Compare Cessna Citation CJ4 vs Dassault Falcon 2000S vs Gulfstream G400
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| Manufacturer | Cessna Citation | Dassault Falcon | Gulfstream |
| Aircraft Type | CJ4 | 2000S | G400 |
| Base Aircraft Price (USD) | $11,290,000 | $ 26,000,000 | 34500000 |
| Direct Operating Cost | $ 1,970 | $ 3,150 | - |
| DOC / nm | $ 4.37 | $ 6.63 | - |
| DOC / nm / Seat | $ 0.62 | $ 0.83 | - |
| Max Cruise Speed (ktas) | 440 | 490 | 539 |
| Max Range (nm) | 2170 | 3540 | 4200 |
| Useful Load (lbs) | 6914 | 18250 | 30650 |
| Total Seats | 9 | 12 | 12 |
| Cockpit | 2 | 2 | - |
| Standard Cabin Seats | 7 | 10 | - |
| Max Cabin Seats | 8 | 10 | 19 |
| Min Crew | 1 | 2 | 4 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line 21 | Honeywell Primus EASy II | Gulfstream Symmetry Flight Deck |
| Certification | FAA / EASA | FAA / EASA | - |
| OEM Verification | VERIFIED | VERIFIED | - |
| Weights | |||
| MRAMP (lbs) | 18497 | 41200 | - |
| MTOW (lbs) | 17110 | 41000 | - |
| MLW (lbs) | 15660 | 39300 | - |
| MZFW (lbs) | 12500 | 29700 | - |
| BOW (lbs) | 10280 | 22750 | - |
| BEW (lbs) | 10196 | 22750 | - |
| Useful Load (lbs) | 6914 | 18250 | 30650 |
| Max Payload (lbs) | 2637 | 4950 | - |
| Fuel Capacity (lbs) | 5830 | 12155 | - |
| Useful Load Max Fuel (lbs) | 1184 | - | - |
| Payload Max Fuel (lbs) | 1122 | 1590 | - |
| Max Baggage Weight (lbs) | 1040 | 1600 | - |
| Dimensions | |||
| Wingspan (ft) | 50 | 70.2 | - |
| Overall Height (ft) | 15.5 | 23.2 | - |
| Length (ft) | 53.4 | 66.4 | - |
| Cabin Height (ft) | 4.8 | 6.2 | - |
| Aisle Step (ft) | 0.4 | Flat Floor | - |
| Cabin Width (ft) | 4.8 | 7.7 | - |
| Cabin Width - Floor (ft) | 3.1 | 6.3 | - |
| Cabin Length (ft) | 17.2 | 26.2 | - |
| Cabin Length - Seating (ft) | 14.8 | 17.1 | - |
| Cabin Volume (cu. ft) | - | 1024 | - |
| Baggage Volume Int. (cu. ft) | 7 | 134 | - |
| Baggage Volume Ext. (cu. ft) | 70 | - | - |
| Engine | |||
| No. of Engines | 2 | 2 | - |
| Manufacturer | Cessna Citation | Dassault Falcon | Gulfstream |
| Model | FJ44-4A | PW308C | - |
| Thrust (lbs) | 3621 | 7000 | - |
| Flat Rating | ISA + 11 | ISA + 15 | - |
| FADEC | Yes | Yes | - |
| TBO (hrs) | 5000 | 7000 | - |
| Fuel Capacity (gal) | 870 | - | - |
| Fuel Burn (lbph) | 757 | - | - |
| Avionics | |||
| Flight Deck | Rockwell Collins Pro Line 21 | Honeywell Primus EASy II | - |
| FMS | 1 | 3 | - |
| Autopilot | 1 | 2 | - |
| PFD | 2 | 2 | - |
| MFD | 2 | 2 | - |
| GPS | 1 | 3 | - |
| AHRS | 2 | 1 | - |
| ADC | 2 | - | - |
| Transponder | 1 | 2 | - |
| VHF Com | 1 | 3 | - |
| VHF NAV | 1 | 3 | - |
| Cabin | |||
| Total Seats | 9 | 12 | 12 |
| Cockpit | 2 | 2 | - |
| Standard Cabin Seats | 7 | 10 | - |
| Max Cabin Seats | 8 | 10 | 19 |
| Min Crew | 1 | 2 | 4 |
| Lavatory | 1 Enclosed Belted Flushing | 1 Enclosed Flushing | - |
| Lavatory Location | AFT | AFT | - |
| Galley / Refreshment | Galley | Galley | - |
| Galley Location | FWD | FWD | - |
| Crew Rest | No | No | - |
| Jump Seat | No | No | - |
| SL Cabin Altitude (ft) | 24005 | 25300 | - |
| Cabin Pressure (psi) | 9 | 9.6 | - |
| Other | |||
| APU Manufacturer | - | - | - |
| APU Model | - | - | - |
| APU TBO (hrs) | - | - | - |
| 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 | 0.862 | - |
| Max Cruise Speed (ktas) | 440 | 490 | 539 |
| Long Range Cruise (Mach) | 0.66 | 0.75 | - |
| Long Range Cruise (ktas) | 377 | 430 | - |
| Vref (kias) | 117 | 106 | - |
| Max Range (nm) | 2170 | 3540 | 4200 |
| Max Range Crew + 4 (nm) | 1918 | 3515 | - |
| Max Range Crew + 6 (nm) | 1790 | 3515 | - |
| Max Range Crew + 8 (nm) | 1612 | - | - |
| Take-off FL (ft) | 3410 | 5436 | - |
| Take-Off (5000 / ISA + 10) | 5180 | - | - |
| Landing Roll (ft) | 2665 | 2315 | - |
| Landing >50ft Obst. (ft) | 2940 | - | - |
| Max Climb Rate (fpm) | 3854 | 3730 | - |
| Service Ceiling (ft) | 45000 | 47000 | - |