LeonardoAW189 vs Airbus Helicopters H225 vs Sikorsky S 92
Aircraft are often compared by category, range, and passenger capacity because these factors roughly determine mission and economics. Small general-aviation pistons and light turboprops typically carry 2–9 passengers and are suited to short hops, usually a few hundred to about 1,500 miles depending on speed, fuel, and payload. Business jets span light, midsize, and large-cabin types, generally carrying 6–19 passengers; their range can vary from roughly 1,500 miles for light jets to 6,000+ miles for long-range models, enabling nonstop regional to intercontinental travel. Regional airliners, including turboprops and regional jets, commonly seat about 30–100 passengers and cover short to medium sectors, often around 300–2,000 miles, feeding larger hubs. Narrow-body mainline jets, such as typical single-aisle airliners, usually carry about 140–240 passengers and are optimized for high-frequency routes of roughly 1,500–4,000 miles. Wide-body jets are built for high capacity and long distances, often seating 250–450+ passengers with ranges around 4,000–9,000 miles, supporting long-haul and ultra-long-haul operations.
| 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 |