Airbus Helicopters H225 vs Beechcraft King Air 360 Er vs Enstrom 480b vs Sikorsky S 92
The Airbus H225 and Sikorsky S-92 are heavy, twin‑engine helicopters typically used for offshore transport, SAR, and government missions. Both prioritize lift and cabin volume over speed and efficiency; typical mission ranges are roughly in the 450–550 nautical mile class depending on payload and reserves, with passenger seating commonly around 16–19. The H225 is often configured for higher-density offshore seating, while the S‑92 is similarly positioned with a reputation for stable offshore operations. The Enstrom 480B is a light, single‑engine helicopter aimed at utility, training, and patrol roles. It carries far fewer people—generally 4–5 including the pilot—with a much shorter practical range, commonly around 250–300 nautical miles. The Beechcraft King Air 360ER is a fixed‑wing twin‑turboprop, optimized for efficient point‑to‑point travel rather than vertical lift. It typically carries about 6–9 passengers in executive layouts (more in commuter configurations) and offers substantially greater range than the helicopters—often around 1,500–2,000+ nautical miles depending on configuration—making it the best fit for longer routes between runways.
| 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 |