R22 Beta II
The two-seat R22 Beta II helicopter is a proven workhorse that has delivered exceptional performance in a variety of applications for over thirty years. The R22 has a two-bladed rotor system, T-bar cyclic and the latest in Robinson technology including crashworthy bladder fuel tanks.
A powder-coated steel tube structure provides a light yet rigid airframe while the aircraft’s aerodynamic fuselage optimizes airspeed and fuel economy. The R22 is powered by Lycoming’s proven O-360 engine that is derated to provide reserve power and better performance at high altitudes and in hot weather.
Features
Removable left seat controls
Center-positioned T-bar cyclic
Integrated cyclic grip controls
Collective-activated hour meter
Under-seat storage
Lycoming O-360 engine
Equipment & Accessories
- Six-hole instrument panel – Detail
- RPM governor
- Throttle correlator
- Carburetor heat assist
- Crashworthy fuel system with bladder tanks
- Engine oil filter and quick drain
- Robinson engine oil filter installation
- Electronic Engine Monitoring Unit for maintenance and engine health tracking – Detail
- Engine overspeed protection during starting
- Removable dual controls – Detail
- Rotor brake – Detail
- Intercom switches – Detail
- Avionics master switch – Detail
- Tinted windows – Detail
- Fabric velour seats
- 3-point shoulder harnesses – Detail
- Door locks – Detail
- Engine muffler
- Sound damping headliner
- Underseat storage – Detail
- Belly hardpoint
- LED anti-collision and navigation lights – Detail
- Dual landing lights
- LED panel and map lights
- Tow cart adapter – Detail
- Ground handling wheels – Detail
- Rotor blade tie downs – Detail
- Windshield cover
- Travel bag – Detail
- Upper sheave – Detail
- Leather seats – Detail
- Cabin heater & defogger (dual forward outlets) – Detail
- Impact-resistant windshields – Detail
- Engine priming system – Detail
- Xenon HID landing lights – Detail
- Metallized upper sheave (replaces standard sheave) – Detail
- Lightweight battery, 15 amp hour (replaces standard battery) – Detail
- Second hourmeter, oil-pressure-activated – Detail
- GPS Fleet Tracking Spidertracks S6 – Detail
- David Clark H10-13H (custom cord) – Detail
- Bose A20 headset with Bluetooth – Detail
- Fire extinguisher (fly away delivery only) – Detail
- Bracket for fire extinguisher – Detail
- Accessories support bar with power plug and dual USB ports (pilot side) – Detail
- Accessories support bar with power plug and dual USB ports (left side) – Detail
- Garmin Flightstream 510 card (exchange for standard database card) – Detail
- Leather seat back booster cushion – Detail
- Velour seat back booster cushion – Detail
- MT950-2 universal tow cart – Detail
Instruments
- Airspeed indicator – Detail
- Altimeter – Detail
- Rotor/engine dual tachometer – Detail
- Manifold pressure gage – Detail
- Vertical speed indicator – Detail
- Magnetic compass – Detail
- Gage panel and Ammeter – Detail
- Carburetor temperature gage – Detail
- Oil Temp and Pressure gages
- Cylinder head temp gage
- Fuel gages
- Digital OAT gage/voltmeter – Detail
- Hourmeter – Detail
- Quartz clock – Detail
- PFD, Aspen Avionics EFD1000H Pilot (with slaved D.G.) – Detail
- PFD, Aspen Avionics EFD1000H Pro with HSI (requires GPS) – Detail
- Garmin GI-106B – Detail
- Kelly Mfg RCA2600-3 Artificial Horizon with Slip Skid – Detail
- Kelly Mfg RCA2600-3 Artificial Horizon with Slip Skid, windshield mount – Detail
- Artificial Horizon, Mid-Continent 4300 with Slip Skid (mechanical gyro) – Detail
- Directional Gyro, Mid-Continent 3300 (mechanical gyro) – Detail
- Turn Coordinator, Mid-Continent (mechanical gyro) – Detail
- Vertical Compass, PAI-700 (replaces standard compass) – Detail
- Digital Chronometer, Davtron 800 (replaces standard clock) – Detail
- Millibar Altimeter (replaces standard in-Hg) – Detail
- Meter Altimeter (replaces standard in-Hg) – Detail
- IVSI – Instantaneous Vertical Speed Indicator (replaces standard VSI) – Detail
Specifications & Dimensions
| Helicopter | R22 Beta II |
| Engine | Lycoming O-360, four cylinder |
| Horsepower | Derated to 131 hp for takeoff and 124 continuous |
| Maximum Gross Weight | 1370 lb (622 kg) |
| Approximate Empty Weight (including oil & standard avionics) | 880 lb (399 kg) |
| Standard Fuel (16.9 gal) | 101 lb (46 kg) |
| Auxiliary Fuel (9.4 gal) | 56 lb (25 kg) |
| Pilot, Passenger, and Baggage (with standard fuel) | 389 lb (176 kg) |
| Max Airspeed (Vne) | 102 kts (189 km/h) |
| Cruise Speed | up to 96 kts (178 km/h) |
| Maximum Range (no reserve) | approx 250 nm (460 km) |
| Hover Ceiling IGE at 1370 lb | 9400 ft |
| Hover Ceiling OGE at 1300 lb | 8000 ft |
| Maximum Operating Altitude | 14,000 ft |
| Electrical System | 14 volt |
