PERFORMANCE
| Maximum Cruise Speed |
210 ktas (380 km/h) |
| Maximum Cruise Speed 75% Power |
200 ktas (360 km/h) |
| Maximum Range |
1297 nm (2,000 km) |
| Takeoff Distance |
984 ft (300 m) |
| Takeoff Roll |
656 ft (200/175/175 m) |
| Landing Roll |
656 ft (200/175/175 m) |
| Service Ceiling |
18,000 ft (5,400 m) |
| Maximum Climb Rate |
1300/1600/2000 fpm |
| Maximum Limit Speed (VNE) |
183 kias (305/340/340 km/h) |
| Stall Speed with Flaps |
42 kcas (78 km/h) |
| Endurance |
7 h |
Engine
| Manufacturer |
Rotax |
| Model |
912 – 914 – 915 |
| Power Output |
100 – 115 – 142 hp |
| Propeller Manufacturer |
DUC , Woodcomp |
| Description |
2 or 3 blade , fixed or variable |
WEIGHTS
| Empty Weight |
683 lb (310/340/360 kg) |
| Maximum Takeoff Weight |
1322 lb (600 kg) |
| Usable Fuel Volume |
36.9 gal (100/120/140 l) |
| Useful Load |
– |
DIMENSIONS
| Length |
20.4 ft (6.24 m) |
| Height |
6.9 ft (2.05 m) |
| Wingspan |
27.6 ft (8.44 m) |
| Wing Area |
– |
CABIN INTERIOR
| Height |
– |
| Width |
3.77 ft (115 cm) |
| Length |
– |
| Maximum Occupants |
2 |
BAGGAGE CAPACITY
Weight |
55 lb (25 kg)
|
| Volume |
– |
|
