Airbus Helicopters H225 vs Bombardier Global 7500 vs Dassault Falcon 8x vs Sikorsky S 92
The Airbus H225 and Sikorsky S-92 are twin‑engine helicopters designed for vertical lift missions such as offshore transport and search-and-rescue, while the Bombardier Global 7500 and Dassault Falcon 8X are long‑range business jets built for intercontinental travel. In category terms, the H225 and S-92 prioritize hover capability, short-field/ship operations, and point-to-point access without runways; the Global 7500 and Falcon 8X prioritize high cruise speeds and high-altitude efficiency between major airports. For range, the jets dominate: the Global 7500 is an ultra‑long‑range jet capable of roughly 7,700 nautical miles, and the Falcon 8X is also ultra‑long‑range at about 6,450 nautical miles. Helicopter range is much shorter by comparison: an H225 is typically on the order of a few hundred nautical miles (often around ~450 nm depending on configuration), and an S-92 is similarly in the several-hundred‑nautical‑mile class (often ~500 nm). Passenger capacity also differs: the Global 7500 and Falcon 8X generally seat around 12–19 in executive layouts, whereas H225 and S-92 can be configured for higher-density seating, commonly around 16–19 and up to the low‑20s in transport layouts.
| Spec | AIRBUS H225 | Bombardier Global 7500 | Dassault Falcon 8X | Sikorsky S-92 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 9.50 | $ 7.66 | $ 19.79 |
| Min Crew | 2 | 2 | 2 | 2 |
| Total Seats | 21 | 14 | 17 | 21 |
| Flight Rules | IFR | — | — | IFR |
| Manufacturer | Airbus Helicopters | Bombardier | Dassault Falcon | Sikorsky |
| Aircraft Name | H225 | Global 7500 | 8X | S-92 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 7700 | 6450 | 439 |
| DOC / nm / Seat | $ 0.99 | $ 0.79 | $ 0.64 | $ 0.94 |
| Max Cabin Seats | 28 | 19 | 16 | 19 |
| OEM Verification | Un-Verified | VERIFIED | VERIFIED | Un-Verified |
| Useful Load (lbs) | 11929 | — | 36900 | 7417 |
| Standard Cabin Seats | 19 | 12 | 14 | 19 |
| Direct Operating Cost | $ 2,963 | $ 4,900 | $ 3,805 | $ 3,068 |
| Flight Deck (Base Spec) | EFIS | Bombardier Vision (Pro Line Fusion) | Honeywell Primus EASy II | EFIS |
| Max Cruise Speed (ktas) | 142 | 516 | 516 | 155 |
| Base Aircraft Price (USD) | $ 29,500,000 | $75,000,000 | $ 62,500,000 | $30,650,000 |
| Aircraft Type | — | Business Jet | — | — |
| Cabin | ||||
| Cockpit | 2 | 2 | 3 | 2 |
| Min Crew | 2 | 2 | 2 | 2 |
| Total Seats | 21 | 14 | 17 | 21 |
| Max Cabin Seats | 28 | 19 | 16 | 19 |
| Standard Cabin Seats | 19 | 12 | 14 | 19 |
| 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 | Yes |
| Model | Makila 2A1 | Passport | PW307D | CT7-8A |
| Fuel Type | JetFuel | — | — | JetFuel |
| TBO (hrs) | 3500 | On-Condition | On-Condition | 4000 |
| Horsepower | 2100 | — | — | 2520 |
| No. of Engines | 2 | 2 | 3 | 1 |
| Fuel Capacity (gal) | 684 | — | — | 760 |
| 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 | 17.8 |
| Rotor Diameter (ft) | 53.2 | — | — | — |
| Cabin Volume (cu. ft) | 547 | — | 1695 | 775 |
| 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 | — |
| Baggage Volume Ext. (cu. ft) | — | — | — | 140 |