|
|
|
|
   |
|
Wings |
|
Span |
11,00
m |
Area |
12,10
m2 |
Aspect
ratio |
10,00 |
Chord |
1,10
m |
Wing
section |
FX
66-17All-182/26 |
Dihedral |
3° |
Slot
flaps deflection |
0°,
15°, 35° |
Ailerons |
22°,
+17° |
Horizontal
tail |
|
Span |
2,48
m |
Area |
1,61
m2 |
Chord |
0,65
m |
Wing
section |
FX
71-L-150/35 |
Rudder
deflection |
-20°,
+20° |
Elevator
deflection |
-8°,
+5° |
Vertical
tail |
|
Height |
1,43m |
Area |
1,08
m2 |
Wing
section |
NACAO009 |
Deflection |
-20°,
+20° |
Fuselage |
|
Overall
length |
7,24
m |
Max
width |
1,10
m |
Luggage
compartment |
0,39
m3 |
Fuel
capacity |
90
l |
Gear |
|
Main
gear |
carbon
spar |
Wheels |
5.00
x 5, hydraulic disc brakes |
Nose
gear |
rudder-pedals
driven |
Wheel |
5.00
x 5 |
Engine |
|
Model |
Jabiru
2200A |
Power |
58
kw @ 3300 t/mn |
Propeller |
|
Make |
Arplast |
Type |
TD
152 |
Blades |
Composite |
Limits |
|
Compliance |
CS-VLA |
Empty
weight |
250
kg |
Gross
weight |
450
kg |
Useful
load |
200
kg |
Manoeuver
load factors |
+5,30
; -2,65 g |
Vs0,
flaps 35° |
55
km/h |
Va |
165
km/h |
Vc |
216
km/h |
Vne |
272
km/h |
Performances |
|
Take
off run |
48
m |
Take
off distance |
153
m |
Landing
distance |
220 m |
Maximum
range |
1560
km |
Cruising
speed |
230 km |
Rate
of climb |
8
m/s |
Minimum
sink |
1,11
m/s |
Maximum
L/D |
22
to 92 km/h |
