The Dassault Falcon 50EX is an advanced evolution of the original Falcon 50, designed to deliver improved range, fuel efficiency, and avionics while retaining the trijet configuration that made the Falcon 50 a benchmark for intercontinental business travel. Announced in 1995, the Falcon 50EX first flew on April 10, 1996, entered service in 1997, and remained in production until 2008. This variant introduced upgraded Honeywell TFE731-40 engines with FADEC controls, reducing fuel burn and enhancing climb performance compared to the earlier TFE731-3 engines.
The Falcon 50EX is powered by three Honeywell TFE731-40 turbofan engines, each producing 3,704 lbs of thrust. It offers a maximum range of 3,350 nautical miles and a high-speed cruise of 480 knots, with a service ceiling of 49,000 ft. The aircraft’s maximum takeoff weight (MTOW) is 39,700 lbs, an increase over the original Falcon 50. Typical takeoff distance at sea level is approximately 4,935 ft, enabling strong short-field performance for a long-range jet.
The cabin measures 23 ft 5 in in length, 6 ft 1 in in width, and 5 ft 9 in in height, providing a total volume of about 600 cu ft. Standard layouts accommodate 8 to 9 passengers, with configurations featuring a four-seat club section, two facing seats, and a three-seat divan. The baggage compartment offers 115 cu ft of space, fully pressurized and accessible in flight. Interior amenities include fold-out work tables, power outlets, and a galley equipped for hot and cold food preparation, ensuring comfort on extended missions.
For operators, the Falcon 50EX combines intercontinental capability with exceptional runway flexibility and reliability. Its trijet design, advanced avionics suite (Collins Pro Line 4), and proven performance make it a preferred choice for corporate flight departments and charter operators seeking versatility in the super midsize category.
