Airbus Helicopters H225 vs Cessna 208b Grand Caravan Ex vs Embraer Legacy 650 E vs Sikorsky S 92
The Airbus H225 and Sikorsky S-92 are large, twin‑engine helicopters typically used for offshore transport, search and rescue, and VIP missions. They generally offer medium ranges for rotorcraft—roughly in the 450–550 nautical mile class depending on fit and reserves—and usually seat around 16–19 passengers in high‑density layouts, though offshore seating is often configured closer to the mid‑teens. The Cessna 208B Grand Caravan EX is a single‑engine turboprop fixed‑wing utility aircraft aimed at short‑to‑medium regional legs, remote access, and cargo/passenger flexibility. Its range is commonly around 900–1,000 nautical miles with typical payload tradeoffs, and it usually carries up to about 9 passengers in commuter configuration. The Embraer Legacy 650E is a long‑range business jet designed for fast intercity travel. It operates in the roughly 3,900–4,000 nautical mile range class and typically seats about 13 passengers in executive cabin layouts (with maximum certified seating higher), prioritizing comfort over density.
| 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 |