| Basic specifications |
| Type
certificate |
ULA |
| Length |
6,87
m |
| Height
|
2,40
m |
| Wing
span |
10,03
m |
| Wing
area |
12,4
m2 |
| Wing
loading |
36,29
kg/m2 |
| SCO |
1,25
m |
| Manoeuvre
load index |
+4,0;
-2,0 |
| Seats |
side by
side |
| Steering |
Twin
steering |
| Maximal
take-off weight |
450
kg |
| Empty
weight |
275
kg |
| Useful load
|
175
kg |
| Minimal crew
weight |
no limit
|
| Fuel tank
capacity |
70
litres |
| Landing gear |
| Landing
gear |
fixed, three
wheels |
| Wheels |
350 x 135 mm
diameter, 25 bar pressure |
| Front
wheel |
with
spring |
| Front wheel
control |
+/-15 by
pedals, coupled with horizontal steering |
| Main
suspension |
composite
spring |
| Brakes
|
hydraulic
disc brakes, separate wheel braking by pedals (or optionally
two-wheel braking by lever) |
| Rescue system |
| Fifth-generation ballistic rescue system |
BRS 5,
1200/Canister type |
| Maximal
launch speed |
235
km/h |
| Weight |
15
kg |
| Time between
inspections |
6
years |
| Pilotage and navigation devices for basic
version |
| Air speed
indicator |
US-250
UBAK |
| Altimeter |
W 12
S |
| Turn and
bank |
EZS-4 |
| Variometer |
WR-10
UAAK |
| Compass |
BS-1 |
| Radio |
ICOM A
200 |
| Engine control instruments |
|
FLYDAT
-integrated indicator module containing:
- Rotation
meter
- Hour
counter
- Cylinder
head temperature meter
- Exhaust gas
temperature meter
- Oil
temperature meter
- Oil
pressure meter
- Fuel
pressure meter, fuel level indicator
- Carburettor
air temperature meter
- Analogue
tachometery
|
| Engine |
| Bombardier Rotax |
912 S or 912 A |
| Number of cylinders / strokes |
4 / 4 |
| Stroke volume |
1211 cm3 |
| Peak power (5 min.) |
81 HP (59.6 kW) 5800 rpm |
| Maximal continuous power |
79 HP (58.0 kW) 5500 rpm |
| Head / cylinder cooling |
fluid / air |
| Carburettors |
2 constant depression |
| Ignition |
Dual breakerless capacitor discharge |
| Alternator |
none |
| Starter |
Electric |
| Internal gear rate |
1:2.27 |
| Fuel |
Euro-Super 95 DIN 51607 or Avgas100LL |
| TBO |
1200 h |
| Propeller |
| Model |
3Xtrim 170 UL |
| Type |
two-blade,adjustable on ground |
| Propeller diameter |
1,7 m |
| Peak power rotation speed |
2550 rpm |
| Max. continuous power rotation speed |
2420 rpm |
| Performance (with Rotax 912S engine) |
| Speed: |
|
|
maximal
speed Vne |
200 km/h |
|
cruise
(max. continuous power) |
165 km/h |
|
cruise
velocity (75% power) |
152 km/h |
|
stall
speed (aflap=0) Vs |
68 km/h |
|
climbing
speed Vz |
4.5 m/s |
| Take-off roll, 15 m obstacle |
250 m |
| Range |
750 km |
