Bombardier Challenger 650 vs Bombardier Global 5500 vs Dassault Falcon 7x vs Dassault Falcon 900lx
In category terms, the Bombardier Challenger 650 is a large-cabin business jet often used for high-comfort regional and transcontinental missions, while the Bombardier Global 5500 steps up into the ultra-long-range class designed for intercontinental flying with a larger, more flexible cabin. The Dassault Falcon 900LX and Falcon 7X are also large-cabin long-range jets, with the 7X positioned as a more modern, longer-range, ultra-long-range-capable option than the 900LX. For range, the Challenger 650 typically covers roughly 4,000 nautical miles, suitable for many North Atlantic or deep U.S. coast-to-coast missions depending on conditions. The Falcon 900LX is generally around the mid‑4,000 nautical mile class, offering solid intercontinental capability. The Falcon 7X commonly reaches around 5,900 nautical miles, enabling more nonstop city pairs. The Global 5500 is usually quoted around 5,900–6,000 nautical miles, competing at the top of this group for nonstop reach. Passenger capacity is broadly similar in typical executive layouts: the Challenger 650 and Falcon 900LX often seat about 8–12, while the Falcon 7X and Global 5500 commonly seat about 10–16, with higher maximums possible in denser configurations.
| Spec | Bombardier Challenger 650 | Bombardier Global 5500 | Dassault Falcon 7X | Dassault Falcon 900LX |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 3 | 2 |
| DOC / nm | $ 7.16 | $ 9.49 | $ 7.75 | $ 7.57 |
| Min Crew | 2 | 2 | 2 | 2 |
| Total Seats | 11 | 14 | 17 | 16 |
| Manufacturer | Bombardier | Bombardier | Dassault Falcon | Dassault Falcon |
| Aircraft Name | Challenger 650 | Global 5500 | 7X | 900LX |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 4085 | 5900 | 5950 | 4750 |
| DOC / nm / Seat | $ 0.80 | $ 0.79 | $ 0.65 | $ 0.63 |
| Max Cabin Seats | 12 | 16 | 16 | 14 |
| OEM Verification | VERIFIED | VERIFIED | VERIFIED | VERIFIED |
| Useful Load (lbs) | 21050 | — | 33600 | 22450 |
| Standard Cabin Seats | 9 | 12 | 14 | 14 |
| Direct Operating Cost | $ 3,365 | $ 4,895 | $ 3,850 | $ 3,588 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line 21 Advanced | Bombardier Vision (Pro Line Fusion) | Honeywell Primus EASy II | Honeywell Primus EASy II |
| Max Cruise Speed (ktas) | 470 | 504 | 516 | 498 |
| Base Aircraft Price (USD) | $32,400,000 | $46,000,000 | $53,800,000 | $44,000,000 |
| Cabin | ||||
| Cockpit | 2 | 2 | 3 | 2 |
| Lavatory | 2 Enclosed Flushing | 2 Enclosed Flushing | 2 Enclosed Flushing | 1 Enclosed Flushing |
| Min Crew | 2 | 2 | 2 | 2 |
| Crew Rest | Yes | No | No | No |
| Jump Seat | Yes | Yes | Yes | No |
| Total Seats | 11 | 14 | 17 | 16 |
| Galley Location | FWD | FWD | FWD | FWD |
| Max Cabin Seats | 12 | 16 | 16 | 14 |
| Lavatory Location | FWD / AFT | FWD / AFT | FWD / AFT | AFT |
| Cabin Pressure (psi) | 8.8 | — | 10.2 | 9.6 |
| Galley / Refreshment | Galley | Galley | Galley | Galley |
| Standard Cabin Seats | 9 | 12 | 14 | 14 |
| SL Cabin Altitude (ft) | 23000 | — | 29200 | 25300 |
| Max Cabin Altitude (ft) | — | — | 3900 | — |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | CF34-3B MTO | Pearl | PW307A | TFE731-60 |
| TBO (hrs) | On-Condition | On-Condition | 7200 | 5000 |
| Flat Rating | ISA + 15 | — | ISA + 17 | ISA + 17 |
| Thrust (lbs) | 9220 | 15125 | 6402 | 5000 |
| No. of Engines | 2 | 2 | 3 | 3 |
| Dimensions | ||||
| Length (ft) | 68.4 | 96 | 76.7 | 66.4 |
| Wingspan (ft) | 64.4 | 94 | 86 | 70.2 |
| Aisle Step (ft) | Flat Floor | — | — | — |
| Cabin Width (ft) | 7.9 | 8 | 7.7 | 7.7 |
| Cabin Height (ft) | 6 | 6.2 | 6.2 | 6.2 |
| Cabin Length (ft) | 25.6 | 40.8 | 39.1 | 33.2 |
| Overall Height (ft) | 20.7 | 25.5 | 25.7 | 24.8 |
| Cabin Width - Floor (ft) | 6.9 | — | 6.3 | 6.3 |
| Cabin Length - Seating (ft) | 15.4 | — | 26.2 | 23.5 |
| Baggage Volume Int. (cu. ft) | 112 | — | 140 | 127 |
| Cabin Volume (cu. ft) | — | — | 1552 | 1264 |