Beechcraft King Air 360 vs Leonardo Aw109 Trekker vs Pilatus Pc 12 Ngx
The Beechcraft King Air 360 and Pilatus PC-12 NGX are pressurized single‑pilot-capable business turboprops, while the Leonardo AW109 Trekker is a light twin‑engine helicopter optimized for vertical access and short-hop flexibility. For range, the PC-12 NGX is generally the longest-legged of the three, commonly cited around 1,800 nautical miles in typical cruise planning, making it well suited to longer point-to-point missions. The King Air 360 is usually quoted in the mid‑1,000‑nautical‑mile class (roughly 1,500 nm depending on load and reserves), offering strong high-altitude performance and cabin comfort for regional to medium trips. The AW109 Trekker’s range is substantially shorter than the fixed‑wing turboprops, typically a few hundred nautical miles (often around 450–500 nm), but it compensates with the ability to land at helipads and unimproved sites. In passenger capacity, both turboprops commonly seat about 6–9 passengers in executive layouts, with the PC-12 often marketed around 6–8, and the King Air 360 around 8–9. The AW109 Trekker typically carries about 6–7 passengers plus pilot(s), depending on configuration.
| Spec | Beechcraft King Air 360 | AGUSTA / LEONARDO AW109 Trekker | Pilatus PC-12 NGX |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 4.20 | $ 7.40 | $ 2.78 |
| Min Crew | 1 | 1 | 1 |
| Total Seats | 10 | 8 | 8 |
| Flight Rules | IFR | VFR | IFR |
| Manufacturer | Beechcraft | Leonardo | Pilatus |
| Aircraft Name | KingAir 350i | AW109 Trekker | PC-12 NGX |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1560 | 450 | 1803 |
| DOC / nm / Seat | $ 0.53 | $ 0.93 | $ 0.46 |
| Max Cabin Seats | 9 | 6 | 9 |
| OEM Verification | VERIFIED | Un-Verified | VERIFIED |
| Useful Load (lbs) | 5145 | — | — |
| Standard Cabin Seats | 8 | 6 | 6 |
| Direct Operating Cost | $ 1,311 | $ 1,125 | $ 793 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line Fusion | Genesys Aerosystems | Honeywell Primus Apex |
| Max Cruise Speed (ktas) | 312 | 152 | 290 |
| Base Aircraft Price (USD) | $7,650,000 | $6,950,000 | $5,350,000 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Lavatory | Optional | — | Optional |
| Min Crew | 1 | 1 | 1 |
| Total Seats | 10 | 8 | 8 |
| Galley Location | FWD | — | — |
| Max Cabin Seats | 9 | 6 | 9 |
| Lavatory Location | AFT | — | FWD |
| Cabin Pressure (psi) | 6.5 | — | 5.8 |
| Galley / Refreshment | Optional | — | No |
| Standard Cabin Seats | 8 | 6 | 6 |
| Cargo Door | — | — | Yes |
| SL Cabin Altitude (ft) | — | — | 13100 |
| Engine | |||
| FADEC | Yes | Yes | Yes |
| Model | PT6A-60A | PW207C | PT6E-67XP |
| TBO (hrs) | 3600 | 4000 | 5000 |
| Horsepower | 1050 | 735 | 1200 |
| Flat Rating | ISA + 10 | — | ISA + 35 |
| No. of Engines | 1 | 2 | 1 |
| Fuel Capacity (gal) | 539 | 152 | — |
| Fuel Type | — | JetFuel | — |
| Usable Fuel (gal) | — | — | 402 |
| Dimensions | |||
| Length (ft) | 46.7 | 42.5 | 47.25 |
| Wingspan (ft) | 57.9 | — | 53.33 |
| Cabin Width (ft) | 4.5 | — | 5 |
| Cabin Height (ft) | 4.8 | — | 4.9 |
| Cabin Length (ft) | 19.5 | — | 16.9 |
| Overall Height (ft) | 14.4 | 11.5 | 14 |
| Cabin Width - Floor (ft) | 4.1 | — | 4.25 |
| Cabin Length - Seating (ft) | 19.5 | — | — |
| Baggage Volume Int. (cu. ft) | 71 | — | 40 |
| Rotor Diameter (ft) | — | 35.5 | — |