Airbus Helicopters H225 vs Cessna 208b Grand Caravan Ex vs Cessna Citation Xls vs Leonardo Aw189
The Airbus H225 and the Agusta/Leonardo AW189 are large, twin‑engine helicopters aimed at offshore, SAR, and utility missions, while the Cessna 208B Grand Caravan EX is a single‑engine turboprop utility airplane optimized for rugged, short‑field regional transport, and the Cessna Citation XLS+ is a midsize business jet focused on fast point‑to‑point travel. In range terms, the Citation XLS+ typically goes the farthest, commonly around 2,000 nautical miles class depending on payload and reserves. The Grand Caravan EX is next, generally in the 900–1,000 nautical miles class. The H225 and AW189 usually sit below that on typical mission profiles, often in the ~450–550 nautical miles class, though exact figures vary widely with fuel fit, winds, and payload. For passenger capacity, the H225 is generally the largest, commonly configured around the high‑teens to low‑20s. The AW189 is slightly smaller, often in the mid‑teens. The Grand Caravan EX typically seats up to about 9 passengers in standard commuter configurations, while the Citation XLS+ usually seats about 8–9 in a typical 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 | — |