R 44 Cadet

Robinson’s R44 Cadet is a versatile two-place helicopter ideally suited for flight schools and operators that want the economy of a small helicopter but desire the comfort, power, and performance of a larger helicopter. The Cadet retains the same basic airframe, rotor system, and Lycoming O-540-F1B5 engine as the proven R44 Raven I except the rear seats have been removed and the aft compartment reconfigured for cargo.
Maximum gross weight is 2200 lb. Engine power is derated to 210 hp takeoff/185 hp continuous. The lower weight and derated power provide increased performance margins at high altitudes and lengthen the time between overhaul (TBO) to 2400 hours. With a newly designed muffler, the Cadet’s flyover noise is more than three decibles lower than the original R44 Raven I. A variety of equipment including air conditioning, autopilot, avionic packages for VFR and IFR training are available.

⇒   R44 Cadet Brochure   ⇐ 

   R44 Cadet Configuration   ⇐

R44 ENG

R44 Cadet Specification

Silnik Lycoming O-540-F1B5, six cylinder, carbureted
Horsepower Derated to 210 hp for takeoff and 185 hp continuous
Max Gross Weight 2200 lb, 988 kg
Approximate Empty Weight
(including oil & std avionics)
1432 lb, 650 kg
Standard Fuel (29.5 gal) (116 l) 177 lb, 80 kg
Auxiliary Fuel (17.0 gal) (69 l) 102 lb, 46 kg
Pilot, Passengers and Baggage, Full Fuel 489 lb , 222 kg
Maximum speed (Vne) up to 110 kts (127 mph), 212,4 km/h
Cruise Speed* 110 kts (127 mph) , 195 km/h
Maximum Range (no reserve)* approx 300 nm (350 sm), 555 km
Hover Ceiling IGE @ 2200 lb, 988 kg 8750 ft,  2667 m
Hover Ceiling OGE @ 2200 lb, 988 kg 5250 ft, 1600 m
Maximum Operating Altitude 14000 ft, 4300 m
Electrical System 28-volt

*for comparison purposes only, actual results may vary