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Flight Design CTLS and CTLS HL 600 kg ClassModel Year 2011
CTLS 600 kg ClassBASIC AIRCRAFT SPECIFICATION - VALID FOR ALL PLATFORMS
Elongated cabin interior sizeHat rack behind the pilot seats
Transponder Garmin GTX 327 Mode A/C installed with antenna
Instrumentation
Two Headset Telex Echelon 25 XT with plug connectors next to the seats
Large instrument console with four single panels Easy accessible fuse and breaker panel on instrument consoleRadio Garmin SL-40 installed with antenna
Carburetor heating
GPS Garmin AERA 510 XM America Database (AirGizmos AERA Panel Mount included)
EngineRotax 912 ULS (100 hp) installed ready to flyAdvanced 3-blade ground adjustable composite propeller, spinner included
Slipper Clutch as protection against shock loading of engine by ground contact of propeller
Two tone cabin interior paint, grey / anthracite, structured surface, high abrasion resistanceOptimized seat adjustment (leg length and seat height coupled, inclination)
Intercom PM 3000 A with aux music input and connection to GPS Audio
Reinforced seatsControls in area of luggage compartment protected with plexiglass covers
Air induction through aluminium Airbox installed to engine frame; round air filter integrated to air path
ELT KANNAD AF 406 Compact (406 MHz / 121.5 MHz transmission)
Rotax engine warranty
Order No.
Access to luggage compartment covered with cloth
Exterior
4-point safety belts for each seat2 storage trays on the cabin floorStrap down hooks in the luggage compartment
Extra wide cabin doors with gas spring
Interior
Improved handling toughness due to reinforced composite layupReinforced fairings
Tires qualified for 120km/h and 300 kg per tire
Cowling hatch for easy oil and water check
Optimised engine shock mounts to improve vibration damping
Instruments certified by FTZ / FAA-TSO / EASA-ETSO (as required)Only available with flight- and engine instrumentation as per one platform selection below
Steerable elastomer damped front wheel
Aeronautical Plexiglass windshield, door windows and skylight, green tinted
Short wings with double winglets to reduce induced drag and increases directional stabilityIncreased vertical fin areaAll- moving stabilator with 75% span antitab as elastic flapOptimized multi- layer two component exterior paint (white) with decals according to selected scheme
Rear side windows to improve oversight
All tires size 4.00 - 6"
Push-to-Talk buttons on each control stick
Long wheelbaseLong fuselage tail boom
Contoured composite main landing gear
2 luggage compartments, accessible through cabin
MATCO main wheels with hydraulic disk brake system
Tires classified for 6 Ply Rating (PR)
Errors and omissions expectedSubject to change without prior notice
Flight Design CTLS and CTLS 600 kg ClassModel Year 2011
Release March 01, 2011Page 3 of 20
Description WeightOrder No.
326,5
349,4Aircraft
Engine Logbook
As per CTLS 600 kg class basic aircraft specification above; with the following modifications:
Rotax 914 UL (115 hp), 4-stroke, 4-cyclinder horizointally opposed spark ignition engine with turbo charger and turbocharge control unit; installed ready to fly
Airplane LogbookFlight Training Supplement in english
ASTM F2245 compliantMaximum Takeoff Mass 600 kg (1320 lbs)
Stretched wings with double winglets to reduce induced drag and increases directional stability
Air induction through aluminium Airbox (loaded by turbo charger) installed to engine frame; round air filter integrated to air path
Systems
CTLS: 70032
Exterior
Components ASTM compliant as required (Engine, Ballistic Recovery System)
CTLS HL LSA (MTOM 600 kg)Basic Aircraft Specification - valid for all CTLS LSA versions
Aircraft
Central, common fuel valveOptimized fuel system
Engine
Manual stabiliser trim by control wheel
Rescue system, suitable for MTOW 600 kg, ASTM compliant
Compliance
Maintenance Manual in english
2 wing tanks, 65l each = 130 l total fuel
Common tank ventilation through winglets
Combination key switch
Dual controls, conventional, three axis
All- moving stabiliser with increased span and antitab as elastic flap
CTLS HL: 70042
CTLS or CTLS HL 600 kg class as per basic aircraft specification above. Platform specific enhancements as follows:
Electronic flap control with pre-selection switchBattery 12V / 7Ah Lead-Acid
DocumentsAircraft Operation Manual in english
Analog oil temperature gauge (small)
Fuel system with two redundant electric fuel pumps, header tank, tank backflow line and fuel tank selector valve
Systems
Analog tachometer (small) Analog oil pressure gauge (small)
Altitude Encoder ACK A30 Analog voltmeter (small)
Slip indicator
Instrumentation
Hobbs hour meter
Flight Instrumentation including:
Magnetic compass with deviation table Analog vertical speed indicator (small) Analog three pointer altimeter (large) Analog airspeed indicator (large)
Engine Instrumentation using:
AIRPLANE BASIC PLATFORM INSTRUMENTATION
Analog cylinder head temperature gauge (small)
CTLS or CTLS HL Club Analog (MTOM 600 kg)
