| DIMENSIONS |
|
ft |
m |
|
| Wing span |
|
27.17 |
8.28 |
| Aspect ratio |
|
7 |
|
| Overall length |
|
19.17 |
5.84 |
| Overall height (Tri-Gear) |
|
7 |
2.13 |
| |
|
ft³ |
m³ |
| Baggage space |
|
22.5 |
0.64 |
| |
|
|
|
| WEIGHTS AND LOADING |
|
lb |
kg |
| Empty weight (typically equipped) |
Tri-gear |
780 |
354 |
| Max
take-off weight* |
Tri-gear |
1370 |
623 |
| Useful load |
Tri-gear |
590 |
268 |
| Wing area |
|
102ft² |
9.48m² |
| Wing loading at max T.O.W. |
|
13.43lb/ft² |
66kg/m² |
| Power loading (Rotax 912S) |
|
13.70lb/hp |
8.4kg/kw |
| g loading |
|
Design |
Ultimate |
| |
|
+3.80/ |
+8.55/ |
| -1.9 |
-4.27 |
| PERFORMANCE |
|
mph |
kts |
kph |
| Stall speed flaps extended |
|
51 |
44 |
81 |
| Stall speed clean |
|
57 |
49 |
90 |
| Cruise speed 8000ft 75% pwr (Rotax 912S) (TAS) |
Tri-gear |
155 |
135 |
250 |
| Max Cruise speed 10000ft 75% pwr (Rotax 914 turbo) (TAS) |
Tri-gear |
191 |
166 |
307 |
| Rate of Climb at 1370 lb gross weight (Rotax 914 turbo) |
|
1300fpm |
6.6m per sec |
| Take-off ground roll at gross weight (Rotax 914 turbo) |
|
500 |
153 |
|
| Landing roll |
|
600 |
184 |
| |
|
imp gal |
us gal |
liters |
| Max fuel (standard) |
|
15 |
18 |
70 |
| Max fuel (with aux tank) |
|
23 |
28 |
105 |
| |
|
imp gal/hr |
ltr/hr |
|
| Fuel consumption at economy cruise 95-100 kts (Rotax 912) |
|
2 |
9 |
| |
|
nm |
km |
sm |
| Range at economy cruise |
Standard tanks |
732 |
1355 |
841 |
| |
Aux tanks |
1093 |
2023 |
1256 |
| Note: performance figures may vary depending on
propeller setting and standard of build |
| *Max takeoff weight can be increased to 1,450lb in the USA only |
