CTLS Lite Floatplane

6

Dynon D100 Electronic Flight Information System (EFIS)

5

Optional FD Pilot 2-axis Autopilot

3

Standby Altimeter

1

Garmin GTX 327 Mode C Transponder

12

406 MHz ELT

11

PS Engineering PM 3000 Intercom

10

Garmin SL40 Com Radio

9

Hobbs Hour Meter

8

UMA Engine Information Display

7

Garmin AERA 510 GPS with XM Weather

7

Garmin AERA 510 GPS with XM Weather

2

Optional Garmin GTX 330 Mode S Transponder

4

Standby Airspeed Indicator

Key Features

• Rotax 912 ULS Engine, 100 hp
• Fast, Comfortable, Fun
• Well-equipped in standard configuration with Dynon D100 EFIS,
Garmin Com & Transponder, Garmin AERA 510 GPS
w/XM Weather, 406 MHz ELT
• Airframe Parachute Recovery System (APRS) installed
• Strutless, cantilevered wing ideal for float operation
• CLAMAR 1400 Amphibious Floats
• 1430 lbs (650 kg) Max Takeoff Weight – Tested to ASTM
Requirements

General Features

Engine

Rotax 912 ULS 100 hp engine, 2,000 hr TBO
Operates on auto fuel or 100LL avgas
Three-blade ground adjustable composite propeller
34 Gal fuel capacity – contained in two wing tanks
Easy-to-manage On/Off fuel selector

Interior

Large window area provides excellent visibility
Attractive and durable two-tone interior
Spacious cabin comfortable for large and tall occupants
Large gullwing doors for easy entry/exit
Adjustable seats with 4-point restraint harnesses
“Safety Cell” Kevlar cockpit design

Systems

Dual control sticks, conventional 3-axis flight control
Three axis trim system
Electric, pre-select flaps
Airframe Parachute Recovery System

Floats

CLAMAR 1400 amphibious floats – 1430 lbs displacement
each float
Composite construction – strong, lightweight, leak proof,
corrosion free
All electric landing gear actuation with spring shock absorption
Four baggage compartments integrated into floats

Performance at MTOW 1430 lbs/650 kg
Vh: maximum horizontal speed 97 kt 180 km/h
Vne: maximum permissible airspeed (red line) 162 kt 300* km/h
Take-off run (flap +15 degree) 820 ft 250 m
Take-off distance over 50 ft obstacle 1476 ft 450 m
Max. range (30 min reserve) 515 NM 950 km
* The never-exceed speed (VNE) limit is defined by the capabilities of the rescue system
Weights, Dimensions and Capacities
Typical Empty Weight, well-equipped including
Airframe Parachute Recovery System (APRS)
954 lbs 434 kg
Max. take off weight 1430 lbs 650 kg
Fuel capacity 34 US Gal 130 l
Maximum weight per seat 265 lb 120 kg
Baggage (55 lbs max each side) 110 lbs 50 kg

Flight Design USA
P.O. Box 325
South Woodstock, CT
06267, USA
[email protected]
www.flightdesignusa.com