Airbus Helicopters H225 vs Boeing Bbj Max 9 vs Daher Tbm 960 vs Dassault Falcon 8x
The Airbus H225 is a long‑range twin‑engine helicopter, typically used for offshore, SAR, and VIP transport. It trades speed and fixed‑wing range for vertical access, with an effective range roughly around 400–500 nautical miles depending on configuration, and it can carry about 16–19 passengers in airline‑style seating (more in high‑density roles, fewer in VIP layouts). The Boeing BBJ MAX 9 is a large, ultra‑long‑range VIP airliner based on the 737 MAX 9. It offers intercontinental capability at roughly 6,000–6,500 nautical miles with auxiliary tanks, and passenger capacity varies widely, commonly around 25–50 in VIP arrangements (far more in standard airline seating). The Daher TBM 960 is a single‑engine turboprop optimized for owner‑pilots and short‑field flexibility. It typically carries 4–6 passengers and flies about 1,400–1,700 nautical miles. The Dassault Falcon 8X is a purpose‑built ultra‑long‑range business jet, generally carrying about 12–16 passengers in comfort with a range near 6,450 nautical miles.
| Spec | AIRBUS H225 | Boeing BBJ MAX 9 | Daher TBM 960 | Dassault Falcon 8X |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 15.74 | $ 2.25 | $ 7.66 |
| Min Crew | 2 | 4 | 1 | 2 |
| Total Seats | 21 | 12 | 6 | 17 |
| Flight Rules | IFR | — | IFR | — |
| Manufacturer | Airbus Helicopters | Boeing | Daher TBM | Dassault Falcon |
| Aircraft Name | H225 | BBJ MAX 9 | TBM 960 | 8X |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 6376 | 1730 | 6450 |
| DOC / nm / Seat | $ 0.99 | $ 1.97 | $ 0.56 | $ 0.64 |
| Max Cabin Seats | 28 | 35 | — | 16 |
| OEM Verification | Un-Verified | VERIFIED | Un-Verified | VERIFIED |
| Useful Load (lbs) | 11929 | 77120 | 2908 | 36900 |
| Standard Cabin Seats | 19 | 8 | 4 | 14 |
| Direct Operating Cost | $ 2,963 | $ 7,396 | $ 744 | $ 3,805 |
| Flight Deck (Base Spec) | EFIS | Honeywell | Garmin G3000 | Honeywell Primus EASy II |
| Max Cruise Speed (ktas) | 142 | 470 | 330 | 516 |
| Base Aircraft Price (USD) | $ 29,500,000 | $107,700,000 | $4,450,000 | $ 62,500,000 |
| Aircraft Type | — | — | Turbo Prop | — |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 3 |
| Min Crew | 2 | 4 | 1 | 2 |
| Total Seats | 21 | 10 | 6 | 17 |
| Max Cabin Seats | 28 | 35 | — | 16 |
| Standard Cabin Seats | 19 | 8 | 4 | 14 |
| Configuration | — | Green Interior | — | — |
| Cabin Pressure (psi) | — | 9 | 6.2 | 10.2 |
| SL Cabin Altitude (ft) | — | 24000 | 14390 | 29200 |
| Lavatory | — | — | No | 2 Enclosed Flushing |
| Galley Location | — | — | MID | FWD |
| Crew Rest | — | — | — | No |
| Jump Seat | — | — | — | Yes |
| Lavatory Location | — | — | — | FWD / AFT |
| Galley / Refreshment | — | — | — | Galley |
| Max Cabin Altitude (ft) | — | — | — | 3900 |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | Makila 2A1 | LEAP-1B | TBM 960 | PW307D |
| Fuel Type | JetFuel | — | — | — |
| TBO (hrs) | 3500 | On-Condition | 3500 | On-Condition |
| Horsepower | 2100 | — | 850 | — |
| No. of Engines | 2 | 2 | — | 3 |
| Fuel Capacity (gal) | 684 | — | — | — |
| Flat Rating | — | ISA + 15 | ISA + 49 | ISA + 17 |
| Thrust (lbs) | — | 28000 | — | 6722 |
| Dimensions | ||||
| Length (ft) | 63.4 | 138.4 | 35.3 | 80.2 |
| Overall Height (ft) | 16.3 | 40.3 | — | 26.1 |
| Rotor Diameter (ft) | 53.2 | — | — | — |
| Cabin Volume (cu. ft) | 547 | — | 123 | 1695 |
| Wingspan (ft) | — | 117.9 | 42.1 | 86.3 |
| Aisle Step (ft) | — | Flat Floor | — | — |
| Cabin Width (ft) | — | 11.6 | 4 | 7.7 |
| Cabin Height (ft) | — | 7.1 | 4.1 | 6.2 |
| Cabin Length (ft) | — | 107.2 | 13.4 | 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 |