Errors and omissions expectedSubject to change without prior notice
Flight Design CTLS and CTLS 600 kg ClassModel Year 2011
Release March 01, 2011Page 4 of 20
Description WeightOrder No.329
351,9
333,1
356
Oil temperature
CTLS HL: 70045
CTLS or CTLS HL 600 kg class as per basic aircraft specification above. Platform specific enhancements as follows:
Tachometer Oil pressure
Exhaust gas temperature
Back-up battery
Amperemeter
Analog oil temperature gauge (small)
Fuel flow
Hobbs hour meter
Angle of Attack warning
Bright LCD Display
Cylinder head temperature
CTLS: 70035
Altitude Encoder Dynon (or ACK A30 for PtF / EASA ELA 1 aircraft)
Attitude indicator
Vertical Speed indicator
Turn coordinator
Vertical speed
Turn Rate
CTLS or CTLS HL Advanced (MTOM 600 kg)
Flight Instrumentation as Glass Cockpit Dynon EFIS 100:
Altimeter
Instrumentation
Analog Instrumentation - providing redundancy together with Glass Screens:
Airspeed indicator
Bright LCD Display
Aircraft
Single screen 7''
Engine Instrumentation using:
Analog oil pressure gauge (small)
Gyro-stabilized magnetic compass
CTLS or CTLS HL 600 kg class as per basic aircraft specification above. Platform specific enhancements as follows:
Voltmeter
Analog airspeed indicator (small) Analog one pointer altimeter (small) Magnetic compass with deviation table
Analog tachometer (small)
Analog cylinder head temperature gauge (small)
Attitude
Instrumentation
Altitude
Super bright screen
CTLS or CTLS HL Club D60 (MTOM 600 kg)CTLS HL: 70043
Airspeed
CTLS: 70033
Engine monitoring as Glass Cockpit Dynon EMS D120:
Gyro-Stabilized Magnetic Compass
Clock/Timer
Slip indicator
Manifold pressure
G-Meter Voltmeter
Fuel pressure
Horizontal Situation indicator
Aircraft
Flight Instrumentation EFIS-D60 providing:
Errors and omissions expectedSubject to change without prior notice
Flight Design CTLS and CTLS 600 kg ClassModel Year 2011
Release March 01, 2011Page 5 of 20
Description WeightOrder No.
EASA Restricted Type Certificate as LSA Aircraft wihin ELA 1 -
CAAC Type Design Approval as LSA Aircraft -
Power Package Rotax 914 Turbo 115 hp(upgrade from 912 ULS for CTLS) 16,0
Thermostat Package 3,8
Comfort Package Club Analog / Club D60 12,8
Omission of sun visors -0,7
Nightflight Package Club Analog (only together with Comfort Package) 1,9
De- selectable:Trutrak ADI- instrument to display bank angle, pitch and direction (electronic directional gyro); including backup battery providing 30 minutes emergency operation (according supplier specification)Attention: Required to fulfill ASTM Nightflight Standard!
-0,3
Analog one pointer altimeter (small) Magnetic compass with deviation table
Analog Instrumentation - providing redundancy together with Glass Screens: Hobbs Hour Meter
Analog airspeed indicator (small)
70130
Acoustic (coupled to Intercom) and optical warnings Voltmeter
Non- certified Engine and Propeller (certified as part of the aircraft)
Altitude Encoder Dynon (or ACK A30 for PtF / EASA ELA 1 aircraft)
Water thermostat installed to the cooling water circuit
70091CERTIFICATION
Oil thermostat installed to the oil circuit
Aircraft produced in conformance with EASA Restricted Type Certificate
70211
Cowling with Camlock quick fasteners
Heat distribution in cockpit to several air nozzles
Anti Collision Lights and Position lights LED version
Door locks on both cabin doors
70201
Parking brake
UMA Light strip for center panel and throttleboxCabin light installed to main bulkhead
Stainless steel exhaust systemManual three axis trim system
OPTIONS ENGINE
Deflectable sun visors
Two trays at the lower side of the instrument consoleMap pockets at the main bulkhead
Instruments with internal lighting or illuminated with UMA Light Bezels
Engine
Oil thermostat installed to the oil circuitWater thermostat installed to the cooling water circuit
70200ACCESSORIES
Aircraft produced under oversight of approved CAAC production organization
70120
Rotax 914 ULS Turbo special version with airbox and fuel selector instead of basic package engine 912 ULS
70092
Aircraft documentation as required for registration in China
Aircraft produced under oversight of approved EASA Part 21 production organizationAircraft documentation as required for registration at a National Aviation Authority in a EASA member state
Aircraft produced in conformance with Chinese CAAC Type Design ApprovalNon- certified Engine and Propeller (certified as part of the aircraft)
Heat exchanger fitted to muffler to generate hot air for cabin heating
Pocket at each door
Sport seat with headrestReinforced landing gear "Cross Country"
Wheelpants and landing gear fairings on main wheels, combined wheelpant and leg fairing on nose wheel12V auxiliary connector in cockpitDouble fresh air windows installed to the door windows
Non- certified landing light, integrated to lower cowling70210
Errors and omissions expectedSubject to change without prior notice
Flight Design CTLS and CTLS 600 kg ClassModel Year 2011
Release March 01, 2011Page 6 of 20
Description WeightOrder No.
