product description ctls and ctls hl 600 kg class … version - ctls and ctls... · basic aircraft...

Product Description CTLS and CTLS HL

600 kg Class

Model Year 2011

Release March 01, 2011

Description Weight

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, 2011 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)




Description WeightOrder No.329

351,9

333,1

356

Oil temperature

CTLS HL: 70045


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


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:





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





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


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


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




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





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


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


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



Independent sensor units supporting all functions, installed at convenient locations

70470


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


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





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


Dynon ADAHRS (Air Data Attitude Heading Reference System) in both wings


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


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


70414

Alternative suite instead of Avionic installed to basic aircraft; including:

Synthetic vision, moving map functionality


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





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




Your Notes




Pric

e Li

st C

TLS

and

CTL

S H

L 600

kg

Cla

ss, M

odel

Yea

r 201

1Pr

ices

and

tech

nica

l spe

cific

atio

ns a

re s

ubje

ct to

cha

nge

with

out p

revi

ous

notic

ePr

ices

for e

quip

men

t are

incl

. ins

talla

tion

on n

ew a

ircra

ftD

eliv

ery

ex F

light

Des

ign

Logi

stik

Bre

tnig

- Hau

swal

de CTL

S / C

TLSH

L

Clu

b A

nalo

gC

TLS/

CTL

SHL

Clu

b D

60C

TLS/

CTL

SHL

Adv

ance

d

AIR

PLA

NE

BA

SIC

PLA

TFO

RM

CTL

S C

lub

Ana

log

7003

232

6,5

84 0

16,9

2 €

CTL

SN

ot a

vaila

ble

Not

ava

ilabl

e

CTL

S C

lub

D60

7003

332

9,0

85 2

61,5

8 €

Not

ava

ilabl

eC

TLS

Not

ava

ilabl

e

CTL

S A

dvan

ced

7003

533

3,1

87 5

86,1

8 €

Not

ava

ilabl

eN

ot a

vaila

ble

CTL

S

CTL

SH

L C

lub

Ana

log

(914

Tur

bo E

ngin

e)70

042

349,

496

416

,92

€C

TLS

HL

Not

ava

ilabl

eN

ot a

vaila

ble

CTL

SH

L C

lub

D60

(914

Tur

bo E

ngin

e)70

043

351,

997

661

,58

€N

ot a

vaila

ble

CTL

SH

LN

ot a

vaila

ble

CTL

SH

L A

dvan

ced

(914

Tur

bo E

ngin

e)70

045

356,

099

986

,19

€N

ot a

vaila

ble

Not

ava

ilabl

eC

TLS

HL

CER

TIFI

CA

TIO

NEA

SA R

estr

icte

d Ty

pe C

ertif

icat

e as

LSA

Airc

raft

with

in E

LA 1

7009

10,

07

500,

00 €

++

+

CA

AC

Typ

e D

esig

n A

ppro

val a

s LS

A A

ircra

ft70

092

0,0

2 50

0,00

€+

++

OPT

ION

S EN

GIN

EPo

wer

Pac

kage

Rot

ax 9

14 T

urbo

115

hp

(upg

rade

from

912

ULS

for C

TLS

)70

130

16,0

12 9

00,0

0 €

++

+

Ther

mos

tat P

acka

ge (

only

for e

ngin

e 91

2 U

LS)

7012

03,

845

3,97

€+

+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




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+




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 €

++

+




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

) **




Your Notes




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 [email protected] - www.flightdesign.com