°
165°
STG15
25 STG
10STG
30 STG
GTS04
T50 S G
REIM
S FIR
LFEE
MUNICH FIR EDMM
LANGEN FIR EDGG
E009°00' E009°30' E010°00'
N48°
30'
N48°
40'
R275
R238 LBU
R243 STG
LBU
X
X
Y
Stuttgart
Karlsruhe/Baden-BadenEDSB
LahrEDTL
Schwabisch HallEDTY
VAR 2° EMAG UP
AD ELEV 1276
0
2
4
6
8
10 NM
US
US
US
US
US
N48 41.8 E009 15.4STGD 116.85 STG
LUBURG
LBUD 109.2 LBU
N48 54.8 E009 20.4
N49 08.6 E010 14.3D 117.8 DKBDINKELSBUHL
DKB
D 115.95 KRHKRH
KARLSRUHE
N48 59.6 E008 35.1
SULN48 22.9 E008 38.7116.1 SUL
SULZ
vuED
ED
ED
ED
AB
ED
AB
ED
ED
AB
ED
AB
vuED
ED
AB
ED ED
AB
AB
AB
AB AB
TRL ATCTA 5000
46
40
54
44
4346
5148 93
32
42
33 33
32 3534 35R131
R150D1R150D2
R307 N
R133
R25
R38
R39
R40
R322
R323
R307
R207A
R307R207B
R207C
R307
D526A
D526B
MTA ADEXA SOUTH E
R132A
R132B
R305B
R305C
R205B
R205C
R207D
R111
MTA LANIA 3
TSA 22AR122
R123
R199
MTA ADEXA SOUTH A
MTA ADEXA SOUTH BMTA ADEXA SOUTH C
MTA ADEXA SOUTH D
R150 GE1-JE1
R150 JD2-JD3R150 JD2-HD1E
R150 JD1-JD2
R150 JD2-KD2
R150 JD1-KD2
R150 KD2-KD3
R150 KD3-KD1
R150 KD3-KC1
R150 KD3-KD6
R150 JE1-JD1
R150 KF2-KE1
R150 JE1-KE1
R150 LE1-KE1
R150 LD1-KD6
AARA ANGIE
AARA GRETCHEN
AARA GRETCHEN LOW
AARA UTE
AARA VIRGIN
CL S-0054
D-FL100
AS
001L-
5500
- CLA
SSF
D
FL75-CLASS D-FL100
1A
75-CL SSL
-FL 00D
F
0053-SCLA DS
S3
0055-CSALC-005
S5
A D-FL1S
0LC-005
0
DKB 9B
ETAS
A 4B
GEBNO 7B
KRH 5B
OKIBA 4B
ROTWE 5
B
TAGI
K 4BVESID 4B
KUNOD 2B
ABTAL 4B
TEDGO 1B
SUL 3B11 240°
6
21
065°
1615
R233
13
5000
R066
602
9°19 50
00
004°
25
5000
6
5000 359°
11337°
13
5000278°
053°
18
5000
R355
9 R226
14 5000
004°
135000
22
137°5000
6000R060
£Y126=
11 253°
6000
MAA FL220
4600
£Y126=
22
6000
MAA FL220
5400
£Y125=
18
£O
R224
7000MAA
FL23
0
4900
£T721=
13£
OR1
8960
00
MAA
FL2
50 4800
N48 52.9E009 05.1
N49 11.4E009 07.7
D18.7 LBUE009 55.9N49 10.0D27.9 LBUD12.1 DKB
E008 55.0N48 57.5
E009 19.0N49 12.9
E008 40.5N48 30.8
D35.7 LBU
E008 57.0N49 11.7
E009 15.6N48 37.1
E008 47.6N49 10.0
D25.7 STG
D13.3 KRHD17 LBU
N48 51.3E010 06.4
D18.1 DKBD35.1 STG
N48 21.9E007 53.0
D25 STG
DS050DS040DS041
DS043
KOVAN
ETASA
DS051
GEBNO
DS042
ABGAN
OKIBA
DS049ROTWE
DS046
DS044
DS045
TAGIK
DS048
TEDGO
VESID
ABTAL
TUBLO
DENEL
NATOR IBINI
N48 20.3E009 37.1
KUNOD
D18.1 LBU
4375
3500 ?
2500 ?
