Beechcraft King Air 360 vs Beechcraft King Air 370er vs Piaggio Avanti Evo
Both the Beechcraft King Air 360 and the Piaggio Avanti EVO are twin‑engine turboprops, but they sit in different niches. The King Air 360 is best viewed as a rugged, traditional utility-oriented business turboprop: it’s widely used for corporate travel, special missions, and operations into shorter or less-developed airports. The Avanti EVO is a high-speed executive turboprop with a more aerodynamic, pusher-prop design aimed at jet-like cruise speeds and efficiency, generally prioritizing speed and cabin refinement over rough-field versatility. On range, the King Air 360 typically offers longer endurance, with published figures commonly around the 1,800 nautical mile class depending on payload and conditions, while the Avanti EVO is usually cited closer to the 1,700 nautical mile class, also highly dependent on reserves, cruise profile, and passenger load. For passenger capacity, both are commonly configured for roughly six to nine passengers in executive layouts. The King Air 360 is often arranged around eight to nine seats, while the Avanti EVO frequently seats about seven to nine, with a cabin that feels more “jet-like” in shape and noise levels for many travelers.
| Spec | Beechcraft King Air 360 | Piaggio Avanti EVO |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| DOC / nm | $ 4.20 | — |
| Min Crew | 1 | 1 |
| Total Seats | 10 | 8 |
| Flight Rules | IFR | IFR |
| Manufacturer | Beechcraft | Piaggio |
| Aircraft Name | KingAir 350i | Avanti EVO |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1560 | 1530 |
| DOC / nm / Seat | $ 0.53 | — |
| Max Cabin Seats | 9 | 7 |
| OEM Verification | VERIFIED | Un-Verified |
| Useful Load (lbs) | 5145 | 3775 |
| Standard Cabin Seats | 8 | 6 |
| Direct Operating Cost | $ 1,311 | — |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line Fusion | Rockwell Collins Pro Line 21 |
| Max Cruise Speed (ktas) | 312 | 400 |
| Base Aircraft Price (USD) | $7,650,000 | $ 7,695,000 |
| Cabin | ||
| Cockpit | 2 | 2 |
| Lavatory | Optional | No |
| Min Crew | 1 | 1 |
| Total Seats | 10 | 8 |
| Galley Location | FWD | — |
| Max Cabin Seats | 9 | 7 |
| Lavatory Location | AFT | — |
| Cabin Pressure (psi) | 6.5 | 9 |
| Galley / Refreshment | Optional | No |
| Standard Cabin Seats | 8 | 6 |
| SL Cabin Altitude (ft) | — | 24000 |
| Max Cabin Altitude (ft) | — | 6600 |
| Engine | ||
| FADEC | Yes | Yes |
| Model | PT6A-60A | PT6A–66B |
| TBO (hrs) | 3600 | 3600 |
| Horsepower | 1050 | 850 |
| Flat Rating | ISA + 10 | ISA + 28 |
| No. of Engines | 1 | 2 |
| Fuel Capacity (gal) | 539 | — |
| Fuel Burn (gph) | — | 100 |
| Dimensions | ||
| Length (ft) | 46.7 | 47.3 |
| Wingspan (ft) | 57.9 | 47.1 |
| Cabin Width (ft) | 4.5 | 6.1 |
| Cabin Height (ft) | 4.8 | 5.8 |
| Cabin Length (ft) | 19.5 | 14.9 |
| Overall Height (ft) | 14.4 | 13.1 |
| Cabin Width - Floor (ft) | 4.1 | 3.5 |
| Cabin Length - Seating (ft) | 19.5 | — |
| Baggage Volume Int. (cu. ft) | 71 | 35.2 |