Robinson Helicopters R44 Raven Ii vs Robinson Helicopters R66
The Robinson R44 Raven II and Robinson R66 are both light, single-rotor helicopters aimed at private, training, and utility flying, but they sit in different categories. The R44 Raven II is generally considered a light piston helicopter, using a piston engine and targeting lower acquisition and operating costs. The R66 is a larger, light turbine helicopter, offering the smoother power delivery and performance characteristics typically associated with turbine operations, along with higher purchase and operating costs. In range, the R66 typically provides a longer practical range than the R44 Raven II, reflecting its greater fuel capacity and turbine mission profile, though real-world range for either aircraft varies with payload, altitude, temperature, and reserve requirements. For passenger capacity, the R44 Raven II is configured for up to four occupants including the pilot, making it well-suited to a pilot plus three passengers in lighter-load scenarios. The R66 is configured for up to five occupants including the pilot, enabling an additional passenger and generally offering more cabin space and useful load flexibility for carrying people and baggage.
| Spec | ROBINSON R44 Raven II | ROBINSON R66 |
|---|---|---|
| Summary | ||
| DOC / nm | $ 2.36 | $ 3.49 |
| Total Seats | 4 | 5 |
| Flight Rules | VFR | VFR |
| Manufacturer | Robinson Helicopters | Robinson Helicopters |
| Aircraft Name | R44 Raven II | R66 |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 300 | 350 |
| DOC / nm / Seat | $ 0.59 | $ 0.70 |
| OEM Verification | Un-Verified | Un-Verified |
| Useful Load (lbs) | 995 | 1355 |
| Direct Operating Cost | $ 257 | $ 384 |
| Flight Deck (Base Spec) | Gyro / Analog | Gyro / Analog |
| Max Cruise Speed (ktas) | 109 | 110 |
| Base Aircraft Price (USD) | $ 490,000 | $ 920,000 |
| Cockpit | — | 2 |
| Min Crew | — | 1 |
| Standard Cabin Seats | — | 3 |
| Cabin | ||
| Total Seats | 4 | 5 |
| Cockpit | — | 2 |
| Min Crew | — | 1 |
| Standard Cabin Seats | — | 3 |
| Engine | ||
| FADEC | No | No |
| Model | IO-540 | RR300 |
| Fuel Type | AvGas | JetFuel |
| TBO (hrs) | 2200 | 2000 |
| TBO (yrs) | 12 | — |
| Horsepower | 245 | 300 |
| Fuel Delivery | Fuel Injected | — |
| No. of Engines | 1 | 1 |
| Fuel Capacity (gal) | 29.5 | 73.6 |
| Dimensions | ||
| Length (ft) | 38.3 | 38.3 |
| Overall Height (ft) | 10.8 | 11.4 |
| Rotor Diameter (ft) | 33 | 33 |
| Baggage Volume Int. (cu. ft) | 2.5 | — |
| Cabin Volume (cu. ft) | — | 50 |
| Baggage Volume Ext. (cu. ft) | — | 18 |