Airbus Helicopters H225 vs Bombardier Global 7500 vs Daher Tbm 960 vs Dassault Falcon 8x
The Airbus H225 is a heavy twin‑engine helicopter, typically configured for around 16–19 passengers depending on mission fit, with a practical range on the order of roughly 450–700 nautical miles (more with auxiliary tanks), optimized for vertical lift operations such as offshore transport and SAR rather than long nonstop travel. The Daher TBM 960 is a single‑engine turboprop airplane aimed at owner‑pilots and fast regional trips, carrying up to about 6 passengers (plus pilot) with a range around 1,400–1,700 nautical miles depending on reserves and conditions. The Dassault Falcon 8X is a long‑range ultra‑long‑haul business jet, typically seating about 12–16 passengers with an advertised range near 6,450 nautical miles, emphasizing cabin comfort and access to shorter runways. The Bombardier Global 7500 sits at the top end of ultra‑long‑range business jets, generally accommodating about 14–19 passengers with a range around 7,700 nautical miles, prioritizing maximum nonstop distance and large-cabin space.
| Spec | AIRBUS H225 | Bombardier Global 7500 | Daher TBM 960 | Dassault Falcon 8X |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 9.50 | $ 2.25 | $ 7.66 |
| Min Crew | 2 | 2 | 1 | 2 |
| Total Seats | 21 | 14 | 6 | 17 |
| Flight Rules | IFR | — | IFR | — |
| Manufacturer | Airbus Helicopters | Bombardier | Daher TBM | Dassault Falcon |
| Aircraft Name | H225 | Global 7500 | TBM 960 | 8X |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 7700 | 1730 | 6450 |
| DOC / nm / Seat | $ 0.99 | $ 0.79 | $ 0.56 | $ 0.64 |
| Max Cabin Seats | 28 | 19 | — | 16 |
| OEM Verification | Un-Verified | VERIFIED | Un-Verified | VERIFIED |
| Useful Load (lbs) | 11929 | — | 2908 | 36900 |
| Standard Cabin Seats | 19 | 12 | 4 | 14 |
| Direct Operating Cost | $ 2,963 | $ 4,900 | $ 744 | $ 3,805 |
| Flight Deck (Base Spec) | EFIS | Bombardier Vision (Pro Line Fusion) | Garmin G3000 | Honeywell Primus EASy II |
| Max Cruise Speed (ktas) | 142 | 516 | 330 | 516 |
| Base Aircraft Price (USD) | $ 29,500,000 | $75,000,000 | $4,450,000 | $ 62,500,000 |
| Aircraft Type | — | Business Jet | Turbo Prop | — |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 3 |
| Min Crew | 2 | 2 | 1 | 2 |
| Total Seats | 21 | 14 | 6 | 17 |
| Max Cabin Seats | 28 | 19 | — | 16 |
| Standard Cabin Seats | 19 | 12 | 4 | 14 |
| Lavatory | — | 2 Enclosed Flushing | No | 2 Enclosed Flushing |
| Crew Rest | — | Yes | — | No |
| Jump Seat | — | Yes | — | Yes |
| Galley Location | — | FWD | MID | FWD |
| Lavatory Location | — | FWD / AFT | — | FWD / AFT |
| Galley / Refreshment | — | Galley | — | Galley |
| Max Cabin Altitude (ft) | — | 4500 | — | 3900 |
| Cabin Pressure (psi) | — | — | 6.2 | 10.2 |
| SL Cabin Altitude (ft) | — | — | 14390 | 29200 |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | Makila 2A1 | Passport | 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) | — | 18920 | — | 6722 |
| Dimensions | ||||
| Length (ft) | 63.4 | 111 | 35.3 | 80.2 |
| Overall Height (ft) | 16.3 | 27 | — | 26.1 |
| Rotor Diameter (ft) | 53.2 | — | — | — |
| Cabin Volume (cu. ft) | 547 | — | 123 | 1695 |
| Wingspan (ft) | — | 104 | 42.1 | 86.3 |
| Cabin Width (ft) | — | 8 | 4 | 7.7 |
| Cabin Height (ft) | — | 6.2 | 4.1 | 6.2 |
| Cabin Length (ft) | — | 54.5 | 13.4 | 42.7 |
| Cabin Width - Floor (ft) | — | — | — | 6.3 |
| Cabin Length - Seating (ft) | — | — | — | 29.2 |
| Baggage Volume Int. (cu. ft) | — | — | — | 140 |