Dassault Falcon 2000lxs vs Dassault Falcon 6x vs Dassault Falcon 900lx vs Gulfstream G650er
In category, the Falcon 2000LXS is a super‑midsize business jet, the Falcon 900LX and Falcon 6X sit in the large‑cabin class (with the 6X being Dassault’s newer ultra‑widebody large‑cabin design), and the Gulfstream G650ER is an ultra‑long‑range, large‑cabin flagship. On range, the Falcon 2000LXS is the shortest‑leg option at roughly 4,000 nautical miles class. The Falcon 900LX steps up to about 4,750 nautical miles. The Falcon 6X extends further into long‑range territory at around 5,500 nautical miles, while the G650ER leads this group with approximately 7,500 nautical miles, enabling the longest nonstop city pairs. For passenger capacity, all are typically configured for about 8–14 passengers depending on cabin layout. The Falcon 2000LXS generally seats fewer in comfort-focused layouts, the 900LX and 6X commonly accommodate mid‑teens in higher-density configurations, and the G650ER similarly supports mid‑teens but with the most space for long-haul comfort.
| Spec | Dassault Falcon 2000LXS | Dassault Falcon 6X | Dassault Falcon 900LX | Gulfstream G650ER |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 3 | 2 | 2 |
| DOC / nm | $ 6.38 | $ 7.74 | $ 7.57 | $ 9.39 |
| Min Crew | 2 | 2 | 2 | 4 |
| Total Seats | 12 | 17 | 16 | 14 |
| Manufacturer | Dassault Falcon | Dassault Falcon | Dassault Falcon | Gulfstream |
| Aircraft Name | 2000LXS | 6X | 900LX | G650ER |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 4155 | 5500 | 4750 | 7500 |
| DOC / nm / Seat | $ 0.80 | $ 0.64 | $ 0.63 | $ 0.78 |
| Max Cabin Seats | 10 | 16 | 14 | 19 |
| OEM Verification | VERIFIED | Un-Verified | VERIFIED | Un-Verified |
| Useful Load (lbs) | 18250 | — | 22450 | 49500 |
| Standard Cabin Seats | 10 | 14 | 14 | 12 |
| Direct Operating Cost | $ 3,073 | $ 3,845 | $ 3,588 | $ 4,844 |
| Flight Deck (Base Spec) | Honeywell Primus EASy II | Honeywell Primus EASy III | Honeywell Primus EASy II | Gulfstream PlaneView II (Primus Epic) |
| Max Cruise Speed (ktas) | 490 | 516 | 498 | 516 |
| Base Aircraft Price (USD) | $35,100,000 | $49,500,000 | $44,000,000 | $60,000,000 |
| Cabin | ||||
| Cockpit | 2 | 3 | 2 | 2 |
| Lavatory | 1 Enclosed Flushing | 2 Enclosed Flushing | 1 Enclosed Flushing | 2 Enclosed Flushing |
| Min Crew | 2 | 2 | 2 | 4 |
| Crew Rest | No | No | No | Yes |
| Jump Seat | No | Yes | No | Yes |
| Total Seats | 12 | 17 | 16 | 14 |
| Galley Location | FWD | FWD | FWD | FWD |
| Max Cabin Seats | 10 | 16 | 14 | 19 |
| Lavatory Location | AFT | FWD / AFT | AFT | FWD / AFT |
| Cabin Pressure (psi) | 9.6 | 10.2 | 9.6 | 10.7 |
| Galley / Refreshment | Galley | Galley | Galley | Galley |
| Standard Cabin Seats | 10 | 14 | 14 | 12 |
| SL Cabin Altitude (ft) | 25300 | 29200 | 25300 | 31900 |
| Max Cabin Altitude (ft) | — | 3900 | — | — |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | PW308C | PW812D | TFE731-60 | BR725 A1-12 |
| TBO (hrs) | 7000 | 5000 | 5000 | On-Condition |
| Flat Rating | ISA + 15 | ISA + 17 | ISA + 17 | ISA + 15 |
| Thrust (lbs) | 7000 | 14000 | 5000 | 16900 |
| No. of Engines | 2 | 2 | 3 | 2 |
| Dimensions | ||||
| Length (ft) | 66.4 | 84.3 | 66.4 | 99.8 |
| Wingspan (ft) | 70.2 | 85.1 | 70.2 | 99.6 |
| Aisle Step (ft) | Flat Floor | — | — | Flat Floor |
| Cabin Width (ft) | 7.7 | 8.5 | 7.7 | 8.2 |
| Cabin Height (ft) | 6.2 | 6.5 | 6.2 | 6.5 |
| Cabin Length (ft) | 26.2 | 40.4 | 33.2 | 46.9 |
| Overall Height (ft) | 23.2 | 24.5 | 24.8 | 25.7 |
| Cabin Volume (cu. ft) | 1024 | 1843 | 1264 | — |
| Cabin Width - Floor (ft) | 6.3 | 6.3 | 6.3 | 6.7 |
| Cabin Length - Seating (ft) | 17.1 | 27.5 | 23.5 | 32.7 |
| Baggage Volume Int. (cu. ft) | 131 | 140 | 127 | 235 |