Compare Bombardier Challenger 650 vs Bombardier Global 6500 vs Gulfstream G400 vs Pilatus PC-12 NGX vs Pilatus PC-24
 |  |  |  |  | |
| Manufacturer | Bombardier | Bombardier | Gulfstream | Pilatus | Pilatus |
| Aircraft Type | Challenger 650 | Global 6500 | G400 | PC-12 NGX | PC-24 |
| Base Aircraft Price (USD) | $32,400,000 | $56,000,000 | 34500000 | $5,350,000 | $11,800,000 |
| Direct Operating Cost | $ 3,365 | $ 4,895 | - | $ 793 | $ 1,619 |
| DOC / nm | $ 7.16 | $ 9.49 | - | $ 2.78 | $ 3.71 |
| DOC / nm / Seat | $ 0.80 | $ 0.68 | - | $ 0.46 | $ 0.62 |
| Max Cruise Speed (ktas) | 470 | 504 | 539 | 290 | 440 |
| Max Range (nm) | 4085 | 6600 | 4200 | 1866 | 2076 |
| Useful Load (lbs) | 21050 | - | 30650 | 3692 | 6680 |
| Total Seats | 11 | 14 | 12 | 8 | 6 |
| Cockpit | 2 | 2 | - | 2 | 2 |
| Standard Cabin Seats | 9 | 12 | - | 6 | 6 |
| Max Cabin Seats | 12 | 17 | 19 | 9 | 10 |
| Min Crew | 2 | 2 | 4 | 1 | 1 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line 21 Advanced | Bombardier Vision (Pro Line Fusion) | Gulfstream Symmetry Flight Deck | Honeywell Primus Apex | Pilatus ACE (Primus Apex) |
| Flight Rules | - | - | - | IFR | - |
| Certification | FAA / EASA | FAA / EASA | - | FAA / EASA | FAA / EASA |
| OEM Verification | VERIFIED | VERIFIED | - | VERIFIED | VERIFIED |
| Weights | |||||
| MRAMP (lbs) | 48300 | 99750 | - | 10495 | 18400 |
| MTOW (lbs) | 48200 | 99500 | - | 10450 | 18300 |
| MLW (lbs) | 38000 | 78600 | - | 9921 | 16900 |
| MZFW (lbs) | 32000 | 58000 | - | 9039 | 14220 |
| BOW (lbs) | 27250 | 52230 | - | 6803 | 11620 |
| BEW (lbs) | 27150 | - | - | 6758 | 11520 |
| Useful Load (lbs) | 21050 | - | 30650 | 3692 | 6680 |
| Max Payload (lbs) | 3750 | - | - | 2235 | 2500 |
| Fuel Capacity (lbs) | 19852 | 45050 | - | 2704 | 5964 |
| Useful Load Max Fuel (lbs) | - | 5770 | - | - | - |
| Payload Max Fuel (lbs) | 1198 | - | - | 988 | 715 |
| Max Baggage Weight (lbs) | 900 | - | - | - | 1000 |
| Dimensions | |||||
| Wingspan (ft) | 64.4 | 94 | - | 53.33 | 55.8 |
| Overall Height (ft) | 20.7 | 25.5 | - | 14 | 17.4 |
| Length (ft) | 68.4 | 99.5 | - | 47.25 | 52.2 |
| Cabin Height (ft) | 6 | 6.2 | - | 4.9 | 5.1 |
| Aisle Step (ft) | Flat Floor | - | - | - | Flat Floor |
| Cabin Width (ft) | 7.9 | 8 | - | 5 | 5.6 |
| Cabin Width - Floor (ft) | 6.9 | - | - | 4.25 | 3.8 |
| Cabin Length (ft) | 25.6 | 43.3 | - | 16.9 | 23 |
| Cabin Length - Seating (ft) | 15.4 | - | - | - | 17 |
| Baggage Volume Int. (cu. ft) | 112 | - | - | 40 | 90 |
| Engine | |||||
| No. of Engines | 2 | 2 | - | 1 | 2 |
| Manufacturer | Bombardier | Bombardier | Gulfstream | Pilatus | Pilatus |
| Model | CF34-3B MTO | Pearl | - | PT6E-67XP | FJ44-4A-QPM |
| Horsepower | - | - | - | 1200 | - |
