Airbus Helicopters H225 vs Beechcraft King Air 360 Er vs Dassault Falcon 8x vs Md Helicopters (mcdonnell Douglas) 902 Explorer
The Airbus H225 and the MD Helicopters (McDonnell Douglas) 902 Explorer are helicopters aimed at vertical-access missions, while the Beechcraft King Air 360ER and Dassault Falcon 8X are fixed‑wing aircraft optimized for longer, faster point‑to‑point travel. The H225 is a heavy twin helicopter typically used for offshore transport, search and rescue, and utility work; it generally carries about 16–19 passengers in transport layouts and offers roughly 500–650 nautical miles of range depending on payload and reserves. The 902 Explorer is a light twin helicopter often used for EMS, law enforcement, and corporate shuttle; it typically seats about 7–8 and has around 300–400 nautical miles of range. The King Air 360ER is a twin‑turboprop business/utility aircraft, commonly configured for about 6–9 passengers, with extended range on the order of 1,500–2,000+ nautical miles depending on configuration. The Falcon 8X is a long‑range tri‑jet business aircraft, usually seating about 12–16, with intercontinental range around 6,400 nautical miles.
| Spec | AIRBUS H225 | Dassault Falcon 8X |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| DOC / nm | $ 20.87 | $ 7.66 |
| Min Crew | 2 | 2 |
| Total Seats | 21 | 17 |
| Flight Rules | IFR | — |
| Manufacturer | Airbus Helicopters | Dassault Falcon |
| Aircraft Name | H225 | 8X |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 6450 |
| DOC / nm / Seat | $ 0.99 | $ 0.64 |
| Max Cabin Seats | 28 | 16 |
| OEM Verification | Un-Verified | VERIFIED |
| Useful Load (lbs) | 11929 | 36900 |
| Standard Cabin Seats | 19 | 14 |
| Direct Operating Cost | $ 2,963 | $ 3,805 |
| Flight Deck (Base Spec) | EFIS | Honeywell Primus EASy II |
| Max Cruise Speed (ktas) | 142 | 516 |
| Base Aircraft Price (USD) | $ 29,500,000 | $ 62,500,000 |
| Cabin | ||
| Cockpit | 2 | 3 |
| Min Crew | 2 | 2 |
| Total Seats | 21 | 17 |
| Max Cabin Seats | 28 | 16 |
| Standard Cabin Seats | 19 | 14 |
| Lavatory | — | 2 Enclosed Flushing |
| Crew Rest | — | No |
| Jump Seat | — | Yes |
| Galley Location | — | FWD |
| Lavatory Location | — | 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 |
| Fuel Type | JetFuel | — |
| TBO (hrs) | 3500 | On-Condition |
| Horsepower | 2100 | — |
| No. of Engines | 2 | 3 |
| Fuel Capacity (gal) | 684 | — |
| Flat Rating | — | ISA + 17 |
| Thrust (lbs) | — | 6722 |
| Dimensions | ||
| Length (ft) | 63.4 | 80.2 |
| Overall Height (ft) | 16.3 | 26.1 |
| Rotor Diameter (ft) | 53.2 | — |
| Cabin Volume (cu. ft) | 547 | 1695 |
| Wingspan (ft) | — | 86.3 |
| Cabin Width (ft) | — | 7.7 |
| Cabin Height (ft) | — | 6.2 |
| Cabin Length (ft) | — | 42.7 |
| Cabin Width - Floor (ft) | — | 6.3 |
| Cabin Length - Seating (ft) | — | 29.2 |
| Baggage Volume Int. (cu. ft) | — | 140 |