M -18 Spartan

Single Seater, Partially Enclosed

The millennium model M-18 is provided with the Rotax 582 engine (65 HP) with standard dual carburetors, "E" gearbox electric start and exhaust silencer. Other standard equipment includes altimeter, airspeed indicator, rotor tachometer, engine tachometer, hobbs hour meter, water temperature gauge, prerotator, rotor brake, wheel brakes, landing light, wheel pants, manual cockpit trim control and 9 gallon fuel capacity.

An EIS instrument monitor may be substituted for the engine instruments. See the extensive list of standard equipment listed below.

TECHNICAL SPECIFICATIONS

WEIGHT
Empty weight 167 Kg (368 lb.)
Maximum take-off gross weight 350 Kg (771 lb.) (Note: European "ultralight" limitations are 300 Kg)
Useful Load 183 Kg (403 lb.)

PERFORMANCE
Maximum speed 169 km/h
Cruising speed 112 km/h
Absolute ceiling 4000 m (13,000 ft)
Service ceiling 3500 m (11,400 ft)
Take-off roll 45 m (150 ft)
Landing roll from 0 to 30 m (0 to 100 ft)
Rate of climb 3.5 m/s (680 ft/min)
Fuel tank capacity 9 gallons
Endurance 1.5 h
Range (no reserve) 180 km

DIMENSIONS  
Rotor diameter 7300 mm (24 ft)
Propeller diameter 1600 mm (63 inch)
Overall width 1780 mm (70 inch)
Overall length 2980 mm (178 inch)
Overall height 2340 mm (92.1 inch)

DESCRIPTION
Airframe: Chrome-alloy aeronautical 4130 steel, tig welded.
Seat: With integral fuel-tank manufactured in epoxy resin reinforced with fiberglass.
Engine: Rotax 582, 2 cyl, two-stroke, water-cooled, with mechanical prerotator.
Propeller: Arplast 63 inch three-blade carbon fiber with ground adjustable pitch.
Rotor: Two-blade, composite materials.
Controls: Single
   

STANDARD EQUIPMENT: Electric Starter
Altimeter
Airspeed Indicator
Hourmeter
Prerotator
Rotor Brake
Engine Tach
Landing Light
Rotor Tach
Water Temp Indicator
Wheel Brakes and Wheel Pants
Cockpit partial enclosure
13 gallon Fuel Tank
Arplast Propeller
Magni Rotor
Manual Trim - cockpit manual control

OPTIONS: Electric Trim

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