Airbus Helicopters H225 vs Beechcraft King Air 360 Er vs Boeing Bbj Max 9 vs Dassault Falcon 8x
The Airbus H225 is a long‑range twin‑engine helicopter suited to offshore and utility missions rather than point‑to‑point airline-style travel. It typically carries about 16–19 passengers in standard transport layouts and offers roughly 500–700 nautical miles of range depending on configuration and reserves. The Beechcraft King Air 360ER is a pressurized twin‑turboprop business/utility aircraft optimized for regional missions and short or unimproved runways. Passenger capacity is commonly 6–9, and its extended-range capability is on the order of about 1,500–1,800 nautical miles. The Boeing BBJ MAX 9 is a large VIP airliner based on the 737 MAX 9, positioned for intercontinental travel with a spacious cabin. Depending on interior, it can accommodate roughly 25–50+ passengers, with range typically cited around 6,000–6,600 nautical miles. The Dassault Falcon 8X is an ultra‑long‑range business jet aimed at nonstop global city pairs. It usually seats about 12–16 passengers and offers approximately 6,450 nautical miles of range.
| 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 |