Airbus Helicopters H225 vs Boeing Bbj Max 9 vs Dassault Falcon 8x vs Robinson R66
The Airbus H225 is a heavy twin‑engine helicopter optimized for vertical lift and offshore or SAR missions. Its range is roughly 450–500 nautical miles, and it typically carries about 16–19 passengers depending on cabin fit and fuel/reserve needs. The Robinson R66 is a light single‑engine helicopter for short hops and utility flying, with about 300–350 nautical miles of range and seating for 4–5 (including the pilot). The Dassault Falcon 8X is a long‑range tri‑jet business aircraft designed for intercontinental travel. It can fly about 5,900–6,450 nautical miles (configuration dependent) and commonly carries 8–16 passengers in executive layouts. The Boeing BBJ MAX 9 is a VIP airliner based on the 737 MAX 9, offering airliner scale cabin volume and typically configured for roughly 19–50+ passengers in corporate/VIP service. Its range is about 6,000–6,500 nautical miles (depending on options such as auxiliary tanks and payload), making it comparable in reach to the Falcon 8X but with far greater cabin space and group capacity.
| 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 |