Compare Bombardier Challenger 650 vs Cessna Citation Latitude vs Pilatus PC-24
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| Manufacturer | Bombardier | Cessna Citation | Pilatus |
| Aircraft Type | Challenger 650 | Latitude | PC-24 |
| Base Aircraft Price (USD) | $32,400,000 | $19,305,000 | $11,800,000 |
| Direct Operating Cost | $ 3,365 | $ 2,936 | $ 1,619 |
| DOC / nm | $ 7.16 | $ 6.80 | $ 3.71 |
| DOC / nm / Seat | $ 0.80 | $ 0.85 | $ 0.62 |
| Max Cruise Speed (ktas) | 470 | 458 | 440 |
| Max Range (nm) | 4085 | 2731 | 2076 |
| Useful Load (lbs) | 21050 | 12394 | 6680 |
| Total Seats | 11 | 10 | 6 |
| Cockpit | 2 | 2 | 2 |
| Standard Cabin Seats | 9 | 8 | 6 |
| Max Cabin Seats | 12 | 9 | 10 |
| Min Crew | 2 | 2 | 1 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line 21 Advanced | Garmin G5000 | Pilatus ACE (Primus Apex) |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| OEM Verification | VERIFIED | VERIFIED | VERIFIED |
| Weights | |||
| MRAMP (lbs) | 48300 | 31050 | 18400 |
| MTOW (lbs) | 48200 | 30800 | 18300 |
| MLW (lbs) | 38000 | 27575 | 16900 |
| MZFW (lbs) | 32000 | 21200 | 14220 |
| BOW (lbs) | 27250 | 18656 | 11620 |
| BEW (lbs) | 27150 | 18406 | 11520 |
| Useful Load (lbs) | 21050 | 12394 | 6680 |
| Max Payload (lbs) | 3750 | 2544 | 2500 |
| Fuel Capacity (lbs) | 19852 | 11394 | 5964 |
| Useful Load Max Fuel (lbs) | - | 1000 | - |
| Payload Max Fuel (lbs) | 1198 | 1000 | 715 |
| Max Baggage Weight (lbs) | 900 | 1245 | 1000 |
| Dimensions | |||
| Wingspan (ft) | 64.4 | 72.3 | 55.8 |
| Overall Height (ft) | 20.7 | 20.9 | 17.4 |
| Length (ft) | 68.4 | 62 | 52.2 |
| Cabin Height (ft) | 6 | 6 | 5.1 |
| Aisle Step (ft) | Flat Floor | Flat Floor | Flat Floor |
| Cabin Width (ft) | 7.9 | 6.4 | 5.6 |
| Cabin Width - Floor (ft) | 6.9 | 4.4 | 3.8 |
| Cabin Length (ft) | 25.6 | 21.8 | 23 |
| Cabin Length - Seating (ft) | 15.4 | 15.9 | 17 |
| Baggage Volume Int. (cu. ft) | 112 | 27 | 90 |
| Baggage Volume Ext. (cu. ft) | - | 100 | - |
| Engine | |||
| No. of Engines | 2 | 2 | 2 |
| Manufacturer | Bombardier | Cessna Citation | Pilatus |
| Model | CF34-3B MTO | PW306D1 | FJ44-4A-QPM |
| Thrust (lbs) | 9220 | 5907 | 3435 |
| Flat Rating | ISA + 15 | ISA + 15 | ISA + 23 |
| FADEC | Yes | Yes | Yes |
| TBO (hrs) | On-Condition | 6000 | 5000 |
| Fuel Capacity (gal) | - | 1700 | - |
| Fuel Burn (lbph) | - | 1114 | - |
| Avionics | |||
| Flight Deck | Rockwell Collins Pro Line 21 Advanced | Garmin G5000 | Pilatus ACE (Primus Apex) |
| FMS | 2 | 1 | 1 |
| Autopilot | 1 | 1 | 1 |
| PFD | 2 | 2 | 2 |
| MFD | 2 | 1 | 1 |
| GPS | 2 | 1 | 1 |
| AHRS | 2 | 1 | 1 |
| ADC | 2 | - | - |
| Transponder | 2 | 1 | 1 |
| VHF Com | 2 | 1 | 1 |
| VHF NAV | 2 | 1 | 1 |
| Cabin | |||
| Total Seats | 11 | 10 | 6 |
| Cockpit | 2 | 2 | 2 |
| Standard Cabin Seats | 9 | 8 | 6 |
| Max Cabin Seats | 12 | 9 | 10 |
| Min Crew | 2 | 2 | 1 |
| Cargo Door | - | - | Yes |
| Lavatory | 2 Enclosed Flushing | 1 Enclosed Belted Flushing | 1 Enclosed Flushing |
| Lavatory Location | FWD / AFT | AFT | FWD |
| Galley / Refreshment | Galley | Galley | Optional Refreshment Center |
| Galley Location | FWD | FWD | FWD |
| Crew Rest | Yes | No | No |
| Jump Seat | Yes | No | No |
| Max Cabin Altitude (ft) | - | 5,950 | - |
| SL Cabin Altitude (ft) | 23000 | 26800 | 23500 |
| Cabin Pressure (psi) | 8.8 | 9.7 | 9.3 |
| Other | |||
| APU Manufacturer | - | Honeywell | - |
| APU Model | - | RE100 | - |
| APU TBO (hrs) | - | - | - |
| Warranty | |||
| Airframe (Yrs) | 3 | 3 | 2 |
| Airframe (Hrs) | 1000 | 1000 | - |
| Engine (Yrs) | 2 | 2 | 5 |
| Engine (Hrs) | 1000 | 1000 | 2000 |
| APU (Hrs) | 2000 | 2000 | - |
| Avionics (Yrs) | - | - | 3 |
| Performance | |||
| Max Cruise Speed (Mach) | 0.82 | 0.8 | 0.74 |
| Max Cruise Speed (ktas) | 470 | 458 | 440 |
| Long Range Cruise (Mach) | 0.8 | 0.71 | 0.62 |
| Long Range Cruise (ktas) | 458 | 404 | 358 |
| Vref (kias) | 117 | 115 | 90 |
| Stall Speed - Flaps (kias) | - | - | 82 |
| Max Range (nm) | 4085 | 2731 | 2076 |
| Max Range Crew + 4 (nm) | 4011 | 2700 | 1882 |
| Max Range Crew + 6 (nm) | 4011 | 2583 | 1689 |
| Max Range Crew + 8 (nm) | - | 2451 | 1498 |
| Take-off FL (ft) | 5640 | 3580 | 2930 |
| Take-Off (5000 / ISA + 10) | - | 5070 | 4720 |
| Landing Roll (ft) | 2402 | 2480 | 2375 |
| Max Climb Rate (fpm) | 4345 | 2313 | 4151 |
| Service Ceiling (ft) | 41000 | 45000 | 45000 |