Robinson R44 II (2007)
Sale price: US $375,000.00 Make an Offer
| Used |
| “Only 95 hours since 2200hr overhaul, done this year. Very nice looking, even better flying helicopter. Has AC, bladder tanks and simplex spraying sys provisions.” |
| Make: | Robinson | Model Year: | 2007 |
East Troy, Wisconsin, United States
Vehicle description
Four-seat Robinson R44 Raven II helicopters are high performing, reliable and easy to maintain. R44s have a two-bladed rotor system, T-bar cyclic and the latest in Robinson technology including streamlined instrument panels and crashworthy bladder fuel tanks. The R44’s aerodynamic fuselage optimizes airspeed and fuel economy. Hydraulic controls eliminate feedback forces and provide responsive handling. A low tail-rotor tip speed, newly designed muffler and large cambered tail reduce flyover noise. Raven II helicopters are powered by Lycoming’s IO-540 fuel injected engine. The IO-540 delivers better altitude performance, increased payload and eliminates the need for carburetor heat. Standard Panel with optional artificial horizon, King KT 76c transponder, and right accessory bar. R44RAVEN II SPECIFICATIONS Helicopter Raven II Engine Lycoming IO-540, six cylinder, fuel injected
Horsepower Derated to 245 for takeoff and 205 max cruise Maximum Gross Weight 2500 lb (1134 kg)
Approximate Empty Weight (nick. oil & standard avionics) 1505 lb (683 kg) Standard Fuel (29.5 gal) 177 lb (80 kg) Auxiliary Fuel (17.0 gal) 102 lb (46 kg) Pilot, Passengers, and Bag- gage (with standard fuel) 818 lb (371 kg) Cruise Speed at Maximum Gross Weight up to 109 kts (202 km/h) Maximum Range (no reserve) approx 300 nm (550 km) Hover Ceiling IGE 8950 ft @ 2500 lb Hover Ceiling OGE 7500 ft @ 2300 lb Rate of Climb over 1000 fpm Maximum Operating Altitude 14,000 ft Electrical System 28 volt STANDARD AVIONICS • Seven-hole instrument panel • FS PM3000 audio panel • King KY 196A radio STANDARD INSTRUMENTS • Airspeed indicator • Altimeter • Rotor/engine dual tachometer • Manifold pressure gage • Vertical speed indicator • Magnetic compass • Cylinder head temperature gage • Oil temperature and pressure gages • Fuel gages • Ammeter • Digital OAT gage/voltmeter • Hourmeter • Quartz clock STANDARD EQUIPMENT • Hydraulic power controls • RPM throttle governor • Throttle correlator • Main and auxiliary crashworthy fuel bladder tanks • Engine oil filter and quick drain • Engine muffler • Cabin heater and defogger • Carbon monoxide detector • Rotor brake • Intercom switches • Avionics master switch • 3-point shoulder harnesses • Pilot-side adjustable pedals • Door locks • Sound damping headliner
Horsepower Derated to 245 for takeoff and 205 max cruise Maximum Gross Weight 2500 lb (1134 kg)
Approximate Empty Weight (nick. oil & standard avionics) 1505 lb (683 kg) Standard Fuel (29.5 gal) 177 lb (80 kg) Auxiliary Fuel (17.0 gal) 102 lb (46 kg) Pilot, Passengers, and Bag- gage (with standard fuel) 818 lb (371 kg) Cruise Speed at Maximum Gross Weight up to 109 kts (202 km/h) Maximum Range (no reserve) approx 300 nm (550 km) Hover Ceiling IGE 8950 ft @ 2500 lb Hover Ceiling OGE 7500 ft @ 2300 lb Rate of Climb over 1000 fpm Maximum Operating Altitude 14,000 ft Electrical System 28 volt STANDARD AVIONICS • Seven-hole instrument panel • FS PM3000 audio panel • King KY 196A radio STANDARD INSTRUMENTS • Airspeed indicator • Altimeter • Rotor/engine dual tachometer • Manifold pressure gage • Vertical speed indicator • Magnetic compass • Cylinder head temperature gage • Oil temperature and pressure gages • Fuel gages • Ammeter • Digital OAT gage/voltmeter • Hourmeter • Quartz clock STANDARD EQUIPMENT • Hydraulic power controls • RPM throttle governor • Throttle correlator • Main and auxiliary crashworthy fuel bladder tanks • Engine oil filter and quick drain • Engine muffler • Cabin heater and defogger • Carbon monoxide detector • Rotor brake • Intercom switches • Avionics master switch • 3-point shoulder harnesses • Pilot-side adjustable pedals • Door locks • Sound damping headliner