Airbus Helicopters H225 vs Dassault Falcon 8x vs Gulfstream G700 vs Leonardo Aw189
The Airbus H225 and Leonardo AW189 are large twin‑engine helicopters suited to vertical lift missions such as offshore transport and rescue, while the Dassault Falcon 8X and Gulfstream G700 are long‑range business jets optimized for fast point‑to‑point travel between major airports. In range terms, the helicopters are short to medium range: the AW189 is roughly around 500 nautical miles and the H225 roughly around 450–500 nautical miles, depending on payload and reserves. The jets operate in an entirely different class: the Falcon 8X is about 6,450 nautical miles, and the G700 is about 7,500 nautical miles. Passenger capacity also differs by mission: the AW189 typically carries about 16–19 passengers and the H225 about 19–24 in high‑density layouts. The Falcon 8X is usually configured for roughly 12–16 passengers, while the G700 typically seats about 13–19, with both jets trading maximum seats for larger cabins, berths, and meeting areas. Overall, choose helicopters for access and flexibility; choose the jets for speed and intercontinental reach.
| Spec | AIRBUS H225 | Dassault Falcon 8X | Gulfstream G700 | AGUSTA / LEONARDO AW189 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 3 | 2 |
| DOC / nm | $ 20.87 | $ 7.66 | — | $ 15.57 |
| Min Crew | 2 | 2 | 4 | 1 |
| Total Seats | 21 | 17 | 16 | 21 |
| Flight Rules | IFR | — | — | IFR |
| Manufacturer | Airbus Helicopters | Dassault Falcon | Gulfstream | Leonardo |
| Aircraft Name | H225 | 8X | G700 | AW189 |
| Certification | FAA / EASA | FAA / EASA | In Development | FAA / EASA |
| Max Range (nm) | 454 | 6450 | 7500 | 651 |
| DOC / nm / Seat | $ 0.99 | $ 0.64 | — | $ 0.74 |
| Max Cabin Seats | 28 | 16 | 19 | 19 |
| OEM Verification | Un-Verified | VERIFIED | Un-Verified | Un-Verified |
| Useful Load (lbs) | 11929 | 36900 | — | — |
| Standard Cabin Seats | 19 | 14 | 12 | 19 |
| Direct Operating Cost | $ 2,963 | $ 3,805 | — | $ 2,413 |
| Flight Deck (Base Spec) | EFIS | Honeywell Primus EASy II | Gulfstream Symmetry Flight Deck | EFIS |
| Max Cruise Speed (ktas) | 142 | 516 | 516 | 155 |
| Base Aircraft Price (USD) | $ 29,500,000 | $ 62,500,000 | $78,000,000 | $2,413,000 |
| Cabin | ||||
| Cockpit | 2 | 3 | 2 | 2 |
| Min Crew | 2 | 2 | 4 | 1 |
| Total Seats | 21 | 17 | 16 | 21 |
| Max Cabin Seats | 28 | 16 | 19 | 19 |
| Standard Cabin Seats | 19 | 14 | 12 | 19 |
| 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 | — | Yes |
| Model | Makila 2A1 | PW307D | Pearl 700 | CT7-2E1 |
| Fuel Type | JetFuel | — | — | JetFuel |
| TBO (hrs) | 3500 | On-Condition | On Condition | 4000 |
| Horsepower | 2100 | — | — | 1983 |
| No. of Engines | 2 | 3 | 2 | 2 |
| Fuel Capacity (gal) | 684 | — | — | — |
| Flat Rating | — | ISA + 17 | — | — |
| Thrust (lbs) | — | 6722 | 18250 | — |
| Dimensions | ||||
| Length (ft) | 63.4 | 80.2 | 109.9 | 57.8 |
| Overall Height (ft) | 16.3 | 26.1 | 25.4 | 16.6 |
| Rotor Diameter (ft) | 53.2 | — | — | 48 |
| Cabin Volume (cu. ft) | 547 | 1695 | — | 395 |
| 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 | — |
| Baggage Volume Ext. (cu. ft) | — | — | — | 85 |