Airbus Helicopters H225 vs Cessna Citation Xls vs Dassault Falcon 8x
The Airbus H225 is a twin‑engine, long‑range helicopter typically used for offshore transport, search and rescue, and utility missions rather than point‑to‑point business travel. Its practical range is roughly 500–700 nautical miles depending on payload and reserves, and it commonly carries about 16–19 passengers in typical transport seating (higher in dense configurations). The Cessna Citation XLS+ is a midsize business jet optimized for short to medium routes and frequent airport access, offering about 1,800–2,100 nautical miles of range and usually seating 7–9 passengers in executive layouts. The Dassault Falcon 8X is an ultra‑long‑range, large‑cabin business jet designed for intercontinental missions, with around 6,400 nautical miles of range and typically accommodating 12–16 passengers in spacious cabin configurations. In short, the H225 prioritizes vertical lift and mission flexibility with shorter range, the XLS+ balances efficiency and cabin comfort for regional missions, and the Falcon 8X delivers the longest range and the largest long‑haul business‑jet capability.
| Spec | AIRBUS H225 | Cessna Citation XLS+ | Dassault Falcon 8X |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 5.34 | $ 7.66 |
| Min Crew | 2 | 2 | 2 |
| Total Seats | 21 | 10 | 17 |
| Flight Rules | IFR | — | — |
| Manufacturer | Airbus Helicopters | Cessna Citation | Dassault Falcon |
| Aircraft Name | H225 | XLS+ | 8X |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 1906 | 6450 |
| DOC / nm / Seat | $ 0.99 | $ 0.67 | $ 0.64 |
| Max Cabin Seats | 28 | 9 | 16 |
| OEM Verification | Un-Verified | VERIFIED | VERIFIED |
| Useful Load (lbs) | 11929 | 7540 | 36900 |
| Standard Cabin Seats | 19 | 8 | 14 |
| Direct Operating Cost | $ 2,963 | $ 2,303 | $ 3,805 |
| Flight Deck (Base Spec) | EFIS | Rockwell Collins Pro Line 21 | Honeywell Primus EASy II |
| Max Cruise Speed (ktas) | 142 | 430 | 516 |
| Base Aircraft Price (USD) | $ 29,500,000 | $15,500,000 | $ 62,500,000 |
| Cabin | |||
| Cockpit | 2 | 2 | 3 |
| Min Crew | 2 | 2 | 2 |
| Total Seats | 21 | 10 | 17 |
| Max Cabin Seats | 28 | 9 | 16 |
| Standard Cabin Seats | 19 | 8 | 14 |
| Lavatory | — | 1 Enclosed Belted Flushing | 2 Enclosed Flushing |
| Crew Rest | — | No | No |
| Jump Seat | — | No | Yes |
| Galley Location | — | FWD | FWD |
| Lavatory Location | — | AFT | FWD / AFT |
| Cabin Pressure (psi) | — | 9.3 | 10.2 |
| Galley / Refreshment | — | Galley | Galley |
| SL Cabin Altitude (ft) | — | 25230 | 29200 |
| Max Cabin Altitude (ft) | — | — | 3900 |
| Engine | |||
| FADEC | Yes | Yes | Yes |
| Model | Makila 2A1 | PW545C | PW307D |
| Fuel Type | JetFuel | — | — |
| TBO (hrs) | 3500 | 5000 | On-Condition |
| Horsepower | 2100 | — | — |
| No. of Engines | 2 | 2 | 3 |
| Fuel Capacity (gal) | 684 | — | — |
| Flat Rating | — | ISA + 10 | ISA + 17 |
| Thrust (lbs) | — | 4119 | 6722 |
| Dimensions | |||
| Length (ft) | 63.4 | 52.5 | 80.2 |
| Overall Height (ft) | 16.3 | 17.2 | 26.1 |
| Rotor Diameter (ft) | 53.2 | — | — |
| Cabin Volume (cu. ft) | 547 | — | 1695 |
| Wingspan (ft) | — | 56.3 | 86.3 |
| Aisle Step (ft) | — | 0.7 | — |
| Cabin Width (ft) | — | 5.5 | 7.7 |
| Cabin Height (ft) | — | 5.7 | 6.2 |
| Cabin Length (ft) | — | 18.5 | 42.7 |
| Cabin Width - Floor (ft) | — | 3.9 | 6.3 |
| Cabin Length - Seating (ft) | — | 14.3 | 29.2 |
| Baggage Volume Ext. (cu. ft) | — | 80 | — |
| Baggage Volume Int. (cu. ft) | — | 10 | 140 |