Airbus Helicopters H225 vs Boeing Bbj Max 9 vs Cessna Citation Xls vs Dassault Falcon 8x
The Airbus H225 is a twin‑engine helicopter suited to offshore and utility missions rather than long-range jet travel. It typically carries around 19 passengers (high-density seating) and has a practical range on the order of roughly 500–700 nautical miles, depending on payload and reserves. The Boeing BBJ MAX 9 is a large VIP airliner based on the 737 MAX 9, aimed at head‑of‑state or corporate shuttle roles. It offers intercontinental capability, commonly cited around 6,000+ nautical miles with auxiliary tanks, and can accommodate anything from a few dozen in VIP layouts to well over 100 in airline-style seating. The Cessna Citation XLS+ is a super‑midsize business jet designed for efficient regional trips. It generally seats about 8–12 passengers and has a range around 2,000–2,100 nautical miles. The Dassault Falcon 8X is an ultra‑long‑range business jet positioned for nonstop intercontinental missions. It typically carries about 12–16 passengers in executive configurations and offers roughly 6,450 nautical miles of range, prioritizing long legs with strong runway flexibility.
| Spec | AIRBUS H225 | Boeing BBJ MAX 9 | Cessna Citation XLS+ | Dassault Falcon 8X |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 15.74 | $ 5.34 | $ 7.66 |
| Min Crew | 2 | 4 | 2 | 2 |
| Total Seats | 21 | 12 | 10 | 17 |
| Flight Rules | IFR | — | — | — |
| Manufacturer | Airbus Helicopters | Boeing | Cessna Citation | Dassault Falcon |
| Aircraft Name | H225 | BBJ MAX 9 | XLS+ | 8X |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 6376 | 1906 | 6450 |
| DOC / nm / Seat | $ 0.99 | $ 1.97 | $ 0.67 | $ 0.64 |
| Max Cabin Seats | 28 | 35 | 9 | 16 |
| OEM Verification | Un-Verified | VERIFIED | VERIFIED | VERIFIED |
| Useful Load (lbs) | 11929 | 77120 | 7540 | 36900 |
| Standard Cabin Seats | 19 | 8 | 8 | 14 |
| Direct Operating Cost | $ 2,963 | $ 7,396 | $ 2,303 | $ 3,805 |
| Flight Deck (Base Spec) | EFIS | Honeywell | Rockwell Collins Pro Line 21 | Honeywell Primus EASy II |
| Max Cruise Speed (ktas) | 142 | 470 | 430 | 516 |
| Base Aircraft Price (USD) | $ 29,500,000 | $107,700,000 | $15,500,000 | $ 62,500,000 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 3 |
| Min Crew | 2 | 4 | 2 | 2 |
| Total Seats | 21 | 10 | 10 | 17 |
| Max Cabin Seats | 28 | 35 | 9 | 16 |
| Standard Cabin Seats | 19 | 8 | 8 | 14 |
| Configuration | — | Green Interior | — | — |
| Cabin Pressure (psi) | — | 9 | 9.3 | 10.2 |
| SL Cabin Altitude (ft) | — | 24000 | 25230 | 29200 |
| 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 |
| Galley / Refreshment | — | — | Galley | Galley |
| Max Cabin Altitude (ft) | — | — | — | 3900 |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | Makila 2A1 | LEAP-1B | 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) | — | 28000 | 4119 | 6722 |
| Dimensions | ||||
| Length (ft) | 63.4 | 138.4 | 52.5 | 80.2 |
| Overall Height (ft) | 16.3 | 40.3 | 17.2 | 26.1 |
| Rotor Diameter (ft) | 53.2 | — | — | — |
| Cabin Volume (cu. ft) | 547 | — | — | 1695 |
| Wingspan (ft) | — | 117.9 | 56.3 | 86.3 |
| Aisle Step (ft) | — | Flat Floor | 0.7 | — |
| Cabin Width (ft) | — | 11.6 | 5.5 | 7.7 |
| Cabin Height (ft) | — | 7.1 | 5.7 | 6.2 |
| Cabin Length (ft) | — | 107.2 | 18.5 | 42.7 |
| Cabin Width - Floor (ft) | — | 10.7 | 3.9 | 6.3 |
| Cabin Length - Seating (ft) | — | 100.6 | 14.3 | 29.2 |
| Baggage Volume Ext. (cu. ft) | — | 1485 | 80 | — |
| Baggage Volume Int. (cu. ft) | — | — | 10 | 140 |