Dassault Falcon 50

Key Specifications

Overview

The Dassault Falcon 50 is a tri-engine, long-range business jet that represents a significant advancement in executive aviation. First introduced in 1976, it combines the fuselage of the earlier Falcon 20 with three Garrett TFE731 turbofan engines, providing superior performance, reliability, and safety margins. The aircraft can accommodate 4-8 passengers depending on configuration, with a maximum range exceeding 3,600 nautical miles. Known for its exceptional fuel efficiency for a tri-engine jet and excellent high-altitude capability, the Falcon 50 became a popular choice among corporate operators, governments, and charter companies worldwide. The aircraft features a pressurized cabin, advanced avionics suites (depending on vintage), and reliable performance in various weather conditions. Its tri-engine configuration provides redundancy and safety benefits, making it attractive for operations over water and remote regions. The Falcon 50 gained particular favor in the Middle East, Europe, and North America. Production continued through 2000, with an improved variant, the Falcon 50EX, introduced in 1994, featuring more powerful engines and updated systems. Despite competition from newer designs, the Falcon 50 remains a respected aircraft in the pre-owned market, valued for its proven reliability and strong resale value.

Technical Specifications

Maximum Speed: 535 mph (464 knots)
Cruise Speed: 510 mph (443 knots)
Range: 3,650 nautical miles
Service Ceiling: 45,000 feet
Maximum Takeoff Weight: 36,400 lbs
Engines: 3x Garrett TFE731-3-2C turbofan (Falcon 50EX: TFE731-40C)
Engine Thrust: 3,700 lbs total (Falcon 50); 5,100 lbs total (50EX)
Cabin Length: 22.5 feet
Cabin Width: 6.7 feet
Cabin Height: 6.2 feet
Pressurization: 10,000 feet cabin at 41,000 feet altitude