Beechcraft King Air 360 vs Pilatus Pc 12 Ngx vs Pilatus Pc 24
The Beechcraft King Air 360 and Pilatus PC-12 NGX are single‑pilot-capable turboprops aimed at efficient regional missions, while the Pilatus PC-24 is a light jet designed for faster point‑to‑point travel with jet performance. In category terms, the King Air 360 is a twin‑engine turboprop, the PC‑12 NGX is a single‑engine turboprop, and the PC‑24 is a twin‑engine light business jet. For range, the PC-12 NGX generally offers the longest reach among the turboprops, typically around 1,700–1,800 nautical miles depending on payload and reserves. The King Air 360 is usually in a similar but slightly shorter band, roughly around 1,500–1,800 nautical miles depending on configuration. The PC‑24’s range is typically around 2,000 nautical miles, varying with passengers, luggage, and cruise profile. Passenger capacity commonly differs by layout: the PC‑12 NGX is typically configured for about 6–9 passengers, the King Air 360 often seats about 6–9 as well, and the PC‑24 typically carries about 6–10 passengers in executive seating.
| Spec | Beechcraft King Air 360 | Pilatus PC-12 NGX | Pilatus PC-24 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 4.20 | $ 2.78 | $ 3.71 |
| Min Crew | 1 | 1 | 1 |
| Total Seats | 10 | 8 | 6 |
| Flight Rules | IFR | IFR | — |
| Manufacturer | Beechcraft | Pilatus | Pilatus |
| Aircraft Name | KingAir 350i | PC-12 NGX | PC-24 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1560 | 1803 | 2076 |
| DOC / nm / Seat | $ 0.53 | $ 0.46 | $ 0.62 |
| Max Cabin Seats | 9 | 9 | 10 |
| OEM Verification | VERIFIED | VERIFIED | VERIFIED |
| Useful Load (lbs) | 5145 | — | 6680 |
| Standard Cabin Seats | 8 | 6 | 6 |
| Direct Operating Cost | $ 1,311 | $ 793 | $ 1,619 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line Fusion | Honeywell Primus Apex | Pilatus ACE (Primus Apex) |
| Max Cruise Speed (ktas) | 312 | 290 | 440 |
| Base Aircraft Price (USD) | $7,650,000 | $5,350,000 | $11,800,000 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Lavatory | Optional | Optional | 1 Enclosed Flushing |
| Min Crew | 1 | 1 | 1 |
| Total Seats | 10 | 8 | 6 |
| Galley Location | FWD | — | FWD |
| Max Cabin Seats | 9 | 9 | 10 |
| Lavatory Location | AFT | FWD | FWD |
| Cabin Pressure (psi) | 6.5 | 5.8 | 9.3 |
| Galley / Refreshment | Optional | No | Optional Refreshment Center |
| Standard Cabin Seats | 8 | 6 | 6 |
| Cargo Door | — | Yes | Yes |
| SL Cabin Altitude (ft) | — | 13100 | 23500 |
| Crew Rest | — | — | No |
| Jump Seat | — | — | No |
| Engine | |||
| FADEC | Yes | Yes | Yes |
| Model | PT6A-60A | PT6E-67XP | FJ44-4A-QPM |
| TBO (hrs) | 3600 | 5000 | 5000 |
| Horsepower | 1050 | 1200 | — |
| Flat Rating | ISA + 10 | ISA + 35 | ISA + 23 |
| No. of Engines | 1 | 1 | 2 |
| Fuel Capacity (gal) | 539 | — | — |
| Usable Fuel (gal) | — | 402 | — |
| Thrust (lbs) | — | — | 3435 |
| Dimensions | |||
| Length (ft) | 46.7 | 47.25 | 52.2 |
| Wingspan (ft) | 57.9 | 53.33 | 55.8 |
| Cabin Width (ft) | 4.5 | 5 | 5.6 |
| Cabin Height (ft) | 4.8 | 4.9 | 5.1 |
| Cabin Length (ft) | 19.5 | 16.9 | 23 |
| Overall Height (ft) | 14.4 | 14 | 17.4 |
| Cabin Width - Floor (ft) | 4.1 | 4.25 | 3.8 |
| Cabin Length - Seating (ft) | 19.5 | — | 17 |
| Baggage Volume Int. (cu. ft) | 71 | 40 | 90 |
| Aisle Step (ft) | — | — | Flat Floor |