Airbus Helicopters H160 vs Sikorsky S 92
The Airbus Helicopters H160 is a modern medium twin designed for efficiency and versatility across offshore transport, emergency medical services, and corporate/VIP missions, while the Sikorsky S-92 is a larger heavy twin optimized for high-capacity offshore and search-and-rescue work with a strong emphasis on payload and all-weather robustness. In category terms, the H160 generally sits in the medium-class segment, whereas the S-92 is typically considered a heavy-class helicopter. For range, the H160 is aimed at medium-range missions and is commonly quoted around the mid-400 to roughly 500 nautical mile class depending on configuration and reserves, while the S-92 is often cited in a similar broad band but can be configured to emphasize longer legs, typically around the 500 nautical mile class, again depending on payload, fuel, and mission equipment. Passenger capacity is where the difference is most pronounced: the H160 typically carries about 12 passengers in an offshore layout, while the S-92 commonly carries around 19 passengers, making it better suited to moving larger crews per flight.
| Spec | AIRBUS H160 | Sikorsky S-92 |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| Min Crew | 2 | 2 |
| Total Seats | 14 | 21 |
| Flight Rules | IFR | IFR |
| Manufacturer | Airbus Helicopters | Sikorsky |
| Aircraft Name | H160 | S-92 |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 460 | 439 |
| Max Cabin Seats | 12 | 19 |
| OEM Verification | Un-Verified | Un-Verified |
| Useful Load (lbs) | 3992 | 7417 |
| Standard Cabin Seats | 12 | 19 |
| Flight Deck (Base Spec) | EFIS | EFIS |
| Max Cruise Speed (ktas) | 155 | 155 |
| Base Aircraft Price (USD) | $14,000,000 | $30,650,000 |
| DOC / nm | — | $ 19.79 |
| DOC / nm / Seat | — | $ 0.94 |
| Direct Operating Cost | — | $ 3,068 |
| Cabin | ||
| Cockpit | 2 | 2 |
| Min Crew | 2 | 2 |
| Total Seats | 14 | 21 |
| Configuration | Green Interior | — |
| Max Cabin Seats | 12 | 19 |
| Standard Cabin Seats | 12 | 19 |
| Engine | ||
| FADEC | Yes | Yes |
| Model | HE Arrano | CT7-8A |
| Fuel Type | JetFuel | JetFuel |
| TBO (hrs) | 4000 | 4000 |
| No. of Engines | 2 | 1 |
| Horsepower | — | 2520 |
| Fuel Capacity (gal) | — | 760 |
| Dimensions | ||
| Length (ft) | 39.4 | — |
| Overall Height (ft) | 13.1 | 17.8 |
| Rotor Diameter (ft) | 45.2 | — |
| Cabin Volume (cu. ft) | — | 775 |
| Baggage Volume Ext. (cu. ft) | — | 140 |