Airbus Helicopters H225 vs Bombardier Global 7500 vs Embraer Legacy 650 E vs Sikorsky S 92
The Airbus H225 and Sikorsky S‑92 are heavy twin‑engine helicopters designed for offshore transport, search and rescue, and utility missions, while the Bombardier Global 7500 and Embraer Legacy 650E are long‑range business jets built for high‑speed intercity travel. In range, the Global 7500 is in a different class, offering roughly 7,700 nautical miles, enabling ultra‑long‑haul nonstop routes. The Legacy 650E is a large‑cabin, long‑range jet at about 3,900 nautical miles, suited to transcontinental missions and some ocean crossings. Helicopter range is much shorter: the H225 is typically around 500–600 nautical miles depending on configuration, and the S‑92 is in a similar band, often around 500 nautical miles, both strongly influenced by payload, reserves, and mission equipment. For passenger capacity, the Global 7500 typically seats about 14–19 in executive layouts. The Legacy 650E commonly seats up to 13–14. The H225 and S‑92 can be configured for higher headcounts in transport roles, often around 16–19 passengers, or fewer in VIP, SAR, or medevac layouts.
| Spec | AIRBUS H225 | Bombardier Global 7500 | Sikorsky S-92 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 9.50 | $ 19.79 |
| Min Crew | 2 | 2 | 2 |
| Total Seats | 21 | 14 | 21 |
| Flight Rules | IFR | — | IFR |
| Manufacturer | Airbus Helicopters | Bombardier | Sikorsky |
| Aircraft Name | H225 | Global 7500 | S-92 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 7700 | 439 |
| DOC / nm / Seat | $ 0.99 | $ 0.79 | $ 0.94 |
| Max Cabin Seats | 28 | 19 | 19 |
| OEM Verification | Un-Verified | VERIFIED | Un-Verified |
| Useful Load (lbs) | 11929 | — | 7417 |
| Standard Cabin Seats | 19 | 12 | 19 |
| Direct Operating Cost | $ 2,963 | $ 4,900 | $ 3,068 |
| Flight Deck (Base Spec) | EFIS | Bombardier Vision (Pro Line Fusion) | EFIS |
| Max Cruise Speed (ktas) | 142 | 516 | 155 |
| Base Aircraft Price (USD) | $ 29,500,000 | $75,000,000 | $30,650,000 |
| Aircraft Type | — | Business Jet | — |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 2 |
| Total Seats | 21 | 14 | 21 |
| Max Cabin Seats | 28 | 19 | 19 |
| Standard Cabin Seats | 19 | 12 | 19 |
| Lavatory | — | 2 Enclosed Flushing | — |
| Crew Rest | — | Yes | — |
| Jump Seat | — | Yes | — |
| Galley Location | — | FWD | — |
| Lavatory Location | — | FWD / AFT | — |
| Galley / Refreshment | — | Galley | — |
| Max Cabin Altitude (ft) | — | 4500 | — |
| Engine | |||
| FADEC | Yes | Yes | Yes |
| Model | Makila 2A1 | Passport | CT7-8A |
| Fuel Type | JetFuel | — | JetFuel |
| TBO (hrs) | 3500 | On-Condition | 4000 |
| Horsepower | 2100 | — | 2520 |
| No. of Engines | 2 | 2 | 1 |
| Fuel Capacity (gal) | 684 | — | 760 |
| Flat Rating | — | ISA + 15 | — |
| Thrust (lbs) | — | 18920 | — |
| Dimensions | |||
| Length (ft) | 63.4 | 111 | — |
| Overall Height (ft) | 16.3 | 27 | 17.8 |
| Rotor Diameter (ft) | 53.2 | — | — |
| Cabin Volume (cu. ft) | 547 | — | 775 |
| Wingspan (ft) | — | 104 | — |
| Cabin Width (ft) | — | 8 | — |
| Cabin Height (ft) | — | 6.2 | — |
| Cabin Length (ft) | — | 54.5 | — |
| Baggage Volume Ext. (cu. ft) | — | — | 140 |