Beechcraft King Air 260 vs Beechcraft King Air 360 vs Beechcraft King Air 360er vs Piaggio Avanti Evo
In category terms, the Beechcraft King Air 260, 360, and 360ER are pressurized twin‑turboprop business/utility aircraft with a conventional cabin and a strong emphasis on short/rough-field versatility, while the Piaggio Avanti EVO is also a twin‑turboprop business aircraft but is positioned more as a high‑speed executive transport with its distinctive three‑surface design and “pusher” propellers. For range, the King Air 260 is generally the shortest‑leg option of the group, suited to regional missions. The King Air 360 extends typical mission capability beyond the 260. The King Air 360ER is the long‑range variant and is intended to fly noticeably farther than the standard 360, making it the best choice when endurance and fewer fuel stops are priorities. The Avanti EVO typically competes strongly on cruise speed and can offer competitive range for executive missions, but the 360ER is usually the range leader among these four. For passenger capacity, all four are commonly configured for about six to nine passengers depending on interior layout; the King Air family often targets eight to nine seats, while the Avanti EVO is often arranged around seven to nine in executive configurations.
| Spec | Beechcraft King Air 260 | Beechcraft King Air 360 | Beechcraft King Air 360ER | Piaggio Avanti EVO |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 4.30 | $ 4.20 | $ 4.37 | — |
| Min Crew | 1 | 1 | 1 | 1 |
| Total Seats | 8 | 10 | 10 | 8 |
| Flight Rules | IFR | IFR | IFR | IFR |
| Manufacturer | Beechcraft | Beechcraft | Beechcraft | Piaggio |
| Aircraft Name | KingAir 250 | KingAir 350i | KingAir 350ER | Avanti EVO |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1420 | 1560 | 2338 | 1530 |
| DOC / nm / Seat | $ 0.72 | $ 0.53 | $ 0.55 | — |
| Max Cabin Seats | 8 | 9 | 9 | 7 |
| OEM Verification | VERIFIED | VERIFIED | VERIFIED | Un-Verified |
| Useful Load (lbs) | 3760 | 5145 | 6585 | 3775 |
| Standard Cabin Seats | 6 | 8 | 8 | 6 |
| Direct Operating Cost | $ 1,333 | $ 1,311 | $ 1,324 | — |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line Fusion | Rockwell Collins Pro Line Fusion | Rockwell Collins Pro Line Fusion | Rockwell Collins Pro Line 21 |
| Max Cruise Speed (ktas) | 310 | 312 | 303 | 400 |
| Base Aircraft Price (USD) | $6,450,000 | $7,650,000 | $8,750,000 | $ 7,695,000 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Lavatory | 1 Flushing | Optional | Yes (Belted Optional) | No |
| Min Crew | 1 | 1 | 1 | 1 |
| Total Seats | 8 | 10 | 10 | 8 |
| Max Cabin Seats | 8 | 9 | 9 | 7 |
| Lavatory Location | AFT | AFT | AFT | — |
| Cabin Pressure (psi) | 6.5 | 6.5 | 6.5 | 9 |
| Galley / Refreshment | No | Optional | Refreshment Center | No |
| Standard Cabin Seats | 6 | 8 | 8 | 6 |
| SL Cabin Altitude (ft) | 15293 | — | — | 24000 |
| Galley Location | — | FWD | FWD | — |
| Cargo Door | — | — | Optional | — |
| Max Cabin Altitude (ft) | — | — | — | 6600 |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | PT6A-52 | PT6A-60A | PT6A-60A | PT6A–66B |
| TBO (hrs) | 3600 | 3600 | 3600 | 3600 |
| Horsepower | 850 | 1050 | 1050 | 850 |
| Flat Rating | ISA + 37 | ISA + 10 | ISA + 10 | ISA + 28 |
| No. of Engines | 1 | 1 | 1 | 2 |
| Fuel Capacity (gal) | 544 | 539 | 775 | — |
| Fuel Burn (gph) | — | — | — | 100 |
| Dimensions | ||||
| Length (ft) | 43.8 | 46.7 | 46.7 | 47.3 |
| Wingspan (ft) | 57.9 | 57.9 | 57.9 | 47.1 |
| Cabin Width (ft) | 4.5 | 4.5 | 4.5 | 6.1 |
| Cabin Height (ft) | 4.8 | 4.8 | 4.8 | 5.8 |
| Cabin Length (ft) | 16.7 | 19.5 | 19.5 | 14.9 |
| Overall Height (ft) | 14.8 | 14.4 | 14.4 | 13.1 |
| Cabin Width - Floor (ft) | 4.1 | 4.1 | 4.1 | 3.5 |
| Cabin Length - Seating (ft) | 16.7 | 19.5 | 19.5 | — |
| Baggage Volume Int. (cu. ft) | 55 | 71 | 71 | 35.2 |