SPECIFICATIONS |
|
PERFORMANCE
(with Hirth 3701 ES) |
| Length Overall
|
6.4m |
|
Take off/rotate
speed(no flaps)
|
45 kts |
| Height |
2.4m |
|
Takeoff Distance, zero
wind, no flaps
|
150m |
| Wheel Base |
2.2m |
|
Takeoff Distance, zero
wind 15 degrees flap
|
120m |
| Wingspan
|
9m |
|
Takeoff Distance, light
headwind no flaps
|
90m |
| Empty Weight |
420kg* |
|
Takeoff Distance, light
headwind 15 degrees flaps
|
80m |
| MTOW |
800kg |
|
Cruise Speed
|
90 kts |
| Motorisation |
100-180hp |
|
Vne
|
100
kts |
| Design Load |
+5/-3 |
|
Distance from takeoff
to clearance of a 50m obstacle
|
250m |
| Standard Fuel Qty |
120 litres |
|
Climb Rate @ 55-60kts |
1500'/min |
| Range standard |
3.7 hours + |
|
Climb Rate @480kg takeoff
weight (prop dependent) |
n/a |
| Long range tanks |
80-160L |
|
Landing Distance over
50m obstacle with 15 degrees flap and brakes applied |
300m |
| Cabin W/L/H |
110cm
wide |
|
Landing Speed (no flaps) |
55 kts |
| Seating |
2 |
|
Stall Speed |
40 kts |
Engines
in use: Rotax 914, ATP2000 Turbine, Lycoming 320 |
All
metal airframe |
Tailwheel |
XL
cargo area |
