 |
 |
| Photo: C22 cockpit customer design |
| |
|
|
|
|
|
|
Technical data
|
C22 C
65 HP
|
C22 CS
80 HP
|
| Max airspeed (IAS) |
110 km/hr
|
130 km/hr
|
| Never exceed airspeed (IAS) |
130 km/hr
|
145 km/hr
|
| Take-off speed |
60 km/hr
|
| Stall speed VSO (IAS) |
63 km/hr
|
Climp-speed
single seater/ double seater
|
3 m/s
|
5 m/s
|
| Span |
10,4 m
|
| Length |
6,25 m
|
| Height |
2,20 m
|
| Area |
15,2 qm
|
| Empty weight with rescue system |
227 kg
|
256 kg
|
| MTOW * |
450 kg
|
| Length of takeoff run / landing run |
80 m
|
50 m
|
| Range |
approx. 400 km
|
Engine
(other engines on inquiry) |
2-stroke Rotax 582
|
4-stroke
Rotax 912 UL
|
| Average consumption of fuel L/ hr |
12 - 18
|
10 - 13
|
| Propeller |
WD
4-blade
|
WD
3-blade
|
* MTOW and
payload may be different according to
national law
State: 04.2003 - Technical changes reserved.
Technical informations are partially approximate values |
|
|
|
|
|
|
