Airbus Helicopters H225 vs Cessna Citation Xls vs Dassault Falcon 8x vs Embraer Legacy 650 E
The Airbus H225 is a large twin‑engine helicopter suited to offshore and utility missions rather than long‑range fixed‑wing travel. It typically carries around 16–19 passengers in transport layouts, with practical range on the order of roughly 400–500 nautical miles depending on payload and reserves. The Cessna Citation XLS+ is a midsize business jet optimized for short‑to‑medium trips and frequent hops. It generally seats about 7–9 passengers in a typical executive cabin and offers range around 2,000 nautical miles. The Embraer Legacy 650E is a large‑cabin business jet aimed at longer nonstop missions with more space. It commonly accommodates about 13 passengers (often up to 14) and has range in the ~3,900 nautical mile class. The Dassault Falcon 8X is an ultra‑long‑range flagship with the greatest reach of the group, typically seating about 12–16 passengers depending on configuration, and offering roughly 6,400 nautical miles of range, enabling intercontinental nonstop city pairs.
| 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 |