Airbus Helicopters H225 vs Beechcraft King Air 360 Er vs Embraer Legacy 650 E vs Leonardo Aw189
The Airbus H225 and Leonardo AW189 are large twin‑engine helicopters suited to offshore, SAR, and utility missions, trading speed and range for vertical lift and access to confined sites. The H225 typically offers longer legs for a helicopter, often around 450–600 nautical miles depending on fit, and can carry roughly 16–19 passengers in high‑density seating (fewer in VIP). The AW189 is in a similar class but generally a bit smaller in capacity, commonly around 12–16 passengers, with range often in the 400–500 nautical mile band. The Beechcraft King Air 360ER is a pressurized twin‑turboprop airplane optimized for efficiency and short/remote runways. It usually seats about 6–9 passengers in executive layouts and has long endurance, with range commonly around 1,500–2,000+ nautical miles depending on payload and reserves. The Embraer Legacy 650E is a long‑range business jet, fastest and highest‑flying of the group, typically carrying about 10–13 passengers with range around 3,700–3,900 nautical miles, making it best for intercontinental missions.
| Spec | AIRBUS H225 | AGUSTA / LEONARDO AW189 |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| DOC / nm | $ 20.87 | $ 15.57 |
| Min Crew | 2 | 1 |
| Total Seats | 21 | 21 |
| Flight Rules | IFR | IFR |
| Manufacturer | Airbus Helicopters | Leonardo |
| Aircraft Name | H225 | AW189 |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 651 |
| DOC / nm / Seat | $ 0.99 | $ 0.74 |
| Max Cabin Seats | 28 | 19 |
| OEM Verification | Un-Verified | Un-Verified |
| Useful Load (lbs) | 11929 | — |
| Standard Cabin Seats | 19 | 19 |
| Direct Operating Cost | $ 2,963 | $ 2,413 |
| Flight Deck (Base Spec) | EFIS | EFIS |
| Max Cruise Speed (ktas) | 142 | 155 |
| Base Aircraft Price (USD) | $ 29,500,000 | $2,413,000 |
| Cabin | ||
| Cockpit | 2 | 2 |
| Min Crew | 2 | 1 |
| Total Seats | 21 | 21 |
| Max Cabin Seats | 28 | 19 |
| Standard Cabin Seats | 19 | 19 |
| Engine | ||
| FADEC | Yes | Yes |
| Model | Makila 2A1 | CT7-2E1 |
| Fuel Type | JetFuel | JetFuel |
| TBO (hrs) | 3500 | 4000 |
| Horsepower | 2100 | 1983 |
| No. of Engines | 2 | 2 |
| Fuel Capacity (gal) | 684 | — |
| Dimensions | ||
| Length (ft) | 63.4 | 57.8 |
| Overall Height (ft) | 16.3 | 16.6 |
| Rotor Diameter (ft) | 53.2 | 48 |
| Cabin Volume (cu. ft) | 547 | 395 |
| Baggage Volume Ext. (cu. ft) | — | 85 |