Airbus Helicopters H225 vs Bombardier Global 7500 vs Cessna Citation Xls vs Leonardo Aw189
The Airbus H225 and Leonardo AW189 are twin‑engine helicopters designed for offshore transport, SAR, and utility missions, trading speed and range for vertical lift and flexible access. The H225 is the larger, higher‑capacity option, typically carrying around 16–19 passengers (high‑density configurations can be more) with a practical range on the order of roughly 450–600 nautical miles depending on payload and reserves. The AW189 is slightly smaller, commonly configured for about 12–16 passengers, with a similar but often somewhat shorter practical range, roughly 400–500 nautical miles. The Bombardier Global 7500 is an ultra‑long‑range business jet optimized for intercontinental travel, typically seating about 14–19 passengers in executive layouts, with a published range around 7,700 nautical miles. The Cessna Citation XLS+ is a midsize business jet aimed at shorter missions and airport flexibility, typically seating about 7–9 passengers, with a range around 2,100 nautical miles. Overall, the jets dominate in range and cruise speed, while the helicopters dominate in access and mission versatility.
| Spec | AIRBUS H225 | Bombardier Global 7500 | Cessna Citation XLS+ | AGUSTA / LEONARDO AW189 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 9.50 | $ 5.34 | $ 15.57 |
| Min Crew | 2 | 2 | 2 | 1 |
| Total Seats | 21 | 14 | 10 | 21 |
| Flight Rules | IFR | — | — | IFR |
| Manufacturer | Airbus Helicopters | Bombardier | Cessna Citation | Leonardo |
| Aircraft Name | H225 | Global 7500 | XLS+ | AW189 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 7700 | 1906 | 651 |
| DOC / nm / Seat | $ 0.99 | $ 0.79 | $ 0.67 | $ 0.74 |
| Max Cabin Seats | 28 | 19 | 9 | 19 |
| OEM Verification | Un-Verified | VERIFIED | VERIFIED | Un-Verified |
| Useful Load (lbs) | 11929 | — | 7540 | — |
| Standard Cabin Seats | 19 | 12 | 8 | 19 |
| Direct Operating Cost | $ 2,963 | $ 4,900 | $ 2,303 | $ 2,413 |
| Flight Deck (Base Spec) | EFIS | Bombardier Vision (Pro Line Fusion) | Rockwell Collins Pro Line 21 | EFIS |
| Max Cruise Speed (ktas) | 142 | 516 | 430 | 155 |
| Base Aircraft Price (USD) | $ 29,500,000 | $75,000,000 | $15,500,000 | $2,413,000 |
| Aircraft Type | — | Business Jet | — | — |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 2 | 1 |
| Total Seats | 21 | 14 | 10 | 21 |
| Max Cabin Seats | 28 | 19 | 9 | 19 |
| Standard Cabin Seats | 19 | 12 | 8 | 19 |
| Lavatory | — | 2 Enclosed Flushing | 1 Enclosed Belted Flushing | — |
| Crew Rest | — | Yes | No | — |
| Jump Seat | — | Yes | No | — |
| Galley Location | — | FWD | FWD | — |
| Lavatory Location | — | FWD / AFT | AFT | — |
| Galley / Refreshment | — | Galley | Galley | — |
| Max Cabin Altitude (ft) | — | 4500 | — | — |
| Cabin Pressure (psi) | — | — | 9.3 | — |
| SL Cabin Altitude (ft) | — | — | 25230 | — |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | Makila 2A1 | Passport | PW545C | CT7-2E1 |
| Fuel Type | JetFuel | — | — | JetFuel |
| TBO (hrs) | 3500 | On-Condition | 5000 | 4000 |
| Horsepower | 2100 | — | — | 1983 |
| No. of Engines | 2 | 2 | 2 | 2 |
| Fuel Capacity (gal) | 684 | — | — | — |
| Flat Rating | — | ISA + 15 | ISA + 10 | — |
| Thrust (lbs) | — | 18920 | 4119 | — |
| Dimensions | ||||
| Length (ft) | 63.4 | 111 | 52.5 | 57.8 |
| Overall Height (ft) | 16.3 | 27 | 17.2 | 16.6 |
| Rotor Diameter (ft) | 53.2 | — | — | 48 |
| Cabin Volume (cu. ft) | 547 | — | — | 395 |
| Wingspan (ft) | — | 104 | 56.3 | — |
| Cabin Width (ft) | — | 8 | 5.5 | — |
| Cabin Height (ft) | — | 6.2 | 5.7 | — |
| Cabin Length (ft) | — | 54.5 | 18.5 | — |
| Aisle Step (ft) | — | — | 0.7 | — |
| 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 | — |