Bombardier Challenger 650 vs Bombardier Global 5500 vs Bombardier Global 6500 vs Gulfstream G650er
The Bombardier Challenger 650 is typically categorized as a large-cabin business jet (often considered “super-midsize/large-cabin” in practice) aimed at shorter intercity missions, with an approximate range around 4,000 nautical miles and a typical passenger load of about 8–12 (with maximum seating usually in the mid-to-high teens depending on layout). The Bombardier Global 5500 and Global 6500 move into the ultra-long-range, large-cabin category, offering substantially more range and space; the Global 5500 is roughly in the 5,900–6,000 nautical mile class, while the Global 6500 is about 6,600 nautical miles, with typical comfortable occupancy around 10–14 passengers (and higher maximums by configuration). The Gulfstream G650ER sits at the very top of the ultra-long-range segment, designed for premier long-haul capability at roughly 7,500 nautical miles, also typically carrying about 10–14 passengers in most executive layouts, with maximum seating varying by interior. Overall, the Challenger 650 prioritizes value and cabin comfort on transcontinental-style trips, while the Global 5500/6500 and G650ER are optimized for true long-range, long-duration missions with larger cabins.
| Spec | Bombardier Challenger 650 | Bombardier Global 5500 | Bombardier Global 6500 | Gulfstream G650ER |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 7.16 | $ 9.49 | $ 9.49 | $ 9.39 |
| Min Crew | 2 | 2 | 2 | 4 |
| Total Seats | 11 | 14 | 14 | 14 |
| Manufacturer | Bombardier | Bombardier | Bombardier | Gulfstream |
| Aircraft Name | Challenger 650 | Global 5500 | Global 6500 | G650ER |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 4085 | 5900 | 6600 | 7500 |
| DOC / nm / Seat | $ 0.80 | $ 0.79 | $ 0.68 | $ 0.78 |
| Max Cabin Seats | 12 | 16 | 17 | 19 |
| OEM Verification | VERIFIED | VERIFIED | VERIFIED | Un-Verified |
| Useful Load (lbs) | 21050 | — | — | 49500 |
| Standard Cabin Seats | 9 | 12 | 12 | 12 |
| Direct Operating Cost | $ 3,365 | $ 4,895 | $ 4,895 | $ 4,844 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line 21 Advanced | Bombardier Vision (Pro Line Fusion) | Bombardier Vision (Pro Line Fusion) | Gulfstream PlaneView II (Primus Epic) |
| Max Cruise Speed (ktas) | 470 | 504 | 504 | 516 |
| Base Aircraft Price (USD) | $32,400,000 | $46,000,000 | $56,000,000 | $60,000,000 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Lavatory | 2 Enclosed Flushing | 2 Enclosed Flushing | 2 Enclosed Flushing | 2 Enclosed Flushing |
| Min Crew | 2 | 2 | 2 | 4 |
| Crew Rest | Yes | No | Yes | Yes |
| Jump Seat | Yes | Yes | Yes | Yes |
| Total Seats | 11 | 14 | 14 | 14 |
| Galley Location | FWD | FWD | FWD | FWD |
| Max Cabin Seats | 12 | 16 | 17 | 19 |
| Lavatory Location | FWD / AFT | FWD / AFT | FWD / AFT | FWD / AFT |
| Cabin Pressure (psi) | 8.8 | — | — | 10.7 |
| Galley / Refreshment | Galley | Galley | Galley | Galley |
| Standard Cabin Seats | 9 | 12 | 12 | 12 |
| SL Cabin Altitude (ft) | 23000 | — | — | 31900 |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | CF34-3B MTO | Pearl | Pearl | BR725 A1-12 |
| TBO (hrs) | On-Condition | On-Condition | On-Condition | On-Condition |
| Flat Rating | ISA + 15 | — | — | ISA + 15 |
| Thrust (lbs) | 9220 | 15125 | 15125 | 16900 |
| No. of Engines | 2 | 2 | 2 | 2 |
| Dimensions | ||||
| Length (ft) | 68.4 | 96 | 99.5 | 99.8 |
| Wingspan (ft) | 64.4 | 94 | 94 | 99.6 |
| Aisle Step (ft) | Flat Floor | — | — | Flat Floor |
| Cabin Width (ft) | 7.9 | 8 | 8 | 8.2 |
| Cabin Height (ft) | 6 | 6.2 | 6.2 | 6.5 |
| Cabin Length (ft) | 25.6 | 40.8 | 43.3 | 46.9 |
| Overall Height (ft) | 20.7 | 25.5 | 25.5 | 25.7 |
| Cabin Width - Floor (ft) | 6.9 | — | — | 6.7 |
| Cabin Length - Seating (ft) | 15.4 | — | — | 32.7 |
| Baggage Volume Int. (cu. ft) | 112 | — | — | 235 |