Leonardo Aw169 vs Robinson Helicopters R44 Raven Ii
The Leonardo AW169 is a modern twin‑engine light‑intermediate helicopter typically used for offshore support, EMS, corporate transport, and public‑service missions, whereas the Robinson R44 Raven II is a smaller, single‑engine light helicopter commonly used for training, private ownership, patrol, and short‑range utility flying. In range, the AW169 generally offers a longer practical mission radius and greater fuel and payload flexibility than the R44, which is optimized for shorter trips and lower operating costs. In passenger capacity, the AW169 usually carries more people and can be configured for multiple roles with a larger cabin; typical layouts allow roughly one to two pilots plus several passengers, depending on mission equipment. The R44 Raven II is limited to four seats total (including the pilot), making it better suited to small groups. Overall, the AW169 prioritizes capability, redundancy, and cabin space, while the R44 emphasizes simplicity and affordability.
| Spec | AGUSTA / LEONARDO AW169 | ROBINSON R44 Raven II |
|---|---|---|
| Summary | ||
| Cockpit | 2 | — |
| DOC / nm | $ 11.84 | $ 2.36 |
| Min Crew | 1 | — |
| Total Seats | 12 | 4 |
| Flight Rules | IFR | VFR |
| Manufacturer | Leonardo | Robinson Helicopters |
| Aircraft Name | AW169 | R44 Raven II |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 440 | 300 |
| DOC / nm / Seat | $ 0.99 | $ 0.59 |
| Max Cabin Seats | 10 | — |
| OEM Verification | Un-Verified | Un-Verified |
| Standard Cabin Seats | 10 | — |
| Direct Operating Cost | $ 1,658 | $ 257 |
| Flight Deck (Base Spec) | EFIS | Gyro / Analog |
| Max Cruise Speed (ktas) | 140 | 109 |
| Base Aircraft Price (USD) | $9,450,000 | $ 490,000 |
| Useful Load (lbs) | — | 995 |
| Cabin | ||
| Cockpit | 2 | — |
| Min Crew | 1 | — |
| Total Seats | 12 | 4 |
| Max Cabin Seats | 10 | — |
| Standard Cabin Seats | 10 | — |
| Engine | ||
| FADEC | Yes | No |
| Model | PW210A | IO-540 |
| Fuel Type | JetFuel | AvGas |
| TBO (hrs) | 4000 | 2200 |
| Horsepower | 1000 | 245 |
| No. of Engines | 2 | 1 |
| TBO (yrs) | — | 12 |
| Fuel Delivery | — | Fuel Injected |
| Fuel Capacity (gal) | — | 29.5 |
| Dimensions | ||
| Length (ft) | 48.1 | 38.3 |
| Overall Height (ft) | 14.8 | 10.8 |
| Cabin Volume (cu. ft) | 222.5 | — |
| Baggage Volume Ext. (cu. ft) | 49.5 | — |
| Rotor Diameter (ft) | — | 33 |
| Baggage Volume Int. (cu. ft) | — | 2.5 |