Compare Beechcraft King Air 360ER vs Dassault Falcon 2000LXS vs Pilatus PC-24
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| Manufacturer | Beechcraft | Dassault Falcon | Pilatus |
| Aircraft Type | KingAir 350ER | 2000LXS | PC-24 |
| Base Aircraft Price (USD) | $8,750,000 | $35,100,000 | $11,800,000 |
| Direct Operating Cost | $ 1,324 | $ 3,073 | $ 1,619 |
| DOC / nm | $ 4.37 | $ 6.38 | $ 3.71 |
| DOC / nm / Seat | $ 0.55 | $ 0.80 | $ 0.62 |
| Max Cruise Speed (ktas) | 303 | 490 | 440 |
| Max Range (nm) | 2338 | 4155 | 2076 |
| Useful Load (lbs) | 6585 | 18250 | 6680 |
| Total Seats | 10 | 12 | 6 |
| Cockpit | 2 | 2 | 2 |
| Standard Cabin Seats | 8 | 10 | 6 |
| Max Cabin Seats | 9 | 10 | 10 |
| Min Crew | 1 | 2 | 1 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line Fusion | Honeywell Primus EASy II | Pilatus ACE (Primus Apex) |
| Flight Rules | IFR | - | - |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| OEM Verification | VERIFIED | VERIFIED | VERIFIED |
| Weights | |||
| MRAMP (lbs) | 16600 | 43000 | 18400 |
| MTOW (lbs) | 16500 | 42800 | 18300 |
| MLW (lbs) | 15675 | 39300 | 16900 |
| MZFW (lbs) | 13000 | 29700 | 14220 |
| BOW (lbs) | 10215 | 24750 | 11620 |
| BEW (lbs) | 9915 | 24550 | 11520 |
| Useful Load (lbs) | 6585 | 18250 | 6680 |
| Max Payload (lbs) | 2785 | 4950 | 2500 |
| Fuel Capacity (lbs) | 5192 | 16660 | 5964 |
| Payload Max Fuel (lbs) | 1193 | 1590 | 715 |
| Max Baggage Weight (lbs) | 1150 | 1600 | 1000 |
| Dimensions | |||
| Wingspan (ft) | 57.9 | 70.2 | 55.8 |
| Overall Height (ft) | 14.4 | 23.2 | 17.4 |
| Length (ft) | 46.7 | 66.4 | 52.2 |
| Cabin Height (ft) | 4.8 | 6.2 | 5.1 |
| Aisle Step (ft) | - | Flat Floor | Flat Floor |
| Cabin Width (ft) | 4.5 | 7.7 | 5.6 |
| Cabin Width - Floor (ft) | 4.1 | 6.3 | 3.8 |
| Cabin Length (ft) | 19.5 | 26.2 | 23 |
| Cabin Length - Seating (ft) | 19.5 | 17.1 | 17 |
| Cabin Volume (cu. ft) | - | 1024 | - |
| Baggage Volume Int. (cu. ft) | 71 | 131 | 90 |
| Engine | |||
| No. of Engines | 1 | 2 | 2 |
| Manufacturer | Beechcraft | Dassault Falcon | Pilatus |
| Model | PT6A-60A | PW308C | FJ44-4A-QPM |
| Horsepower | 1050 | - | - |
| Thrust (lbs) | - | 7000 | 3435 |
| Flat Rating | ISA + 10 | ISA + 15 | ISA + 23 |
| FADEC | Yes | Yes | Yes |
| TBO (hrs) | 3600 | 7000 | 5000 |
| Fuel Capacity (gal) | 775 | - | - |
| Avionics | |||
| Flight Deck | Rockwell Collins Pro Line Fusion | Honeywell Primus EASy II | Pilatus ACE (Primus Apex) |
| Flight Rules | IFR | - | - |
| FMS | 2 | 3 | 1 |
| Autopilot | 1 | 2 | 1 |
| PFD | 2 | 2 | 2 |
| MFD | 1 | 2 | 1 |
| GPS | 1 | 3 | 1 |
| AHRS | 1 | 1 | 1 |
| Transponder | 1 | 2 | 1 |
| VHF Com | 2 | 3 | 1 |
| VHF NAV | 2 | 3 | 1 |
| Cabin | |||
| Total Seats | 10 | 12 | 6 |
| Cockpit | 2 | 2 | 2 |
| Standard Cabin Seats | 8 | 10 | 6 |
| Max Cabin Seats | 9 | 10 | 10 |
| Min Crew | 1 | 2 | 1 |
| Cargo Door | Optional | - | Yes |
| Lavatory | Yes (Belted Optional) | 1 Enclosed Flushing | 1 Enclosed Flushing |
| Lavatory Location | AFT | AFT | FWD |
| Galley / Refreshment | Refreshment Center | Galley | Optional Refreshment Center |
| Galley Location | FWD | FWD | FWD |
| Crew Rest | - | No | No |
| Jump Seat | - | No | No |
| SL Cabin Altitude (ft) | - | 25300 | 23500 |
| Cabin Pressure (psi) | 6.5 | 9.6 | 9.3 |
| Other | |||
| Prop Manufacturer | Hartzell | - | - |
| Prop Description | 4-Blade Constant Feathering Reverse | - | - |
| APU Manufacturer | - | - | - |
| APU Model | - | - | - |
| APU TBO (hrs) | - | - | - |
| Gear Type | Retractable | - | - |
| Warranty | |||
| Airframe (Yrs) | - | 3 | 2 |
| Airframe (Hrs) | - | 1000 | - |
| Engine (Yrs) | - | 2 | 5 |
| Engine (Hrs) | - | 1000 | 2000 |
| APU (Hrs) | - | 2000 | - |
| Avionics (Yrs) | - | - | 3 |
| Performance | |||
| Max Cruise Speed (Mach) | 0.58 | 0.86 | 0.74 |
| Max Cruise Speed (ktas) | 303 | 490 | 440 |
| Long Range Cruise (Mach) | - | 0.77 | 0.62 |
| Long Range Cruise (ktas) | 238 | 440 | 358 |
| Vref (kias) | 104 | 106 | 90 |
| Stall Speed - Clean (kias) | 82 | - | - |
| Stall Speed - Flaps (kias) | - | - | 82 |
| Max Range (nm) | 2338 | 4155 | 2076 |
| Max Range Crew + 4 (nm) | 2271 | 4065 | 1882 |
| Max Range Crew + 6 (nm) | - | 4065 | 1689 |
| Max Range Crew + 8 (nm) | - | - | 1498 |
| Take-off FL (ft) | 4057 | 5878 | 2930 |
| Take-Off (5000 / ISA + 10) | 7675 | - | 4720 |
| Landing Roll (ft) | - | 2315 | 2375 |
| Landing >50ft Obst. (ft) | 2728 | - | - |
| Max Climb Rate (fpm) | 2400 | 4350 | 4151 |
| Service Ceiling (ft) | 35000 | 47000 | 45000 |