Dassault Falcon 2000lxs vs Dassault Falcon 2000s vs Dassault Falcon 900lx vs Gulfstream G650er
The Dassault Falcon 2000S and 2000LXS sit in the large-cabin, twin‑engine category, while the Falcon 900LX is a larger long‑range trijet in the heavy/long‑range class, and the Gulfstream G650ER is an ultra‑long‑range flagship. In range terms, the Falcon 2000S is the shortest-legged of the group at roughly 3,350 nm, the Falcon 2000LXS extends that to about 4,000 nm, and the Falcon 900LX reaches about 4,750 nm. The G650ER is in a different tier, typically quoted around 7,500 nm, enabling true intercontinental city pairs with fewer stops. Passenger capacity follows a similar progression: Falcon 2000S and 2000LXS are commonly configured for about 8–10 passengers (with higher-density layouts possible), the Falcon 900LX typically seats around 12–14 in standard arrangements, and the G650ER commonly carries about 14–16, also configurable higher. Overall, the 2000S/LXS emphasize efficient large-cabin travel, the 900LX adds range and cabin flexibility, and the G650ER maximizes global reach and premium cabin scale.
| Spec | Dassault Falcon 2000LXS | Dassault Falcon 2000S | Dassault Falcon 900LX | Gulfstream G650ER |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 6.38 | $ 6.63 | $ 7.57 | $ 9.39 |
| Min Crew | 2 | 2 | 2 | 4 |
| Total Seats | 12 | 12 | 16 | 14 |
| Manufacturer | Dassault Falcon | Dassault Falcon | Dassault Falcon | Gulfstream |
| Aircraft Name | 2000LXS | 2000S | 900LX | G650ER |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 4155 | 3540 | 4750 | 7500 |
| DOC / nm / Seat | $ 0.80 | $ 0.83 | $ 0.63 | $ 0.78 |
| Max Cabin Seats | 10 | 10 | 14 | 19 |
| OEM Verification | VERIFIED | VERIFIED | VERIFIED | Un-Verified |
| Useful Load (lbs) | 18250 | 18250 | 22450 | 49500 |
| Standard Cabin Seats | 10 | 10 | 14 | 12 |
| Direct Operating Cost | $ 3,073 | $ 3,150 | $ 3,588 | $ 4,844 |
| Flight Deck (Base Spec) | Honeywell Primus EASy II | Honeywell Primus EASy II | Honeywell Primus EASy II | Gulfstream PlaneView II (Primus Epic) |
| Max Cruise Speed (ktas) | 490 | 490 | 498 | 516 |
| Base Aircraft Price (USD) | $35,100,000 | $ 26,000,000 | $44,000,000 | $60,000,000 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Lavatory | 1 Enclosed Flushing | 1 Enclosed Flushing | 1 Enclosed Flushing | 2 Enclosed Flushing |
| Min Crew | 2 | 2 | 2 | 4 |
| Crew Rest | No | No | No | Yes |
| Jump Seat | No | No | No | Yes |
| Total Seats | 12 | 12 | 16 | 14 |
| Galley Location | FWD | FWD | FWD | FWD |
| Max Cabin Seats | 10 | 10 | 14 | 19 |
| Lavatory Location | AFT | AFT | AFT | FWD / AFT |
| Cabin Pressure (psi) | 9.6 | 9.6 | 9.6 | 10.7 |
| Galley / Refreshment | Galley | Galley | Galley | Galley |
| Standard Cabin Seats | 10 | 10 | 14 | 12 |
| SL Cabin Altitude (ft) | 25300 | 25300 | 25300 | 31900 |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | PW308C | PW308C | TFE731-60 | BR725 A1-12 |
| TBO (hrs) | 7000 | 7000 | 5000 | On-Condition |
| Flat Rating | ISA + 15 | ISA + 15 | ISA + 17 | ISA + 15 |
| Thrust (lbs) | 7000 | 7000 | 5000 | 16900 |
| No. of Engines | 2 | 2 | 3 | 2 |
| Dimensions | ||||
| Length (ft) | 66.4 | 66.4 | 66.4 | 99.8 |
| Wingspan (ft) | 70.2 | 70.2 | 70.2 | 99.6 |
| Aisle Step (ft) | Flat Floor | Flat Floor | — | Flat Floor |
| Cabin Width (ft) | 7.7 | 7.7 | 7.7 | 8.2 |
| Cabin Height (ft) | 6.2 | 6.2 | 6.2 | 6.5 |
| Cabin Length (ft) | 26.2 | 26.2 | 33.2 | 46.9 |
| Overall Height (ft) | 23.2 | 23.2 | 24.8 | 25.7 |
| Cabin Volume (cu. ft) | 1024 | 1024 | 1264 | — |
| Cabin Width - Floor (ft) | 6.3 | 6.3 | 6.3 | 6.7 |
| Cabin Length - Seating (ft) | 17.1 | 17.1 | 23.5 | 32.7 |
| Baggage Volume Int. (cu. ft) | 131 | 134 | 127 | 235 |