Specifications

Description

Capabilities of the Falcon 2000 The Falcon 2000 comes equipped with two CFE738-1-1B axial centrifugal flow turbofan engines. Each engine is rated at 5,918 pounds of thrust with an inspection interval of 6,000 hours. These engines are controlled by dual FADECs with engine parameter displayed on three LCD EIECs. Even with these advanced engines, the fuel consumption rate of the Falcon 2000 is only 283 gallons per hour, making this private business jet an economical choice. For a flight to a further destination, this private business jet is capable of maintaining 417 knots at an altitude of 43,000 feet. In a high-speed cruise configuration, the Falcon 2000 is capable of maintaining 479 knots at an altitude of 39,000 feet, still well above most aviation traffic. The Dassault Falcon 2000 is capable of getting you to even far-reaching destinations, with an impressive transcontinental range of 3,450 nautical miles. The Dassault Aviation Corporation selected the Collins Pro Line 4 avionics suite for the Falcon 2000. This avionics suite utilizes four 7.25 by 7.25 inch liquid crystal display screens. Designed to be as functional as possible, systems are grouped by function with the display screens close to the functions they control. Some of the avionics systems incorporated into this suite include a Collins TWR-850 Doppler weather radar, an Allied Signal GNS-XES Flight Management System (FMS), and a dual channel Integrated Avionics Processor System (IAPS).