Airbus Helicopters H225 vs Bombardier Global 7500 vs Dassault Falcon 8x vs Md Helicopters (mcdonnell Douglas) 902 Explorer
The Airbus H225 and the MD Helicopters (McDonnell Douglas) 902 Explorer are helicopters, while the Bombardier Global 7500 and Dassault Falcon 8X are long‑range business jets. In category terms, the H225 is a heavy, twin‑engine utility/transport helicopter often used for offshore and SAR missions, whereas the 902 Explorer is a light twin‑engine helicopter typically used for EMS, law enforcement, and corporate shuttle roles. The Global 7500 and Falcon 8X are ultra‑long‑range corporate jets designed for intercontinental travel. For range, the jets dominate: the Global 7500 is roughly 7,700 nautical miles, and the Falcon 8X about 6,450 nautical miles (both depending on payload and conditions). The H225 is typically around 500–600 nautical miles, and the 902 Explorer around 300–400 nautical miles, varying with reserves, load, and mission profile. Passenger capacity also differs: the Global 7500 and Falcon 8X commonly seat about 8–16 passengers in executive layouts. The H225 can carry far more in transport configurations (often around 19, up to roughly two dozen), while the 902 Explorer is usually around 6–8 passengers.
| Spec | AIRBUS H225 | Bombardier Global 7500 | Dassault Falcon 8X |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 9.50 | $ 7.66 |
| Min Crew | 2 | 2 | 2 |
| Total Seats | 21 | 14 | 17 |
| Flight Rules | IFR | — | — |
| Manufacturer | Airbus Helicopters | Bombardier | Dassault Falcon |
| Aircraft Name | H225 | Global 7500 | 8X |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 7700 | 6450 |
| DOC / nm / Seat | $ 0.99 | $ 0.79 | $ 0.64 |
| Max Cabin Seats | 28 | 19 | 16 |
| OEM Verification | Un-Verified | VERIFIED | VERIFIED |
| Useful Load (lbs) | 11929 | — | 36900 |
| Standard Cabin Seats | 19 | 12 | 14 |
| Direct Operating Cost | $ 2,963 | $ 4,900 | $ 3,805 |
| Flight Deck (Base Spec) | EFIS | Bombardier Vision (Pro Line Fusion) | Honeywell Primus EASy II |
| Max Cruise Speed (ktas) | 142 | 516 | 516 |
| Base Aircraft Price (USD) | $ 29,500,000 | $75,000,000 | $ 62,500,000 |
| Aircraft Type | — | Business Jet | — |
| Cabin | |||
| Cockpit | 2 | 2 | 3 |
| Min Crew | 2 | 2 | 2 |
| Total Seats | 21 | 14 | 17 |
| Max Cabin Seats | 28 | 19 | 16 |
| Standard Cabin Seats | 19 | 12 | 14 |
| Lavatory | — | 2 Enclosed Flushing | 2 Enclosed Flushing |
| Crew Rest | — | Yes | No |
| Jump Seat | — | Yes | Yes |
| Galley Location | — | FWD | FWD |
| Lavatory Location | — | FWD / AFT | FWD / AFT |
| Galley / Refreshment | — | Galley | Galley |
| Max Cabin Altitude (ft) | — | 4500 | 3900 |
| Cabin Pressure (psi) | — | — | 10.2 |
| SL Cabin Altitude (ft) | — | — | 29200 |
| Engine | |||
| FADEC | Yes | Yes | Yes |
| Model | Makila 2A1 | Passport | PW307D |
| Fuel Type | JetFuel | — | — |
| TBO (hrs) | 3500 | On-Condition | On-Condition |
| Horsepower | 2100 | — | — |
| No. of Engines | 2 | 2 | 3 |
| Fuel Capacity (gal) | 684 | — | — |
| Flat Rating | — | ISA + 15 | ISA + 17 |
| Thrust (lbs) | — | 18920 | 6722 |
| Dimensions | |||
| Length (ft) | 63.4 | 111 | 80.2 |
| Overall Height (ft) | 16.3 | 27 | 26.1 |
| Rotor Diameter (ft) | 53.2 | — | — |
| Cabin Volume (cu. ft) | 547 | — | 1695 |
| Wingspan (ft) | — | 104 | 86.3 |
| Cabin Width (ft) | — | 8 | 7.7 |
| Cabin Height (ft) | — | 6.2 | 6.2 |
| Cabin Length (ft) | — | 54.5 | 42.7 |
| Cabin Width - Floor (ft) | — | — | 6.3 |
| Cabin Length - Seating (ft) | — | — | 29.2 |
| Baggage Volume Int. (cu. ft) | — | — | 140 |