| Summary |
| Cockpit | 2 | 3 |
| DOC / nm | $ 7.16 | $ 7.74 |
| Min Crew | 2 | 2 |
| Total Seats | 11 | 17 |
| Manufacturer | Bombardier | Dassault Falcon |
| Aircraft Name | Challenger 650 | 6X |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 4085 | 5500 |
| DOC / nm / Seat | $ 0.80 | $ 0.64 |
| Max Cabin Seats | 12 | 16 |
| OEM Verification | VERIFIED | Un-Verified |
| Useful Load (lbs) | 21050 | — |
| Standard Cabin Seats | 9 | 14 |
| Direct Operating Cost | $ 3,365 | $ 3,845 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line 21 Advanced | Honeywell Primus EASy III |
| Max Cruise Speed (ktas) | 470 | 516 |
| Base Aircraft Price (USD) | $32,400,000 | $49,500,000 |
| Cabin |
| Cockpit | 2 | 3 |
| Lavatory | 2 Enclosed Flushing | 2 Enclosed Flushing |
| Min Crew | 2 | 2 |
| Crew Rest | Yes | No |
| Jump Seat | Yes | Yes |
| Total Seats | 11 | 17 |
| Galley Location | FWD | FWD |
| Max Cabin Seats | 12 | 16 |
| Lavatory Location | FWD / AFT | FWD / AFT |
| Cabin Pressure (psi) | 8.8 | 10.2 |
| Galley / Refreshment | Galley | Galley |
| Standard Cabin Seats | 9 | 14 |
| SL Cabin Altitude (ft) | 23000 | 29200 |
| Max Cabin Altitude (ft) | — | 3900 |
| Engine |
| FADEC | Yes | Yes |
| Model | CF34-3B MTO | PW812D |
| TBO (hrs) | On-Condition | 5000 |
| Flat Rating | ISA + 15 | ISA + 17 |
| Thrust (lbs) | 9220 | 14000 |
| No. of Engines | 2 | 2 |
| Dimensions |
| Length (ft) | 68.4 | 84.3 |
| Wingspan (ft) | 64.4 | 85.1 |
| Aisle Step (ft) | Flat Floor | — |
| Cabin Width (ft) | 7.9 | 8.5 |
| Cabin Height (ft) | 6 | 6.5 |
| Cabin Length (ft) | 25.6 | 40.4 |
| Overall Height (ft) | 20.7 | 24.5 |
| Cabin Width - Floor (ft) | 6.9 | 6.3 |
| Cabin Length - Seating (ft) | 15.4 | 27.5 |
| Baggage Volume Int. (cu. ft) | 112 | 140 |
| Cabin Volume (cu. ft) | — | 1843 |
