Bombardier Challenger 3500 vs Dassault Falcon 2000s vs Gulfstream G280 vs Pilatus Pc 12 Ngx
The Bombardier Challenger 3500, Dassault Falcon 2000S, and Gulfstream G280 are midsize-to-super-midsize business jets aimed at fast, long nonstop trips, while the Pilatus PC-12 NGX is a single‑engine turboprop optimized for flexibility and short or unimproved runways. In category, the Challenger 3500 is a super‑midsize jet with a spacious cabin for its class; the Falcon 2000S is a larger “large‑cabin” twinjet prioritizing comfort and runway performance; the G280 is a super‑midsize jet emphasizing high speed and long legs; the PC‑12 NGX is a utility‑minded turboprop rather than a jet. For range, the G280 is typically the longest‑leg option at roughly 3,600 nm, the Challenger 3500 follows around 3,400 nm, and the Falcon 2000S is generally in the ~3,300 nm class. The PC‑12 NGX is shorter at roughly 1,800–2,000 nm but can access more airports. For passenger capacity, typical configurations are about 8–10 for the Challenger 3500, 8–10 (often up to 12) for the Falcon 2000S, 8–10 for the G280, and about 6–9 for the PC‑12 NGX.
| Spec | Bombardier Challenger 3500 | Dassault Falcon 2000S | Gulfstream G280 | Pilatus PC-12 NGX |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 6.71 | $ 6.63 | $ 6.57 | $ 2.78 |
| Min Crew | 2 | 2 | 2 | 1 |
| Total Seats | 10 | 12 | 10 | 8 |
| Manufacturer | Bombardier | Dassault Falcon | Gulfstream | Pilatus |
| Aircraft Name | Challenger 3500 | 2000S | G280 | PC-12 NGX |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 3400 | 3540 | 3600 | 1803 |
| DOC / nm / Seat | $ 0.84 | $ 0.83 | $ 0.82 | $ 0.46 |
| Max Cabin Seats | 10 | 10 | 10 | 9 |
| OEM Verification | VERIFIED | VERIFIED | Un-Verified | VERIFIED |
| Useful Load (lbs) | 15950 | 18250 | 15550 | — |
| Standard Cabin Seats | 8 | 10 | 8 | 6 |
| Direct Operating Cost | $ 3,152 | $ 3,150 | $ 3,168 | $ 793 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line 21 Advanced | Honeywell Primus EASy II | Gulfstream PlaneView (Pro Line Fusion) | Honeywell Primus Apex |
| Max Cruise Speed (ktas) | 533 | 490 | 481 | 290 |
| Base Aircraft Price (USD) | $26,950,000 | $ 26,000,000 | $24,900,000 | $5,350,000 |
| Flight Rules | — | — | — | IFR |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Lavatory | 1 Enclosed Flushing | 1 Enclosed Flushing | 1 Enclosed Belted Flushing | Optional |
| Min Crew | 2 | 2 | 2 | 1 |
| Crew Rest | No | No | No | — |
| Jump Seat | Yes | No | No | — |
| Total Seats | 10 | 12 | 10 | 8 |
| Galley Location | FWD | FWD | FWD | — |
| Max Cabin Seats | 10 | 10 | 10 | 9 |
| Lavatory Location | AFT | AFT | AFT | FWD |
| Cabin Pressure (psi) | 8.8 | 9.6 | 9.2 | 5.8 |
| Galley / Refreshment | Galley | Galley | Galley | No |
| Standard Cabin Seats | 8 | 10 | 8 | 6 |
| SL Cabin Altitude (ft) | 23338 | 25300 | 25000 | 13100 |
| Max Cabin Altitude (ft) | — | — | 5800 | — |
| Cargo Door | — | — | — | Yes |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | HTF73500 | PW308C | HTF7250G | PT6E-67XP |
| TBO (hrs) | On-Condition | 7000 | On-Condition | 5000 |
| Flat Rating | ISA + 15 | ISA + 15 | ISA + 17 | ISA + 35 |
| Thrust (lbs) | 7323 | 7000 | 7624 | — |
| No. of Engines | 2 | 2 | 2 | 1 |
| Horsepower | — | — | — | 1200 |
| Usable Fuel (gal) | — | — | — | 402 |
| Dimensions | ||||
| Length (ft) | 68.7 | 66.4 | 66.9 | 47.25 |
| Wingspan (ft) | 69 | 70.2 | 63 | 53.33 |
| Aisle Step (ft) | Flat Floor | Flat Floor | 0.3 | — |
| Cabin Width (ft) | 7.2 | 7.7 | 6.9 | 5 |
| Cabin Height (ft) | 6 | 6.2 | 6.3 | 4.9 |
| Cabin Length (ft) | 25.2 | 26.2 | 25.9 | 16.9 |
| Overall Height (ft) | 20 | 23.2 | 21.4 | 14 |
| Cabin Width - Floor (ft) | 5.1 | 6.3 | 5.4 | 4.25 |
| Cabin Length - Seating (ft) | 16.6 | 17.1 | 17.7 | — |
| Baggage Volume Int. (cu. ft) | 106 | 134 | 154 | 40 |
| Cabin Volume (cu. ft) | — | 1024 | — | — |