The Dassault Falcon 50 is a long-range business jet that introduced the trijet configuration to the Falcon family, combining intercontinental capability with exceptional runway performance. Developed as an evolution of the Falcon 20, the Falcon 50 first flew on November 7, 1976, entered service in 1979, and remained in production until 2008, later spawning upgraded variants such as the Falcon 50EX. Its design leveraged Dassault’s military aerodynamics expertise, featuring a supercritical wing for improved efficiency.
Powered by three Honeywell TFE731-3-1C turbofan engines, each producing 3,700 lbs of thrust, the Falcon 50 achieves a maximum range of 3,020 nautical miles and cruises at approximately 470 knots. The aircraft’s maximum takeoff weight is 38,000 lbs, and it requires about 4,700 ft of runway for takeoff. Certified to a service ceiling of 49,000 ft, the Falcon 50 offers robust performance for transcontinental and select transatlantic missions, with the added safety and flexibility of a third engine for extended overwater operations.
The cabin measures 23 ft 2 in in length, 6 ft 1 in in width, and 5 ft 9 in in height, providing a volume of roughly 600 cu ft. Typical layouts accommodate 8 to 10 passengers in executive configurations featuring club seating and conference arrangements. The baggage compartment offers 115 cu ft of space. Interior amenities include a galley, enclosed lavatory, and options for connectivity upgrades in later refurbishments.
For operators, the Falcon 50 delivers a unique combination of range, reliability, and short-field capability. Its trijet design and proven systems make it a favored choice for missions requiring flexibility and safety, particularly for operators flying over remote or oceanic routes.
