Airbus Helicopters H225 vs Cessna 208b Grand Caravan Ex vs Leonardo Aw189 vs Piaggio Avanti Evo
The Airbus H225 and Leonardo AW189 are large, twin‑engine helicopters aimed at offshore, SAR, and utility missions. Both trade speed and range for vertical lift; typical passenger capacity is about 16–19, with practical ranges commonly around 400–500 nautical miles depending on payload and reserves. The AW189 is slightly smaller and is often configured around 16–18 passengers, while the H225 can be set up toward the higher end and supports heavier lifting. The Cessna 208B Grand Caravan EX is a single‑engine turboprop airplane optimized for rugged short‑field operations and low operating cost. It typically seats 9–14 passengers and offers longer point‑to‑point range than the helicopters, commonly around 800–900 nautical miles, but it requires a runway. The Piaggio Avanti EVO is a pressurized twin‑turboprop business aircraft focused on speed and efficiency. It usually carries 6–9 passengers and has the longest range of this group, roughly 1,000–1,700 nautical miles depending on configuration, while cruising much faster than the Caravan and far faster than either helicopter.
| Spec | AIRBUS H225 | AGUSTA / LEONARDO AW189 | Piaggio Avanti EVO |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 15.57 | — |
| Min Crew | 2 | 1 | 1 |
| Total Seats | 21 | 21 | 8 |
| Flight Rules | IFR | IFR | IFR |
| Manufacturer | Airbus Helicopters | Leonardo | Piaggio |
| Aircraft Name | H225 | AW189 | Avanti EVO |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 651 | 1530 |
| DOC / nm / Seat | $ 0.99 | $ 0.74 | — |
| Max Cabin Seats | 28 | 19 | 7 |
| OEM Verification | Un-Verified | Un-Verified | Un-Verified |
| Useful Load (lbs) | 11929 | — | 3775 |
| Standard Cabin Seats | 19 | 19 | 6 |
| Direct Operating Cost | $ 2,963 | $ 2,413 | — |
| Flight Deck (Base Spec) | EFIS | EFIS | Rockwell Collins Pro Line 21 |
| Max Cruise Speed (ktas) | 142 | 155 | 400 |
| Base Aircraft Price (USD) | $ 29,500,000 | $2,413,000 | $ 7,695,000 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 1 | 1 |
| Total Seats | 21 | 21 | 8 |
| Max Cabin Seats | 28 | 19 | 7 |
| Standard Cabin Seats | 19 | 19 | 6 |
| Lavatory | — | — | No |
| Cabin Pressure (psi) | — | — | 9 |
| Galley / Refreshment | — | — | No |
| SL Cabin Altitude (ft) | — | — | 24000 |
| Max Cabin Altitude (ft) | — | — | 6600 |
| Engine | |||
| FADEC | Yes | Yes | Yes |
| Model | Makila 2A1 | CT7-2E1 | PT6A–66B |
| Fuel Type | JetFuel | JetFuel | — |
| TBO (hrs) | 3500 | 4000 | 3600 |
| Horsepower | 2100 | 1983 | 850 |
| No. of Engines | 2 | 2 | 2 |
| Fuel Capacity (gal) | 684 | — | — |
| Flat Rating | — | — | ISA + 28 |
| Fuel Burn (gph) | — | — | 100 |
| Dimensions | |||
| Length (ft) | 63.4 | 57.8 | 47.3 |
| Overall Height (ft) | 16.3 | 16.6 | 13.1 |
| Rotor Diameter (ft) | 53.2 | 48 | — |
| Cabin Volume (cu. ft) | 547 | 395 | — |
| Baggage Volume Ext. (cu. ft) | — | 85 | — |
| Wingspan (ft) | — | — | 47.1 |
| Cabin Width (ft) | — | — | 6.1 |
| Cabin Height (ft) | — | — | 5.8 |
| Cabin Length (ft) | — | — | 14.9 |
| Cabin Width - Floor (ft) | — | — | 3.5 |
| Baggage Volume Int. (cu. ft) | — | — | 35.2 |