Compare Beechcraft King Air 360 vs Gulfstream G600 vs Pilatus PC-12 NGX
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| Manufacturer | Beechcraft | Gulfstream | Pilatus |
| Aircraft Type | KingAir 350i | G600 | PC-12 NGX |
| Base Aircraft Price (USD) | $7,650,000 | $58,500,000 | $5,350,000 |
| Direct Operating Cost | $ 1,311 | $ 4,789 | $ 793 |
| DOC / nm | $ 4.20 | $ 9.28 | $ 2.78 |
| DOC / nm / Seat | $ 0.53 | $ 0.93 | $ 0.46 |
| Max Cruise Speed (ktas) | 312 | 516 | 290 |
| Max Range (nm) | 1560 | 6500 | 1866 |
| Useful Load (lbs) | 5145 | 40560 | 3692 |
| Total Seats | 10 | 12 | 8 |
| Cockpit | 2 | 2 | 2 |
| Standard Cabin Seats | 8 | 10 | 6 |
| Max Cabin Seats | 9 | 19 | 9 |
| Min Crew | 1 | 4 | 1 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line Fusion | Gulfstream Symmetry Flight Deck | Honeywell Primus Apex |
| Flight Rules | IFR | - | IFR |
| Certification | FAA / EASA | FAA | FAA / EASA |
| OEM Verification | VERIFIED | Un-Verified | VERIFIED |
| Weights | |||
| MRAMP (lbs) | 15100 | 92000 | 10495 |
| MTOW (lbs) | 15000 | 94600 | 10450 |
| MLW (lbs) | 15000 | 76800 | 9921 |
| MZFW (lbs) | 12500 | 57440 | 9039 |
| BOW (lbs) | 9955 | 51470 | 6803 |
| BEW (lbs) | 9855 | 54040 | 6758 |
| Useful Load (lbs) | 5145 | 40560 | 3692 |
| Max Payload (lbs) | 2545 | 6000 | 2235 |
| Fuel Capacity (lbs) | 3611 | 38760 | 2704 |
| Payload Max Fuel (lbs) | 1534 | 1800 | 988 |
| Max Baggage Weight (lbs) | 1150 | 2250 | - |
| Dimensions | |||
| Wingspan (ft) | 57.9 | 94.1 | 53.33 |
| Overall Height (ft) | 14.4 | 25.3 | 14 |
| Length (ft) | 46.7 | 96.1 | 47.25 |
| Cabin Height (ft) | 4.8 | 6.4 | 4.9 |
| Aisle Step (ft) | - | Flat Floor | - |
| Cabin Width (ft) | 4.5 | 7.6 | 5 |
| Cabin Width - Floor (ft) | 4.1 | 6.1 | 4.25 |
| Cabin Length (ft) | 19.5 | 45.2 | 16.9 |
| Cabin Length - Seating (ft) | 19.5 | 30.2 | - |
| Baggage Volume Int. (cu. ft) | 71 | 230 | 40 |
| Engine | |||
| No. of Engines | 1 | 2 | 1 |
| Manufacturer | Beechcraft | Gulfstream | Pilatus |
| Model | PT6A-60A | PW815GA | PT6E-67XP |
| Horsepower | 1050 | - | 1200 |
| Thrust (lbs) | - | 15680 | - |
| Flat Rating | ISA + 10 | ISA + 15 | ISA + 35 |
| FADEC | Yes | Yes | Yes |
| TBO (hrs) | 3600 | 10000 | 5000 |
| Fuel Capacity (gal) | 539 | - | - |
| Usable Fuel (gal) | - | - | 402 |
| Avionics | |||
| Flight Deck | Rockwell Collins Pro Line Fusion | Gulfstream Symmetry Flight Deck | Honeywell Primus Apex |
| Flight Rules | IFR | - | 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 | 2 |
| VHF NAV | 2 | 3 | 2 |
| Cabin | |||
| Total Seats | 10 | 12 | 8 |
| Cockpit | 2 | 2 | 2 |
| Standard Cabin Seats | 8 | 10 | 6 |
| Max Cabin Seats | 9 | 19 | 9 |
| Min Crew | 1 | 4 | 1 |
| Cargo Door | - | - | Yes |
| Lavatory | Optional | 2 Enclosed Flushing | Optional |
| Lavatory Location | AFT | FWD / AFT | FWD |
| Galley / Refreshment | Optional | Galley | No |
| Galley Location | FWD | FWD | - |
| Crew Rest | - | Yes | - |
| Jump Seat | - | Yes | - |
| SL Cabin Altitude (ft) | - | 31900 | 13100 |
| Cabin Pressure (psi) | 6.5 | 10.7 | 5.8 |
| Other | |||
| Prop Manufacturer | Hartzell | - | Hartzell |
| Prop Description | 4-Blade Constant Feathering Reverse | - | 5-Blade Comp |
| APU Manufacturer | - | - | - |
| APU Model | - | - | - |
| APU TBO (hrs) | - | - | - |
| Gear Type | Retractable | - | Retractable |
| Warranty | |||
| Airframe (Yrs) | - | 3 | - |
| Airframe (Hrs) | - | 1000 | - |
| Engine (Yrs) | - | 2 | - |
| Engine (Hrs) | - | 1000 | - |
| APU (Hrs) | - | 2000 | - |
| Performance | |||
| Max Cruise Speed (Mach) | 0.58 | 0.9 | - |
| Max Cruise Speed (ktas) | 312 | 516 | 290 |
| Long Range Cruise (Mach) | - | 0.85 | - |
| Long Range Cruise (ktas) | 235 | 487 | 225 |
| Vref (kias) | 100 | - | - |
| Stall Speed - Clean (kias) | 82 | - | - |
| Stall Speed - Flaps (kias) | - | - | 67 |
| Max Range (nm) | 1560 | 6500 | 1866 |
| Max Range Crew + 4 (nm) | 1533 | 6500 | 1803 |
| Max Range Crew + 6 (nm) | - | 6500 | 1568 |
| Max Range Crew + 8 (nm) | - | 6500 | 1057 |
| Take-off FL (ft) | 3300 | 5900 | - |
| Take-Off >50ft Obst. (ft) | - | - | 2602 |
| Take-Off (5000 / ISA + 10) | 5376 | - | 4270 |
| Landing Roll (ft) | - | 3100 | - |
| Landing >50ft Obst. (ft) | 2692 | - | 2170 |
| Max Climb Rate (fpm) | 2731 | - | 1920 |
| Service Ceiling (ft) | 35000 | 51000 | 30000 |