Dassault - Falcon 2000
Description:
Transcontinental range, adequate power, and a comfortable interior makes the Dassault Falcon 2000 a serious contender in its already stacked class. Based on the Dassault Falcon 900 tri-jet, the Falcon 2000 has a rich heritage and a history of reliability. Although smaller than the Falcon 900, the 2000 still boasts of a spacious cabin that can give its competitor in the mid to large size class a run for their money.
Specs:
Passengers: 8-19
Lavatory: Full Enclosed
Maximum Speed: 879 km/h
Maximum Altitude: 47,000 ft.
Range: 3,424nm (default)
Cabin Size: 7’7” (width) x 26’ (length) x 6’2” (height)
Baggage Capacity: 134 cu. ft. (default)
Cabin
The cabin can accommodate up to 19 passengers. The forward part of the passenger cabin is arranged as a four-seat lounge. The rear part of the cabin is set out with a two-seat sofa and four seats. The cabin is 1.88m high, 2.34m wide and the cabin floor has a length of 7.98m. The 3.79m³ pressurized baggage compartment is externally loaded, internally accessible and stows up to 725kg.
Flight deck
The two-man Falcon 2000 flight deck has a Rockwell Collins Pro Line 4 electronic flight and information system with EFI-4000 four-tube display. The instrument panel is also fitted with a three-tube Engine Indicating Electronic Display (EIED) supplied by Thales Avionics. The pilot is equipped with a Flight Dynamics HGS-2850 head-up display.
The communications suite includes a dual communications and navigation system with dual TRD-94D Mode-S transponders, dual RTU-4420 radio tuners and a Rockwell Collins HF-9000 transmit / receive unit. A satellite communications unit can be fitted with the podded antenna installed in the fin tip.
The aircraft's flight management system is the Rockwell Collins FMS-6100 with a Cat II autopilot. The flight systems include Rockwell Collins DME-442 distance measuring equipment, dual automatic direction finder, dual attitude and heading reference system and dual digital air data computers with integrated avionics processors. The aircraft is fitted with Rockwell Collins WXR-840 color weather radar. Optional radar fit is the TWR-850 Doppler weather radar.
Optional systems include a dual Honeywell electronic ground proximity warning system (EGPWS) with wind shear detection, dual Honeywell Laser inertial reference system, a backup flight management system (with a global positioning system), a flight data recorder and a Traffic Alert and Collision System (TCAS).
Engines
The Falcon 2000 has two rear-mounted General Electric / Honeywell CFE738-1-1B turbofan engines, each providing 26.3kN thrust. The engines are fitted with Dee-Howard clamshell-type thrust reversers, which open in upper and lower halves about the engine centerline and are hinged at the nozzle. The fuel tanks have a capacity of 5,513kg.




