Airbus Helicopters H225 vs Boeing Bbj Max 9 vs Dassault Falcon 8x vs Piaggio Avanti Evo
The Airbus H225 is a heavy twin‑engine helicopter optimized for vertical lift and offshore/utility missions rather than long, high‑speed point‑to‑point travel. Its practical range is typically a few hundred nautical miles (with auxiliary tanks extending it), and passenger seating is commonly around 16–19 depending on configuration. The Boeing BBJ MAX 9 is a large VIP airliner based on the 737 MAX 9, offering intercontinental range on the order of roughly 5,000–6,000 nautical miles and the greatest capacity of this group, often configured for several dozen passengers (frequently around 25–50 in VIP layouts, far more in airline seating). The Dassault Falcon 8X is a long‑range tri‑jet business jet, designed for nonstop intercontinental trips with roughly 6,000+ nautical miles of range and a typical executive load around 12–16 passengers (with higher maximums possible depending on layout). The Piaggio Avanti EVO is a light twin‑turboprop business aircraft suited to regional missions, generally around 1,500–1,800 nautical miles of range and typically 6–7 passengers.
| Spec | AIRBUS H225 | Boeing BBJ MAX 9 | Dassault Falcon 8X | Piaggio Avanti EVO |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 15.74 | $ 7.66 | — |
| Min Crew | 2 | 4 | 2 | 1 |
| Total Seats | 21 | 12 | 17 | 8 |
| Flight Rules | IFR | — | — | IFR |
| Manufacturer | Airbus Helicopters | Boeing | Dassault Falcon | Piaggio |
| Aircraft Name | H225 | BBJ MAX 9 | 8X | Avanti EVO |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 6376 | 6450 | 1530 |
| DOC / nm / Seat | $ 0.99 | $ 1.97 | $ 0.64 | — |
| Max Cabin Seats | 28 | 35 | 16 | 7 |
| OEM Verification | Un-Verified | VERIFIED | VERIFIED | Un-Verified |
| Useful Load (lbs) | 11929 | 77120 | 36900 | 3775 |
| Standard Cabin Seats | 19 | 8 | 14 | 6 |
| Direct Operating Cost | $ 2,963 | $ 7,396 | $ 3,805 | — |
| Flight Deck (Base Spec) | EFIS | Honeywell | Honeywell Primus EASy II | Rockwell Collins Pro Line 21 |
| Max Cruise Speed (ktas) | 142 | 470 | 516 | 400 |
| Base Aircraft Price (USD) | $ 29,500,000 | $107,700,000 | $ 62,500,000 | $ 7,695,000 |
| Cabin | ||||
| Cockpit | 2 | 2 | 3 | 2 |
| Min Crew | 2 | 4 | 2 | 1 |
| Total Seats | 21 | 10 | 17 | 8 |
| Max Cabin Seats | 28 | 35 | 16 | 7 |
| Standard Cabin Seats | 19 | 8 | 14 | 6 |
| Configuration | — | Green Interior | — | — |
| Cabin Pressure (psi) | — | 9 | 10.2 | 9 |
| SL Cabin Altitude (ft) | — | 24000 | 29200 | 24000 |
| Lavatory | — | — | 2 Enclosed Flushing | No |
| Crew Rest | — | — | No | — |
| Jump Seat | — | — | Yes | — |
| Galley Location | — | — | FWD | — |
| Lavatory Location | — | — | FWD / AFT | — |
| Galley / Refreshment | — | — | Galley | No |
| Max Cabin Altitude (ft) | — | — | 3900 | 6600 |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | Makila 2A1 | LEAP-1B | PW307D | PT6A–66B |
| Fuel Type | JetFuel | — | — | — |
| TBO (hrs) | 3500 | On-Condition | On-Condition | 3600 |
| Horsepower | 2100 | — | — | 850 |
| No. of Engines | 2 | 2 | 3 | 2 |
| Fuel Capacity (gal) | 684 | — | — | — |
| Flat Rating | — | ISA + 15 | ISA + 17 | ISA + 28 |
| Thrust (lbs) | — | 28000 | 6722 | — |
| Fuel Burn (gph) | — | — | — | 100 |
| Dimensions | ||||
| Length (ft) | 63.4 | 138.4 | 80.2 | 47.3 |
| Overall Height (ft) | 16.3 | 40.3 | 26.1 | 13.1 |
| Rotor Diameter (ft) | 53.2 | — | — | — |
| Cabin Volume (cu. ft) | 547 | — | 1695 | — |
| Wingspan (ft) | — | 117.9 | 86.3 | 47.1 |
| Aisle Step (ft) | — | Flat Floor | — | — |
| Cabin Width (ft) | — | 11.6 | 7.7 | 6.1 |
| Cabin Height (ft) | — | 7.1 | 6.2 | 5.8 |
| Cabin Length (ft) | — | 107.2 | 42.7 | 14.9 |
| Cabin Width - Floor (ft) | — | 10.7 | 6.3 | 3.5 |
| Cabin Length - Seating (ft) | — | 100.6 | 29.2 | — |
| Baggage Volume Ext. (cu. ft) | — | 1485 | — | — |
| Baggage Volume Int. (cu. ft) | — | — | 140 | 35.2 |