2503
25222559
2588
a
a
a
a
a
a
a
a
a
a
a
a
a
a
b
a
a
b
b
b
a
a
a
b
b
2783
2844
2648
2803
2297
4375
3563
3760
2635
3527
2619
2825
1726
2663
2692
2780
2763
28582740
2718
267829533191
2540
2582
15.5 to ABTALInitial climb See Inset
D15.2 DKB
D16 STG
R231 STG
Stuttgart
Not to scale
US
N48 41.8 E009 15.4D 116.85 STGSTG
vu
ED
ED vu
EDED
R
R bank 25°, MAX 230KT
ROTWE 5BSU
L 3B TEDGO 1B
KUNOD 2B
ABTAL 4B21
065°
5339°
11
4
9
198°
2 R252
4
5
22
137°
084°
ABTA
LDS050
DS040
DS041DS
049
DS044
DS045
DS046
DS048 TEDGO
KUNOD
D5.6 STG
D5.9 STG
bank 25°, MAX 230KT
Langen RAD 125.050 119.200DIR 119.850 TEDGO
Changes: PROC renamed, MGA, OBST, SUAs
SunExpress (SunExpress)
Effective_18-AUG-201611-AUG-2016
SIDP
TGermany Stuttgart
© L
ido
2016
STR-EDDS SIDs RWY 25 (RNAV Overlay)5-30ABTAL 4B / DINKELSBUHL 9B / ETASA 4B / GEBNO 7B / KARLSRUHE 5BRWY 25 (252°)
After take-off, contact Langen RAD.
GS 120 150 180 210 240 270
4.0% ft/MIN 500 700 800 900 1000 1100
5.0% ft/MIN 700 800 1000 1100 1300 1400
5.1% ft/MIN 700 800 1000 1100 1300 1400
DESIGNATOR ROUTING ALTITUDES
Runway 25
ABTAL 4B4.0% to 19005.1% to 4000
125.050 1
R252 STG - at D5.9 STG LT (25? bank, MAX 230KT) - crossingR231 STG LT 084? to TEDGO - LT 065? to ABTAL
FMS[A1700+] - DS046 [L] - DS048 [K230-] - TEDGO [L] - ABTAL initial climb 5000
DINKELSBUHL 9BDKB 9B
4.0% to 19005.0% to 4000
125.050 2
R252 STG - at D5.6 STG RT 339° (25? bank, MAX 230KT)intercept R233 LBU to LBU - R066 LBU to DKB
FMS[A1700+] - DS050 [R] - DS040 [K230-] - DS041 [R] - LBU [R] -DKB initial climb 5000
ETASA 4B4.0% to 19005.0% to 4000
125.050 2
R252 STG - at D5.6 STG RT 339° (25? bank, MAX 230KT) -crossing R238 LBU RT 029? to KOVAN - ETASA
FMS[A1700+] - DS050 [R] - DS040 [K230-] - DS043 [R] - KOVAN [L]- ETASA initial climb 5000
GEBNO 7B4.0% to 19005.0% to 4000
125.050 2
R252 STG - at D5.6 STG RT 339° (25? bank, MAX 230KT) -intercept R233 LBU to LBU - R066 LBU - at D15.2 DKB LT 359°to GEBNO
FMS[A1700+] - DS050 [R] - DS040 [K230-] - DS041 [R] - LBU [R] -DS051 [L] - GEBNO initial climb 5000
KARLSRUHE 5BKRH 5B
4.0% to 19005.0% to 4000
125.050 2
R252 STG - at D5.6 STG RT 339° (25? bank, MAX 230KT) -crossing R238 LBU LT 337° to ABGAN - KRH
FMS[A1700+] - DS050 [R] - DS040 [K230-] - DS042 [L] - ABGAN [L]- KRH
initial climb 5000
1 Climb gradient 4.0% due to obstacles, 5.1% due to airspace structure. If unable to comply, inform ATC.2 Climb gradient 4.0% due to obstacles, 5.0% due to airspace structure. If unable to comply, inform ATC.
