Compare Beechcraft King Air 360 vs Pilatus PC-12 NGX vs Piper M600 SLS
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| Manufacturer | Beechcraft | Pilatus | Piper |
| Aircraft Type | KingAir 350i | PC-12 NGX | M600 |
| Base Aircraft Price (USD) | $7,650,000 | $5,350,000 | $3,081,400 |
| Direct Operating Cost | $ 1,311 | $ 793 | $ 603 |
| DOC / nm | $ 4.20 | $ 2.78 | $ 2.19 |
| DOC / nm / Seat | $ 0.53 | $ 0.46 | $ 0.55 |
| Max Cruise Speed (ktas) | 312 | 290 | 274 |
| Max Range (nm) | 1560 | 1866 | 1658 |
| Useful Load (lbs) | 5145 | 3692 | 2350 |
| Total Seats | 10 | 8 | 5 |
| Cockpit | 2 | 2 | 2 |
| Standard Cabin Seats | 8 | 6 | 4 |
| Max Cabin Seats | 9 | 9 | - |
| Min Crew | 1 | 1 | 1 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line Fusion | Honeywell Primus Apex | Garmin G3000 |
| Flight Rules | IFR | IFR | IFR |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| OEM Verification | VERIFIED | VERIFIED | VERIFIED |
| Weights | |||
| MRAMP (lbs) | 15100 | 10495 | 6050 |
| MTOW (lbs) | 15000 | 10450 | 6000 |
| MLW (lbs) | 15000 | 9921 | 5800 |
| MZFW (lbs) | 12500 | 9039 | 4850 |
| BOW (lbs) | 9955 | 6803 | 3700 |
| BEW (lbs) | 9855 | 6758 | 3650 |
| Useful Load (lbs) | 5145 | 3692 | 2350 |
| Max Payload (lbs) | 2545 | 2235 | 2300 |
| Fuel Capacity (lbs) | 3611 | 2704 | 1642 |
| Useful Load Max Fuel (lbs) | - | - | 1692 |
| Payload Max Fuel (lbs) | 1534 | 988 | 658 |
| Max Baggage Weight (lbs) | 1150 | - | - |
| Dimensions | |||
| Wingspan (ft) | 57.9 | 53.33 | 43.2 |
| Overall Height (ft) | 14.4 | 14 | 11.3 |
| Length (ft) | 46.7 | 47.25 | 29.7 |
| Cabin Height (ft) | 4.8 | 4.9 | 4 |
| Cabin Width (ft) | 4.5 | 5 | 4.1 |
| Cabin Width - Floor (ft) | 4.1 | 4.25 | - |
| Cabin Length (ft) | 19.5 | 16.9 | 12.3 |
| Cabin Length - Seating (ft) | 19.5 | - | - |
| Cabin Volume (cu. ft) | - | - | 165 |
| Baggage Volume Int. (cu. ft) | 71 | 40 | 20 |
| Engine | |||
| No. of Engines | 1 | 1 | 1 |
| Manufacturer | Beechcraft | Pilatus | Piper |
| Model | PT6A-60A | PT6E-67XP | PT6A-42A |
| Horsepower | 1050 | 1200 | 600 |
| Flat Rating | ISA + 10 | ISA + 35 | ISA + 55 |
| FADEC | Yes | Yes | No |
| TBO (hrs) | 3600 | 5000 | 3600 |
| Fuel Capacity (gal) | 539 | - | 260 |
| Usable Fuel (gal) | - | 402 | - |
| Avionics | |||
| Flight Deck | Rockwell Collins Pro Line Fusion | Honeywell Primus Apex | Garmin G3000 |
| Flight Rules | IFR | IFR | IFR |
| Standby Instrument | - | - | Aspen Avionics EFD1000 |
| FMS | 2 | 1 | - |
| Autopilot | 1 | 1 | 1 x Garmin GFC-700 |
| PFD | 2 | 2 | 2 |
| MFD | 1 | 1 | 1 |
| GPS | 1 | 1 | 2 x Garmin GIA64W |
| AHRS | 1 | 1 | 2 |
| ADC | - | - | 2 |
| Transponder | 1 | 1 | 1 x Garmin GTX-335R (ADS-B OUT) |
| VHF Com | 2 | 2 | 2 |
| VHF NAV | 2 | 2 | 2 |
| Cabin | |||
| Total Seats | 10 | 8 | 5 |
| Cockpit | 2 | 2 | 2 |
| Standard Cabin Seats | 8 | 6 | 4 |
| Max Cabin Seats | 9 | 9 | - |
| Min Crew | 1 | 1 | 1 |
| Cargo Door | - | Yes | - |
| Lavatory | Optional | Optional | No |
| Lavatory Location | AFT | FWD | - |
| Galley / Refreshment | Optional | No | Refreshment Centre |
| Galley Location | FWD | - | MID |
| Max Cabin Altitude (ft) | - | - | 8644 |
| SL Cabin Altitude (ft) | - | 13100 | 12600 |
| Cabin Pressure (psi) | 6.5 | 5.8 | 5.6 |
| Other | |||
| Prop Manufacturer | Hartzell | Hartzell | Hartzell |
| Prop Description | 4-Blade Constant Feathering Reverse | 5-Blade Comp | 4-Blade Constant Speed Reverse |
| Gear Type | Retractable | Retractable | Retractable |
| Warranty | |||
| Pilot Training Credits | - | - | 1 |
| Airframe (Yrs) | - | - | 5 |
| Airframe (Hrs) | - | - | 1500 |
| Engine (Yrs) | - | - | 7 |
| Engine (Hrs) | - | - | 2500 |
| Prop (Yrs) | - | - | 5 |
| Prop (Hrs) | - | - | 1500 |
| Avionics (Yrs) | - | - | 5 |
| Performance | |||
| Max Cruise Speed (Mach) | 0.58 | - | - |
| Max Cruise Speed (ktas) | 312 | 290 | 274 |
| Long Range Cruise (ktas) | 235 | 225 | 184 |
| Vref (kias) | 100 | - | - |
| Stall Speed - Clean (kias) | 82 | - | - |
| Stall Speed - Flaps (kias) | - | 67 | - |
| Max Range (nm) | 1560 | 1866 | 1658 |
| Range @ 75% | - | - | 1385 |
| Max Range Crew + 4 (nm) | 1533 | 1803 | - |
| Max Range Crew + 6 (nm) | - | 1568 | - |
| Max Range Crew + 8 (nm) | - | 1057 | - |
| Take-off FL (ft) | 3300 | - | - |
| Take-off Roll (ft) | - | - | 2635 |
| Take-Off >50ft Obst. (ft) | - | 2602 | - |
| Take-Off (5000 / ISA + 10) | 5376 | 4270 | 3998 |
| Landing >50ft Obst. (ft) | 2692 | 2170 | 2659 |
| Max Climb Rate (fpm) | 2731 | 1920 | 1556 |
| Service Ceiling (ft) | 35000 | 30000 | 30000 |