Nightflight Package Club D60 (only together with Comfort Package) 1,6
Comfort Package Advanced incl. Nightflight Package 13,5
Omission of sun visors -0,7
Complete System for Glider and Banner Towing 5,8
Landing Light(only with Comfort Package; included to Nightflight Package) 0,3
Landing Light in LED technology (only with Comfort Package) 0,5
Tundra Wheels CTLS (only with Comfort Package) 6,5
Photowindow 0,7
3-Blade Variable Pitch Propeller 5,5
Heat exchanger fitted to muffler to generate hot air for cabin heating
70230
Heat distribution in cockpit to several air nozzles
Parking brakeCowling with Camlock quick fasteners
Instruments with internal lighting or illuminated with UMA Light BezelsUMA Light strip for center panel and throttlebox
Illumination brightness continuously variable
Cabin light installed to main bulkheadIllumination of the fuel indicators
Wheelpants and landing gear fairings on main wheels, combined wheelpant and leg fairing on nose wheel
Illumination of the fuel indicators
Non- certified landing light, integrated to lower cowlingAll instruments illuminated, including backup instruments
12V auxiliary power connector in cockpit
Two trays at the lower side of the instrument consoleDouble fresh air windows installed to the door windows
Deflectable sun visors70231
UMA Light strip for center panel and throttlebox
Elastic luggage net on each hat rack side
70240
Illumination brightness continuously variable
Reduced power consumption due to LED technology (15W)
Cabin light installed to cabin ceiling
Anti- Collision- Light & Position Lights to ASTM Nightflight requirement
Anti- Collision- Light & Position Lights according ASTM Nightflight requirement included in Comfort Package
70285
Acces to luggage compartment from outside, with separate door locks
Illumination brightness continuously variable
Door locks on both cabin doors
Manual three axis trim system
Pocket at each door
Stainless steel exhaust system
70212
Illumination of the fuel indicators
Anti- Collision- Light & Position Lights according ASTM Nightflight requirement included in Comfort Package
Non- certified landing light, integrated to lower cowling
Reinforced ventral fin
Removable rearview mirror attached under wing leading edgeLarge oil- and water cooler
Reinforced fuselage tail boom
70270
70251
Aerotow coupling with actuation handles in cockpit and at ventral fin
70250
High efficient, composite propeller bladesComposite spinner fitted for three bladed variable pitch propeller
Additional photowindow in left door, 165 x 260 mm, sliding upwards
In-flight adjustable 3-blade propeller, mechanical-hydraulicMechanically adjustable propeller hub
70265Main wheels 6.00 - 6"Wheel pants fitted to match changed wheel size
Fresh air window from Comfort Package remains unaffected
Errors and omissions expectedSubject to change without prior notice
Flight Design CTLS and CTLS 600 kg ClassModel Year 2011
Release March 01, 2011Page 7 of 20
Description WeightOrder No.3-Blade Constant Speed Variable Pitch Propeller 5,6
Interior leather "Pegaso" brown including improved upholstery(only together with Comfort Package and Sport Seat) 2,5
Interior leather "Noir" black including improved upholstery(only together with Comfort Package and Sport Seat) 2,5
70295-1 Two tone cabin interior paint, grey / anthracite matching with leather color structured surface, high abrasion resistance 0
70295-2 Two tone cabin interior paint, brown / beige structured surface, high abrasion resistance 0
Seat Belts Amsafe with Airbags for Both Seats 3,3
Large Battery (required for advanced avionic) 3,2
Advanced Battery Lithium-Iron-Phosphate Technology (10Ah) -0,8
Upgrade Garmin 328 Mode S Transponder 0,5
Upgrade Garmin 330 Mode S Transponder 0,5
Upgrade Garmin GPS 696 XM 0,8
Avionic Package Garmin G3X 4,3
70445
70295
70287
Anthracite carpets on the floor
Specifically cast-to-form upholstery
Modification of variable pitch hub for electric actuation
Inflatable cushions to allow fine adjustment of upholstery
Implementation of fast speed electric actuator
70310
Control stick covers in leather "Noir" black
Anthracite carpets on the floorMap pockets in synthetic leather black
Seat covers for sport seat with headrest in leather "Noir" blackSpecifically cast-to-form upholsteryInflatable cushions to allow fine adjustment of upholstery
Battery 12V / 14Ah Lead-Acid instead of Battery 12V / 7Ah Lead-Acid
70450
Enhanced (wider) instrument console with four individual panels
Reduced transmission power, and therefore reduced power consumption compared to GTX 330
GPS Garmin 696 with XM function - Americas database
Transponder Garmin GTX 330 Mode S installed with antenna instead GTX 327
70460
70407
Designed to replace 14 to 20 Ah Lead-Acid battery, fast recharge, low self discharge rate
Required when one of the advanced avionic packages is selected
70300
Constant speed controller, 2 ¼”, installed to the instrument panel
Seat covers for sport seat with headrest in leather "Pegaso" brown
Map pockets in synthetic leather blackTwo tone cabin interior paint, brown / beige matching with leather color, structured surface, high abrasion resistance
220V Battery Charger included in package
Crash sensors installed under passenger seat
Lithium-Iron-Phosphate Battery 12V / 10Ah instead of Lead-Acid Battery 12V / 7Ah or 14Ah
Four- Point belt with airbag integrated to cabin inside shoulder belt
70311
Inertia reel for shoulder belts, installed to main bulkhead
70290
BASIC AVIONIC PACKAGES(no combination with Advanced Avionic Packages possible)
ADVANCED AVIONIC PACKAGES (no combination with Basic Avionic Packages possible)
Control stick covers in leather "Pegaso" brown
Alternative suite instead of Avionic installed to basic aircraft; including:Garmin Double Screens GDU 370 and GDU 375 (7'' landscape format) provide full PFD and full MFD functionality
Transponder Garmin GTX 328 Mode S installed with antenna instead GTX 327No support of TIS functionality
Errors and omissions expectedSubject to change without prior notice
Flight Design CTLS and CTLS 600 kg ClassModel Year 2011
Release March 01, 2011Page 8 of 20
Description WeightOrder No.
