Launched at EBACE in May 2008, the 4,750 nm/8,800 km trijet offers 7% additional range over the Falcon 900EX.
Climb performance is also improved by 10%, allowing the airplane to reach FL390 in just 20 minutes.
The 900LX features 35-40% better efficiency than other airplanes in its class.
It can fly from New York to Moscow; Paris to Beijing and Mumbai to London.
EASA and FAA certifications were achieved in July of 2010.
© Dassault Aviation – M. Lystseva
Falcon 900LX
Datasheet
External dimensions
| Height | 24 ft 9 in / 7.55 m |
| Length Overall | 66 ft 4 in / 20.21 m |
| Wing Span | 70 ft 2 in / 21.38 m |
Weights
| Max. Takeoff Weight | 49,000 lb / 22,225 kg |
| Max. Landing Weight | 44,500 lb / 20,185 kg |
| Max. Zero Fuel Weight | 30,864 lb / 14,000 kg |
| Max. Fuel Weight | 20,905 lb / 9,480 kg |
Engines & avionics
| Type | 3 Honeywell TFE731-60 5,000 lb / 22.24 kN (Max Thrust, ISA + 17°C, SL) |
| Cockpit | EASy II Flight Deck (with Honeywell Primus Epic System) |
Cabin dimensions
| Cabin Length (excluding cockpit & baggage) | 33 ft 2 in / 10.11 m |
| Cabin Height | 74 in / 1.88 m |
| Cabin Width | 92 in / 2.34 m |
| Cabin Volume (excluding cockpit & baggage) | 1,264 ft3 / 35.79 m3 |
| Baggage Volume | 127 ft3 / 3.6m3 |
Performances
| Range @ Long Range Cruise (6 pax, 2 crew, NBAA IFR reserves) | 4,750 nm / 8,800 km |
| MMO (Maximum Operating Mach Number) | Mach 0.87 |
| Takeoff Distance (BFL) (S L – ISA, Max Take Off Weight) | 5,360 ft / 1,633 m |
| Landing Distance (Typical) (FAR Part 91, 6 pax, SL, NBAA IFR reserves) | 2,415 ft / 736 m |
| Approach Speed (Typical Landing Weight) | 110 kias / 204 km/h |
| Max. Certified Altitude | 51,000 ft / 15,545 m |