Airbus Helicopters H225 vs Beechcraft King Air 360 Er vs Cessna 208b Grand Caravan Ex vs Sikorsky S 92
The Airbus H225 and Sikorsky S-92 are large, twin‑engine helicopters typically used for offshore, SAR, and utility missions; they carry roughly 16–19 passengers in airline-style seating (more in high-density layouts) and generally offer medium ranges on the order of about 450–550 nautical miles depending on payload and reserves. The S-92 is broadly comparable in category and capacity, while specific range and payload tradeoffs vary by configuration. The Beechcraft King Air 360ER is a pressurized twin‑turboprop fixed‑wing aircraft aimed at longer point‑to‑point transport; it typically seats about 8–11 passengers and has a substantially longer range, commonly around 1,500–1,800 nautical miles with appropriate cabin and fuel configuration. The Cessna 208B Grand Caravan EX is a single‑engine turboprop utility aircraft optimized for short/rough fields and regional hops; it usually carries about 9–14 passengers and has a moderate range, often roughly 800–1,000 nautical miles, again highly dependent on payload and fuel reserves.
| 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 |