Airbus Helicopters H225 vs Beechcraft King Air 360 Er vs Dassault Falcon 8x vs Gulfstream G700
The Airbus H225 is a heavy twin‑engine helicopter suited to offshore, SAR, and utility missions rather than long-distance point‑to‑point travel. Its range is typically on the order of roughly 500–700 nautical miles (mission and tank fit dependent) and it can carry about 19 passengers in a high‑density layout, with fewer in VIP or mission configurations. The Beechcraft King Air 360ER is a twin‑turboprop airplane optimized for regional missions and short/medium runways. It offers roughly 1,500–1,800 nautical miles of range (depending on payload and reserves) and typically seats about 6–9 passengers in executive layouts, with higher-density options. The Dassault Falcon 8X is an ultra‑long‑range trijet business jet designed for intercontinental travel, offering about 6,400 nautical miles of range and commonly accommodating around 12–16 passengers (with certified maximums higher, depending on configuration). The Gulfstream G700 is a flagship large‑cabin ultra‑long‑range business jet, generally around 7,500 nautical miles of range and typically configured for about 12–19 passengers, emphasizing spacious cabin zones and nonstop global city pairs.
| 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 |