Robinson Helicopters R44 Cadet vs Robinson Helicopters R44 Raven I vs Robinson Helicopters R44 Raven Ii
All three are light, single‑engine, four‑seat piston helicopters in the R44 family, typically used for training, touring, and utility flying. The R44 Cadet is optimized for training and lower operating cost: it keeps the same basic airframe category but is generally configured for two main seats with reduced rear-seat/passenger capability compared with the Ravens, and it tends to have the shortest practical range because it’s commonly set up with more limited usable capacity and mission equipment. The R44 Raven I is the standard four‑place version, offering full passenger capability (pilot plus up to three passengers) and a moderate range typical of the type for cross‑country training and local transport. The R44 Raven II remains a four‑place helicopter (pilot plus up to three passengers) but features a higher‑power, fuel‑injected engine, which generally improves hot‑and‑high performance and can translate to more flexible real‑world range and payload planning, even if published range figures are often similar depending on tanks, power settings, and reserve assumptions.
| Spec | ROBINSON R44 Cadet | ROBINSON R44 Raven I | ROBINSON R44 Raven II |
|---|---|---|---|
| Summary | |||
| DOC / nm | $ 2.22 | $ 2.30 | $ 2.36 |
| Total Seats | 2 | 4 | 4 |
| Flight Rules | VFR | VFR | VFR |
| Manufacturer | Robinson Helicopters | Robinson Helicopters | Robinson Helicopters |
| Aircraft Name | R44 Cadet | R44 Raven I | R44 Raven II |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 300 | 300 | 300 |
| DOC / nm / Seat | $ 1.11 | $ 0.57 | $ 0.59 |
| OEM Verification | Un-Verified | Un-Verified | Un-Verified |
| Useful Load (lbs) | 763 | 950 | 995 |
| Direct Operating Cost | $ 238 | $ 248 | $ 257 |
| Flight Deck (Base Spec) | Gyro / Analog | Gyro / Analog | Gyro / Analog |
| Max Cruise Speed (ktas) | 107 | 108 | 109 |
| Base Aircraft Price (USD) | $344,000 | $ 412,000 | $ 490,000 |
| Cabin | |||
| Total Seats | 2 | 4 | 4 |
| Engine | |||
| FADEC | No | No | No |
| Model | O-540 | O-540 | IO-540 |
| Fuel Type | AvGas | AvGas | AvGas |
| TBO (hrs) | 2200 | 2200 | 2200 |
| TBO (yrs) | 12 | 12 | 12 |
| Horsepower | 210 | 225 | 245 |
| Fuel Delivery | Carbureted | Carbureted | Fuel Injected |
| No. of Engines | 1 | 1 | 1 |
| Fuel Capacity (gal) | 29.5 | 29.5 | 29.5 |
| Dimensions | |||
| Length (ft) | 38.3 | 38.3 | 38.3 |
| Overall Height (ft) | 10.8 | 10.8 | 10.8 |
| Rotor Diameter (ft) | 33 | 33 | 33 |
| Baggage Volume Int. (cu. ft) | 2.5 | 2.5 | 2.5 |