Leonardo Sh09 vs Robinson Helicopters R44 Raven Ii
The Leonardo SH09 and the Robinson R44 Raven II sit in different helicopter categories and are aimed at different mission profiles. The SH09 is a modern, single‑engine light helicopter positioned toward utility and professional operations, whereas the R44 Raven II is a widely used light piston helicopter most commonly found in private, training, and light commercial roles. In passenger capacity, the SH09 is typically configured for up to around six occupants including the pilot, giving it an edge in cabin volume and people-carrying flexibility. The R44 Raven II is generally a four‑seat aircraft including the pilot, which suits shorter trips and lower operating costs but limits payload and seating. On range, the SH09 is designed for longer legs than many piston light helicopters, with expected ranges in the several‑hundred‑nautical‑mile class depending on configuration and reserves. The R44 Raven II’s practical range is also several hundred nautical miles, but it is more sensitive to payload, density altitude, and fuel reserves, and it is usually chosen for shorter point‑to‑point missions rather than extended utility work.
| Spec | AGUSTA / LEONARDO SH09 | ROBINSON R44 Raven II |
|---|---|---|
| Summary | ||
| Cockpit | 2 | — |
| DOC / nm | $4.48 | $ 2.36 |
| Min Crew | 1 | — |
| Total Seats | 8 | 4 |
| Flight Rules | VFR | VFR |
| Manufacturer | Leonardo | Robinson Helicopters |
| Aircraft Name | SH09 | R44 Raven II |
| Certification | In-Development | FAA / EASA |
| Max Passengers | 7 | — |
| Max Range (nm) | 430 | 300 |
| DOC / nm / Seat | $0.56 | $ 0.59 |
| Max Cabin Seats | 6 | — |
| OEM Verification | Un-Verified | Un-Verified |
| Standard Cabin Seats | 6 | — |
| Direct Operating Cost | $627 | $ 257 |
| Flight Deck (Base Spec) | EFIS | Gyro / Analog |
| Max Cruise Speed (ktas) | 140 | 109 |
| Base Aircraft Price (USD) | $3,500,000 | $ 490,000 |
| Useful Load (lbs) | — | 995 |
| Cabin | ||
| Cockpit | 2 | — |
| Min Crew | 1 | — |
| Total Seats | 8 | 4 |
| Standard Cabin Seats | 6 | — |
| Engine | ||
| FADEC | Yes | No |
| Model | HTS 900 | IO-540 |
| Fuel Type | JetFuel | AvGas |
| TBO (hrs) | 5500 | 2200 |
| Horsepower | 1020 | 245 |
| No. of Engines | 1 | 1 |
| TBO (yrs) | — | 12 |
| Fuel Delivery | — | Fuel Injected |
| Fuel Capacity (gal) | — | 29.5 |
| Dimensions | ||
| Length (ft) | — | 38.3 |
| Overall Height (ft) | — | 10.8 |
| Rotor Diameter (ft) | — | 33 |
| Baggage Volume Int. (cu. ft) | — | 2.5 |