Airbus Helicopters H225 vs Cessna Citation Xls vs Leonardo Aw189
The Airbus H225 and Leonardo AW189 are twin‑engine helicopters, while the Cessna Citation XLS+ is a light business jet, so their strengths differ sharply. In category, the H225 is a heavy, long‑range utility helicopter optimized for offshore transport, SAR, and high payload operations; the AW189 sits a step lower as a super‑medium helicopter aimed at similar missions with slightly smaller overall capacity and footprint. The Citation XLS+ is designed for fast point‑to‑point executive travel from airports, prioritizing speed, altitude, and cabin comfort over vertical lift. In range, the Citation XLS+ typically offers the greatest cruise range, on the order of roughly 2,000 nautical miles depending on reserves and payload, making it best for longer nonstop city pairs. The H225 and AW189 generally deliver helicopter ranges in the several‑hundred‑nautical‑mile class, commonly around 400–500 nautical miles depending on configuration. For passenger capacity, the H225 is usually configured for the most seats, often up to about 19, the AW189 commonly up to about 16–19, and the Citation XLS+ typically carries about 8–9 passengers in executive layout.
| 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 | — |