Leonardo Aw139 vs Leonardo Aw189 vs Sikorsky S 92 vs Airbus Helicopters H225
Commercial aircraft are often compared by category, which broadly tracks size and mission. Regional aircraft, including small regional jets and turboprops, typically serve short, high-frequency routes between smaller cities and hubs. Their range is generally short to lower-medium, and passenger capacity is usually modest, making them efficient when demand is thinner or runways are constrained. Narrow-body mainline jets cover the core of domestic and short international flying; they offer medium range with higher capacity, balancing operating cost and flexibility for routes that are too long or too busy for regional types. Wide-body jets are built for long-haul and high-demand markets, providing long to ultra-long range and substantially larger passenger capacity, which helps spread fuel and crew costs over more seats on intercontinental flights. At the top end, very large wide-bodies maximize capacity for slot-constrained airports and dense trunk routes, though many airlines now prefer smaller wide-bodies with long range because they can profitably serve more city pairs with fewer seats. Overall, increasing category size generally raises both range and capacity, but with higher trip costs and greater dependence on strong demand.
| Spec | AIRBUS H225 | AGUSTA / LEONARDO AW139 | AGUSTA / LEONARDO AW189 | Sikorsky S-92 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 11.69 | $ 15.57 | $ 19.79 |
| Min Crew | 2 | 2 | 1 | 2 |
| Total Seats | 21 | 17 | 21 | 21 |
| Flight Rules | IFR | IFR | IFR | IFR |
| Manufacturer | Airbus Helicopters | Leonardo | Leonardo | Sikorsky |
| Aircraft Name | H225 | AW139 | AW189 | S-92 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 573 | 651 | 439 |
| DOC / nm / Seat | $ 0.99 | $ 0.69 | $ 0.74 | $ 0.94 |
| Max Cabin Seats | 28 | 15 | 19 | 19 |
| OEM Verification | Un-Verified | Un-Verified | Un-Verified | Un-Verified |
| Useful Load (lbs) | 11929 | 4701 | — | 7417 |
| Standard Cabin Seats | 19 | 15 | 19 | 19 |
| Direct Operating Cost | $ 2,963 | $ 1,929 | $ 2,413 | $ 3,068 |
| Flight Deck (Base Spec) | EFIS | EFIS | EFIS | EFIS |
| Max Cruise Speed (ktas) | 142 | 165 | 155 | 155 |
| Base Aircraft Price (USD) | $ 29,500,000 | $15,900,000 | $2,413,000 | $30,650,000 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 1 | 2 |
| Total Seats | 21 | 17 | 21 | 21 |
| Max Cabin Seats | 28 | 15 | 19 | 19 |
| Standard Cabin Seats | 19 | 15 | 19 | 19 |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | Makila 2A1 | PT6C-67C | CT7-2E1 | CT7-8A |
| Fuel Type | JetFuel | JetFuel | JetFuel | JetFuel |
| TBO (hrs) | 3500 | 5000 | 4000 | 4000 |
| Horsepower | 2100 | 1679 | 1983 | 2520 |
| No. of Engines | 2 | 2 | 2 | 1 |
| Fuel Capacity (gal) | 684 | 414 | — | 760 |
| Dimensions | ||||
| Length (ft) | 63.4 | 54.7 | 57.8 | — |
| Overall Height (ft) | 16.3 | 16.4 | 16.6 | 17.8 |
| Rotor Diameter (ft) | 53.2 | 54.7 | 48 | — |
| Cabin Volume (cu. ft) | 547 | 282 | 395 | 775 |
| Baggage Volume Ext. (cu. ft) | — | 120 | 85 | 140 |