Any mission. Every mission. Like all Robinson helicopters, the R44 Raven II and Clipper II are easy to maintain, inexpensive to own and operate, and known for steadfast performance. So what makes these stand out from the rest? In a word: versatility
Standard features: The R44 Raven II and Clipper II have a two-bladed rotor system, streamlined instrument panels and a crashworthy fuel system. An aluminum monocoque and powder-coated steel tube structure provide a lightweight, yet robust airframe while the aerodynamic fuselage optimizes airspeed and fuel economy. Hydraulically boosted controls eliminate cyclic and collective feedback forces and provide responsive handling. A low tail-rotor tip speed and large cambered tail reduce flyover noise. Raven II and Clipper II helicopters are powered by Lycoming’s IO-540 fuel injected engine. The IO-540 delivers improved altitude performance, an increased payload of 2500 lbs, and eliminates the need for carburetor heat.
Our patented Cyclic design offers increased safety, comfort and ease of operation for pilots:
The Clipper II may be equipped with either fixed utility or pop-out floats, offering safety for over-water travel. Designed for emergencies, pop-out floats inflate within 2-3 seconds of activation. When not in use, pop-out floats roll-up and stow in protective covers along the aircraft’s landing skids. The streamlined, low-profile design minimizes drag and allows for easy entry and exit of the cabin. Fixed utility floats remain fully inflated, add approximately 50 pounds to the aircraft’s empty weight, and reduce cruise speed by approximately ten knots.
A hardpoint is a location on the belly designed to carry an external or internal load.
The Hydraulically Boosted Controls on the R44 Raven II assist the pilot in controlling the helicopter's flight surfaces, such as the cyclic, collective, and tail rotor by significantly reducing the manual force required to operate the controls. They enable for more precise and smoother control inputs, improving the overall handling characteristics of the helicopter. Enhanced control responsiveness contributes to the overall safety of helicopter operations, particularly during critical phases of flight such as takeoff, landing, and emergency maneuvers.
The R44 Raven II features a Crashworthy Fuel System with a Bladder Tank designed to prevent fuel leakage and reduce the risk of fire in the event of a crash. The system incorporates several features and design elements to enhance safety for both the helicopter and its occupants. The R44's fuel tank is constructed of an aluminum enclosure containing a flexible, puncture- and tear-resistant bladder that can withstand significant impact without rupturing. Additionally, the fuel system includes flexible joints or self-sealing breakaway couplings that absorb energy and prevent breakage. These are designed to disconnect safely and seal off the fuel line if excessive force is applied, preventing fuel spillage.
Our patented cyclic design enhances safety, comfort, and ease of operation by minimizing flight control interference, ensuring consistent handling across Robinson models, and reducing pilot fatigue. Its streamlined design eliminates the need for separate cockpit controls, simplifying operation and maintenance.
The Engine Monitoring Unit tracks key engine parameters such as engine-related exceedances and flight data. Also, the Robinson EMU App gives pilots, operators, and maintenance personnel the capability to wirelessly connect to the onboard EMU unit on properly-equipped Robinson R44 helicopters to view certain aircraft performance parameters recorded during operation.
ITEM | Raven II | Clipper II pop out floats | Clipper II fixed floats |
---|---|---|---|
Engine | Lycoming IO-540, six cylinder, fuel injected | ||
Horsepower | Derated to 245 for takeoff and 205 continuous | ||
Maximum Gross Weight | 2500 lb (1134 kg) | ||
Approximate Empty Weight (including oil & standard avionics) | 1505 lb (683 kg) | 1500 lb (680 kg) | 1570 lb (712 kg) |
Standard Fuel (29.5 gal) | 177 lb (80 kg) | ||
Auxiliary Fuel (17.0 gal) | 102 lb (46 kg) | ||
Pilot, Passengers, and Baggage (with maximum fuel) | 818 lb (371 kg) | 721 lb (327 kg) | 651 lb (295 kg) |
Cruise Speed at Maximum Gross Weight | Up to 109 kts (202 km/h) | Up to 106 kts (196 km/h) | |
Maximum Range (no reserve) | Approximately 350 nm (650 km) | ||
Hover Ceiling IGE at Maximum Gross Weight | 8950 ft @ 2500 lb | ||
Hover Ceiling OGE at Maximum Gross Weight | 7500 ft @ 2300 lb | ||
Rate of Climb | Over 1000 fpm | ||
Maximum Operating Altitude | 14,000 ft | ||
Electrical System | 28 volt |