Leonardo Aw189 vs Sikorsky S 92
The Leonardo AW189 and Sikorsky S-92 sit in different weight and mission categories, which drives most of their practical differences. The AW189 is generally considered a “super-medium” twin, optimized for offshore transport and SAR-style flexibility with lower operating weight and typically lower trip costs. The S-92 is a heavier, “heavy” twin designed for higher payload and more demanding offshore missions, and it is often selected where maximum capacity and cabin volume are priorities. On range, both are offshore-capable, but the S-92 commonly offers greater practical reach when configured for longer legs because of its larger fuel and payload margins, while the AW189’s range is strong for the super-medium class but usually comes in below a heavy twin in comparable mission configurations. For passenger capacity, AW189 layouts are typically in the mid-to-high teens, while the S-92 commonly seats more, often around the high teens to low twenties depending on interior and regulatory configuration. Exact figures vary by cabin fit, fuel reserves, and mission equipment.
| Spec | AGUSTA / LEONARDO AW189 | Sikorsky S-92 |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| DOC / nm | $ 15.57 | $ 19.79 |
| Min Crew | 1 | 2 |
| Total Seats | 21 | 21 |
| Flight Rules | IFR | IFR |
| Manufacturer | Leonardo | Sikorsky |
| Aircraft Name | AW189 | S-92 |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 651 | 439 |
| DOC / nm / Seat | $ 0.74 | $ 0.94 |
| Max Cabin Seats | 19 | 19 |
| OEM Verification | Un-Verified | Un-Verified |
| Standard Cabin Seats | 19 | 19 |
| Direct Operating Cost | $ 2,413 | $ 3,068 |
| Flight Deck (Base Spec) | EFIS | EFIS |
| Max Cruise Speed (ktas) | 155 | 155 |
| Base Aircraft Price (USD) | $2,413,000 | $30,650,000 |
| Useful Load (lbs) | — | 7417 |
| Cabin | ||
| Cockpit | 2 | 2 |
| Min Crew | 1 | 2 |
| Total Seats | 21 | 21 |
| Max Cabin Seats | 19 | 19 |
| Standard Cabin Seats | 19 | 19 |
| Engine | ||
| FADEC | Yes | Yes |
| Model | CT7-2E1 | CT7-8A |
| Fuel Type | JetFuel | JetFuel |
| TBO (hrs) | 4000 | 4000 |
| Horsepower | 1983 | 2520 |
| No. of Engines | 2 | 1 |
| Fuel Capacity (gal) | — | 760 |
| Dimensions | ||
| Length (ft) | 57.8 | — |
| Overall Height (ft) | 16.6 | 17.8 |
| Rotor Diameter (ft) | 48 | — |
| Cabin Volume (cu. ft) | 395 | 775 |
| Baggage Volume Ext. (cu. ft) | 85 | 140 |