Beechcraft King Air 360 Er vs Cessna 208b Grand Caravan Ex vs Leonardo Aw189 vs Piaggio Avanti Evo
The Beechcraft King Air 360ER and Piaggio Avanti EVO are both pressurized twin‑turboprop airplanes aimed at fast, efficient business and special‑mission flying. The 360ER is typically configured around 8–9 passengers and emphasizes runway flexibility and endurance; with its extended‑range setup it can cover roughly 1,800–2,000 nautical miles depending on payload and conditions. The Avanti EVO generally carries about 7–9 passengers and is usually faster than the King Air class, with a typical range around 1,700–1,800 nautical miles. The Cessna 208B Grand Caravan EX is a single‑turboprop utility aircraft optimized for rugged, short‑field operations and freight/passenger versatility rather than speed; it commonly seats 9–14 passengers, with range typically about 900–1,200 nautical miles depending on load and tanks. The Agusta/Leonardo AW189 is a medium twin‑engine helicopter, trading cruise speed and range for vertical lift and offshore/EMS capability. It commonly carries about 16–19 passengers in transport layouts, with typical range roughly 450–550 nautical miles, though auxiliary tanks can extend this.
| Spec | AGUSTA / LEONARDO AW189 | Piaggio Avanti EVO |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| DOC / nm | $ 15.57 | — |
| Min Crew | 1 | 1 |
| Total Seats | 21 | 8 |
| Flight Rules | IFR | IFR |
| Manufacturer | Leonardo | Piaggio |
| Aircraft Name | AW189 | Avanti EVO |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 651 | 1530 |
| DOC / nm / Seat | $ 0.74 | — |
| Max Cabin Seats | 19 | 7 |
| OEM Verification | Un-Verified | Un-Verified |
| Standard Cabin Seats | 19 | 6 |
| Direct Operating Cost | $ 2,413 | — |
| Flight Deck (Base Spec) | EFIS | Rockwell Collins Pro Line 21 |
| Max Cruise Speed (ktas) | 155 | 400 |
| Base Aircraft Price (USD) | $2,413,000 | $ 7,695,000 |
| Useful Load (lbs) | — | 3775 |
| Cabin | ||
| Cockpit | 2 | 2 |
| Min Crew | 1 | 1 |
| Total Seats | 21 | 8 |
| Max Cabin Seats | 19 | 7 |
| Standard Cabin Seats | 19 | 6 |
| Lavatory | — | No |
| Cabin Pressure (psi) | — | 9 |
| Galley / Refreshment | — | No |
| SL Cabin Altitude (ft) | — | 24000 |
| Max Cabin Altitude (ft) | — | 6600 |
| Engine | ||
| FADEC | Yes | Yes |
| Model | CT7-2E1 | PT6A–66B |
| Fuel Type | JetFuel | — |
| TBO (hrs) | 4000 | 3600 |
| Horsepower | 1983 | 850 |
| No. of Engines | 2 | 2 |
| Flat Rating | — | ISA + 28 |
| Fuel Burn (gph) | — | 100 |
| Dimensions | ||
| Length (ft) | 57.8 | 47.3 |
| Overall Height (ft) | 16.6 | 13.1 |
| Rotor Diameter (ft) | 48 | — |
| Cabin Volume (cu. ft) | 395 | — |
| Baggage Volume Ext. (cu. ft) | 85 | — |
| 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 |