Beechcraft King Air 260 vs Piaggio Avanti Evo vs Pilatus Pc 12 Ngx
The Beechcraft King Air 260 and Piaggio Avanti EVO are both twin‑engine turboprops aimed at fast, comfortable short‑to‑medium missions, while the Pilatus PC‑12 NGX is a single‑engine turboprop optimized for versatility and cabin utility. In range, all three are broadly in the same class, but the PC‑12 NGX is typically the longest‑legged, commonly offering roughly 1,700–1,800 nm depending on payload and reserves. The Avanti EVO is generally next, often around 1,500–1,700 nm, and the King Air 260 is usually in the 1,300–1,700 nm band depending on configuration and mission profile. For passenger capacity, the King Air 260 and Avanti EVO are commonly arranged for about six to eight passengers in executive layouts, while the PC‑12 NGX is often configured for six to nine passengers and can be adapted for more utility‑oriented missions. Overall, the King Air 260 emphasizes proven twin‑turboprop familiarity, the Avanti EVO emphasizes speed and distinctive aerodynamics, and the PC‑12 NGX emphasizes range, single‑engine simplicity, and flexible cabin use.
| Spec | Beechcraft King Air 260 | Piaggio Avanti EVO | Pilatus PC-12 NGX |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 4.30 | — | $ 2.78 |
| Min Crew | 1 | 1 | 1 |
| Total Seats | 8 | 8 | 8 |
| Flight Rules | IFR | IFR | IFR |
| Manufacturer | Beechcraft | Piaggio | Pilatus |
| Aircraft Name | KingAir 250 | Avanti EVO | PC-12 NGX |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1420 | 1530 | 1803 |
| DOC / nm / Seat | $ 0.72 | — | $ 0.46 |
| Max Cabin Seats | 8 | 7 | 9 |
| OEM Verification | VERIFIED | Un-Verified | VERIFIED |
| Useful Load (lbs) | 3760 | 3775 | — |
| Standard Cabin Seats | 6 | 6 | 6 |
| Direct Operating Cost | $ 1,333 | — | $ 793 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line Fusion | Rockwell Collins Pro Line 21 | Honeywell Primus Apex |
| Max Cruise Speed (ktas) | 310 | 400 | 290 |
| Base Aircraft Price (USD) | $6,450,000 | $ 7,695,000 | $5,350,000 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Lavatory | 1 Flushing | No | Optional |
| Min Crew | 1 | 1 | 1 |
| Total Seats | 8 | 8 | 8 |
| Max Cabin Seats | 8 | 7 | 9 |
| Lavatory Location | AFT | — | FWD |
| Cabin Pressure (psi) | 6.5 | 9 | 5.8 |
| Galley / Refreshment | No | No | No |
| Standard Cabin Seats | 6 | 6 | 6 |
| SL Cabin Altitude (ft) | 15293 | 24000 | 13100 |
| Max Cabin Altitude (ft) | — | 6600 | — |
| Cargo Door | — | — | Yes |
| Engine | |||
| FADEC | Yes | Yes | Yes |
| Model | PT6A-52 | PT6A–66B | PT6E-67XP |
| TBO (hrs) | 3600 | 3600 | 5000 |
| Horsepower | 850 | 850 | 1200 |
| Flat Rating | ISA + 37 | ISA + 28 | ISA + 35 |
| No. of Engines | 1 | 2 | 1 |
| Fuel Capacity (gal) | 544 | — | — |
| Fuel Burn (gph) | — | 100 | — |
| Usable Fuel (gal) | — | — | 402 |
| Dimensions | |||
| Length (ft) | 43.8 | 47.3 | 47.25 |
| Wingspan (ft) | 57.9 | 47.1 | 53.33 |
| Cabin Width (ft) | 4.5 | 6.1 | 5 |
| Cabin Height (ft) | 4.8 | 5.8 | 4.9 |
| Cabin Length (ft) | 16.7 | 14.9 | 16.9 |
| Overall Height (ft) | 14.8 | 13.1 | 14 |
| Cabin Width - Floor (ft) | 4.1 | 3.5 | 4.25 |
| Cabin Length - Seating (ft) | 16.7 | — | — |
| Baggage Volume Int. (cu. ft) | 55 | 35.2 | 40 |