WEIGHT
 
Empty weight (914) 270 Kg (595 lb.)
Empty weight (912 ULS) 265 Kg (585 lb.)
Maximum take-off gross wt - USA 550 Kg (1212 lb.) (Note: European "ultralight" limitations are 450 Kg)
Useful Load - USA 280 Kg (617 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.
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. Available also with Rotax 912 ULS (100 HP).
Propeller: Arplast 67 inch three-blade carbon fiber with ground adjustable pitch.
Rotor: two-blade, composite materials.
Controls: Dual.
Trim Electric
STANDARD EQUIPMENT
  • Electric Starter
  • Airpeed Indicator
  • Altimeter
  • Flydat or EIS Instrument Monitor
  • Cockpit partial enclosure
  • Prerotator
  • Rotor Brake
  • Carburetor Heat and Temperature Gauge - 912 (non-turbo) only
  • Wheel Brakes and Wheel Pants
  • Landing Light
  • Electric Trim - Front
  • 19 gallon Fuel Tank
  • Arplast Propeller
  • Magni Rotor
OPTIONS:


  • Electric trim control - rear seat
  • Removable Rear Seat Windscreen