Specifications
| |
|
|
| Wingspan: |
|
6.63 |
| Wing
area: |
|
5.20
m² |
| Cabin
Width: |
|
1,12 |
| Seats: |
|
2 |
| Fuel
capacity: |
|
60
l |
| Extended
range fuel tanks |
|
2x50
l |
Power
Plant
| |
|
|
| Engine: |
|
100-hp
4 Stroke Rotax 914 Turbo charged max. 115-hp |
| Gear
reduction: |
|
1 :
2.27 |
| Fuel
G.P.H.: |
|
21,3
liters/h
@ 75% |
| Propeller:
|
|
three blade
fix |
|
Performance
|
|
| Cruising
75%, FL 0 (km/h) |
295
|
| Cruising
75%, FL 80 (km/h) |
318
|
| Range
,std Tanks 75% (km) |
1
194
|
| Cruising
65% FL110 (km/h) |
312
|
| Fuel
consumption 65% (liters/h) |
18,5
|
| Range
,std Tanks 65% (km) |
1
375
|
| Takeoff
roll; CS. Prop (m) |
152
|
| Climb
rate FL 0, CS. Prop (ft/min) |
1
750
|
| VSO
(stall speed landing configuration) |
87 km/h |
| Va (Maneuvering
speed) |
225 km/h |
| Vne (
Never exceeding speed) |
320
km/h |
| Design
maneuvering speed |
355
km/h ! |
| Vno
(Normal Operation Speed) |
260 km/h |
| G
loading |
+4 /-2 g |
| Vfe
(Flaps extended speed) |
170 km/h |
|
Weights
and loading
|
|
| Aspect
ratio |
8.45 |
|
Empty weight
(Basic version |
220 kg |
| Equipped empty
weight |
260 kg |
| Max. Takeoff
weight |
490 kg |
| Wing loading |
86 kg/m² |
|
