Airbus Helicopters H225 vs Boeing Bbj Max 9 vs Bombardier Global 7500 vs Dassault Falcon 8x
The Airbus H225 is a heavy twin‑engine helicopter used for offshore, rescue, and utility missions rather than long‑haul point‑to‑point travel. Its practical range is roughly 500–700 nautical miles depending on payload and reserves, and it typically carries about 16–19 passengers (higher-density seating is possible in utility layouts). The Boeing BBJ MAX 9 is an airliner‑derived VIP jet focused on long-range corporate or government transport with large cabin volume. Its range is about 6,000–6,500 nautical miles, and typical VIP configurations seat roughly 25–50 passengers (it can be configured much higher for airline-style seating). The Bombardier Global 7500 is an ultra‑long‑range business jet optimized for nonstop intercontinental missions, with a range around 7,700 nautical miles and a typical passenger load of about 8–19. The Dassault Falcon 8X is also an ultra‑long‑range business jet, generally a bit shorter-ranged than the Global 7500 at about 6,450 nautical miles, with typical seating around 8–16.
| Spec | AIRBUS H225 | Boeing BBJ MAX 9 | Bombardier Global 7500 | Dassault Falcon 8X |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 15.74 | $ 9.50 | $ 7.66 |
| Min Crew | 2 | 4 | 2 | 2 |
| Total Seats | 21 | 12 | 14 | 17 |
| Flight Rules | IFR | — | — | — |
| Manufacturer | Airbus Helicopters | Boeing | Bombardier | Dassault Falcon |
| Aircraft Name | H225 | BBJ MAX 9 | Global 7500 | 8X |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 6376 | 7700 | 6450 |
| DOC / nm / Seat | $ 0.99 | $ 1.97 | $ 0.79 | $ 0.64 |
| Max Cabin Seats | 28 | 35 | 19 | 16 |
| OEM Verification | Un-Verified | VERIFIED | VERIFIED | VERIFIED |
| Useful Load (lbs) | 11929 | 77120 | — | 36900 |
| Standard Cabin Seats | 19 | 8 | 12 | 14 |
| Direct Operating Cost | $ 2,963 | $ 7,396 | $ 4,900 | $ 3,805 |
| Flight Deck (Base Spec) | EFIS | Honeywell | Bombardier Vision (Pro Line Fusion) | Honeywell Primus EASy II |
| Max Cruise Speed (ktas) | 142 | 470 | 516 | 516 |
| Base Aircraft Price (USD) | $ 29,500,000 | $107,700,000 | $75,000,000 | $ 62,500,000 |
| Aircraft Type | — | — | Business Jet | — |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 3 |
| Min Crew | 2 | 4 | 2 | 2 |
| Total Seats | 21 | 10 | 14 | 17 |
| Max Cabin Seats | 28 | 35 | 19 | 16 |
| Standard Cabin Seats | 19 | 8 | 12 | 14 |
| Configuration | — | Green Interior | — | — |
| Cabin Pressure (psi) | — | 9 | — | 10.2 |
| SL Cabin Altitude (ft) | — | 24000 | — | 29200 |
| Lavatory | — | — | 2 Enclosed Flushing | 2 Enclosed Flushing |
| Crew Rest | — | — | Yes | No |
| Jump Seat | — | — | Yes | Yes |
| Galley Location | — | — | FWD | FWD |
| Lavatory Location | — | — | FWD / AFT | FWD / AFT |
| Galley / Refreshment | — | — | Galley | Galley |
| Max Cabin Altitude (ft) | — | — | 4500 | 3900 |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | Makila 2A1 | LEAP-1B | Passport | PW307D |
| Fuel Type | JetFuel | — | — | — |
| TBO (hrs) | 3500 | On-Condition | On-Condition | On-Condition |
| Horsepower | 2100 | — | — | — |
| No. of Engines | 2 | 2 | 2 | 3 |
| Fuel Capacity (gal) | 684 | — | — | — |
| Flat Rating | — | ISA + 15 | ISA + 15 | ISA + 17 |
| Thrust (lbs) | — | 28000 | 18920 | 6722 |
| Dimensions | ||||
| Length (ft) | 63.4 | 138.4 | 111 | 80.2 |
| Overall Height (ft) | 16.3 | 40.3 | 27 | 26.1 |
| Rotor Diameter (ft) | 53.2 | — | — | — |
| Cabin Volume (cu. ft) | 547 | — | — | 1695 |
| Wingspan (ft) | — | 117.9 | 104 | 86.3 |
| Aisle Step (ft) | — | Flat Floor | — | — |
| Cabin Width (ft) | — | 11.6 | 8 | 7.7 |
| Cabin Height (ft) | — | 7.1 | 6.2 | 6.2 |
| Cabin Length (ft) | — | 107.2 | 54.5 | 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 |