2000 Dassault Falcon 2000

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The Dassault Falcon 2000 is a twin-engine business jet aircraft developed by Dassault Aviation in the late 1980s and early 1990s. It is part of the Falcon family of business jets and is derived from the Falcon 900. The Falcon 2000 was the first aircraft in the series to be designed with a supercritical wing and it has a range of up to 5,360km and can carry up to 10 passengers. It is powered by two Pratt & Whitney PW308C turbofan engines, each rated at 6,400lb of thrust. The aircraft has a maximum cruise speed of Mach 0.80 and can climb to a maximum altitude of 45,000 feet. It is equipped with a Honeywell Primus Epic avionics suite and is certified for single-pilot operations.


  • Airframe
  • Total Time: 8,829.3
  • Landings: 4,430
  • Engine(s)
  • Hours: (L) 8,183.7 / (R) 8,044.8
  • Cycles: (L) 4,105 / (R) 4,022
  • Avionics
  • Collins 4-Tube EFIS 4000
  • Collins APS-4000 Autopilot
  • Dual Collins VHF 422C Comms
  • Dual Collins TDR-94 Mode S Transponders
  • Dual Collins ADF-462
  • Dual Collins DME-422 w/8.33 Spacing
  • Collins ALT 55-B Radar Altimeter
  • Dual Collins FMS-6100 w/Dual Collins 4000 GPS
  • Dual Honeywell Laseref IV
  • Collins TTR-920 TCAS 7.1
  • Collins AHC-85 AHRS
  • Allied Signal Mark V Enhanced GPWS
  • Dual Allied Signal KTR-953 HF's w/SELCAL
  • Collins RTA-858 Weather Radar
  • ADS-B
  • Dual Collins ADC-850 Air Data Computers
  • Collins PCD-3000 Data Loader
  • Collins DAU 4000 Data Acquisition Unit
  • Sunstrand CVR & FDR
  • Socata ELT 97

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