Downgrade no XM functionality for Garmin G3X package (only with Garmin Package G3X) -0,1
Upgrade Garmin GNS 430 Nav/Com/GPS (only with Garmin Package G3X) 1,8
Upgrade Garmin GNS 530 Nav/Com/GPS (only with Garmin Package G3X) 2,7
Avionic Package Dynon SkyView (alternative to all of the above Advanced Avionic selections) 2,9
2 x LEMO Redell Connectors installed for ANR Headset, in addition to standard plugs
Synthetic vision, moving map functionality
70412
Functionality identical to GDU 375, only no XM receiver and functionality included
Dynon SV-XPNDR-261 Class 1 Transponder
KANNAD AF 406 Compact ELT 406 MHz
SkyView suite linked up with COM and Transponder
Intercom PM 3000 A with aux music input and connection to GPS Audio
Airspeed indicator 2 ¼”
KANNAD AF 406 Compact ELT 406 MHzAnalog Instrumentation - providing redundancy together with Glass Screens:
Magnetic compass with deviation table
Altimeter 2 ¼”Trutrak ADI 2 ¼” with built-in backup battery
Hobbs hour meter
Integrated GPS functionality with XM capability allows full navigation support
2 x LEMO Redell Connectors installed for ANR Headset, in addition to standard plugs
Required to support GPS steering on FD Pilot VSGV
Garmin GMA 240 audio panel replacing Intercom PM 3000 A
Required to support GPS steering on FD Pilot VSGV
Second COM antenna installed to the underside of the fuselageAntenna splitter and diplexer to support both VOR / GS receivers from one VOR antenna with all signals
Altitude Encoder Dynon
TIS functionality through link-up with GTX 330
Jeppesen NAV/VFR and Obstacle Database available (subscription) - not included!
Alternative suite instead of Avionic installed to basic aircraft; including:Dynon Double Screens SkyView SV-D1000 (10'' portrait format) with integrated backup batteriesDynon ADAHRS (Air Data Attitude Heading Reference System) in both wings
Magnetic compass with deviation table
Two Headset Telex Echelon 25 XT with plug connectors next to the seats
Independent sensor units supporting all functions, installed at convenient locations
70470
Enhanced (wider) instrument console with four individual panels
Dynon system with two pitot / AoA tubes, one per wing attached to the respective ADAHRS
Garmin SL-30 NAV/COM Transceiver installed with GS capable NAV Antenna CI 158 at the upper vertical tail
Intercom PM 3000 A with aux music input and connection to GPS Audio
Full EMS functionality
Garmin GTX 330 Transponder Mode S
70465
Option removes XM receiver and therefore XM functionality from the units. XM is only available in North America, due to satellite coverage.
G3X suite linked up with Transponder and Transceiver
Jeppesen aviation database with terrain and obstacle database (updates / subscription not included!)
Garmin SL-40 COM installed with antenna
Implementation of Garmin GDU 370 Display Unit instead of GDU 375
Garmin GMA 240 audio panel replacing Intercom PM 3000 A
Hobbs hour meter
Independent sensor and GPS units supporting all functions, installed at convenient locations
70413
Antenna splitter and diplexer to support both VOR / GS receivers from one VOR antenna with all signalsSecond COM antenna installed to the underside of the fuselage
Two Headset Telex Echelon 25 XT with plug connectors next to the seats
Errors and omissions expectedSubject to change without prior notice
Flight Design CTLS and CTLS 600 kg ClassModel Year 2011
Release March 01, 2011Page 9 of 20
Description WeightOrder No.Avionic Package Dynon SkyView (PtF / EASA ELA 1 aircraft)(alternative to all of the above Advanced Avionic selections) 3,2
Upgrade Dynon SV-Map-270 Navigation Mapping Software 0
Upgrade Garmin GPS AERA 510 XM (only with Dynon Package SkyView) 0,8
Upgrade Garmin GPS 696 XM (only with Dynon Package SkyView) 1,1
Upgrade Garmin SL-30 Nav/Com (only with Dynon SkyView Package, replacing SL-40 Com) 1,0
Upgrade Garmin GNS 430 Nav/Com/GPS (only with Dynon SkyView Package)(for PtF / EASA ELA 1 aircraft not possible to select GPS 695 with this option) 1,5
Upgrade Garmin SL-30 Nav/Com (only for Club Analog and Club D60) 1,0
Garmin GPS AERA 500 / 695 without XM Function - Americas Database -0,3
Garmin GPS AERA 500 / 695 without XM Function - Atlantic Database -0,3
Garmin GPS AERA 500 / 695 without XM Function - Pacific Database -0,3
Omission of Headsets -1,2
2 x LEMO Redell Connectors installed for ANR Headset, in addition to standard plugs
Dynon ADAHRS (Air Data Attitude Heading Reference System) in both wings
Two Headset Telex Echelon 25 XT with plug connectors next to the seats
70472
GPS Garmin AERA 510 with XM function - Americas database70473
AirGizmos AERA Panel Mount included
SL-40 COM or SL-30 NAV/COM Transceiver (depending order selection)
70474
Interfaces to:
Altitude Encoder ACK A30
70471
Enhanced (wider) instrument console with four individual panels
Hobbs hour meter
70406
GPS Garmin AERA 500 / 695 without XM Function for countries covered by Atlantic Database
GPS Garmin AERA 500 / 695 without XM Function for countries covered by Pacific Database
GENERAL AVIONIC OPTIONS
70405
Garmin SL-30 NAV/COM installed instead of SL-40 COM, with GS capable NAV Antenna CI 158 at the upper vertical tail
70475
GTX 330 or SV-XPNDR-261 Transponder
GPS Garmin 696 with XM function - Americas database
