Airbus Helicopters H225 vs Embraer Legacy 650 E vs Sikorsky S 92
The Airbus H225 and Sikorsky S-92 are large twin‑engine helicopters, typically used for offshore transport, SAR, and utility missions, while the Embraer Legacy 650E is a long‑range business jet aimed at corporate and VIP travel. In range, the Legacy 650E generally leads, offering intercity and some transcontinental capability (roughly around 3,900 nautical miles depending on conditions and payload), whereas the H225 and S-92 have much shorter ranges typical of heavy helicopters (commonly in the few‑hundred‑nautical‑mile class, varying widely with reserves, payload, and mission equipment). Passenger capacity also differs by role: the Legacy 650E is usually configured for about 13 passengers in an executive cabin, while the H225 and S-92 can be arranged for higher headcounts in transport layouts, often around the high‑teens to low‑twenties, with offshore seating commonly near 19. Overall, choose the Legacy 650E for speed and long point‑to‑point travel between airports, and the H225 or S-92 when vertical lift, remote access, and specialized mission capability matter more than range.
| Spec | AIRBUS H225 | Sikorsky S-92 |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| DOC / nm | $ 20.87 | $ 19.79 |
| Min Crew | 2 | 2 |
| Total Seats | 21 | 21 |
| Flight Rules | IFR | IFR |
| Manufacturer | Airbus Helicopters | Sikorsky |
| Aircraft Name | H225 | S-92 |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 439 |
| DOC / nm / Seat | $ 0.99 | $ 0.94 |
| Max Cabin Seats | 28 | 19 |
| OEM Verification | Un-Verified | Un-Verified |
| Useful Load (lbs) | 11929 | 7417 |
| Standard Cabin Seats | 19 | 19 |
| Direct Operating Cost | $ 2,963 | $ 3,068 |
| Flight Deck (Base Spec) | EFIS | EFIS |
| Max Cruise Speed (ktas) | 142 | 155 |
| Base Aircraft Price (USD) | $ 29,500,000 | $30,650,000 |
| Cabin | ||
| Cockpit | 2 | 2 |
| Min Crew | 2 | 2 |
| Total Seats | 21 | 21 |
| Max Cabin Seats | 28 | 19 |
| Standard Cabin Seats | 19 | 19 |
| Engine | ||
| FADEC | Yes | Yes |
| Model | Makila 2A1 | CT7-8A |
| Fuel Type | JetFuel | JetFuel |
| TBO (hrs) | 3500 | 4000 |
| Horsepower | 2100 | 2520 |
| No. of Engines | 2 | 1 |
| Fuel Capacity (gal) | 684 | 760 |
| Dimensions | ||
| Length (ft) | 63.4 | — |
| Overall Height (ft) | 16.3 | 17.8 |
| Rotor Diameter (ft) | 53.2 | — |
| Cabin Volume (cu. ft) | 547 | 775 |
| Baggage Volume Ext. (cu. ft) | — | 140 |