Airbus Helicopters H225 vs Boeing Bbj Max 9 vs Dassault Falcon 8x vs Leonardo Aw189
The Airbus H225 and Leonardo AW189 are twin‑engine helicopters optimized for vertical access to offshore platforms and remote sites. Their typical passenger loads are roughly 16–19 in high‑density seating (often fewer in VIP layouts). Range is comparatively short: about 450–500 nautical miles for the AW189 and around 450–540 nautical miles for the H225 depending on fit, reserves, and payload. The Boeing BBJ MAX 9 is a large, long‑range airliner‑based business jet intended for intercontinental travel with airline levels of space. It can carry well over 100 passengers in dense airline seating, but BBJ/VIP configurations commonly seat far fewer (often a few dozen). Range is roughly 3,400–3,600 nautical miles, again highly dependent on configuration. The Dassault Falcon 8X is a purpose‑built long‑range business jet focused on efficient, non‑stop intercontinental missions and access to smaller airports. Typical capacity is about 12–16 passengers in executive layouts, with a maximum around 19. Its range is about 6,000+ nautical miles, generally exceeding the BBJ MAX 9 while carrying far fewer people.
| Spec | AIRBUS H225 | Boeing BBJ MAX 9 | Dassault Falcon 8X | AGUSTA / LEONARDO AW189 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 15.74 | $ 7.66 | $ 15.57 |
| Min Crew | 2 | 4 | 2 | 1 |
| Total Seats | 21 | 12 | 17 | 21 |
| Flight Rules | IFR | — | — | IFR |
| Manufacturer | Airbus Helicopters | Boeing | Dassault Falcon | Leonardo |
| Aircraft Name | H225 | BBJ MAX 9 | 8X | AW189 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 6376 | 6450 | 651 |
| DOC / nm / Seat | $ 0.99 | $ 1.97 | $ 0.64 | $ 0.74 |
| Max Cabin Seats | 28 | 35 | 16 | 19 |
| OEM Verification | Un-Verified | VERIFIED | VERIFIED | Un-Verified |
| Useful Load (lbs) | 11929 | 77120 | 36900 | — |
| Standard Cabin Seats | 19 | 8 | 14 | 19 |
| Direct Operating Cost | $ 2,963 | $ 7,396 | $ 3,805 | $ 2,413 |
| Flight Deck (Base Spec) | EFIS | Honeywell | Honeywell Primus EASy II | EFIS |
| Max Cruise Speed (ktas) | 142 | 470 | 516 | 155 |
| Base Aircraft Price (USD) | $ 29,500,000 | $107,700,000 | $ 62,500,000 | $2,413,000 |
| Cabin | ||||
| Cockpit | 2 | 2 | 3 | 2 |
| Min Crew | 2 | 4 | 2 | 1 |
| Total Seats | 21 | 10 | 17 | 21 |
| Max Cabin Seats | 28 | 35 | 16 | 19 |
| Standard Cabin Seats | 19 | 8 | 14 | 19 |
| 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 | Yes |
| Model | Makila 2A1 | LEAP-1B | PW307D | CT7-2E1 |
| Fuel Type | JetFuel | — | — | JetFuel |
| TBO (hrs) | 3500 | On-Condition | On-Condition | 4000 |
| Horsepower | 2100 | — | — | 1983 |
| No. of Engines | 2 | 2 | 3 | 2 |
| Fuel Capacity (gal) | 684 | — | — | — |
| Flat Rating | — | ISA + 15 | ISA + 17 | — |
| Thrust (lbs) | — | 28000 | 6722 | — |
| Dimensions | ||||
| Length (ft) | 63.4 | 138.4 | 80.2 | 57.8 |
| Overall Height (ft) | 16.3 | 40.3 | 26.1 | 16.6 |
| Rotor Diameter (ft) | 53.2 | — | — | 48 |
| Cabin Volume (cu. ft) | 547 | — | 1695 | 395 |
| 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 | — | 85 |
| Baggage Volume Int. (cu. ft) | — | — | 140 | — |