Airbus Helicopters H225 vs Beechcraft King Air 360 Er vs Piaggio Avanti Evo vs Sikorsky S 92
The Airbus H225 and Sikorsky S-92 are large twin‑engine helicopters aimed at offshore, search-and-rescue, and utility missions. They typically carry around 16–19 passengers in airline-style seating (configurations vary widely) and offer practical ranges on the order of roughly 450–550 nautical miles, depending on payload, reserves, and tanking. The Beechcraft King Air 360ER and Piaggio Avanti EVO are pressurized fixed‑wing turboprops oriented toward business, special mission, and regional transport. In category, they trade vertical lift for higher cruise efficiency and speed. The King Air 360ER is optimized for long legs and endurance, with a typical range roughly around 1,500 nautical miles and seating commonly 6–9 passengers (higher-density layouts possible). The Piaggio Avanti EVO generally seats about 7–9 and offers a typical range around 1,400–1,700 nautical miles, depending on configuration. Overall, the helicopters excel in point-to-point access without runways and higher cabin volume for mission equipment, while the turboprops generally deliver much longer range and faster cruise for comparable passenger counts.
| Spec | AIRBUS H225 | Piaggio Avanti EVO | Sikorsky S-92 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | — | $ 19.79 |
| Min Crew | 2 | 1 | 2 |
| Total Seats | 21 | 8 | 21 |
| Flight Rules | IFR | IFR | IFR |
| Manufacturer | Airbus Helicopters | Piaggio | Sikorsky |
| Aircraft Name | H225 | Avanti EVO | S-92 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 1530 | 439 |
| DOC / nm / Seat | $ 0.99 | — | $ 0.94 |
| Max Cabin Seats | 28 | 7 | 19 |
| OEM Verification | Un-Verified | Un-Verified | Un-Verified |
| Useful Load (lbs) | 11929 | 3775 | 7417 |
| Standard Cabin Seats | 19 | 6 | 19 |
| Direct Operating Cost | $ 2,963 | — | $ 3,068 |
| Flight Deck (Base Spec) | EFIS | Rockwell Collins Pro Line 21 | EFIS |
| Max Cruise Speed (ktas) | 142 | 400 | 155 |
| Base Aircraft Price (USD) | $ 29,500,000 | $ 7,695,000 | $30,650,000 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 1 | 2 |
| Total Seats | 21 | 8 | 21 |
| Max Cabin Seats | 28 | 7 | 19 |
| Standard Cabin Seats | 19 | 6 | 19 |
| Lavatory | — | No | — |
| Cabin Pressure (psi) | — | 9 | — |
| Galley / Refreshment | — | No | — |
| SL Cabin Altitude (ft) | — | 24000 | — |
| Max Cabin Altitude (ft) | — | 6600 | — |
| Engine | |||
| FADEC | Yes | Yes | Yes |
| Model | Makila 2A1 | PT6A–66B | CT7-8A |
| Fuel Type | JetFuel | — | JetFuel |
| TBO (hrs) | 3500 | 3600 | 4000 |
| Horsepower | 2100 | 850 | 2520 |
| No. of Engines | 2 | 2 | 1 |
| Fuel Capacity (gal) | 684 | — | 760 |
| Flat Rating | — | ISA + 28 | — |
| Fuel Burn (gph) | — | 100 | — |
| Dimensions | |||
| Length (ft) | 63.4 | 47.3 | — |
| Overall Height (ft) | 16.3 | 13.1 | 17.8 |
| Rotor Diameter (ft) | 53.2 | — | — |
| Cabin Volume (cu. ft) | 547 | — | 775 |
| Wingspan (ft) | — | 47.1 | — |
| Cabin Width (ft) | — | 6.1 | — |
| Cabin Height (ft) | — | 5.8 | — |
| Cabin Length (ft) | — | 14.9 | — |
| Cabin Width - Floor (ft) | — | 3.5 | — |
| Baggage Volume Int. (cu. ft) | — | 35.2 | — |
| Baggage Volume Ext. (cu. ft) | — | — | 140 |