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