Airbus Helicopters H175 vs Airbus Helicopters H225 vs Leonardo Aw139 vs Sikorsky S 76d vs Sikorsky S 92
The Airbus H175 and Leonardo AW139 sit in the “medium” twin category, typically used for offshore transport and corporate/VIP missions. In general terms, the H175 offers a strong blend of range and cabin volume, while the AW139 is known for versatile configurations and competitive reach; both commonly seat around 12–16 passengers depending on layout and mission equipment. The Sikorsky S-76D is a smaller “medium/light-medium” twin, optimized for efficient short-to-medium sectors; it usually carries fewer passengers, often about 8–12, and tends to have shorter range than the larger medium twins. Stepping up, the Airbus H225 and Sikorsky S-92 are “heavy” twin helicopters aimed at higher-capacity offshore and SAR roles. They typically provide the longest ranges of this group and the largest cabins, with common passenger capacities roughly in the 16–19 range (again configuration-dependent). Overall, AW139/H175 balance medium-range efficiency and cabin space, S-76D prioritizes smaller-cabin efficiency, and H225/S-92 emphasize maximum payload, capacity, and longer-range offshore capability.
| Spec | AIRBUS H175 | AIRBUS H225 | AGUSTA / LEONARDO AW139 | Sikorsky S-76D | Sikorsky S-92 |
|---|---|---|---|---|---|
| Summary | |||||
| Cockpit | 2 | 2 | 2 | 2 | 2 |
| DOC / nm | $ 13.53 | $ 20.87 | $ 11.69 | $ 11.49 | $ 19.79 |
| Min Crew | 2 | 2 | 2 | 2 | 2 |
| Total Seats | 18 | 21 | 17 | 12 | 21 |
| Flight Rules | IFR | IFR | IFR | IFR | IFR |
| Manufacturer | Airbus Helicopters | Airbus Helicopters | Leonardo | Sikorsky | Sikorsky |
| Aircraft Name | H175 | H225 | AW139 | S-76D | S-92 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 573 | 454 | 573 | 441 | 439 |
| DOC / nm / Seat | $ 0.75 | $ 0.99 | $ 0.69 | $ 0.96 | $ 0.94 |
| Max Cabin Seats | 18 | 28 | 15 | 10 | 19 |
| OEM Verification | Un-Verified | Un-Verified | Un-Verified | Un-Verified | Un-Verified |
| Useful Load (lbs) | 6797 | 11929 | 4701 | — | 7417 |
| Standard Cabin Seats | 16 | 19 | 15 | 10 | 19 |
| Direct Operating Cost | $ 2,016 | $ 2,963 | $ 1,929 | $ 1,781 | $ 3,068 |
| Flight Deck (Base Spec) | EFIS | EFIS | EFIS | Thales TopDeck | EFIS |
| Max Cruise Speed (ktas) | 149 | 142 | 165 | 155 | 155 |
| Base Aircraft Price (USD) | $17,900,000 | $ 29,500,000 | $15,900,000 | $14,900,000 | $30,650,000 |
| Cabin | |||||
| Cockpit | 2 | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 2 | 2 | 2 |
| Total Seats | 18 | 21 | 17 | 12 | 21 |
| Max Cabin Seats | 18 | 28 | 15 | 10 | 19 |
| Standard Cabin Seats | 16 | 19 | 15 | 10 | 19 |
| Engine | |||||
| FADEC | Yes | Yes | Yes | Yes | Yes |
| Model | PT6A-67E | Makila 2A1 | PT6C-67C | PW210S | CT7-8A |
| Fuel Type | JetFuel | JetFuel | JetFuel | JetFuel | JetFuel |
| TBO (hrs) | 3500 | 3500 | 5000 | 4000 | 4000 |
| Horsepower | 1775 | 2100 | 1679 | 1077 | 2520 |
| No. of Engines | 2 | 2 | 2 | 1 | 1 |
| Fuel Capacity (gal) | — | 684 | 414 | 296 | 760 |
| Dimensions | |||||
| Length (ft) | 59.2 | 63.4 | 54.7 | 52.5 | — |
| Overall Height (ft) | 17.5 | 16.3 | 16.4 | 14.5 | 17.8 |
| Rotor Diameter (ft) | 48.5 | 53.2 | 54.7 | 44 | — |
| Cabin Volume (cu. ft) | 423.8 | 547 | 282 | — | 775 |
| Baggage Volume Ext. (cu. ft) | 81.9 | — | 120 | — | 140 |