Garmin SL-30 NAV/COM installed instead of SL-40 COM, with GS capable NAV Antenna CI 158 at the upper vertical tail
KANNAD AF 406 Compact ELT 406 MHz
TIS functionality (availability depending from ground station coverage)
70476
Intercom PM 3000 A with aux music input and connection to GPS Audio
70414
Alternative suite instead of Avionic installed to basic aircraft; including:
Synthetic vision, moving map functionality
Magnetic compass with deviation table
Dynon Double Screens SkyView SV-D1000 (10'' portrait format) with integrated backup batteries
SkyView suite linked up with COM and Transponder
Dynon system with two pitot / AoA tubes, one per wing attached to the respective ADAHRSIndependent sensor and GPS units supporting all functions, installed at convenient locationsGarmin SL-40 COM installed with antennaGarmin GTX 330 Transponder Mode S
70404GPS Garmin AERA 500 / 695 without XM Function for countries covered by Americas Database
Antenna diplexer to support both VOR / GS receivers from one VOR antenna with all signals
When linked to Dynon EFIS D60, CDI NAV display; no separate CDI
CDI / NAV display on SkyView through Dynon ARINC 429; no separate CDI
Garmin GNS 430 Nav/Com/GPS installed instead of SL-40 COM, with GS capable NAV Antenna CI 158 at the upper vertical tail
Jeppesen NAV/VFR and Obstacle Database available (subscription) - not included!
70490
Errors and omissions expectedSubject to change without prior notice
Flight Design CTLS and CTLS 600 kg ClassModel Year 2011
Release March 01, 2011Page 10 of 20
Description WeightOrder No.
FD Pilot 2 Axis (not for Dynon SkyView) 3,4
FD Pilot 2 Axis + vertical speed (not for Dynon SkyView) 3,4
FD Pilot VSGV (only together with Garmin Package G3X) 3,4
Dynon Autopilot (with Dynon Package SkyView - Servos only) 2,5
Display in km/h, °C, Altitude ft - mbar and Vario ft/min 0Display in kts, °C, Altitude ft - mbar and Vario ft/min 0Display in kts, °F, Altitude ft - in Hg and Vario ft/min 0
Four color decals "Wave 1" 0Four color decals "Wave 2" 0Four color decals "Wave 3" 0Four color decals "Wave 4" 0Four color decals "Wave 5" 0Four color decals "Storm 1" 0Four color decals "Storm 2" 0Four color decals "Storm 3" 0Four color decals "Storm 4" 0Four color decals "Storm 5" 0Three color decals "Classic 1" 0Three color decals "Classic 2" 0Call Signs 0,3
LSA Conformity Statement -
EASA approved Flight Conditions for PtF -
Export Paperwork -
Aileron control according GPS route, GPS track or wing leveling
Aileron control includes: Heading hold, Track hold, Bug select, Bug preselect, HSI nav, GPS steering
Automatic altitude hold
Autopilot commanded directly from Dynon SkyView Screens and Controls
Automatic altitude holdAutomatic vertical speed control
Automatic altitude hold
70940
70610
DISPLAY UNITS
Aileron control according GPS route, GPS track or wing leveling
Future software update planned with Vertical speed hold, Vertical speed select, Vertical Nav
70950
7094370944
70941
70600
Autopilot based on Trutrak Digiflight II FP, customised for Flight Design70530
Conformity statement
70942
70620
ADDITIONAL PAPERWORK
70990
70951
Call signs as decals in black prepared and attached(1x per fuselage side, 1x lower wing skin, depending on national regulations)
7095470955
70800
70510AUTOPILOT (non- certified)
70956
Elevator Control includes: Altitude hold, Altitude select / change, Altitude preselect, Airspeed limits
Autopilot based on Trutrak Digiflight II FP, customised for Flight Design
Export Certificate
70540
GPS Steering, including vertical profile (requires connection to GNS 430 or 530)Automatic vertical speed control
DESIGN SELECTION AND MARKINGS
7095270953
70520
Later upgrade possible
Autopilot based on Trutrak Digiflight II FP, customised for Flight DesignAileron control according GPS route, GPS track or wing leveling
Engine ASTM compliantLSA Conformity statement (FAA Form 8130-15 or equivalent, as required by country)EASA Permit to Fly EASA approved Flight Conditions (required to register the Aircraft at NAA with PtF)
70090-1Aircraft produced in conformance with LSA design standard and applicable LSA rule Engine ASTM compliantLSA Conformity statement (FAA Form 8130-15 or equivalent, as required by country)
70090-2Aircraft produced in conformance with LSA design standard and applicable LSA rule
Errors and omissions expectedSubject to change without prior notice
Flight Design CTLS and CTLS 600 kg ClassModel Year 2011
Release March 01, 2011Page 11 of 20
Your Notes
Errors and omissions expectedSubject to change without prior notice
Flight Design CTLS and CTLS 600 kg ClassModel Year 2011
Release March 01, 2011Page 12 of 20
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€+
+in
clud
ed
AC
CES
SOR
IES
Com
fort
Pac
kage
Clu
b A
nalo
g / C
lub
D60
7020
012
,86
699,
74 €
++
Not
ava
ilabl
e
Om
issi
on o
f sun
vis
ors
7020
1-0
,7-1
50,0
0 €
++
Not
ava
ilabl
e
Nig
htfli
ght P
acka
ge C
lub
Ana
log
(onl
y to
geth
er w
ith C
omfo
rt P
acka
ge)
7021
01,
92
521,
05 €
+N
ot a
vaila
ble
Not
ava
ilabl
e
De-
sel
ecta
ble:
Trut
rak
AD
I- in
stru
men
t to
disp
lay
bank
ang
le, p
itch
and
dire
ctio
n (e
lect
roni
c di
rect
iona
l gyr
o); i
nclu
ding
bac
kup
batte
ry p
rovi
ding
30
min
utes
em
erge
ncy
oper
atio
n (a
ccor
ding
sup
plie
r spe
cific
atio
n)A
ttent
ion:
Req
uire
d to
fulfi
ll A
STM
Nig
htfli
ght S
tand
ard!
