Airbus Helicopters H225 vs Beechcraft King Air 360 Er vs Cessna 208b Grand Caravan Ex vs Leonardo Aw189
The Airbus H225 and Leonardo AW189 are medium twin‑engine helicopters optimized for offshore transport and SAR-style missions, with typical ranges around 450–550 nautical miles depending on configuration and reserves. Passenger capacity is generally in the mid‑teens: the AW189 is commonly arranged for about 16–19 passengers, while the H225 is often configured around 16–19 and can be higher in dense seating layouts. The Beechcraft King Air 360ER is a pressurized twin‑turboprop fixed‑wing aircraft aimed at long-range utility and executive roles. It offers substantially greater range than the helicopters—typically on the order of 1,500–2,000+ nautical miles depending on payload and fuel—and usually carries about 6–9 passengers in executive configurations, with higher-capacity commuter layouts possible by operator choice. The Cessna 208B Grand Caravan EX is a single‑engine turboprop fixed‑wing utility aircraft focused on rugged, short‑field operations. It generally carries about 9–14 passengers and typically ranges around 800–1,000+ nautical miles, varying with load, speed, and reserves.
| 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 |