Airbus Helicopters H225 vs Beechcraft King Air 360 Er vs Leonardo Aw189 vs Pilatus Pc 24
The Airbus H225 and Leonardo AW189 are twin‑engine helicopters optimized for vertical lift missions such as offshore transport and SAR; they trade speed and long-range efficiency for the ability to operate without runways. Typical range is roughly 450–600 nautical miles depending on payload and reserves. In passenger configuration, both commonly carry about 16–19 passengers, with the H225 generally at the higher end in cabin volume and maximum seating. The Beechcraft King Air 360ER is a twin‑turboprop fixed‑wing aircraft focused on efficient regional and special‑mission flying. It offers substantially longer range than the helicopters, typically around 1,500–1,800 nautical miles, with a typical passenger load of about 6–9 in executive layouts (higher in commuter or mission configurations). The Pilatus PC‑24 is a twin‑jet designed for fast point‑to‑point travel and short/rough-field capability. It generally carries about 6–10 passengers and offers range roughly in the 1,700–2,000 nautical mile class, combining jet speed with more flexible airport access than many light jets.
| Spec | AIRBUS H225 | AGUSTA / LEONARDO AW189 | Pilatus PC-24 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 15.57 | $ 3.71 |
| Min Crew | 2 | 1 | 1 |
| Total Seats | 21 | 21 | 6 |
| Flight Rules | IFR | IFR | — |
| Manufacturer | Airbus Helicopters | Leonardo | Pilatus |
| Aircraft Name | H225 | AW189 | PC-24 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 651 | 2076 |
| DOC / nm / Seat | $ 0.99 | $ 0.74 | $ 0.62 |
| Max Cabin Seats | 28 | 19 | 10 |
| OEM Verification | Un-Verified | Un-Verified | VERIFIED |
| Useful Load (lbs) | 11929 | — | 6680 |
| Standard Cabin Seats | 19 | 19 | 6 |
| Direct Operating Cost | $ 2,963 | $ 2,413 | $ 1,619 |
| Flight Deck (Base Spec) | EFIS | EFIS | Pilatus ACE (Primus Apex) |
| Max Cruise Speed (ktas) | 142 | 155 | 440 |
| Base Aircraft Price (USD) | $ 29,500,000 | $2,413,000 | $11,800,000 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 1 | 1 |
| Total Seats | 21 | 21 | 6 |
| Max Cabin Seats | 28 | 19 | 10 |
| Standard Cabin Seats | 19 | 19 | 6 |
| Lavatory | — | — | 1 Enclosed Flushing |
| Crew Rest | — | — | No |
| Jump Seat | — | — | No |
| Cargo Door | — | — | Yes |
| Galley Location | — | — | FWD |
| Lavatory Location | — | — | FWD |
| Cabin Pressure (psi) | — | — | 9.3 |
| Galley / Refreshment | — | — | Optional Refreshment Center |
| SL Cabin Altitude (ft) | — | — | 23500 |
| Engine | |||
| FADEC | Yes | Yes | Yes |
| Model | Makila 2A1 | CT7-2E1 | FJ44-4A-QPM |
| Fuel Type | JetFuel | JetFuel | — |
| TBO (hrs) | 3500 | 4000 | 5000 |
| Horsepower | 2100 | 1983 | — |
| No. of Engines | 2 | 2 | 2 |
| Fuel Capacity (gal) | 684 | — | — |
| Flat Rating | — | — | ISA + 23 |
| Thrust (lbs) | — | — | 3435 |
| Dimensions | |||
| Length (ft) | 63.4 | 57.8 | 52.2 |
| Overall Height (ft) | 16.3 | 16.6 | 17.4 |
| Rotor Diameter (ft) | 53.2 | 48 | — |
| Cabin Volume (cu. ft) | 547 | 395 | — |
| Baggage Volume Ext. (cu. ft) | — | 85 | — |
| Wingspan (ft) | — | — | 55.8 |
| Aisle Step (ft) | — | — | Flat Floor |
| Cabin Width (ft) | — | — | 5.6 |
| Cabin Height (ft) | — | — | 5.1 |
| Cabin Length (ft) | — | — | 23 |
| Cabin Width - Floor (ft) | — | — | 3.8 |
| Cabin Length - Seating (ft) | — | — | 17 |
| Baggage Volume Int. (cu. ft) | — | — | 90 |