Compare Beechcraft King Air 360 vs Embraer Phenom 300E vs Pilatus PC-12 NGX
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| Manufacturer | Beechcraft | Embraer | Pilatus |
| Aircraft Type | KingAir 350i | Phenom 300E | PC-12 NGX |
| Base Aircraft Price (USD) | $7,650,000 | $9,650,000 | $5,350,000 |
| Direct Operating Cost | $ 1,311 | $ 1,758 | $ 793 |
| DOC / nm | $ 4.20 | $ 3.88 | $ 2.78 |
| DOC / nm / Seat | $ 0.53 | $ 0.55 | $ 0.46 |
| Max Cruise Speed (ktas) | 312 | 447 | 290 |
| Max Range (nm) | 1560 | 1971 | 1866 |
| Useful Load (lbs) | 5145 | 6914 | 3692 |
| Total Seats | 10 | 9 | 8 |
| Cockpit | 2 | 2 | 2 |
| Standard Cabin Seats | 8 | 7 | 6 |
| Max Cabin Seats | 9 | 9 | 9 |
| Min Crew | 1 | 1 | 1 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line Fusion | Prodigy Touch (G3000) | Honeywell Primus Apex |
| Flight Rules | IFR | - | IFR |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| OEM Verification | VERIFIED | VERIFIED | VERIFIED |
| Weights | |||
| MRAMP (lbs) | 15100 | 18497 | 10495 |
| MTOW (lbs) | 15000 | 18387 | 10450 |
| MLW (lbs) | 15000 | 17043 | 9921 |
| MZFW (lbs) | 12500 | 14220 | 9039 |
| BOW (lbs) | 9955 | 11583 | 6803 |
| BEW (lbs) | 9855 | 11473 | 6758 |
| Useful Load (lbs) | 5145 | 6914 | 3692 |
| Max Payload (lbs) | 2545 | 2637 | 2235 |
| Fuel Capacity (lbs) | 3611 | 5353 | 2704 |
| Payload Max Fuel (lbs) | 1534 | 1561 | 988 |
| Max Baggage Weight (lbs) | 1150 | 650 | - |
| Dimensions | |||
| Wingspan (ft) | 57.9 | 52.16 | 53.33 |
| Overall Height (ft) | 14.4 | 16.75 | 14 |
| Length (ft) | 46.7 | 51.2 | 47.25 |
| Cabin Height (ft) | 4.8 | 4.9 | 4.9 |
| Aisle Step (ft) | - | 0.3 | - |
| Cabin Width (ft) | 4.5 | 5.1 | 5 |
| Cabin Width - Floor (ft) | 4.1 | 3.6 | 4.25 |
| Cabin Length (ft) | 19.5 | 17.2 | 16.9 |
| Cabin Length - Seating (ft) | 19.5 | 14.8 | - |
| Baggage Volume Int. (cu. ft) | 71 | 10 | 40 |
| Baggage Volume Ext. (cu. ft) | - | 74 | - |
| Engine | |||
| No. of Engines | 1 | 2 | 1 |
| Manufacturer | Beechcraft | Embraer | Pilatus |
| Model | PT6A-60A | Canada PW535E1 | PT6E-67XP |
| Horsepower | 1050 | - | 1200 |
| Thrust (lbs) | - | 3360 | - |
| Flat Rating | ISA + 10 | ISA + 15 | ISA + 35 |
| FADEC | Yes | Yes | Yes |
| TBO (hrs) | 3600 | 5000 | 5000 |
| Fuel Capacity (gal) | 539 | - | - |
| Usable Fuel (gal) | - | - | 402 |
| Fuel Burn (lbph) | - | 757 | - |
| Avionics | |||
| Flight Deck | Rockwell Collins Pro Line Fusion | Prodigy Touch (G3000) | Honeywell Primus Apex |
| Flight Rules | IFR | - | IFR |
| FMS | 2 | 2 | 1 |
| Autopilot | 1 | 1 | 1 |
| PFD | 2 | 2 | 2 |
| MFD | 1 | 2 | 1 |
| GPS | 1 | 1 | 1 |
| AHRS | 1 | 1 | 1 |
| Transponder | 1 | 1 | 1 |
| VHF Com | 2 | 1 | 2 |
| VHF NAV | 2 | 1 | 2 |
| Cabin | |||
| Total Seats | 10 | 9 | 8 |
| Cockpit | 2 | 2 | 2 |
| Standard Cabin Seats | 8 | 7 | 6 |
| Max Cabin Seats | 9 | 9 | 9 |
| Min Crew | 1 | 1 | 1 |
| Cargo Door | - | - | Yes |
| Lavatory | Optional | 1 Enclosed Flushing | Optional |
| Lavatory Location | AFT | AFT | FWD |
| Galley / Refreshment | Optional | Galley | No |
| Galley Location | FWD | FWD | - |
| Crew Rest | - | No | - |
| Jump Seat | - | No | - |
| SL Cabin Altitude (ft) | - | 25560 | 13100 |
| Cabin Pressure (psi) | 6.5 | 9.4 | 5.8 |
| Other | |||
| Prop Manufacturer | Hartzell | - | Hartzell |
| Prop Description | 4-Blade Constant Feathering Reverse | - | 5-Blade Comp |
| 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 | 0.78 | - |
| Max Cruise Speed (ktas) | 312 | 447 | 290 |
| Long Range Cruise (Mach) | - | 0.67 | - |
| Long Range Cruise (ktas) | 235 | 383 | 225 |
| Vref (kias) | 100 | 104 | - |
| Stall Speed - Clean (kias) | 82 | - | - |
| Stall Speed - Flaps (kias) | - | - | 67 |
| Max Range (nm) | 1560 | 1971 | 1866 |
| Max Range Crew + 4 (nm) | 1533 | 1936 | 1803 |
| Max Range Crew + 6 (nm) | - | - | 1568 |
| Max Range Crew + 8 (nm) | - | - | 1057 |
| Take-off FL (ft) | 3300 | 3138 | - |
| Take-Off >50ft Obst. (ft) | - | - | 2602 |
| Take-Off (5000 / ISA + 10) | 5376 | 5400 | 4270 |
| Landing Roll (ft) | - | 2200 | - |
| Landing >50ft Obst. (ft) | 2692 | - | 2170 |
| Max Climb Rate (fpm) | 2731 | - | 1920 |
| Service Ceiling (ft) | 35000 | 45000 | 30000 |