WEIGHT |
|
| Empty weight (914) |
285 Kg (629 lb.) |
| Maximum take-off gross wt - USA |
550 Kg (1212 lb.) (Note: European "ultralight" limitations are 450 Kg) |
| Useful Load - USA |
280 Kg (583 lb.) |
PERFORMANCE |
|
| Maximum speed |
105 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 |
82 lt (21 gal) |
| Endurance |
3.0 h (with 1/2 hour reserve) |
| 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. Carbon fiber fuselage and instrument panel. Fiberglass tail, landing gear and wheel pants. |
| Seat: |
Padded with integral 21 gallon fuel-tank manufactured in epoxy resin reinforced with fiberglass. |
| 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: |
28 ft diameter, two-blade, composite materials manufactured by Magni Gyro. |
| Controls: |
Dual, all steel linkage, all ball bearing joints. |
| Trim |
Electric |
STANDARD EQUIPMENT |
- Electric Starter
- Airpeed Indicator
- Altimeter
- EIS Instrument Monitor
- Vertical Card Magnetic Compass
- Fuel Level Indicator
- Prerotator capable of 200 - 300 RRPM
- Rotor Brake
- Rotor RPM Tachometer
- Wheel Brakes and Wheel Pants
- Landing Light
- Electric Trim - Left Seat
- 21 gallon Fuel Tank
- Arplast Propeller
- Magni Rotor
|
OPTIONS: (factory available)
|
- Com Radio
- Transponder
- GPS
- Strobe and NAV lights
- 12 Volt Power outlet - cigarette type
- Variometer
|