Airbus Helicopters H225 vs Beechcraft King Air 360 Er vs Cessna Citation Xls vs Leonardo Aw189
The Airbus H225 and Leonardo AW189 are large twin‑engine helicopters, best suited to offshore, SAR, and utility roles where vertical access matters. They typically carry around 16–19 passengers in high‑density layouts (often fewer for comfort or mission equipment) and offer practical ranges roughly in the 450–600+ nautical mile class depending on payload and tanks. The Beechcraft King Air 360ER is a pressurized twin‑turboprop fixed‑wing aircraft optimized for regional and special‑mission flying. It usually seats about 8–11 passengers in executive configurations and is valued for long endurance, with range commonly around 1,500–1,800 nautical miles. The Cessna Citation XLS+ is a midsize business jet focused on faster point‑to‑point travel. Typical seating is about 7–9 passengers (up to roughly 12 in higher‑density layouts), with range generally around 2,000 nautical miles, making it the longest‑range option here for nonstop city‑pair travel.
| Spec | AIRBUS H225 | Cessna Citation XLS+ | AGUSTA / LEONARDO AW189 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 5.34 | $ 15.57 |
| Min Crew | 2 | 2 | 1 |
| Total Seats | 21 | 10 | 21 |
| Flight Rules | IFR | — | IFR |
| Manufacturer | Airbus Helicopters | Cessna Citation | Leonardo |
| Aircraft Name | H225 | XLS+ | AW189 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 1906 | 651 |
| DOC / nm / Seat | $ 0.99 | $ 0.67 | $ 0.74 |
| Max Cabin Seats | 28 | 9 | 19 |
| OEM Verification | Un-Verified | VERIFIED | Un-Verified |
| Useful Load (lbs) | 11929 | 7540 | — |
| Standard Cabin Seats | 19 | 8 | 19 |
| Direct Operating Cost | $ 2,963 | $ 2,303 | $ 2,413 |
| Flight Deck (Base Spec) | EFIS | Rockwell Collins Pro Line 21 | EFIS |
| Max Cruise Speed (ktas) | 142 | 430 | 155 |
| Base Aircraft Price (USD) | $ 29,500,000 | $15,500,000 | $2,413,000 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 1 |
| Total Seats | 21 | 10 | 21 |
| Max Cabin Seats | 28 | 9 | 19 |
| Standard Cabin Seats | 19 | 8 | 19 |
| Lavatory | — | 1 Enclosed Belted Flushing | — |
| Crew Rest | — | No | — |
| Jump Seat | — | No | — |
| Galley Location | — | FWD | — |
| Lavatory Location | — | AFT | — |
| Cabin Pressure (psi) | — | 9.3 | — |
| Galley / Refreshment | — | Galley | — |
| SL Cabin Altitude (ft) | — | 25230 | — |
| Engine | |||
| FADEC | Yes | Yes | Yes |
| Model | Makila 2A1 | PW545C | CT7-2E1 |
| Fuel Type | JetFuel | — | JetFuel |
| TBO (hrs) | 3500 | 5000 | 4000 |
| Horsepower | 2100 | — | 1983 |
| No. of Engines | 2 | 2 | 2 |
| Fuel Capacity (gal) | 684 | — | — |
| Flat Rating | — | ISA + 10 | — |
| Thrust (lbs) | — | 4119 | — |
| Dimensions | |||
| Length (ft) | 63.4 | 52.5 | 57.8 |
| Overall Height (ft) | 16.3 | 17.2 | 16.6 |
| Rotor Diameter (ft) | 53.2 | — | 48 |
| Cabin Volume (cu. ft) | 547 | — | 395 |
| Wingspan (ft) | — | 56.3 | — |
| Aisle Step (ft) | — | 0.7 | — |
| Cabin Width (ft) | — | 5.5 | — |
| Cabin Height (ft) | — | 5.7 | — |
| Cabin Length (ft) | — | 18.5 | — |
| Cabin Width - Floor (ft) | — | 3.9 | — |
| Cabin Length - Seating (ft) | — | 14.3 | — |
| Baggage Volume Ext. (cu. ft) | — | 80 | 85 |
| Baggage Volume Int. (cu. ft) | — | 10 | — |