| Thrust (lbs) | 9220 | 15125 | - | - | 3435 |
| Flat Rating | ISA + 15 | - | - | ISA + 35 | ISA + 23 |
| FADEC | Yes | Yes | - | Yes | Yes |
| TBO (hrs) | On-Condition | On-Condition | - | 5000 | 5000 |
| Usable Fuel (gal) | - | - | - | 402 | - |
| Avionics | |||||
| Flight Deck | Rockwell Collins Pro Line 21 Advanced | Bombardier Vision (Pro Line Fusion) | - | Honeywell Primus Apex | Pilatus ACE (Primus Apex) |
| Flight Rules | - | - | - | IFR | - |
| FMS | 2 | 1 | - | 1 | 1 |
| Autopilot | 1 | 1 | - | 1 | 1 |
| PFD | 2 | 2 | - | 2 | 2 |
| MFD | 2 | 2 | - | 1 | 1 |
| GPS | 2 | 2 | - | 1 | 1 |
| AHRS | 2 | 2 | - | 1 | 1 |
| ADC | 2 | 2 | - | - | - |
| Transponder | 2 | 2 | - | 1 | 1 |
| VHF Com | 2 | 2 | - | 2 | 1 |
| VHF NAV | 2 | 2 | - | 2 | 1 |
| Cabin | |||||
| Total Seats | 11 | 14 | 12 | 8 | 6 |
| Cockpit | 2 | 2 | - | 2 | 2 |
| Standard Cabin Seats | 9 | 12 | - | 6 | 6 |
| Max Cabin Seats | 12 | 17 | 19 | 9 | 10 |
| Min Crew | 2 | 2 | 4 | 1 | 1 |
| Cargo Door | - | - | - | Yes | Yes |
| Lavatory | 2 Enclosed Flushing | 2 Enclosed Flushing | - | Optional | 1 Enclosed Flushing |
| Lavatory Location | FWD / AFT | FWD / AFT | - | FWD | FWD |
| Galley / Refreshment | Galley | Galley | - | No | Optional Refreshment Center |
| Galley Location | FWD | FWD | - | - | FWD |
| Crew Rest | Yes | Yes | - | - | No |
| Jump Seat | Yes | Yes | - | - | No |
| SL Cabin Altitude (ft) | 23000 | - | - | 13100 | 23500 |
| Cabin Pressure (psi) | 8.8 | - | - | 5.8 | 9.3 |
| Other | |||||
| Prop Manufacturer | - | - | - | Hartzell | - |
| Prop Description | - | - | - | 5-Blade Comp | - |
| APU Manufacturer | - | - | - | - | - |
| APU Model | - | - | - | - | - |
| APU TBO (hrs) | - | - | - | - | - |
| Gear Type | - | - | - | Retractable | - |
| 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 | 0.88 | - | - | 0.74 |
| Max Cruise Speed (ktas) | 470 | 504 | 539 | 290 | 440 |
| Long Range Cruise (Mach) | 0.8 | 0.85 | - | - | 0.62 |
| Long Range Cruise (ktas) | 458 | 487 | - | 225 | 358 |
| Vref (kias) | 117 | - | - | - | 90 |
| Stall Speed - Flaps (kias) | - | - | - | 67 | 82 |
| Max Range (nm) | 4085 | 6600 | 4200 | 1866 | 2076 |
| Max Range Crew + 4 (nm) | 4011 | 6600 | - | 1803 | 1882 |
| Max Range Crew + 6 (nm) | 4011 | 6600 | - | 1568 | 1689 |
| Max Range Crew + 8 (nm) | - | 6600 | - | 1057 | 1498 |
| Take-off FL (ft) | 5640 | 6370 | - | - | 2930 |
| Take-Off >50ft Obst. (ft) | - | - | - | 2602 | - |
| Take-Off (5000 / ISA + 10) | - | - | - | 4270 | 4720 |
| Landing Roll (ft) | 2402 | 2236 | - | - | 2375 |
| Landing >50ft Obst. (ft) | - | - | - | 2170 | - |
| Max Climb Rate (fpm) | 4345 | - | - | 1920 | 4151 |
| Service Ceiling (ft) | 41000 | 51000 | - | 30000 | 45000 |