Airbus Helicopters H135 vs Sikorsky S 92
The Airbus Helicopters H135 is a light twin-engine helicopter typically used for short-range missions such as emergency medical services, law enforcement, training, and corporate transport. Its practical range is generally in the few-hundred–nautical-mile class (often around 300–350 nm depending on configuration and reserves), and it commonly carries a pilot plus about five to six passengers in a standard cabin layout, with seating varying by mission equipment. The Sikorsky S-92 is a heavy twin-engine helicopter designed for longer-range, higher-payload operations, notably offshore oil and gas transport, search and rescue, and VIP/utility roles. It offers substantially greater range, commonly on the order of roughly 500–600+ nm depending on configuration, and a much larger cabin that is often configured for around 19 passengers plus crew in offshore transport layouts. In short, the H135 fits light, cost-efficient, shorter-hop work with smaller groups, while the S-92 is built for moving larger passenger loads farther, with more endurance and capability in demanding environments.
| Spec | AIRBUS H135 | Sikorsky S-92 |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| DOC / nm | $ 6.33 | $ 19.79 |
| Min Crew | 1 | 2 |
| Total Seats | 9 | 21 |
| Flight Rules | IFR | IFR |
| Manufacturer | Airbus Helicopters | Sikorsky |
| Aircraft Name | H135 | S-92 |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 342 | 439 |
| DOC / nm / Seat | $ 0.79 | $ 0.94 |
| Max Cabin Seats | 7 | 19 |
| OEM Verification | Un-Verified | Un-Verified |
| Useful Load (lbs) | 3124 | 7417 |
| Standard Cabin Seats | 7 | 19 |
| Direct Operating Cost | $ 861 | $ 3,068 |
| Flight Deck (Base Spec) | Helionix | EFIS |
| Max Cruise Speed (ktas) | 136 | 155 |
| Base Aircraft Price (USD) | $6,150,000 | $30,650,000 |
| Cabin | ||
| Cockpit | 2 | 2 |
| Min Crew | 1 | 2 |
| Total Seats | 9 | 21 |
| Configuration | Green Interior | — |
| Max Cabin Seats | 7 | 19 |
| Standard Cabin Seats | 7 | 19 |
| Engine | ||
| FADEC | Yes | Yes |
| Model | Arrius 2B2+ | CT7-8A |
| Fuel Type | JetFuel | JetFuel |
| TBO (hrs) | 4000 | 4000 |
| Horsepower | 660 | 2520 |
| No. of Engines | 2 | 1 |
| Fuel Capacity (gal) | — | 760 |
| Dimensions | ||
| Length (ft) | 33.5 | — |
| Overall Height (ft) | 12.6 | 17.8 |
| Rotor Diameter (ft) | 34 | — |
| Cabin Volume (cu. ft) | 173 | 775 |
| Baggage Volume Ext. (cu. ft) | — | 140 |