Leonardo Aw139 vs Leonardo Aw609 Tiltrotor
The Leonardo AW139 is a conventional twin‑engine, medium helicopter typically used for offshore transport, EMS, SAR, and utility missions. In category terms it is a rotorcraft optimized for vertical lift, hovering, and low‑speed maneuvering, with straightforward operation from helipads and confined areas. The Leonardo AW609 is a twin‑engine tiltrotor, bridging helicopter and fixed‑wing capability by rotating its nacelles for vertical takeoff and landing, then cruising like a turboprop airplane; it is aimed at faster point‑to‑point transport over longer legs while still using vertiports and helipads. On range, the AW139 generally offers moderate helicopter-range suitable for regional missions, while the AW609 is designed for substantially longer range because it transitions to efficient wing-borne flight in cruise. On passenger capacity, the AW139 commonly carries more people in typical transport configurations, whereas the AW609 usually seats fewer passengers in a pressurized cabin focused on speed and range rather than maximum cabin volume.
| Spec | AGUSTA / LEONARDO AW139 | AGUSTA / LEONARDO AW609 Tiltrotor |
|---|---|---|
| Summary | ||
| Cockpit | 2 | — |
| DOC / nm | $ 11.69 | — |
| Min Crew | 2 | — |
| Total Seats | 17 | — |
| Flight Rules | IFR | — |
| Manufacturer | Leonardo | Leonardo |
| Aircraft Name | AW139 | AW609 Tiltrotor |
| Certification | FAA / EASA | — |
| Max Range (nm) | 573 | — |
| DOC / nm / Seat | $ 0.69 | — |
| Max Cabin Seats | 15 | — |
| OEM Verification | Un-Verified | — |
| Useful Load (lbs) | 4701 | — |
| Standard Cabin Seats | 15 | — |
| Direct Operating Cost | $ 1,929 | — |
| Flight Deck (Base Spec) | EFIS | — |
| Max Cruise Speed (ktas) | 165 | — |
| Base Aircraft Price (USD) | $15,900,000 | $20,000,000 |
| Cabin | ||
| Cockpit | 2 | — |
| Min Crew | 2 | — |
| Total Seats | 17 | — |
| Max Cabin Seats | 15 | — |
| Standard Cabin Seats | 15 | — |
| Engine | ||
| FADEC | Yes | — |
| Model | PT6C-67C | — |
| Fuel Type | JetFuel | — |
| TBO (hrs) | 5000 | — |
| Horsepower | 1679 | — |
| No. of Engines | 2 | — |
| Fuel Capacity (gal) | 414 | — |
| Dimensions | ||
| Length (ft) | 54.7 | — |
| Overall Height (ft) | 16.4 | — |
| Rotor Diameter (ft) | 54.7 | — |
| Cabin Volume (cu. ft) | 282 | — |
| Baggage Volume Ext. (cu. ft) | 120 | — |