Airbus Helicopters H175 vs Sikorsky S 92
The Airbus Helicopters H175 and Sikorsky S-92 are both medium, twin‑engine offshore-capable helicopters, but they sit in slightly different weight and mission emphases. The H175 is typically positioned in the “super-medium” class, optimized for offshore transport and SAR with a strong focus on efficiency and modern avionics. The S-92 is generally considered a heavier “medium” helicopter and is widely used for offshore oil and gas and government/VIP roles, often valued for its robust payload and mature global support base. In range, both can be equipped for long offshore legs, but the S-92 commonly offers a longer published maximum range depending on configuration, while the H175 is competitive on practical offshore mission ranges where reserves and payload matter. For passenger capacity, both can be configured for offshore seating around the high teens. The H175 is often arranged around 16–18 passengers, while the S-92 is frequently configured around 19 passengers, with layouts varying by operator, fuel tanks, and mission equipment.
| Spec | AIRBUS H175 | Sikorsky S-92 |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| DOC / nm | $ 13.53 | $ 19.79 |
| Min Crew | 2 | 2 |
| Total Seats | 18 | 21 |
| Flight Rules | IFR | IFR |
| Manufacturer | Airbus Helicopters | Sikorsky |
| Aircraft Name | H175 | S-92 |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 573 | 439 |
| DOC / nm / Seat | $ 0.75 | $ 0.94 |
| Max Cabin Seats | 18 | 19 |
| OEM Verification | Un-Verified | Un-Verified |
| Useful Load (lbs) | 6797 | 7417 |
| Standard Cabin Seats | 16 | 19 |
| Direct Operating Cost | $ 2,016 | $ 3,068 |
| Flight Deck (Base Spec) | EFIS | EFIS |
| Max Cruise Speed (ktas) | 149 | 155 |
| Base Aircraft Price (USD) | $17,900,000 | $30,650,000 |
| Cabin | ||
| Cockpit | 2 | 2 |
| Min Crew | 2 | 2 |
| Total Seats | 18 | 21 |
| Max Cabin Seats | 18 | 19 |
| Standard Cabin Seats | 16 | 19 |
| Engine | ||
| FADEC | Yes | Yes |
| Model | PT6A-67E | CT7-8A |
| Fuel Type | JetFuel | JetFuel |
| TBO (hrs) | 3500 | 4000 |
| Horsepower | 1775 | 2520 |
| No. of Engines | 2 | 1 |
| Fuel Capacity (gal) | — | 760 |
| Dimensions | ||
| Length (ft) | 59.2 | — |
| Overall Height (ft) | 17.5 | 17.8 |
| Rotor Diameter (ft) | 48.5 | — |
| Cabin Volume (cu. ft) | 423.8 | 775 |
| Baggage Volume Ext. (cu. ft) | 81.9 | 140 |