CT Supralight: Engines: CTSL - 912 CTSL - 912S CTSL - 912is CTSL - 914T Avionics: Basic Advanced
CT Supralight: Engines: CTSL - 912 CTSL - 912S CTSL - 912is CTSL - 914T Avionics: Basic Advanced
CT Supralight: Engines: CTSL - 912 CTSL - 912S CTSL - 912is CTSL - 914T Avionics: Basic Advanced
Avionics:
Basic
Advanced
Engines:
CTSL 912
CTSL 912S
CTSL 912iS
CTSL 914T
General information
CT Supralight cockpit Dynon SkyView Touch 10
5
6
7
8a
1
2
3
4
5
6
7
8
8a
9
Key facts
The real Ultralight aircraft
Equipped empty weight 279,5kg onwards
80hp Rotax 912, 2000 hrs. TBO
100hp Rotax 912S, 2000 hrs. TBO
100hp Rotax 912iS with electric fuel injection and 2000 hrs. TBO
115hp Rotax 914T with turbo charger, turbocharge control unit and 2000 hrs. TBO
Mission optimized avionic and equipment packages
Capable for glider and banner towing
472,5kg class, with ultralight certification as by national requirements
Design Weight 600 kg MTOW, certified weight 472,5 kg
Airframe emergency parachute already installed
Single beam composite landing gear with improved damping characteristics
Aircraft Specification
Systems
Dual controls, conventional, three axis
Three axis trim available
Electronic flap control with preselection switch
Airframe emergency parachute included
(suitable for MTOW 472,5 kg)
Exterior
High quality exterior finish
Single beam composite landing gear
Hydraulic disc brakes and qualified tires
Steerable nose wheel
Large baggage capacity
Interior
Superior overview through large window areas
Attractive interior color selection
Wide and comfortable cabin
Large gullwing doors
Adjustable seats with 4point harness
Huge variety of cockpit options
Engine
80hp Rotax 912 with 2000 hrs. TBO
100hp Rotax 912S with 2000 hrs. TBO
100hp Rotax 912iS with 2000 hrs. TBO
115hp Rotax 914T with 2000 hrs. TBO
Two blade ground adjustable composite propeller
Optionally three blade up to constant speed control
Weight optimized and rugged fuel and air intake system
2 wing tanks per 65 l
Light weight and effective tank venting
Performance Data
Performance at MTOW 472,5 kg
VH: maximum horizontal speed
VNE: maximum permissible airspeed (red line)
Takeoff run (flap +15 degree)
Takeoff distance over 15 m obstacle
Max. range (30 min reserve)
Rotax 912
240 km/h
300* km/h
140 m
250 m
2000 km
* The neverexceed speed (VNE) limit is defined by the capabilities of the rescue system
279,5
472,5
130
120
25
kg
kg
l
kg
kg
The Information provided in this leaflet is of preliminary nature and represents the development status of the
project at the date of issue. This information may be changed by Flight Design at any time without notice.
Edition: March 2015