Airbus Helicopters H225 vs Boeing Bbj Max 9 vs Dassault Falcon 8x vs Piper M600 Sls
The Airbus H225 is a large twin‑engine helicopter, best suited to short‑to‑medium missions such as offshore transport, search and rescue, or VIP shuttle work. It typically carries around 19 passengers in high‑density seating (fewer in VIP layouts) and, depending on fuel and mission profile, offers roughly 400–500 nautical miles of practical range. The Boeing BBJ MAX 9 is a long‑range, large‑cabin business airliner derived from the 737 MAX 9. In VIP configuration it generally carries a few dozen passengers (often around 25–50, depending on layout) and can reach roughly 6,000+ nautical miles, making it appropriate for intercontinental travel with extensive cabin amenities. The Dassault Falcon 8X is an ultra‑long‑range business jet, typically seating about 12–16 passengers, with a range around 6,450 nautical miles, emphasizing nonstop long‑haul capability and access to shorter business‑jet runways. The Piper M600 SLS is a single‑engine turboprop in the owner‑pilot category, usually seating 4–6, with about 1,400–1,500 nautical miles of range, optimized for efficient regional travel.
| Spec | AIRBUS H225 | Boeing BBJ MAX 9 | Dassault Falcon 8X | Piper M600 SLS |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 15.74 | $ 7.66 | $ 2.19 |
| Min Crew | 2 | 4 | 2 | 1 |
| Total Seats | 21 | 12 | 17 | 6 |
| Flight Rules | IFR | — | — | IFR |
| Manufacturer | Airbus Helicopters | Boeing | Dassault Falcon | Piper |
| Aircraft Name | H225 | BBJ MAX 9 | 8X | M600 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 6376 | 6450 | 1406 |
| DOC / nm / Seat | $ 0.99 | $ 1.97 | $ 0.64 | $ 0.55 |
| Max Cabin Seats | 28 | 35 | 16 | — |
| OEM Verification | Un-Verified | VERIFIED | VERIFIED | VERIFIED |
| Useful Load (lbs) | 11929 | 77120 | 36900 | 2200 |
| Standard Cabin Seats | 19 | 8 | 14 | 4 |
| Direct Operating Cost | $ 2,963 | $ 7,396 | $ 3,805 | $ 603 |
| Flight Deck (Base Spec) | EFIS | Honeywell | Honeywell Primus EASy II | Garmin G3000 |
| Max Cruise Speed (ktas) | 142 | 470 | 516 | 274 |
| Base Aircraft Price (USD) | $ 29,500,000 | $107,700,000 | $ 62,500,000 | $3,081,400 |
| Cabin | ||||
| Cockpit | 2 | 2 | 3 | 2 |
| Min Crew | 2 | 4 | 2 | 1 |
| Total Seats | 21 | 10 | 17 | 5 |
| Max Cabin Seats | 28 | 35 | 16 | — |
| Standard Cabin Seats | 19 | 8 | 14 | 4 |
| Configuration | — | Green Interior | — | — |
| Cabin Pressure (psi) | — | 9 | 10.2 | 5.6 |
| SL Cabin Altitude (ft) | — | 24000 | 29200 | 12600 |
| Lavatory | — | — | 2 Enclosed Flushing | No |
| Crew Rest | — | — | No | — |
| Jump Seat | — | — | Yes | — |
| Galley Location | — | — | FWD | MID |
| Lavatory Location | — | — | FWD / AFT | — |
| Galley / Refreshment | — | — | Galley | Refreshment Centre |
| Max Cabin Altitude (ft) | — | — | 3900 | 8644 |
| Engine | ||||
| FADEC | Yes | Yes | Yes | No |
| Model | Makila 2A1 | LEAP-1B | PW307D | PT6A-42A |
| Fuel Type | JetFuel | — | — | — |
| TBO (hrs) | 3500 | On-Condition | On-Condition | 3600 |
| Horsepower | 2100 | — | — | 600 |
| No. of Engines | 2 | 2 | 3 | 1 |
| Fuel Capacity (gal) | 684 | — | — | 260 |
| Flat Rating | — | ISA + 15 | ISA + 17 | ISA + 55 |
| Thrust (lbs) | — | 28000 | 6722 | — |
| Dimensions | ||||
| Length (ft) | 63.4 | 138.4 | 80.2 | 29.7 |
| Overall Height (ft) | 16.3 | 40.3 | 26.1 | 11.3 |
| Rotor Diameter (ft) | 53.2 | — | — | — |
| Cabin Volume (cu. ft) | 547 | — | 1695 | 165 |
| Wingspan (ft) | — | 117.9 | 86.3 | 43.2 |
| Aisle Step (ft) | — | Flat Floor | — | — |
| Cabin Width (ft) | — | 11.6 | 7.7 | 4.1 |
| Cabin Height (ft) | — | 7.1 | 6.2 | 4 |
| Cabin Length (ft) | — | 107.2 | 42.7 | 12.3 |
| 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 | 20 |