| |
| Empty weight (914) |
270 Kg (595 lb.) |
| Maximum take-off gross wt - USA |
550 Kg (1212 lb.) (Note: European "ultralight" limitations are 450 Kg) |
| Useful Load - USA |
277 Kg (612 lb.) |
PERFORMANCE |
|
| Maximum speed |
115 mph |
| Cruising speed |
90 mph |
| Absolute ceiling |
4000 m (13,000 ft) |
| Service ceiling |
3500 m (11,400 ft) |
| Take-off roll |
70 m (230 ft) |
| Landing roll |
from 0 to 30 m (0 to 100 ft) |
| Rate of climb |
5 m/s (950 ft/min) |
| Fuel tank capacity |
72 lt (19 gal) |
| Endurance |
3.4 h |
| Range (no reserve) |
300 miles |
DIMENSIONS |
|
| Rotor diameter |
8535 mm (28 ft) |
| Propeller diameter |
1700 mm (67 inch) |
| Overall width |
1800 mm (71 inch) |
| Overall lenght |
4655 mm (184 inch) |
| Overall height |
2600 mm (103 inch) |
DESCRIPTION |
|
| Airframe: |
Chrome-alloy aeronautical 4130 steel, tig welded. Fiberglass fuselage canopy. Fiberglass wheel pants. Fiberglass instrument panel. |
| Seat: |
With integral fuel-tank manufactured in epoxy resin reinforced with fiberglass. |
| Baggage Capacity |
150 Liters |
| Instruments: |
Rotor Tach, Altimeter, Airspeed Indicator, Flydat or EIS engine monitor |
| Engine: |
914 Rotax Turbo, 4 cylinders, 4-stroke, water-cooled, 115 hp with electric starter and mechanical prerotator. |
| Propeller: |
Arplast 67 inch three-blade carbon fiber with ground adjustable pitch. |
| Rotor: |
two-blade, composite materials. |
| Controls: |
Single - Front Seat |
| Trim |
Electric |
STANDARD EQUIPMENT |
- Electric Starter
- Airpeed Indicator
- Altimeter
- Flydat or EIS Instrument Monitor
- Cockpit partial enclosure
- Prerotator
- Rotor Brake
- Wheel Brakes and Wheel Pants
- Landing Light
- Electric Trim - Front
- 19 gallon Fuel Tank
- Arplast Propeller
- Magni Rotor
|
OPTIONS:
|
- Electric trim control
- Removable Rear Seat Windscreen
|