Airbus Helicopters H225 vs Cessna 208b Grand Caravan Ex vs Leonardo Aw189 vs Sikorsky S 92
The Airbus H225, Leonardo AW189, and Sikorsky S-92 are large twin‑engine helicopters typically used for offshore transport, SAR, and heavy utility work, while the Cessna 208B Grand Caravan EX is a single‑engine fixed‑wing turboprop optimized for short‑haul regional and remote airstrip operations. In range terms, the S-92 and H225 generally sit at the higher end among the helicopters for longer offshore legs, with the AW189 usually somewhat shorter but still in a similar long‑range class; the Grand Caravan EX often achieves comparable or better point‑to‑point range than many helicopters thanks to fixed‑wing efficiency, though its mission profile differs (runways required). For passenger capacity, the S-92 and H225 commonly carry the most in typical transport layouts (often around the high‑teens to low‑twenties), the AW189 is generally slightly below them (often mid‑teens to high‑teens), and the Grand Caravan EX is usually configured for up to 9 passengers, prioritizing payload flexibility over high seating density.
| Spec | AIRBUS H225 | AGUSTA / LEONARDO AW189 | Sikorsky S-92 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 15.57 | $ 19.79 |
| Min Crew | 2 | 1 | 2 |
| Total Seats | 21 | 21 | 21 |
| Flight Rules | IFR | IFR | IFR |
| Manufacturer | Airbus Helicopters | Leonardo | Sikorsky |
| Aircraft Name | H225 | AW189 | S-92 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 651 | 439 |
| DOC / nm / Seat | $ 0.99 | $ 0.74 | $ 0.94 |
| Max Cabin Seats | 28 | 19 | 19 |
| OEM Verification | Un-Verified | Un-Verified | Un-Verified |
| Useful Load (lbs) | 11929 | — | 7417 |
| Standard Cabin Seats | 19 | 19 | 19 |
| Direct Operating Cost | $ 2,963 | $ 2,413 | $ 3,068 |
| Flight Deck (Base Spec) | EFIS | EFIS | EFIS |
| Max Cruise Speed (ktas) | 142 | 155 | 155 |
| Base Aircraft Price (USD) | $ 29,500,000 | $2,413,000 | $30,650,000 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 1 | 2 |
| Total Seats | 21 | 21 | 21 |
| Max Cabin Seats | 28 | 19 | 19 |
| Standard Cabin Seats | 19 | 19 | 19 |
| Engine | |||
| FADEC | Yes | Yes | Yes |
| Model | Makila 2A1 | CT7-2E1 | CT7-8A |
| Fuel Type | JetFuel | JetFuel | JetFuel |
| TBO (hrs) | 3500 | 4000 | 4000 |
| Horsepower | 2100 | 1983 | 2520 |
| No. of Engines | 2 | 2 | 1 |
| Fuel Capacity (gal) | 684 | — | 760 |
| Dimensions | |||
| Length (ft) | 63.4 | 57.8 | — |
| Overall Height (ft) | 16.3 | 16.6 | 17.8 |
| Rotor Diameter (ft) | 53.2 | 48 | — |
| Cabin Volume (cu. ft) | 547 | 395 | 775 |
| Baggage Volume Ext. (cu. ft) | — | 85 | 140 |