Beechcraft King Air 360 Er vs Enstrom 480b vs Piaggio Avanti Evo vs Sikorsky S 92
The Beechcraft King Air 360ER is a twin‑turboprop fixed‑wing aircraft in the light utility/air taxi category. It is optimized for efficient regional missions, typically carrying about 6–9 passengers, with an extended range on the order of roughly 1,500–1,800 nautical miles depending on configuration and reserves. The Piaggio Avanti EVO is a twin‑turboprop fixed‑wing aircraft positioned as a high‑speed business/utility aircraft. It commonly seats around 7–9 passengers and generally offers a longer, business‑jet‑like trip capability, typically around 1,600–1,800 nautical miles. The Enstrom 480B is a single‑engine turbine helicopter in the light helicopter category. It usually carries a pilot plus up to about 4 passengers, with a much shorter range, commonly a few hundred nautical miles (roughly 250–350), trading speed and range for vertical access and point‑to‑point utility. The Sikorsky S‑92 is a large twin‑engine helicopter used for offshore transport, SAR, and executive/VIP roles. It can carry around 12–19 passengers (layout dependent) with a typical range roughly in the 450–550 nautical mile class, prioritizing payload and overwater capability over fixed‑wing range.
| Spec | Piaggio Avanti EVO | Sikorsky S-92 |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| Min Crew | 1 | 2 |
| Total Seats | 8 | 21 |
| Flight Rules | IFR | IFR |
| Manufacturer | Piaggio | Sikorsky |
| Aircraft Name | Avanti EVO | S-92 |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1530 | 439 |
| Max Cabin Seats | 7 | 19 |
| OEM Verification | Un-Verified | Un-Verified |
| Useful Load (lbs) | 3775 | 7417 |
| Standard Cabin Seats | 6 | 19 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line 21 | EFIS |
| Max Cruise Speed (ktas) | 400 | 155 |
| Base Aircraft Price (USD) | $ 7,695,000 | $30,650,000 |
| DOC / nm | — | $ 19.79 |
| DOC / nm / Seat | — | $ 0.94 |
| Direct Operating Cost | — | $ 3,068 |
| Cabin | ||
| Cockpit | 2 | 2 |
| Lavatory | No | — |
| Min Crew | 1 | 2 |
| Total Seats | 8 | 21 |
| Max Cabin Seats | 7 | 19 |
| Cabin Pressure (psi) | 9 | — |
| Galley / Refreshment | No | — |
| Standard Cabin Seats | 6 | 19 |
| SL Cabin Altitude (ft) | 24000 | — |
| Max Cabin Altitude (ft) | 6600 | — |
| Engine | ||
| FADEC | Yes | Yes |
| Model | PT6A–66B | CT7-8A |
| TBO (hrs) | 3600 | 4000 |
| Horsepower | 850 | 2520 |
| Flat Rating | ISA + 28 | — |
| No. of Engines | 2 | 1 |
| Fuel Burn (gph) | 100 | — |
| Fuel Type | — | JetFuel |
| Fuel Capacity (gal) | — | 760 |
| Dimensions | ||
| Length (ft) | 47.3 | — |
| Wingspan (ft) | 47.1 | — |
| Cabin Width (ft) | 6.1 | — |
| Cabin Height (ft) | 5.8 | — |
| Cabin Length (ft) | 14.9 | — |
| Overall Height (ft) | 13.1 | 17.8 |
| Cabin Width - Floor (ft) | 3.5 | — |
| Baggage Volume Int. (cu. ft) | 35.2 | — |
| Cabin Volume (cu. ft) | — | 775 |
| Baggage Volume Ext. (cu. ft) | — | 140 |