Airbus Helicopters H225 vs Cessna 208b Grand Caravan Ex vs Sikorsky S 92
The Airbus H225 and Sikorsky S‑92 are twin‑engine, heavy helicopters designed for offshore transport, search and rescue, and other demanding missions, while the Cessna 208B Grand Caravan EX is a single‑engine, fixed‑wing turboprop aimed at regional utility and short‑haul passenger or cargo service. In range, the Grand Caravan EX typically offers the longest reach in practical point‑to‑point operations for its class (often on the order of 900–1,000+ nautical miles depending on payload and reserves), whereas the H225 and S‑92 generally fall in the mid‑hundreds of nautical miles (commonly around 450–600 nautical miles, mission‑equipped and payload dependent). For passenger capacity, the Grand Caravan EX is usually configured for about 9 passengers, while the H225 and S‑92 can carry substantially more, often around 16–19 passengers in typical offshore layouts, with higher maximum seating possible in denser configurations. Overall, choose the Caravan for economical runway‑based regional range, and the H225 or S‑92 when vertical lift and offshore capability matter most.
| Spec | AIRBUS H225 | Sikorsky S-92 |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| DOC / nm | $ 20.87 | $ 19.79 |
| Min Crew | 2 | 2 |
| Total Seats | 21 | 21 |
| Flight Rules | IFR | IFR |
| Manufacturer | Airbus Helicopters | Sikorsky |
| Aircraft Name | H225 | S-92 |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 439 |
| DOC / nm / Seat | $ 0.99 | $ 0.94 |
| Max Cabin Seats | 28 | 19 |
| OEM Verification | Un-Verified | Un-Verified |
| Useful Load (lbs) | 11929 | 7417 |
| Standard Cabin Seats | 19 | 19 |
| Direct Operating Cost | $ 2,963 | $ 3,068 |
| Flight Deck (Base Spec) | EFIS | EFIS |
| Max Cruise Speed (ktas) | 142 | 155 |
| Base Aircraft Price (USD) | $ 29,500,000 | $30,650,000 |
| Cabin | ||
| Cockpit | 2 | 2 |
| Min Crew | 2 | 2 |
| Total Seats | 21 | 21 |
| Max Cabin Seats | 28 | 19 |
| Standard Cabin Seats | 19 | 19 |
| Engine | ||
| FADEC | Yes | Yes |
| Model | Makila 2A1 | CT7-8A |
| Fuel Type | JetFuel | JetFuel |
| TBO (hrs) | 3500 | 4000 |
| Horsepower | 2100 | 2520 |
| No. of Engines | 2 | 1 |
| Fuel Capacity (gal) | 684 | 760 |
| Dimensions | ||
| Length (ft) | 63.4 | — |
| Overall Height (ft) | 16.3 | 17.8 |
| Rotor Diameter (ft) | 53.2 | — |
| Cabin Volume (cu. ft) | 547 | 775 |
| Baggage Volume Ext. (cu. ft) | — | 140 |