Airbus Helicopters H155 vs Airbus Helicopters H215 vs Sikorsky S 92
The Airbus Helicopters H155 is a medium twin typically positioned for corporate, EMS, and offshore support in shorter to mid-range missions. It generally carries around 12–13 passengers in a high-density layout (often fewer in VIP/EMS configurations) and offers a practical range on the order of roughly 450–550 nautical miles depending on equipment, fuel options, and reserves. The Airbus Helicopters H215 (Super Puma family) sits in the heavy/large twin class, aimed at utility and offshore transport with higher payload and cabin volume. It is commonly configured for about 19 passengers and typically achieves a range in the neighborhood of about 430–540 nautical miles, varying with tanking, payload, and environmental conditions. The Sikorsky S-92 is also a heavy twin, widely used for offshore oil and gas and SAR, generally comparable to or slightly above the H215 in offshore transport role. It is often configured for 19 passengers and typically offers around 500–600 nautical miles of range, again depending on configuration, reserves, and operating profile.
| Spec | AIRBUS H155 | AIRBUS H215 | Sikorsky S-92 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 11.06 | $ 19.07 | $ 19.79 |
| Min Crew | 2 | 2 | 2 |
| Total Seats | 14 | 21 | 21 |
| Flight Rules | IFR | IFR | IFR |
| Manufacturer | Airbus Helicopters | Airbus Helicopters | Sikorsky |
| Aircraft Name | H155 | H215 | S-92 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 423 | 468 | 439 |
| DOC / nm / Seat | $ 0.74 | $ 0.91 | $ 0.94 |
| Max Cabin Seats | 12 | 22 | 19 |
| OEM Verification | Un-Verified | Un-Verified | Un-Verified |
| Useful Load (lbs) | 4012 | 8903 | 7417 |
| Standard Cabin Seats | 12 | 19 | 19 |
| Direct Operating Cost | $ 1,593 | $ 2,708 | $ 3,068 |
| Flight Deck (Base Spec) | EFIS | EFIS | EFIS |
| Max Cruise Speed (ktas) | 144 | 142 | 155 |
| Base Aircraft Price (USD) | $14,800,000 | $27,500,000 | $30,650,000 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 2 |
| Total Seats | 14 | 21 | 21 |
| Configuration | Green Interior | — | — |
| Max Cabin Seats | 12 | 22 | 19 |
| Standard Cabin Seats | 12 | 19 | 19 |
| Engine | |||
| FADEC | Yes | Yes | Yes |
| Model | Arriel 2C2 | Makila 1A1 | CT7-8A |
| Fuel Type | JetFuel | JetFuel | JetFuel |
| TBO (hrs) | 4000 | 3000 | 4000 |
| Horsepower | 943 | 1820 | 2520 |
| No. of Engines | 2 | 2 | 1 |
| Fuel Capacity (gal) | 332 | 540 | 760 |
| Dimensions | |||
| Length (ft) | 46.9 | 61.4 | — |
| Overall Height (ft) | 14.3 | 16.2 | 17.8 |
| Rotor Diameter (ft) | 41.1 | 51.2 | — |
| Cabin Volume (cu. ft) | 235.2 | 473.9 | 775 |
| Baggage Volume Ext. (cu. ft) | 88.3 | — | 140 |