Compare Embraer Phenom 300E vs Embraer Praetor 600 vs Pilatus PC-12 NGX
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| Manufacturer | Embraer | Embraer | Pilatus |
| Aircraft Type | Phenom 300E | Praetor 600 | PC-12 NGX |
| Base Aircraft Price (USD) | $9,650,000 | $20,995,000 | $5,350,000 |
| Direct Operating Cost | $ 1,758 | $ 3,141 | $ 793 |
| DOC / nm | $ 3.88 | $ 6.74 | $ 2.78 |
| DOC / nm / Seat | $ 0.55 | $ 0.84 | $ 0.46 |
| Max Cruise Speed (ktas) | 447 | 476 | 290 |
| Max Range (nm) | 1971 | 4018 | 1866 |
| Useful Load (lbs) | 6914 | - | 3692 |
| Total Seats | 9 | 10 | 8 |
| Cockpit | 2 | 2 | 2 |
| Standard Cabin Seats | 7 | 8 | 6 |
| Max Cabin Seats | 9 | 12 | 9 |
| Min Crew | 1 | 2 | 1 |
| Flight Deck (Base Spec) | Prodigy Touch (G3000) | Rockwell Collins Pro Line Fusion | Honeywell Primus Apex |
| Flight Rules | - | - | IFR |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| OEM Verification | VERIFIED | VERIFIED | VERIFIED |
| Weights | |||
| MRAMP (lbs) | 18497 | - | 10495 |
| MTOW (lbs) | 18387 | - | 10450 |
| MLW (lbs) | 17043 | - | 9921 |
| MZFW (lbs) | 14220 | - | 9039 |
| BOW (lbs) | 11583 | - | 6803 |
| BEW (lbs) | 11473 | - | 6758 |
| Useful Load (lbs) | 6914 | - | 3692 |
| Max Payload (lbs) | 2637 | 4001 | 2235 |
| Fuel Capacity (lbs) | 5353 | - | 2704 |
| Payload Max Fuel (lbs) | 1561 | - | 988 |
| Max Baggage Weight (lbs) | 650 | - | - |
| Dimensions | |||
| Wingspan (ft) | 52.16 | 70.5 | 53.33 |
| Overall Height (ft) | 16.75 | 21 | 14 |
| Length (ft) | 51.2 | 68.1 | 47.25 |
| Cabin Height (ft) | 4.9 | 6 | 4.9 |
| Aisle Step (ft) | 0.3 | Flat Floor | - |
| Cabin Width (ft) | 5.1 | 6.8 | 5 |
| Cabin Width - Floor (ft) | 3.6 | 4.7 | 4.25 |
| Cabin Length (ft) | 17.2 | 24.1 | 16.9 |
| Cabin Length - Seating (ft) | 14.8 | 21.3 | - |
| Baggage Volume Int. (cu. ft) | 10 | 45 | 40 |
| Baggage Volume Ext. (cu. ft) | 74 | 110 | - |
| Engine | |||
| No. of Engines | 2 | 2 | 1 |
| Manufacturer | Embraer | Embraer | Pilatus |
| Model | Canada PW535E1 | HTF7500E | PT6E-67XP |
| Horsepower | - | - | 1200 |
| Thrust (lbs) | 3360 | 7528 | - |
| Flat Rating | ISA + 15 | ISA + 18 | ISA + 35 |
| FADEC | Yes | Yes | Yes |
| TBO (hrs) | 5000 | On-Condition | 5000 |
| Fuel Capacity (gal) | - | 1963 | - |
| Usable Fuel (gal) | - | - | 402 |
| Fuel Burn (lbph) | 757 | - | - |
| Avionics | |||
| Flight Deck | Prodigy Touch (G3000) | Rockwell Collins Pro Line Fusion | Honeywell Primus Apex |
| Flight Rules | - | - | IFR |
| FMS | 2 | 2 | 1 |
| Autopilot | 1 | 2 | 1 |
| PFD | 2 | 2 | 2 |
| MFD | 2 | 2 | 1 |
| GPS | 1 | 2 | 1 |
| AHRS | 1 | 1 | 1 |
| Transponder | 1 | 2 | 1 |
| VHF Com | 1 | 2 | 2 |
| VHF NAV | 1 | 2 | 2 |
| Cabin | |||
| Total Seats | 9 | 10 | 8 |
| Cockpit | 2 | 2 | 2 |
| Standard Cabin Seats | 7 | 8 | 6 |
| Max Cabin Seats | 9 | 12 | 9 |
| Min Crew | 1 | 2 | 1 |
| Cargo Door | - | - | Yes |
| Connectivity | - | Gogo AVANCE L5 | - |
| Lavatory | 1 Enclosed Flushing | 1 Enclosed Belted Flushing | Optional |
| Lavatory Location | AFT | AFT | FWD |
| Galley / Refreshment | Galley | Galley | No |
| Galley Location | FWD | FWD | - |
| Crew Rest | No | No | - |
| Jump Seat | No | No | - |
| Max Cabin Altitude (ft) | - | 5800 | - |
| SL Cabin Altitude (ft) | 25560 | 27140 | 13100 |
| Cabin Pressure (psi) | 9.4 | 9.7 | 5.8 |
| Other | |||
| Prop Manufacturer | - | - | Hartzell |
| Prop Description | - | - | 5-Blade Comp |
| Gear Type | - | - | Retractable |
| Warranty | |||
| Airframe (Yrs) | 3 | 3 | - |
| Airframe (Hrs) | 1000 | 1000 | - |
| Engine (Yrs) | 2 | 2 | - |
| Engine (Hrs) | 1000 | 1000 | - |
| APU (Hrs) | 2000 | 2000 | - |
| Performance | |||
| Max Cruise Speed (Mach) | 0.78 | 0.83 | - |
| Max Cruise Speed (ktas) | 447 | 476 | 290 |
| Long Range Cruise (Mach) | 0.67 | 0.77 | - |
| Long Range Cruise (ktas) | 383 | 440 | 225 |
| Vref (kias) | 104 | 102 | - |
| Stall Speed - Flaps (kias) | - | - | 67 |
| Max Range (nm) | 1971 | 4018 | 1866 |
| Max Range Crew + 4 (nm) | 1936 | 4018 | 1803 |
| Max Range Crew + 6 (nm) | - | - | 1568 |
| Max Range Crew + 8 (nm) | - | - | 1057 |
| Take-off FL (ft) | 3138 | 4717 | - |
| Take-Off >50ft Obst. (ft) | - | - | 2602 |
| Take-Off (5000 / ISA + 10) | 5400 | - | 4270 |
| Landing Roll (ft) | 2200 | 2165 | - |
| Landing >50ft Obst. (ft) | - | - | 2170 |
| Max Climb Rate (fpm) | - | - | 1920 |
| Service Ceiling (ft) | 45000 | 45000 | 30000 |