Changes: Track
SunExpress (SunExpress)
16-MAR-2017 IACGermany Stuttgart
© L
ido
2017
STR-EDDS ILS or LOC 257-40
IAC
ILS or LOC 25
Stuttgart Germany
33
34
424693
225°
300°
065°
165°
15STG
STG25
20TG
S
3GT
S0
GTS
04
E008°30' E009°00' E009°30' E010°20'
N48°
40'
N48°
30'
R233
R174 D 115.95 KRH
R166
R088 STGR277
R223
Stuttgart
VAR 2° EMAG UP
AD ELEV 1276
0
2
4
6
8
10 NM
e
d
d
d
268°
088°6000
174°
354°7000
346°
166°5000
177°
357°5000(6000)
US
US
US
STGD 116.85 STG
D 109.2 LBULBU
LUBURG
SGD? 115.45 SGD
UI
ED
ED
ED
ED
EDED
ED
ED
ED
EDED
ED
ED
ED
ED
ED
EDED
ED
EDED
ED
EDED
TRL ATCTA 5000
ILS or LOC25
D 109.9 ISTWISTW
? 115.45 SGD
R307R207A
R307R207B
R207C
R307
MTA ADEXA SOUTH E
R207D
MTA ADEXA SOUTH B
MTA ADEXA SOUTH A
MTA ADEXA SOUTH C
MTA ADEXA SOUTH D
R307 N
MTA LANIA 3
R150 JD1-JD2
R150 JD2-KD2
R150 JD1-KD2
R150 KD2-KD3R150 KD3-KD6
R150 JE1-JD1 R150 LD1-KD6
AARA ANGIE
AARA GRETCHEN AARA GRETCHEN LOW
Caution
ALTs in brackets are operational
DME required
Use of transition proceduresonly when cleared by ATC
On downwind expect vectors to final
Turbulence must be expectedduring moderate WX conditions,wind 6KT or less, on extended
STGover power plant cooling tower.RWY centerline (D4.6 )
67
54
47
70
39
43
BADSO 25
LBU 25
REUTL 25
ARSU
T 25
TEKSI 25IBIRU 25 (ATC)
252°
17
6000
012°
1660
00
020°
44
166000
346°
12
6000
7
6000261°
4 253°
4343°
97000158°
22
6000
072°
5
76000R156
073°
56000163°
070°
073°
46000343°
6
6000253°
4
R252
339°
053°
6000
6000
4
6000
6000
60004
6
4
6000
5500
4500
4000
6000
UNSER4000
5000
ARSUT
DS520
DS522
DS525
DS515DS514DS513
DS512
FL100
FL8065005500
4500
REUTL
IBIRU
FL100
TEKSI
DS545
DS542
FL100
FL90
BADSO
D10.4 KRH
DS529
DS531
DS535
FL100FL100
D20.1 STG
D4.6 SGD
DS532DS533
DS534
DS523DS524
DS530
D32.3 STGDS543
DS544D3.9 ISTW
D8.8 ISTWD9.5 SGD
D5.6 STG orD4.2 SGD
WH
WH
FL100
D0.7 ISTWD1.4 SGD
3339
2500 ?
2000 ?
2011
2040
2070
2096
2214
2503
2588
a
a
aa
a
a
a
a
a
a
a
b
b
a
a
b
b
b
a
b
b
b
2844
2648
2897
2803
2297
2117
2635
2008
2825
2305
1727
2400
2692
2780
2763
2858
2678
2254
2597
3191
2773
3339Ü
60006000
4
6
7
6000
Clearance Limit
Clearance Limit
Clearance Limit
6000
3
60004
HP STGHP REUTL
d d346°
166°5000
346°
166°6000
US
D 116.85 STGSTG
ED REUTLD20.1 STG
WH Clearance LimitR060 STG
R033
STG
Stuttgart
0
2
4
6
8
10 NM
d177°
357°5000(6000)
US
US
US
D 116.85 STGSTG
D 109.2 LBULUBURG
LBU
SGD? 115.45 SGD
UI
MTA ADEXA SOUTH BMTA ADEXA SOUTH C
R307 N
DME required
5
5000R139
54000
5
9
5000
R052
4000
252°
D5 LBUD10.1 LBU
UNSER
D9.2 STG
D3.9 ISTWD4.6 SGD
D10.6 SGD
D8.8 ISTWD9.5 SGD
WH
WH
D0.7 ISTWD1.4 SGD
Non-FMS ACFT
D-ATIS 126.125DIR 119.850TWR 118.800 119.050GND 118.600
3.80.5 DIST to THR0 5
R252 STGat D4.2 SGD (D5.6 STG) or MNM5000, whichever is later, RT 339 ° - when crossing R277 STG(R223 LBU) RT intercept R233 LBUto LBUmaintain 5000
2410MDA50
D8.8 ISTWD9.5 SGD
UNSERD3.9D4.6
2410
D0.7D1.4
STGISTW
SGD
GS 120 140 160D3.9 ISTW
-MAPt640NA
740NA
850NA
4000 252 °
GP 3.00°LILJ
25
HL-P2F+0.8%
3.0 ° TDZ --- (+0.8%) / THR 1181 (42hPa)
45 x 334515 H60 H 2
1820
3
2140
4
2460
5
2780
7
3410
8.8
4000
3.00 ° LOCD ISTW
25 Cat 3b DME Cat 2 DMEACFT MAX 65/7
Cat 2 DMELTSCat 1 DME
1)Cat 1 DME
1)Circling
C ft - m/kmft
0 - 75R Company
100 - 300R 108 RA
110 - 300R 115 RA
200 - 4001390
200 - 5501390 Not published
D ft - m/kmft
0 - 75R Company
110 - 300R 115 RA 2)
110 - 300R 115 RA 2)
200 - 4001390
200 - 5501390 Not published
1) With EVS 350m 2) If not conducting autoland RVR 350m required
Changes: Nil
SunExpress (SunExpress)
top related