Airbus Helicopters H225 vs Dassault Falcon 8x vs Gulfstream G700
The Airbus H225 is a long‑range heavy helicopter designed for vertical lift missions such as offshore transport and search and rescue. Compared with the two business jets, its range is much shorter, typically on the order of a few hundred nautical miles depending on payload and reserves, and passenger capacity is often higher in a high‑density cabin (commonly around the high teens to mid‑20s) because it is optimized for utility seating rather than executive layouts. The Dassault Falcon 8X is an ultra‑long‑range business jet focused on efficiency and flexible cabin configurations. It typically offers seating for about 12–16 passengers in executive arrangements and has intercontinental range around 6,000+ nautical miles, making it suitable for nonstop city pairs across oceans. The Gulfstream G700 sits at the top end of the large‑cabin business jet category, prioritizing space and speed with very long legs. It generally carries a similar number of passengers in executive service (often 12–16, with higher maximum seating possible) and delivers roughly 7,000+ nautical miles of range, enabling longer nonstop missions than the 8X in many profiles.
| Spec | AIRBUS H225 | Dassault Falcon 8X | Gulfstream G700 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 3 |
| DOC / nm | $ 20.87 | $ 7.66 | — |
| Min Crew | 2 | 2 | 4 |
| Total Seats | 21 | 17 | 16 |
| Flight Rules | IFR | — | — |
| Manufacturer | Airbus Helicopters | Dassault Falcon | Gulfstream |
| Aircraft Name | H225 | 8X | G700 |
| Certification | FAA / EASA | FAA / EASA | In Development |
| Max Range (nm) | 454 | 6450 | 7500 |
| DOC / nm / Seat | $ 0.99 | $ 0.64 | — |
| Max Cabin Seats | 28 | 16 | 19 |
| OEM Verification | Un-Verified | VERIFIED | Un-Verified |
| Useful Load (lbs) | 11929 | 36900 | — |
| Standard Cabin Seats | 19 | 14 | 12 |
| Direct Operating Cost | $ 2,963 | $ 3,805 | — |
| Flight Deck (Base Spec) | EFIS | Honeywell Primus EASy II | Gulfstream Symmetry Flight Deck |
| Max Cruise Speed (ktas) | 142 | 516 | 516 |
| Base Aircraft Price (USD) | $ 29,500,000 | $ 62,500,000 | $78,000,000 |
| Cabin | |||
| Cockpit | 2 | 3 | 2 |
| Min Crew | 2 | 2 | 4 |
| Total Seats | 21 | 17 | 16 |
| Max Cabin Seats | 28 | 16 | 19 |
| Standard Cabin Seats | 19 | 14 | 12 |
| Lavatory | — | 2 Enclosed Flushing | — |
| Crew Rest | — | No | Optional |
| Jump Seat | — | Yes | Yes |
| Galley Location | — | FWD | FWD |
| Lavatory Location | — | FWD / AFT | FWD / AFT |
| Cabin Pressure (psi) | — | 10.2 | — |
| Galley / Refreshment | — | Galley | — |
| SL Cabin Altitude (ft) | — | 29200 | — |
| Max Cabin Altitude (ft) | — | 3900 | — |
| Engine | |||
| FADEC | Yes | Yes | — |
| Model | Makila 2A1 | PW307D | Pearl 700 |
| Fuel Type | JetFuel | — | — |
| TBO (hrs) | 3500 | On-Condition | On Condition |
| Horsepower | 2100 | — | — |
| No. of Engines | 2 | 3 | 2 |
| Fuel Capacity (gal) | 684 | — | — |
| Flat Rating | — | ISA + 17 | — |
| Thrust (lbs) | — | 6722 | 18250 |
| Dimensions | |||
| Length (ft) | 63.4 | 80.2 | 109.9 |
| Overall Height (ft) | 16.3 | 26.1 | 25.4 |
| Rotor Diameter (ft) | 53.2 | — | — |
| Cabin Volume (cu. ft) | 547 | 1695 | — |
| Wingspan (ft) | — | 86.3 | 103 |
| Cabin Width (ft) | — | 7.7 | 8.2 |
| Cabin Height (ft) | — | 6.2 | 6.25 |
| Cabin Length (ft) | — | 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 |