Airbus Helicopters H225 vs Dassault Falcon 8x vs Gulfstream G700 vs Piaggio Avanti Evo
The Airbus H225 is a heavy twin‑engine helicopter, best suited to offshore, search‑and‑rescue, and utility missions rather than point‑to‑point jet travel. It typically carries around 16–19 passengers (higher in certain layouts) and has a range on the order of roughly 450–500 nautical miles, depending on reserves and configuration. The Dassault Falcon 8X is a long‑range trijet business jet focused on efficiency and field performance, commonly seating about 12–16 passengers in executive layouts and offering roughly 6,400 nautical miles of range. The Gulfstream G700 is an ultra‑long‑range large‑cabin business jet emphasizing maximum cabin volume and speed; it typically accommodates about 13–19 passengers and delivers about 7,500 nautical miles of range. The Piaggio Avanti EVO is a high‑speed twin turboprop business aircraft aimed at shorter regional missions and lower operating costs. It generally seats about 6–9 passengers and offers roughly 1,500–1,800 nautical miles of range, depending on payload and conditions.
| Spec | AIRBUS H225 | Dassault Falcon 8X | Gulfstream G700 | Piaggio Avanti EVO |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 3 | 2 |
| DOC / nm | $ 20.87 | $ 7.66 | — | — |
| Min Crew | 2 | 2 | 4 | 1 |
| Total Seats | 21 | 17 | 16 | 8 |
| Flight Rules | IFR | — | — | IFR |
| Manufacturer | Airbus Helicopters | Dassault Falcon | Gulfstream | Piaggio |
| Aircraft Name | H225 | 8X | G700 | Avanti EVO |
| Certification | FAA / EASA | FAA / EASA | In Development | FAA / EASA |
| Max Range (nm) | 454 | 6450 | 7500 | 1530 |
| DOC / nm / Seat | $ 0.99 | $ 0.64 | — | — |
| Max Cabin Seats | 28 | 16 | 19 | 7 |
| OEM Verification | Un-Verified | VERIFIED | Un-Verified | Un-Verified |
| Useful Load (lbs) | 11929 | 36900 | — | 3775 |
| Standard Cabin Seats | 19 | 14 | 12 | 6 |
| Direct Operating Cost | $ 2,963 | $ 3,805 | — | — |
| Flight Deck (Base Spec) | EFIS | Honeywell Primus EASy II | Gulfstream Symmetry Flight Deck | Rockwell Collins Pro Line 21 |
| Max Cruise Speed (ktas) | 142 | 516 | 516 | 400 |
| Base Aircraft Price (USD) | $ 29,500,000 | $ 62,500,000 | $78,000,000 | $ 7,695,000 |
| Cabin | ||||
| Cockpit | 2 | 3 | 2 | 2 |
| Min Crew | 2 | 2 | 4 | 1 |
| Total Seats | 21 | 17 | 16 | 8 |
| Max Cabin Seats | 28 | 16 | 19 | 7 |
| Standard Cabin Seats | 19 | 14 | 12 | 6 |
| Lavatory | — | 2 Enclosed Flushing | — | No |
| Crew Rest | — | No | Optional | — |
| Jump Seat | — | Yes | Yes | — |
| Galley Location | — | FWD | FWD | — |
| Lavatory Location | — | FWD / AFT | FWD / AFT | — |
| Cabin Pressure (psi) | — | 10.2 | — | 9 |
| Galley / Refreshment | — | Galley | — | No |
| SL Cabin Altitude (ft) | — | 29200 | — | 24000 |
| Max Cabin Altitude (ft) | — | 3900 | — | 6600 |
| Engine | ||||
| FADEC | Yes | Yes | — | Yes |
| Model | Makila 2A1 | PW307D | Pearl 700 | PT6A–66B |
| Fuel Type | JetFuel | — | — | — |
| TBO (hrs) | 3500 | On-Condition | On Condition | 3600 |
| Horsepower | 2100 | — | — | 850 |
| No. of Engines | 2 | 3 | 2 | 2 |
| Fuel Capacity (gal) | 684 | — | — | — |
| Flat Rating | — | ISA + 17 | — | ISA + 28 |
| Thrust (lbs) | — | 6722 | 18250 | — |
| Fuel Burn (gph) | — | — | — | 100 |
| Dimensions | ||||
| Length (ft) | 63.4 | 80.2 | 109.9 | 47.3 |
| Overall Height (ft) | 16.3 | 26.1 | 25.4 | 13.1 |
| Rotor Diameter (ft) | 53.2 | — | — | — |
| Cabin Volume (cu. ft) | 547 | 1695 | — | — |
| Wingspan (ft) | — | 86.3 | 103 | 47.1 |
| Cabin Width (ft) | — | 7.7 | 8.2 | 6.1 |
| Cabin Height (ft) | — | 6.2 | 6.25 | 5.8 |
| Cabin Length (ft) | — | 42.7 | 56.9 | 14.9 |
| Cabin Width - Floor (ft) | — | 6.3 | — | 3.5 |
| Cabin Length - Seating (ft) | — | 29.2 | — | — |
| Baggage Volume Int. (cu. ft) | — | 140 | 195 | 35.2 |
| Aisle Step (ft) | — | — | Flat Floor | — |