7021
1-0
,3-5
50,0
0 €
+N
ot a
vaila
ble
Not
ava
ilabl
e
Nig
htfli
ght P
acka
ge C
lub
D60
(on
ly to
geth
er w
ith C
omfo
rt P
acka
ge)
7021
21,
61
971,
05 €
Not
ava
ilabl
e+
Not
ava
ilabl
e
Ava
ilabi
lity
per A
ircra
ft Pl
atfo
rmO
rder
Se
lect
ion
Pric
e €
excl
. VA
T W
eigh
t [k
g]O
rder
Num
ber
Errors and omissions expectedSubject to change without prior notice
Flight Design CTLS and CTLS 600 kg ClassModel Year 2011
Release March 01, 2011Page 13 of 20
CTL
S / C
TLSH
L
Clu
b A
nalo
gC
TLS/
CTL
SHL
Clu
b D
60C
TLS/
CTL
SHL
Adv
ance
d
Ava
ilabi
lity
per A
ircra
ft Pl
atfo
rmO
rder
Se
lect
ion
Pric
e €
excl
. VA
T W
eigh
t [k
g]O
rder
Num
ber
Com
fort
Pac
kage
Adv
ance
d in
cl. N
ight
fligh
t Pac
kage
7023
013
,56
694,
00 €
Not
ava
ilabl
eN
ot a
vaila
ble
+
Om
issi
on o
f sun
vis
ors
7023
1-0
,7-1
50,0
0 €
Not
ava
ilabl
eN
ot a
vaila
ble
+
Com
plet
e Sy
stem
for G
lider
and
Ban
ner T
owin
g70
240
5,8
1 97
1,53
€+
++
Land
ing
Ligh
t (o
nly
with
Com
fort
Pac
kage
; inc
lude
d to
Nig
htfli
ght P
acka
ge)
7025
00,
320
0,20
€+
+in
clud
edC
omf P
kg.
Land
ing
Ligh
t in
LED
tech
nolo
gy (
only
with
Com
fort
Pac
kage
)70
251
0,5
514,
50 €
++
+
Tund
ra W
heel
s C
TLS
(onl
y w
ith C
omfo
rt P
acka
ge)
7026
56,
599
0,00
€+
++
Phot
owin
dow
7027
00,
754
3,90
€+
++
3-B
lade
Var
iabl
e Pi
tch
Prop
elle
r70
285
5,5
3 67
0,00
€+
++
3-B
lade
Con
stan
t Spe
ed V
aria
ble
Pitc
h Pr
opel
ler
7028
75,
64
720,
00 €
++
+In
terio
r lea
ther
"Pe
gaso
" br
own
incl
udin
g im
prov
ed u
phol
ster
y(o
nly
toge
ther
with
Com
fort
Pac
kage
and
Spo
rt S
eat)
7029
02,
586
2,98
€+
++
Inte
rior l
eath
er "
Noi
r" b
lack
incl
udin
g im
prov
ed u
phol
ster
y(o
nly
toge
ther
with
Com
fort
Pac
kage
and
Spo
rt S
eat)
7029
52,
586
2,98
€+
++
Two
tone
cab
in in
terio
r pai
nt, g
rey
/ ant
hrac
ite m
atch
ing
with
leat
her c
olor
st
ruct
ured
sur
face
, hig
h ab
rasi
on re
sist
ance
7029
5-1
0,0
0,00
€+
++
Two
tone
cab
in in
terio
r pai
nt, b
row
n / b
eige
st
ruct
ured
sur
face
, hig
h ab
rasi
on re
sist
ance
7029
5-2
0,0
0,00
€+
++
Seat
Bel
ts A
msa
fe w
ith A
irbag
s fo
r Bot
h Se
ats
7030
03,
34
250,
00 €
++
+
Larg
e B
atte
ry (
requ
ired
for a
dvan
ced
avio
nic)
7031
03,
280
,00
€+
++
Adv
ance
d B
atte
ry L
ithiu
m-Ir
on-P
hosp
hate
Tec
hnol
ogy
(10A
h)70
311
-0,8
628,
00 €
++
+
BA
SIC
AVI
ON
IC P
AC
KA
GES
(no
com
bina
tion
with
Adv
ance
d A
vion
ic P
acka
ges
poss
ible
) U
pgra
de G
arm
in 3
28 M
ode
S Tr
ansp
onde
r70
445
0,5
950,
00 €
++
+
Upg
rade
Gar
min
330
Mod
e S
Tran
spon
der
7045
00,
51
980,
00 €
++
+
Upg
rade
Gar
min
GPS
696
XM
7040
70,
81
670,
00 €
++
+
AD
VAN
CED
AVI
ON
IC P
AC
KA
GES
(n
o co
mbi
natio
n w
ith B
asic
Avi
onic
Pac
kage
s po
ssib
le)
A
vion
ic P
acka
ge G
arm
in G
3X
7046
04,
3on
requ
est
Not
ava
ilabl
eN
ot a
vaila
ble
+D
owng
rade
no
XM fu
nctio
nalit
y fo
r Gar
min
G3X
pac
kage
(onl
y w
ith G
arm
in P
acka
ge G
3X)
7046
5-0
,1-4
50,0
0 €
Not
ava
ilabl
