The Dassault Falcon 900 is a large-cabin, long-range business jet that introduced tri-jet architecture to Dassault’s heavy jet segment. Developed from the Falcon 50, the Falcon 900 first flew on September 21, 1984, and entered service in 1986. Production of the original Falcon 900 continued until 1991, after which Dassault introduced successive variants including the 900B, 900EX, and 900LX. The Falcon 900 series remains in production today, with over 500 units delivered worldwide.
Powered by three Honeywell TFE731-5AR-1C turbofan engines, each producing 4,500 lbs of thrust, the Falcon 900 offers a maximum cruise speed of Mach 0.84 (500 knots) and a typical long-range cruise of 456 knots. Its range is approximately 3,970 nautical miles for the baseline model, with later variants extending up to 4,750 nm. The aircraft’s maximum takeoff weight (MTOW) is 45,500 lbs, and it requires about 5,300–5,800 ft of runway for takeoff. Certified to a service ceiling of 51,000 ft, the Falcon 900 combines intercontinental capability with short-field performance, aided by its tri-jet configuration.
The cabin measures 39 ft in length, 7 ft 7 in in width, and 6 ft 2 in in height, providing a volume of roughly 1,270 cu ft. Standard layouts accommodate 12 passengers, with options for up to 14 in executive configurations featuring a forward club section, mid-cabin conference group, and aft divans. The baggage compartment offers 127 cu ft of pressurized storage, accessible during flight. Interior amenities include a full-service galley, enclosed lavatory, and advanced connectivity options in later variants.
For operators, the Falcon 900 delivers a unique blend of range, efficiency, and operational flexibility.
Its tri-jet design enhances safety margins for overwater flights and provides superior climb performance, making it a preferred choice for corporate flight departments and charter operators seeking reliability and comfort in the large-cabin category.
