technical data / performance
|
wing span
|
28.7' |
|
engine (Rotax) |
912S (100 hp) |
| wing area |
130 sqft |
|
propeller |
warp drive 3 blades |
| aspect ratio |
6.24 |
|
stall speed flaps up |
41 mph |
| length |
18.6' |
|
stall speed flaps down |
36 mph |
| empty with fluids |
750 lbs |
|
cruising speed |
115 mph |
| max. take off weight |
1,320 lbs |
|
max. cruise |
130 mph |
| load factor |
+5 G's / -3 G's |
|
VNE |
160 mph |
| max. fuel capacity |
25 gal |
|
rate of climb |
1000 ft/min |
| cabin widht |
46.9' |
|
take off (land) |
300 ft |
|
take off (water) |
350 ft |
|
Note: Some modifications can be made to
|
landing (land) |
300 ft |
|
the aircraft to meet different country
|
landing (water) |
350 ft |
|
requirements.
|
endurance |
4.5 hrs |
|