eN
ot a
vaila
ble
+U
pgra
de G
arm
in G
NS
430
Nav
/Com
/GPS
(o
nly
with
Gar
min
Pac
kage
G3X
; on
top
of S
L-30
)70
412
1,8
8 70
0,00
€N
ot a
vaila
ble
Not
ava
ilabl
e+
Errors and omissions expectedSubject to change without prior notice
Flight Design CTLS and CTLS 600 kg ClassModel Year 2011
Release March 01, 2011Page 14 of 20
CTL
S / C
TLSH
L
Clu
b A
nalo
gC
TLS/
CTL
SHL
Clu
b D
60C
TLS/
CTL
SHL
Adv
ance
d
Ava
ilabi
lity
per A
ircra
ft Pl
atfo
rmO
rder
Se
lect
ion
Pric
e €
excl
. VA
T W
eigh
t [k
g]O
rder
Num
ber
Upg
rade
Gar
min
GN
S 53
0 N
av/C
om/G
PS
(onl
y w
ith G
arm
in P
acka
ge G
3X; o
n to
p of
SL-
30)
7041
32,
712
400
,00
€N
ot a
vaila
ble
Not
ava
ilabl
e+
Avi
onic
Pac
kage
Dyn
on S
kyVi
ew
7047
02,
94
680,
00 €
Not
ava
ilabl
eN
ot a
vaila
ble
+
Avi
onic
Pac
kage
Dyn
on S
kyVi
ew (P
tF /
EASA
ELA
1 a
ircra
ft)70
471
3,2
5 98
0,00
€N
ot a
vaila
ble
Not
ava
ilabl
e+
Upg
rade
Dyn
on S
V-M
ap-2
70 N
avig
atio
n M
appi
ng S
oftw
are
7047
20,
043
8,00
€N
ot a
vaila
ble
Not
ava
ilabl
e+
Upg
rade
GPS
Gar
min
AER
A 5
10 X
M (
only
with
Dyn
on P
acka
ge S
kyV
iew
)70
473
0,8
1 59
8,00
€N
ot a
vaila
ble
Not
ava
ilabl
e+
Upg
rade
GPS
Gar
min
696
XM
(on
ly w
ith D
ynon
Pac
kage
Sky
Vie
w)
7047
41,
12
570,
00 €
Not
ava
ilabl
eN
ot a
vaila
ble
+U
pgra
de G
arm
in S
L-30
Nav
/Com
(o
nly
with
Dyn
on S
kyV
iew
Pac
kage
, rep
laci
ng S
L-40
Com
)70
476
1,0
2 57
5,00
€N
ot a
vaila
ble
Not
ava
ilabl
e+
Upg
rade
Gar
min
GN
S 43
0 N
av/C
om/G
PS
(onl
y w
ith D
ynon
Sky
Vie
w P
acka
ge, r
epla
cing
SL-
40 C
om)
(for P
tF /
EA
SA
ELA
1 a
ircra
ft no
t pos
sibl
e to
sel
ect G
PS
695
with
this
opt
ion)
7041
41,
57
380,
00 €
Not
ava
ilabl
eN
ot a
vaila
ble
+
GEN
ERA
L A
VIO
NIC
OPT
ION
SU
pgra
de G
arm
in S
L-30
Nav
/Com
7047
51,
02
075,
00 €
++
Not
ava
ilabl
e
Gar
min
GPS
AER
A 5
00 /
695
with
out X
M F
unct
ion
- Am
eric
as D
atab
ase
7040
4-0
,3-3
44,5
4 €
++
+
Gar
min
GPS
AER
A 5
00 /
695
with
out X
M F
unct
ion
- Atla
ntic
Dat
abas
e70
405
-0,3
-344
,54
€+
++
Gar
min
GPS
AER
A 5
00 /
695
with
out X
M F
unct
ion
- Pac
ific
Dat
abas
e70
406
-0,3
-344
,54
€+
++
Om
issi
on o
f Hea
dset
s70
490
-1,2
-280
,00
€+
++
AU
TOPI
LOT
(non
- cer
tifie
d)FD
Pilo
t 2 A
xis
(not
for D
ynon
Sky
Vie
w)
7051
03,
43
580,
00 €
++
+
FD P
ilot 2
Axi
s +
vert
ical
spe
ed (
not f
or D
ynon
Sky
Vie
w)
7052
03,
44
040,
00 €
++
+
FD P
ilot V
SGV
(onl
y to
geth
er w
ith G
arm
in P
acka
ge G
3X)
7053
03,
44
850,
00 €
Not
ava
ilabl
eN
ot a
vaila
ble
+
Dyn
on A
utop
ilot
(onl
y w
ith D
ynon
Pac
kage
Sky
Vie
w -
Ser
vos
only
)70
540
2,5
1 78
0,00
€N
ot a
vaila
ble
Not
ava
ilabl
e+
DIS
PLA
Y U
NIT
SD
ispl
ay in
km
/h, °
C, A
ltitu
de ft
- m
bar a
nd V
ario
ft/m
in
7060
00,
00,
00 €
++
+
Dis
play
in k
ts, °
C, A
ltitu
de ft
- m
bar a
nd V
ario
ft/m
in
7061
00,
00,
00 €
++
+
Dis
play
in k
ts, °
F, A
ltitu
de ft
- in
Hg
and
Vario
ft/m
in
7062
00,
00,
00 €
++
+
