Airbus Helicopters H225 vs Boeing Bbj Max 9 vs Dassault Falcon 8x
The Airbus H225 is a large twin‑engine helicopter suited to offshore, SAR, and utility missions rather than long‑haul point‑to‑point travel. Its range is roughly 500–650 nautical miles depending on fit and reserves, and it typically carries about 19 passengers (up to around two dozen in high‑density layouts). The Boeing BBJ MAX 9 is a VIP airliner based on the 737 MAX 9, positioned for intercontinental government or corporate transport with airline reliability. In executive configuration it commonly carries a few dozen passengers in high comfort, though it can be arranged for far more if density is prioritized. Its range is about 6,200 nautical miles with auxiliary tanks, enabling long nonstop sectors. The Dassault Falcon 8X is a purpose‑built ultra‑long‑range business jet optimized for flexibility and access to smaller airports. It typically seats 12–16 passengers in a luxury layout, with a range around 6,450 nautical miles, often edging the BBJ MAX 9 while carrying fewer people and requiring less infrastructure than an airliner.
| Spec | AIRBUS H225 | Boeing BBJ MAX 9 | Dassault Falcon 8X |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 15.74 | $ 7.66 |
| Min Crew | 2 | 4 | 2 |
| Total Seats | 21 | 12 | 17 |
| Flight Rules | IFR | — | — |
| Manufacturer | Airbus Helicopters | Boeing | Dassault Falcon |
| Aircraft Name | H225 | BBJ MAX 9 | 8X |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 6376 | 6450 |
| DOC / nm / Seat | $ 0.99 | $ 1.97 | $ 0.64 |
| Max Cabin Seats | 28 | 35 | 16 |
| OEM Verification | Un-Verified | VERIFIED | VERIFIED |
| Useful Load (lbs) | 11929 | 77120 | 36900 |
| Standard Cabin Seats | 19 | 8 | 14 |
| Direct Operating Cost | $ 2,963 | $ 7,396 | $ 3,805 |
| Flight Deck (Base Spec) | EFIS | Honeywell | Honeywell Primus EASy II |
| Max Cruise Speed (ktas) | 142 | 470 | 516 |
| Base Aircraft Price (USD) | $ 29,500,000 | $107,700,000 | $ 62,500,000 |
| Cabin | |||
| Cockpit | 2 | 2 | 3 |
| Min Crew | 2 | 4 | 2 |
| Total Seats | 21 | 10 | 17 |
| Max Cabin Seats | 28 | 35 | 16 |
| Standard Cabin Seats | 19 | 8 | 14 |
| Configuration | — | Green Interior | — |
| Cabin Pressure (psi) | — | 9 | 10.2 |
| SL Cabin Altitude (ft) | — | 24000 | 29200 |
| Lavatory | — | — | 2 Enclosed Flushing |
| Crew Rest | — | — | No |
| Jump Seat | — | — | Yes |
| Galley Location | — | — | FWD |
| Lavatory Location | — | — | FWD / AFT |
| Galley / Refreshment | — | — | Galley |
| Max Cabin Altitude (ft) | — | — | 3900 |
| Engine | |||
| FADEC | Yes | Yes | Yes |
| Model | Makila 2A1 | LEAP-1B | PW307D |
| Fuel Type | JetFuel | — | — |
| TBO (hrs) | 3500 | On-Condition | On-Condition |
| Horsepower | 2100 | — | — |
| No. of Engines | 2 | 2 | 3 |
| Fuel Capacity (gal) | 684 | — | — |
| Flat Rating | — | ISA + 15 | ISA + 17 |
| Thrust (lbs) | — | 28000 | 6722 |
| Dimensions | |||
| Length (ft) | 63.4 | 138.4 | 80.2 |
| Overall Height (ft) | 16.3 | 40.3 | 26.1 |
| Rotor Diameter (ft) | 53.2 | — | — |
| Cabin Volume (cu. ft) | 547 | — | 1695 |
| Wingspan (ft) | — | 117.9 | 86.3 |
| Aisle Step (ft) | — | Flat Floor | — |
| Cabin Width (ft) | — | 11.6 | 7.7 |
| Cabin Height (ft) | — | 7.1 | 6.2 |
| Cabin Length (ft) | — | 107.2 | 42.7 |
| Cabin Width - Floor (ft) | — | 10.7 | 6.3 |
| Cabin Length - Seating (ft) | — | 100.6 | 29.2 |
| Baggage Volume Ext. (cu. ft) | — | 1485 | — |
| Baggage Volume Int. (cu. ft) | — | — | 140 |