Airbus Helicopters H225 vs Bombardier Global 7500 vs Cessna Citation Xls vs Dassault Falcon 8x
The Airbus H225 is a heavy twin‑engine helicopter rather than a fixed‑wing business jet. It is typically used for offshore, utility, and government missions, carries roughly 16–19 passengers depending on layout, and has a much shorter range than the jets, on the order of a few hundred nautical miles in typical passenger configurations. The Cessna Citation XLS+ is a midsize business jet designed for shorter regional missions. It commonly seats about 8–9 passengers and offers a range around 2,000 nautical miles, making it suitable for city pairs within a continent. The Dassault Falcon 8X is an ultra‑long‑range large‑cabin business jet. It typically carries about 12–16 passengers and can fly roughly 6,400 nautical miles, emphasizing comfort, runway flexibility, and long nonstop legs. The Bombardier Global 7500 is a flagship long‑range large‑cabin jet, generally accommodating about 14–19 passengers depending on configuration, with a range around 7,700 nautical miles, aimed at the longest nonstop intercontinental missions.
| Spec | AIRBUS H225 | Bombardier Global 7500 | Cessna Citation XLS+ | Dassault Falcon 8X |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 9.50 | $ 5.34 | $ 7.66 |
| Min Crew | 2 | 2 | 2 | 2 |
| Total Seats | 21 | 14 | 10 | 17 |
| Flight Rules | IFR | — | — | — |
| Manufacturer | Airbus Helicopters | Bombardier | Cessna Citation | Dassault Falcon |
| Aircraft Name | H225 | Global 7500 | XLS+ | 8X |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 7700 | 1906 | 6450 |
| DOC / nm / Seat | $ 0.99 | $ 0.79 | $ 0.67 | $ 0.64 |
| Max Cabin Seats | 28 | 19 | 9 | 16 |
| OEM Verification | Un-Verified | VERIFIED | VERIFIED | VERIFIED |
| Useful Load (lbs) | 11929 | — | 7540 | 36900 |
| Standard Cabin Seats | 19 | 12 | 8 | 14 |
| Direct Operating Cost | $ 2,963 | $ 4,900 | $ 2,303 | $ 3,805 |
| Flight Deck (Base Spec) | EFIS | Bombardier Vision (Pro Line Fusion) | Rockwell Collins Pro Line 21 | Honeywell Primus EASy II |
| Max Cruise Speed (ktas) | 142 | 516 | 430 | 516 |
| Base Aircraft Price (USD) | $ 29,500,000 | $75,000,000 | $15,500,000 | $ 62,500,000 |
| Aircraft Type | — | Business Jet | — | — |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 3 |
| Min Crew | 2 | 2 | 2 | 2 |
| Total Seats | 21 | 14 | 10 | 17 |
| Max Cabin Seats | 28 | 19 | 9 | 16 |
| Standard Cabin Seats | 19 | 12 | 8 | 14 |
| Lavatory | — | 2 Enclosed Flushing | 1 Enclosed Belted Flushing | 2 Enclosed Flushing |
| Crew Rest | — | Yes | No | No |
| Jump Seat | — | Yes | No | Yes |
| Galley Location | — | FWD | FWD | FWD |
| Lavatory Location | — | FWD / AFT | AFT | FWD / AFT |
| Galley / Refreshment | — | Galley | Galley | Galley |
| Max Cabin Altitude (ft) | — | 4500 | — | 3900 |
| Cabin Pressure (psi) | — | — | 9.3 | 10.2 |
| SL Cabin Altitude (ft) | — | — | 25230 | 29200 |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | Makila 2A1 | Passport | PW545C | PW307D |
| Fuel Type | JetFuel | — | — | — |
| TBO (hrs) | 3500 | On-Condition | 5000 | On-Condition |
| Horsepower | 2100 | — | — | — |
| No. of Engines | 2 | 2 | 2 | 3 |
| Fuel Capacity (gal) | 684 | — | — | — |
| Flat Rating | — | ISA + 15 | ISA + 10 | ISA + 17 |
| Thrust (lbs) | — | 18920 | 4119 | 6722 |
| Dimensions | ||||
| Length (ft) | 63.4 | 111 | 52.5 | 80.2 |
| Overall Height (ft) | 16.3 | 27 | 17.2 | 26.1 |
| Rotor Diameter (ft) | 53.2 | — | — | — |
| Cabin Volume (cu. ft) | 547 | — | — | 1695 |
| Wingspan (ft) | — | 104 | 56.3 | 86.3 |
| Cabin Width (ft) | — | 8 | 5.5 | 7.7 |
| Cabin Height (ft) | — | 6.2 | 5.7 | 6.2 |
| Cabin Length (ft) | — | 54.5 | 18.5 | 42.7 |
| Aisle Step (ft) | — | — | 0.7 | — |
| 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 |