Errors and omissions expectedSubject to change without prior notice
Flight Design CTLS and CTLS 600 kg ClassModel Year 2011
Release March 01, 2011Page 15 of 20
CTL
S / C
TLSH
L
Clu
b A
nalo
gC
TLS/
CTL
SHL
Clu
b D
60C
TLS/
CTL
SHL
Adv
ance
d
Ava
ilabi
lity
per A
ircra
ft Pl
atfo
rmO
rder
Se
lect
ion
Pric
e €
excl
. VA
T W
eigh
t [k
g]O
rder
Num
ber
DES
IGN
SEL
ECTI
ON
AN
D M
AR
KIN
GS
Four
col
or d
ecal
s "W
ave
1"70
940
0,0
0,00
€+
++
Four
col
or d
ecal
s "W
ave
2"70
941
0,0
0,00
€+
++
Four
col
or d
ecal
s "W
ave
3"70
942
0,0
0,00
€+
++
Four
col
or d
ecal
s "W
ave
4"70
943
0,0
0,00
€+
++
Four
col
or d
ecal
s "W
ave
5"70
944
0,0
0,00
€+
++
Four
col
or d
ecal
s "S
torm
1"
7095
00,
00,
00 €
++
+
Four
col
or d
ecal
s "S
torm
2"
7095
10,
00,
00 €
++
+
Four
col
or d
ecal
s "S
torm
3"
7095
20,
00,
00 €
++
+
Four
col
or d
ecal
s "S
torm
4"
7095
30,
00,
00 €
++
+
Four
col
or d
ecal
s "S
torm
5"
7095
40,
00,
00 €
++
+
Thre
e co
lor d
ecal
s "C
lass
ic 1
"70
955
0,0
0,00
€+
++
Thre
e co
lor d
ecal
s "C
lass
ic 2
"70
956
0,0
0,00
€+
++
Cal
l Sig
ns70
990
0,3
0,00
€+
++
AD
DIT
ION
AL
PAPE
RW
OR
KLS
A C
onfo
rmity
Sta
tem
ent
7009
0-1
0,0
0,00
€in
clud
edin
clud
edin
clud
ed
EASA
app
rove
d Fl
ight
Con
ditio
ns fo
r PtF
(a
ctua
l EA
SA
Fee
s, s
ubje
ct to
cha
nge)
7009
0-2
0,0
723,
94 €
++
+
Expo
rt P
aper
wor
k70
800
0,0
on
effo
rt
++
+
Sum
acc
ordi
ng
to s
elec
tion
*0,
00,
00 €
5 00
0,00
€20
000
,00
€25
000
,00
€-2
5 00
0,00
€0,
00 €
Paym
ent S
ched
ule:
* wei
ghts
can
diff
er b
y 3%
of t
he to
tal s
peci
fied
wei
ght
**
Tot
al p
aym
ent v
alue
enh
ance
s by
lega
lly re
quire
d sa
les
taxe
s as
app
licab
leTo
tal p
aym
ent (
Net
val
ue) *
*
Firs
t dow
n pa
ymen
t on
orde
r, w
hen
expe
cted
dat
e of
del
iver
y is
mor
e th
an 5
mon
ths
away
Seco
nd d
own
paym
ent a
t lea
st 5
mon
ths
befo
re e
xpec
ted
deliv
ery
date
Tota
l dow
n pa
ymen
tFi
nal p
aym
ent r
ight
bef
ore
deliv
ery
ex U
krai
ne (N
et v
alue
) **
Errors and omissions expectedSubject to change without prior notice
Flight Design CTLS and CTLS 600 kg ClassModel Year 2011
Release March 01, 2011Page 16 of 20
Your Notes
Errors and omissions expectedSubject to change without prior notice
Flight Design CTLS and CTLS 600 kg ClassModel Year 2011
Release March 01, 2011Page 17 of 20
Your Notes
Errors and omissions expectedSubject to change without prior notice
Flight Design CTLS and CTLS 600 kg ClassModel Year 2011
Release March 01, 2011Page 18 of 20
Flight Design GmbH Entwicklung und Vertrieb von Flugsportgeräten Sielminger Str. 51 - D-70771 L.-Echterdingen Handelsregister Stuttgart HRB 222689 VAT ID No.: DE 147857992 Geschäftsführer: Matthias Betsch(CEO)-Oliver Reinhardt-Christian Wenger
Administration & Sales – Airfield NabernSeestr. 30 D-73230 Kirchheim u. Teck / Nabern Tel.: +49 (0) 7021 / 80 460 – 0 Fax: +49 (0) 7021 / 80 460 – 69 info@flightdesign.com - www.flightdesign.com
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