Airbus Helicopters H225 vs Daher Tbm 960 vs Dassault Falcon 8x vs Gulfstream G700
The Airbus H225 is a twin‑engine helicopter typically used for offshore, SAR, and utility missions rather than point‑to‑point business travel. It generally carries around 19 passengers (high‑density) and has a practical range on the order of roughly 400–500 nautical miles, depending on load and reserves. The Daher TBM 960 is a single‑engine turboprop airplane optimized for fast personal and small‑team travel; it typically seats 4–6 passengers and offers about 1,500–1,700 nautical miles of range. The Dassault Falcon 8X is a long‑range, large‑cabin business jet suited to intercontinental missions, usually carrying about 12–16 passengers with a range around 6,400–6,500 nautical miles. The Gulfstream G700 sits at the ultra‑long‑range, flagship end of business aviation with a very large cabin; it commonly accommodates about 13–19 passengers and offers roughly 7,500 nautical miles of range. Overall, the H225 prioritizes vertical lift and access, the TBM 960 prioritizes efficiency and speed for smaller groups, and the Falcon 8X and G700 prioritize long‑range comfort, with the G700 generally offering the longest range and largest cabin.
| Spec | AIRBUS H225 | Daher TBM 960 | Dassault Falcon 8X | Gulfstream G700 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 3 |
| DOC / nm | $ 20.87 | $ 2.25 | $ 7.66 | — |
| Min Crew | 2 | 1 | 2 | 4 |
| Total Seats | 21 | 6 | 17 | 16 |
| Flight Rules | IFR | IFR | — | — |
| Manufacturer | Airbus Helicopters | Daher TBM | Dassault Falcon | Gulfstream |
| Aircraft Name | H225 | TBM 960 | 8X | G700 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | In Development |
| Max Range (nm) | 454 | 1730 | 6450 | 7500 |
| DOC / nm / Seat | $ 0.99 | $ 0.56 | $ 0.64 | — |
| Max Cabin Seats | 28 | — | 16 | 19 |
| OEM Verification | Un-Verified | Un-Verified | VERIFIED | Un-Verified |
| Useful Load (lbs) | 11929 | 2908 | 36900 | — |
| Standard Cabin Seats | 19 | 4 | 14 | 12 |
| Direct Operating Cost | $ 2,963 | $ 744 | $ 3,805 | — |
| Flight Deck (Base Spec) | EFIS | Garmin G3000 | Honeywell Primus EASy II | Gulfstream Symmetry Flight Deck |
| Max Cruise Speed (ktas) | 142 | 330 | 516 | 516 |
| Base Aircraft Price (USD) | $ 29,500,000 | $4,450,000 | $ 62,500,000 | $78,000,000 |
| Aircraft Type | — | Turbo Prop | — | — |
| Cabin | ||||
| Cockpit | 2 | 2 | 3 | 2 |
| Min Crew | 2 | 1 | 2 | 4 |
| Total Seats | 21 | 6 | 17 | 16 |
| Max Cabin Seats | 28 | — | 16 | 19 |
| Standard Cabin Seats | 19 | 4 | 14 | 12 |
| Lavatory | — | No | 2 Enclosed Flushing | — |
| Galley Location | — | MID | FWD | FWD |
| Cabin Pressure (psi) | — | 6.2 | 10.2 | — |
| SL Cabin Altitude (ft) | — | 14390 | 29200 | — |
| Crew Rest | — | — | No | Optional |
| Jump Seat | — | — | Yes | Yes |
| Lavatory Location | — | — | FWD / AFT | FWD / AFT |
| Galley / Refreshment | — | — | Galley | — |
| Max Cabin Altitude (ft) | — | — | 3900 | — |
| Engine | ||||
| FADEC | Yes | Yes | Yes | — |
| Model | Makila 2A1 | TBM 960 | PW307D | Pearl 700 |
| Fuel Type | JetFuel | — | — | — |
| TBO (hrs) | 3500 | 3500 | On-Condition | On Condition |
| Horsepower | 2100 | 850 | — | — |
| No. of Engines | 2 | — | 3 | 2 |
| Fuel Capacity (gal) | 684 | — | — | — |
| Flat Rating | — | ISA + 49 | ISA + 17 | — |
| Thrust (lbs) | — | — | 6722 | 18250 |
| Dimensions | ||||
| Length (ft) | 63.4 | 35.3 | 80.2 | 109.9 |
| Overall Height (ft) | 16.3 | — | 26.1 | 25.4 |
| Rotor Diameter (ft) | 53.2 | — | — | — |
| Cabin Volume (cu. ft) | 547 | 123 | 1695 | — |
| Wingspan (ft) | — | 42.1 | 86.3 | 103 |
| Cabin Width (ft) | — | 4 | 7.7 | 8.2 |
| Cabin Height (ft) | — | 4.1 | 6.2 | 6.25 |
| Cabin Length (ft) | — | 13.4 | 42.7 | 56.9 |
| Cabin Width - Floor (ft) | — | — | 6.3 | — |
| Cabin Length - Seating (ft) | — | — | 29.2 | — |
| Baggage Volume Int. (cu. ft) | — | — | 140 | 195 |
| Aisle Step (ft) | — | — | — | Flat Floor |