Airbus Helicopters H225 vs Embraer Legacy 650 E vs Robinson R66 vs Sikorsky S 92
The Airbus H225 and Sikorsky S-92 are heavy, twin‑engine transport helicopters typically used for offshore energy, search and rescue, and government/VIP missions. Both prioritize lift and cabin volume over speed, with typical practical ranges on the order of roughly 450–550 nautical miles depending on payload and reserves. Passenger capacity is commonly configured around 16–19 seats, though layouts vary widely by mission equipment and safety requirements. The Robinson R66 is a light, single‑engine helicopter aimed at private, training, and light utility roles. It has a much smaller cabin and payload, carrying about 4 passengers plus a pilot (around 5 seats total), and a shorter typical range, roughly 300–350 nautical miles. The Embraer Legacy 650E is a long‑range business jet, not a helicopter, optimized for fast point‑to‑point travel. It offers far greater range than the rotorcraft—about 3,900–4,000 nautical miles—and typically seats around 13 passengers in an executive cabin (with a maximum certification closer to the high teens, depending on configuration).
| 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 |