Beechcraft King Air 360 vs Pilatus Pc 24
The Beechcraft King Air 360 and Pilatus PC-24 sit in different aircraft categories, which drives most of the practical differences. The King Air 360 is a pressurized twin‑engine turboprop, typically chosen for efficient short-to-medium missions, frequent regional hops, and access to shorter runways with strong low-speed performance. The Pilatus PC-24 is a twin‑engine business jet, aimed at higher cruise speeds and jet operating profiles while still retaining unusually good short and semi‑prepared runway capability for a jet. On range, the PC-24 generally offers a longer maximum range than the King Air 360, enabling more nonstop city pairs and better high-speed legs, though real-world range depends heavily on passenger load, reserves, and weather. The King Air 360’s range is competitive for regional missions but is usually shorter than the PC-24’s headline figures. On passenger capacity, both can be configured for roughly eight to nine passengers in typical executive layouts, but the PC-24 often provides a roomier jet-style cabin and baggage flexibility, while the King Air 360 emphasizes versatile cabin arrangements and mission efficiency.
| Spec | Beechcraft King Air 360 | Pilatus PC-24 |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| DOC / nm | $ 4.20 | $ 3.71 |
| Min Crew | 1 | 1 |
| Total Seats | 10 | 6 |
| Flight Rules | IFR | — |
| Manufacturer | Beechcraft | Pilatus |
| Aircraft Name | KingAir 350i | PC-24 |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1560 | 2076 |
| DOC / nm / Seat | $ 0.53 | $ 0.62 |
| Max Cabin Seats | 9 | 10 |
| OEM Verification | VERIFIED | VERIFIED |
| Useful Load (lbs) | 5145 | 6680 |
| Standard Cabin Seats | 8 | 6 |
| Direct Operating Cost | $ 1,311 | $ 1,619 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line Fusion | Pilatus ACE (Primus Apex) |
| Max Cruise Speed (ktas) | 312 | 440 |
| Base Aircraft Price (USD) | $7,650,000 | $11,800,000 |
| Cabin | ||
| Cockpit | 2 | 2 |
| Lavatory | Optional | 1 Enclosed Flushing |
| Min Crew | 1 | 1 |
| Total Seats | 10 | 6 |
| Galley Location | FWD | FWD |
| Max Cabin Seats | 9 | 10 |
| Lavatory Location | AFT | FWD |
| Cabin Pressure (psi) | 6.5 | 9.3 |
| Galley / Refreshment | Optional | Optional Refreshment Center |
| Standard Cabin Seats | 8 | 6 |
| Crew Rest | — | No |
| Jump Seat | — | No |
| Cargo Door | — | Yes |
| SL Cabin Altitude (ft) | — | 23500 |
| Engine | ||
| FADEC | Yes | Yes |
| Model | PT6A-60A | FJ44-4A-QPM |
| TBO (hrs) | 3600 | 5000 |
| Horsepower | 1050 | — |
| Flat Rating | ISA + 10 | ISA + 23 |
| No. of Engines | 1 | 2 |
| Fuel Capacity (gal) | 539 | — |
| Thrust (lbs) | — | 3435 |
| Dimensions | ||
| Length (ft) | 46.7 | 52.2 |
| Wingspan (ft) | 57.9 | 55.8 |
| Cabin Width (ft) | 4.5 | 5.6 |
| Cabin Height (ft) | 4.8 | 5.1 |
| Cabin Length (ft) | 19.5 | 23 |
| Overall Height (ft) | 14.4 | 17.4 |
| Cabin Width - Floor (ft) | 4.1 | 3.8 |
| Cabin Length - Seating (ft) | 19.5 | 17 |
| Baggage Volume Int. (cu. ft) | 71 | 90 |
| Aisle Step (ft) | — | Flat Floor |