Airbus Helicopters H225 vs Cessna Citation Xls vs Gulfstream G700 vs Leonardo Aw189
The Airbus H225 and Leonardo AW189 are large twin‑engine helicopters, while the Cessna Citation XLS+ is a midsize business jet and the Gulfstream G700 is an ultra‑long‑range large‑cabin business jet. In category and mission, the H225 and AW189 excel at vertical lift for offshore transport, SAR, and utility roles; the Citation XLS+ focuses on efficient regional point‑to‑point travel; and the G700 targets intercontinental nonstop capability with maximum cabin comfort. For range, the helicopters are shortest, generally a few hundred nautical miles depending on payload and reserves, with the H225 typically edging the AW189 in maximum range. The Citation XLS+ sits well above both helicopters, offering roughly 2,000 nautical miles class range, suitable for many domestic or short transatlantic-style legs with favorable winds and payload. The G700 is far ahead, around 7,000+ nautical miles, enabling nonstop city pairs like New York–Tokyo in the right conditions. Passenger capacity also separates them: AW189 typically carries around 16–19, H225 often 19+ in transport layouts, the XLS+ usually seats about 8–12, and the G700 commonly 13–19 depending on configuration.
| Spec | AIRBUS H225 | Cessna Citation XLS+ | Gulfstream G700 | AGUSTA / LEONARDO AW189 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 3 | 2 |
| DOC / nm | $ 20.87 | $ 5.34 | — | $ 15.57 |
| Min Crew | 2 | 2 | 4 | 1 |
| Total Seats | 21 | 10 | 16 | 21 |
| Flight Rules | IFR | — | — | IFR |
| Manufacturer | Airbus Helicopters | Cessna Citation | Gulfstream | Leonardo |
| Aircraft Name | H225 | XLS+ | G700 | AW189 |
| Certification | FAA / EASA | FAA / EASA | In Development | FAA / EASA |
| Max Range (nm) | 454 | 1906 | 7500 | 651 |
| DOC / nm / Seat | $ 0.99 | $ 0.67 | — | $ 0.74 |
| Max Cabin Seats | 28 | 9 | 19 | 19 |
| OEM Verification | Un-Verified | VERIFIED | Un-Verified | Un-Verified |
| Useful Load (lbs) | 11929 | 7540 | — | — |
| Standard Cabin Seats | 19 | 8 | 12 | 19 |
| Direct Operating Cost | $ 2,963 | $ 2,303 | — | $ 2,413 |
| Flight Deck (Base Spec) | EFIS | Rockwell Collins Pro Line 21 | Gulfstream Symmetry Flight Deck | EFIS |
| Max Cruise Speed (ktas) | 142 | 430 | 516 | 155 |
| Base Aircraft Price (USD) | $ 29,500,000 | $15,500,000 | $78,000,000 | $2,413,000 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 4 | 1 |
| Total Seats | 21 | 10 | 16 | 21 |
| Max Cabin Seats | 28 | 9 | 19 | 19 |
| Standard Cabin Seats | 19 | 8 | 12 | 19 |
| Lavatory | — | 1 Enclosed Belted Flushing | — | — |
| Crew Rest | — | No | Optional | — |
| Jump Seat | — | No | Yes | — |
| Galley Location | — | FWD | FWD | — |
| Lavatory Location | — | AFT | FWD / AFT | — |
| Cabin Pressure (psi) | — | 9.3 | — | — |
| Galley / Refreshment | — | Galley | — | — |
| SL Cabin Altitude (ft) | — | 25230 | — | — |
| Engine | ||||
| FADEC | Yes | Yes | — | Yes |
| Model | Makila 2A1 | PW545C | Pearl 700 | CT7-2E1 |
| Fuel Type | JetFuel | — | — | JetFuel |
| TBO (hrs) | 3500 | 5000 | On Condition | 4000 |
| Horsepower | 2100 | — | — | 1983 |
| No. of Engines | 2 | 2 | 2 | 2 |
| Fuel Capacity (gal) | 684 | — | — | — |
| Flat Rating | — | ISA + 10 | — | — |
| Thrust (lbs) | — | 4119 | 18250 | — |
| Dimensions | ||||
| Length (ft) | 63.4 | 52.5 | 109.9 | 57.8 |
| Overall Height (ft) | 16.3 | 17.2 | 25.4 | 16.6 |
| Rotor Diameter (ft) | 53.2 | — | — | 48 |
| Cabin Volume (cu. ft) | 547 | — | — | 395 |
| Wingspan (ft) | — | 56.3 | 103 | — |
| Aisle Step (ft) | — | 0.7 | Flat Floor | — |
| Cabin Width (ft) | — | 5.5 | 8.2 | — |
| Cabin Height (ft) | — | 5.7 | 6.25 | — |
| Cabin Length (ft) | — | 18.5 | 56.9 | — |
| 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 | 195 | — |