Airbus Helicopters H175 vs Airbus Helicopters H215 vs Sikorsky S 92
The Airbus Helicopters H175 is a modern medium twin aimed at offshore transport and search-and-rescue, typically optimized for medium-range missions with a practical range on the order of a few hundred nautical miles, and it commonly carries around 16 passengers in offshore seating (with higher-density layouts possible depending on regulations and operator choices). The Airbus Helicopters H215 is a heavier, Super Puma–class twin designed for utility and offshore work; it generally offers similar passenger counts in the mid-to-high teens, but its strengths are robust lifting capability and proven operations, with range broadly comparable to other heavy twins depending heavily on fuel fit and payload. The Sikorsky S-92 is a heavy twin purpose-built for offshore oil and gas and SAR; it is typically configured for about 19 passengers in standard offshore layouts and is often chosen for longer offshore legs, with a practical range that is usually competitive at the upper end of this group. Overall, H175 sits in the medium category, while H215 and S-92 are heavy helicopters, with S-92 commonly leading in standard passenger capacity and often in offshore mission radius.
| Spec | AIRBUS H175 | AIRBUS H215 | Sikorsky S-92 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 13.53 | $ 19.07 | $ 19.79 |
| Min Crew | 2 | 2 | 2 |
| Total Seats | 18 | 21 | 21 |
| Flight Rules | IFR | IFR | IFR |
| Manufacturer | Airbus Helicopters | Airbus Helicopters | Sikorsky |
| Aircraft Name | H175 | H215 | S-92 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 573 | 468 | 439 |
| DOC / nm / Seat | $ 0.75 | $ 0.91 | $ 0.94 |
| Max Cabin Seats | 18 | 22 | 19 |
| OEM Verification | Un-Verified | Un-Verified | Un-Verified |
| Useful Load (lbs) | 6797 | 8903 | 7417 |
| Standard Cabin Seats | 16 | 19 | 19 |
| Direct Operating Cost | $ 2,016 | $ 2,708 | $ 3,068 |
| Flight Deck (Base Spec) | EFIS | EFIS | EFIS |
| Max Cruise Speed (ktas) | 149 | 142 | 155 |
| Base Aircraft Price (USD) | $17,900,000 | $27,500,000 | $30,650,000 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 2 |
| Total Seats | 18 | 21 | 21 |
| Max Cabin Seats | 18 | 22 | 19 |
| Standard Cabin Seats | 16 | 19 | 19 |
| Engine | |||
| FADEC | Yes | Yes | Yes |
| Model | PT6A-67E | Makila 1A1 | CT7-8A |
| Fuel Type | JetFuel | JetFuel | JetFuel |
| TBO (hrs) | 3500 | 3000 | 4000 |
| Horsepower | 1775 | 1820 | 2520 |
| No. of Engines | 2 | 2 | 1 |
| Fuel Capacity (gal) | — | 540 | 760 |
| Dimensions | |||
| Length (ft) | 59.2 | 61.4 | — |
| Overall Height (ft) | 17.5 | 16.2 | 17.8 |
| Rotor Diameter (ft) | 48.5 | 51.2 | — |
| Cabin Volume (cu. ft) | 423.8 | 473.9 | 775 |
| Baggage Volume Ext. (cu. ft) | 81.9 | — | 140 |