Compare Cessna Citation CJ4 vs Dassault Falcon 10X vs Embraer Praetor 600
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| Manufacturer | Cessna Citation | Dassault Falcon | Embraer |
| Aircraft Type | CJ4 | 10X | Praetor 600 |
| Base Aircraft Price (USD) | $11,290,000 | $ 75,000,000 | $20,995,000 |
| Direct Operating Cost | $ 1,970 | $2,770 | $ 3,141 |
| DOC / nm | $ 4.37 | - | $ 6.74 |
| DOC / nm / Seat | $ 0.62 | - | $ 0.84 |
| Max Cruise Speed (ktas) | 440 | 516 | 476 |
| Max Range (nm) | 2170 | 7505 | 4018 |
| Useful Load (lbs) | 6914 | 36900 | - |
| Total Seats | 9 | 17 | 10 |
| Cockpit | 2 | 2 | 2 |
| Standard Cabin Seats | 7 | 14 | 8 |
| Max Cabin Seats | 8 | 16 | 12 |
| Min Crew | 1 | 2 | 2 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line 21 | Digital Flight Control System | Rockwell Collins Pro Line Fusion |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| OEM Verification | VERIFIED | VERIFIED | VERIFIED |
| Weights | |||
| MRAMP (lbs) | 18497 | - | - |
| MTOW (lbs) | 17110 | - | - |
| MLW (lbs) | 15660 | - | - |
| MZFW (lbs) | 12500 | - | - |
| BOW (lbs) | 10280 | - | - |
| BEW (lbs) | 10196 | - | - |
| Useful Load (lbs) | 6914 | 36900 | - |
| Max Payload (lbs) | 2637 | - | 4001 |
| Fuel Capacity (lbs) | 5830 | - | - |
| Useful Load Max Fuel (lbs) | 1184 | - | - |
| Payload Max Fuel (lbs) | 1122 | - | - |
| Max Baggage Weight (lbs) | 1040 | - | - |
| Dimensions | |||
| Wingspan (ft) | 50 | - | 70.5 |
| Overall Height (ft) | 15.5 | - | 21 |
| Length (ft) | 53.4 | - | 68.1 |
| Cabin Height (ft) | 4.8 | - | 6 |
| Aisle Step (ft) | 0.4 | - | Flat Floor |
| Cabin Width (ft) | 4.8 | - | 6.8 |
| Cabin Width - Floor (ft) | 3.1 | - | 4.7 |
| Cabin Length (ft) | 17.2 | - | 24.1 |
| Cabin Length - Seating (ft) | 14.8 | - | 21.3 |
| Baggage Volume Int. (cu. ft) | 7 | - | 45 |
| Baggage Volume Ext. (cu. ft) | 70 | - | 110 |
| Engine | |||
| No. of Engines | 2 | - | 2 |
| Manufacturer | Cessna Citation | Dassault Falcon | Embraer |
| Model | FJ44-4A | - | HTF7500E |
| Thrust (lbs) | 3621 | - | 7528 |
| Flat Rating | ISA + 11 | - | ISA + 18 |
| FADEC | Yes | - | Yes |
| TBO (hrs) | 5000 | - | On-Condition |
| Fuel Capacity (gal) | 870 | - | 1963 |
| Fuel Burn (lbph) | 757 | - | - |
| Avionics | |||
| Flight Deck | Rockwell Collins Pro Line 21 | NeXus | Rockwell Collins Pro Line Fusion |
| FMS | 1 | - | 2 |
| Autopilot | 1 | - | 2 |
| PFD | 2 | - | 2 |
| MFD | 2 | - | 2 |
| GPS | 1 | - | 2 |
| AHRS | 2 | - | 1 |
| ADC | 2 | - | - |
| Transponder | 1 | - | 2 |
| VHF Com | 1 | - | 2 |
| VHF NAV | 1 | - | 2 |
| Cabin | |||
| Total Seats | 9 | 17 | 10 |
| Cockpit | 2 | 2 | 2 |
| Standard Cabin Seats | 7 | 14 | 8 |
| Max Cabin Seats | 8 | 16 | 12 |
| Min Crew | 1 | 2 | 2 |
| Connectivity | - | - | Gogo AVANCE L5 |
| Lavatory | 1 Enclosed Belted Flushing | - | 1 Enclosed Belted Flushing |
| Lavatory Location | AFT | - | AFT |
| Galley / Refreshment | Galley | - | Galley |
| Galley Location | FWD | - | FWD |
| Crew Rest | No | - | No |
| Jump Seat | No | - | No |
| Max Cabin Altitude (ft) | - | - | 5800 |
| SL Cabin Altitude (ft) | 24005 | - | 27140 |
| Cabin Pressure (psi) | 9 | - | 9.7 |
| 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) | 0.77 | .925 | 0.83 |
| Max Cruise Speed (ktas) | 440 | 516 | 476 |
| Long Range Cruise (Mach) | 0.66 | - | 0.77 |
| Long Range Cruise (ktas) | 377 | - | 440 |
| Vref (kias) | 117 | - | 102 |
| Max Range (nm) | 2170 | 7505 | 4018 |
| Max Range Crew + 4 (nm) | 1918 | - | 4018 |
| Max Range Crew + 6 (nm) | 1790 | - | - |
| Max Range Crew + 8 (nm) | 1612 | - | - |
| Take-off FL (ft) | 3410 | - | 4717 |
| Take-Off (5000 / ISA + 10) | 5180 | - | - |
| Landing Roll (ft) | 2665 | - | 2165 |
| Landing >50ft Obst. (ft) | 2940 | - | - |
| Max Climb Rate (fpm) | 3854 | - | - |
| Service Ceiling (ft) | 45000 | - | 45000 |