Beechcraft King Air 360 Er vs Leonardo Aw189 vs Piaggio Avanti Evo vs Sikorsky S 92
The Beechcraft King Air 360ER is a twin‑turboprop fixed‑wing aircraft aimed at efficient short-to-medium missions; it typically carries about 6–9 passengers in executive seating and offers long endurance for its class, with range generally in the roughly 1,500–2,000+ nautical mile band depending on payload and reserves. The Piaggio Avanti EVO is also a twin‑turboprop fixed‑wing aircraft, optimized for speed and cabin comfort; it commonly seats about 6–9 passengers and has a similar mission radius, often around 1,500–1,800 nautical miles. The Leonardo AW189 is a medium twin‑engine helicopter designed for offshore and utility transport; it usually accommodates about 12–16 passengers and has a shorter range than the fixed‑wing options, commonly in the several-hundred‑nautical‑mile range (often roughly 450–500 nautical miles, mission‑dependent). The Sikorsky S‑92 is a larger medium/heavy twin‑engine helicopter frequently used offshore; it typically carries about 16–19 passengers with range broadly comparable to, or somewhat greater than, the AW189 (often around 500 nautical miles, depending on configuration).
| Spec | AGUSTA / LEONARDO AW189 | Piaggio Avanti EVO | Sikorsky S-92 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 15.57 | — | $ 19.79 |
| Min Crew | 1 | 1 | 2 |
| Total Seats | 21 | 8 | 21 |
| Flight Rules | IFR | IFR | IFR |
| Manufacturer | Leonardo | Piaggio | Sikorsky |
| Aircraft Name | AW189 | Avanti EVO | S-92 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 651 | 1530 | 439 |
| DOC / nm / Seat | $ 0.74 | — | $ 0.94 |
| Max Cabin Seats | 19 | 7 | 19 |
| OEM Verification | Un-Verified | Un-Verified | Un-Verified |
| Standard Cabin Seats | 19 | 6 | 19 |
| Direct Operating Cost | $ 2,413 | — | $ 3,068 |
| Flight Deck (Base Spec) | EFIS | Rockwell Collins Pro Line 21 | EFIS |
| Max Cruise Speed (ktas) | 155 | 400 | 155 |
| Base Aircraft Price (USD) | $2,413,000 | $ 7,695,000 | $30,650,000 |
| Useful Load (lbs) | — | 3775 | 7417 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 1 | 1 | 2 |
| Total Seats | 21 | 8 | 21 |
| Max Cabin Seats | 19 | 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 | CT7-2E1 | PT6A–66B | CT7-8A |
| Fuel Type | JetFuel | — | JetFuel |
| TBO (hrs) | 4000 | 3600 | 4000 |
| Horsepower | 1983 | 850 | 2520 |
| No. of Engines | 2 | 2 | 1 |
| Flat Rating | — | ISA + 28 | — |
| Fuel Burn (gph) | — | 100 | — |
| Fuel Capacity (gal) | — | — | 760 |
| Dimensions | |||
| Length (ft) | 57.8 | 47.3 | — |
| Overall Height (ft) | 16.6 | 13.1 | 17.8 |
| Rotor Diameter (ft) | 48 | — | — |
| Cabin Volume (cu. ft) | 395 | — | 775 |
| Baggage Volume Ext. (cu. ft) | 85 | — | 140 |
| 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 | — |