Airbus Helicopters H225 vs Boeing Bbj Max 9 vs Dassault Falcon 8x vs Enstrom 480b
The Airbus H225 and Enstrom 480B are helicopters, while the Boeing BBJ MAX 9 and Dassault Falcon 8X are fixed‑wing business aircraft, so their strengths differ sharply. The Airbus H225 is a heavy, long‑range twin‑engine helicopter aimed at offshore transport, search and rescue, and utility missions; it typically carries roughly 19 passengers and offers a range on the order of about 450–600 nautical miles depending on configuration. The Enstrom 480B is a light single‑engine helicopter for training, patrol, and personal/utility flying, seating up to 5 with a range roughly around 250–350 nautical miles. The Dassault Falcon 8X is a long‑range large‑cabin business jet optimized for intercontinental trips; it usually seats about 12–16 passengers and can fly roughly 6,450 nautical miles. The Boeing BBJ MAX 9 is an airline‑derived VIP jet designed for very high capacity and large cabin volume; typical VIP layouts may carry about 25–50+ passengers (far more if configured densely) with range roughly in the 6,000–6,600 nautical mile class.
| 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 |