Beechcraft Kingair 250 vs Piaggio Avanti Evo vs Pilatus Pc 12 Ngx
The Beechcraft King Air 260, Piaggio Avanti EVO, and Pilatus PC-12 NGX all sit in the single‑engine or light twin turboprop business aircraft space, but they prioritize different missions. The King Air 260 is a light twin‑engine turboprop typically used for corporate and utility flying, offering a practical cabin and strong short‑field flexibility. Its typical range is roughly 1,700–2,000 nautical miles depending on payload and reserves, and it generally seats about 6–9 passengers in common executive layouts. The Piaggio Avanti EVO is a high‑speed, twin‑engine turboprop positioned closer to a “turboprop alternative to light jets,” with cruise speed as a key differentiator; its range is commonly around 1,700–1,900 nautical miles, and typical configurations seat about 6–8 passengers in a comparatively roomy cabin. The Pilatus PC‑12 NGX is a single‑engine turboprop optimized for versatility, cargo capability, and unimproved/short runways; range is often around 1,700–1,800 nautical miles, and it commonly carries 6–9 passengers, with higher maximum seating possible in commuter-style layouts.
| Spec | Piaggio Avanti EVO | Pilatus PC-12 NGX |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| Min Crew | 1 | 1 |
| Total Seats | 8 | 8 |
| Flight Rules | IFR | IFR |
| Manufacturer | Piaggio | Pilatus |
| Aircraft Name | Avanti EVO | PC-12 NGX |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1530 | 1803 |
| Max Cabin Seats | 7 | 9 |
| OEM Verification | Un-Verified | VERIFIED |
| Useful Load (lbs) | 3775 | — |
| Standard Cabin Seats | 6 | 6 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line 21 | Honeywell Primus Apex |
| Max Cruise Speed (ktas) | 400 | 290 |
| Base Aircraft Price (USD) | $ 7,695,000 | $5,350,000 |
| DOC / nm | — | $ 2.78 |
| DOC / nm / Seat | — | $ 0.46 |
| Direct Operating Cost | — | $ 793 |
| Cabin | ||
| Cockpit | 2 | 2 |
| Lavatory | No | Optional |
| Min Crew | 1 | 1 |
| Total Seats | 8 | 8 |
| Max Cabin Seats | 7 | 9 |
| Cabin Pressure (psi) | 9 | 5.8 |
| Galley / Refreshment | No | No |
| Standard Cabin Seats | 6 | 6 |
| SL Cabin Altitude (ft) | 24000 | 13100 |
| Max Cabin Altitude (ft) | 6600 | — |
| Cargo Door | — | Yes |
| Lavatory Location | — | FWD |
| Engine | ||
| FADEC | Yes | Yes |
| Model | PT6A–66B | PT6E-67XP |
| TBO (hrs) | 3600 | 5000 |
| Horsepower | 850 | 1200 |
| Flat Rating | ISA + 28 | ISA + 35 |
| No. of Engines | 2 | 1 |
| Fuel Burn (gph) | 100 | — |
| Usable Fuel (gal) | — | 402 |
| Dimensions | ||
| Length (ft) | 47.3 | 47.25 |
| Wingspan (ft) | 47.1 | 53.33 |
| Cabin Width (ft) | 6.1 | 5 |
| Cabin Height (ft) | 5.8 | 4.9 |
| Cabin Length (ft) | 14.9 | 16.9 |
| Overall Height (ft) | 13.1 | 14 |
| Cabin Width - Floor (ft) | 3.5 | 4.25 |
| Baggage Volume Int. (cu. ft) | 35.2 | 40 |