Airbus Helicopters H225 vs Sikorsky S 92 vs Leonardaw189
Commercial aircraft are often compared by category, which broadly tracks mission and size. Regional jets and turboprops serve short-haul routes between smaller cities, typically flying a few hundred to around 1,500 nautical miles and carrying roughly 30 to 90 passengers, prioritizing frequency and lower operating costs on thinner demand. Single-aisle narrowbody airliners are the workhorses of domestic and short-to-medium international travel, commonly offering about 150 to 220 seats with ranges that often span roughly 2,500 to 4,000+ nautical miles, balancing capacity, efficiency, and airport compatibility. Widebody twin-aisle aircraft are built for long-haul and high-density markets, usually seating about 250 to 400+ passengers and reaching 6,000 to 8,000+ nautical miles, enabling nonstop intercontinental routes with greater cargo capability and passenger comfort options. At the top end, very large widebodies maximize capacity on slot-constrained hubs, often carrying 450+ passengers, but they are less common today as airlines favor flexible, long-range midsize widebodies. Ultimately, higher passenger capacity generally correlates with longer range and higher trip costs, while smaller categories emphasize access and frequency.
| 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 |