The Robinson R22 Beta II is flown throughout the world for many applications, ranging from flight training to livestock mustering to patrolling pipelines that require dependability, low operating costs, and performance.

The R22 Beta II incorporates a Lycoming O-360 four-cylinder, carburetor-equipped engine fueled with 100L grade aviation gasoline. This 145 hp engine is derated to 131 hp for five minutes at takeoff and 124 hp for continuous operation. A powerful engine, a lightweight steel-tube airframe, and aerodynamic shape gives the R22 a cruise speed of up to 90 kts and an average fuel consumption of only 7-10 gallons per hour.

The R22 seats two adults and occupants have panoramic views due to R22’s large windows. Acoustical foam lowers cabin noise. A heavy-duty muffler and low tail-rotor tip speed lessen flyover noise.

SPECIFICATONS

PERFORMANCE

Standard day, sea level, maximum gross weight unless otherwise noted

  Maximum cruise speed (VH) 102kts  
  Hover ceiling, In-Ground-Effect (1370 lb) 9400ft  
  Hover ceiling, Out-of-Ground-Effect (1300 lb) 8000ft  
  Range (long range cruise* 224nm  
  Max operating altitude 14000ft  
WEIGHTS
  Gross Weight 137s  
  Empty Weight Equipped (including oil & avionics) 880lbs  
  Passengers and Baggage with Standard Fuel 389lbs  
ACCOMMODATION
  Normal cabin seating (training) 2  
  Maximum certified cabin seating (utility) 2  
  Cabin length 4.3ft  
  Cabin width 3.6ft  
POWERPLANT
  Lycoming O-360 four-cylinder, carbureted  
FUEL CAPACITY
  16.9 USG  

SPECIFICATIONS

PERFORMANCE

Standard day, sea level, maximum gross weight unless otherwise noted

  Maximum cruise speed (VH) 117kts  
  Hover ceiling, In-Ground-Effect (2500 lb) 8950ft  
  Hover ceiling, Out-of-Ground-Effect (2300 lb) 7500ft  
  Range (long range cruise* speed @ 4,000 feet) (no reserve) 64.0 gallon 350nm  
  Max operating altitude 14000ft  
WEIGHTS
  Gross Weight 2500lbs  
  Empty Weight Equipped (including oil & avionics) 1500lbs  
  Passengers and Baggage with Standard Fuel 816lbs  
ACCOMMODATIONS
  Normal cabin seating (training) 2  
  Maximum certified cabin seating (utility) 4  
  Cabin length 5.7ft  
  Cabin width 3.8ft  
POWERPLANT
  Engine Type Lycoming IO-540 fuel injected cylinders 6    
FUEL CAPACITY
  Standard Fuel 30.6USG  
  Auxiliary Fuel 18.3USG  

Robinson’s R44 Raven Series Helicopters provide excellent reliability, responsive handling, and altitude performance, making the R44 the ideal helicopter for training, high altitude operations in mountainous terrain, as well as a great platform for aerial missions of most any type.

Key Features:

  • Lightweight airframe and streamlined fuselage enhances airspeed and fuel economy
  • Comfortably seats 4 adults with unobstructed views due to open cabin design
  • Aerodynamic rotor blade tips, low tail-rotor tip speed, heavy-duty muffler, and large cambered tail decrease noise and increase comfort
  • Powerful Lycoming 6-cylinder engine gets you anywhere you want to go
  • Center-positioned, teetering T-bar makes it easy to enter and exit the cockpit
  • Rotor brake enables the pilot to stop the rotor blades more quickly, reducing shutdown time and increasing safety
  • Hydraulic power controls eliminates stick shake and control forces, enabling precise hovering and a smooth ride

SPECIFICATIONS

PERFORMANCE

Standard day, sea level, maximum gross weight unless otherwise noted

  Maximum speed (VNE) 95kts  
  Maximum cruise speed (VH) 86kts  
  Hover ceiling, In-Ground-Effect (1700 lb) 10 800ft  
  Hover ceiling, Out-of-Ground-Effect (1700 lb) 8 600ft  
  Range (long range cruise* speed @ 4,000 feet) (no reserve) 64.0 gallon 375nm  
WEIGHTS
  Maximum takeoff gross weight 2050lb  
  Empty weight, standard configuration 1100lb  
  Useful load 950lb  
ACCOMMODATIONS
  Normal cabin seating (training) 2  
  Maximum certified cabin seating (utility) 3  
  Cabin length 4.75 ft  
  Cabin width 4.92ft  
POWERPLANT
  Textron Lycoming HIO-360-D1A    
  Powerplant ratings (per engine, standard day, sea level)    
  – Takeoff (5-minute) 190 shp  
  – Maximum continuous 190 shp  
FUEL CAPACITY
  Extended range capacity 64 USG  

The S-300C helicopter is known as one of the finest and most versatile piston-engine rotorcraft. A proven aircraft that has seen roles from combat missions to search and rescue Colorado Heliops has found this great machine perfect for flight training, scenic flights and as a stable platform for surveys and aerial photography.

Key features:

  • Strategic placement of engine for low center of gravity
  • Shock absorbing landing gear
  • Energy absorbing fuselage structure
  • Three-bladed, fully articulated rotor system eliminates mast bumping
  • Instrument training package for IFR instruction
  • Basic aircraft useful load of 950 lbs.
  • Doors-off operation ideal for photography, aerial video, and training operations in warm climates
  • Military and civilian training value the 300C’s rugged design. Many high-time airframes have more than 20,000 flight hours
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Performance

Standard day, sea level, maximum gross weight unless otherwise noted

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