Sportcopter II – Fully Loaded
FUSELAGE :
• Composite Cabin Assembly w/ Two Removable Doors
• Tinted Plexiglass Windscreens, Front and Side Windows
• Empennage w/Fixed Incidence Horizontal Stabilizer
• Heavy-Duty Main Gear with Suspension
• Nosewheel w/ Suspension and Full Castering Capabilities
CABIN ACCOMMODATIONS:
• Center Pedestal Instrument Console
• Dual Controls
• 49″ wide cabin accommodates occupants 4’6″ -6’6″
• 2 seats w/Comfer™Cushions, adjust. back, lumbar support
• Map Pockets
• Two Pop-Out Vents, 1 per Window
• Rudder/Brake Pedals, Adjustable, State-of-the-Art
POWER PLANT:
• Lycoming I0 360
• Aircraft Engine 225 hp.
• Mounted fuel pump in line oil filter w/visual bypass alert button
FUEL SYSTEM:
• All aluminum welded 28 gallon fuel cell
ROTORSYSTEM:
• Sport Rotor Rotorblades
• 8.5″ X 31′ High Performance
• Corrosion Protected “On Condition” Aluminum Blades
• Standard Mechanical Prerotator Controls w/ Low Friction Bearings
• Tracking Provisions
• Heavy-Duty 3 ft. Hub Bar w/ Dampening System & Spherical Bearings
• Heavy-Duty Rotorhead
PROPELLOR:
• MT• 72″ Carbon Fiber Propeller
• Three Bladed, Constant Speed
• Controllable Pitch w/ Nickel Leading Edge
EFIS INSTRUMENTS:
• Air Speed Indicator
• Vertical Speed Indicator
• CHT/EGT
• Altimeter
• EGT Probes
• Hobbs Meter
• Oil Temperature Sensor
• Oil Pressure Sensor
• Voltmeter
• Manifold Pressure Sensor
• Fuel Flow Transducer
• Water Temperature
• RPM Sensor
• Compass
• Rotortach w/ Sensors
• Fuel Pressure Sensor
ELECTRICAL EQUIPMENT:
AVIONICS:
• Avionics Master Switch
OPTIONS AVAILABLE:
• Thermal Image Cameras
• Searchlights
• Hard Points installed
• Full Lotus Floats
MISCELLANEOUS:
• Engine Operating Manual
• Engine Parts Manual
• Operating Manuals
Standard Features
STANDARD FEATURES INCLUDE:
LOW-RATIO ROTO-CONTROL SYSTEM – humanized control response
DUAL CONTROLS – co-pilot separate and similar controls
INCREDIBLE HIGH-IMPACT SUSPENSION SYSTEM – 11″ Of Travel!
SHOCK-ISOLATED ROTORHEAD W/SUSPENSION -reduced vibration
ERGONOMIC ADJUSTABLE CYBER SEATS – w/ injection seat impact cushioning
INDEPENDENT TOE-OPERATED HYDRAULIC DISC BRAKES
PREROTATOR -Powerful Hydraulic System
SWING-ARM NOSEWHEEL SUSPENSION -high viscosity damper
MAIN GEAR, TAILWHEEL AND MAST SUSPENSION
NOSEWHEEL SUSPENSION – swing arm, castering abilities for self-tracking
INDEPENDENT STEERING – rudder and nosewheel controlled separately
HIGH PERFORMANCE SPORT ROTORS -adjustable pitch w/ dampening system
OUTSTANDING POINTS:
MORE SPEED
LARGER CABIN SPACE
POWERFUL PREROTATOR for short take-off
HIGHER ENGINE HP OUTPUT
INCREDIBLE SUSPENSION
FULLY ENCLOSED all weather capability
INDEPENDENT STEERING
CASTERING NOSEWHEEL with nose gear suspension
LOW RATIO ROTO-CONTROL system, expert maneuverability
SCII Specifications
Aircraft Length: 176″ (14.5′ / 4.419m)
Cabin Inside Dimensions: 49″
Height: 10′
Width: 83″
Rotor Diameter: 31′
Engine: Lycoming IO 360 (200-220 hp)
Fuel: 100LL AV Gas
Fuel Consumption: 8-10 gph
Fuel Capacity: 27 gal.
Empty Weight: 1000 lbs.
Useful Load: 500-600 lbs.
Gross Weight: 1700 lbs.