Dassault Aviation
Falcon 2000
The Falcon 2000 combines a wide passenger cabin with a two-engine layout. It brought the interior scale of Dassault’s larger business jets to a transcontinental twinjet, offering operators a different balance of cabin space, range and complexity from the company’s trijet aircraft.
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Aircraft profile
Development and lineage
- Manufacturer
- Dassault Aviation
- Family
- Falcon 2000
- Aircraft category
- Business Jet
- Propulsion
- Jet
Aircraft data
Key specifications
- PAX
- 10
- Crew
- 2
- Range
- 3,130 nm
- Max operating speed
- 382 KIAS
- Max ceiling
- 47,000 ft
- Engines
- 2
- Engine model
- CFE Company CFE738-1-1B
- Thrust per engine
- 5,918 lbf
- MTOW
- 35,800 lbs
- Cabin height
- 74 in
- Cabin width
- 91 in
- Cabin length
- 374 in
- Cabin volume
- 1,028 cu ft
- Baggage volume
- 134 cu ft
- Overall length
- 66.3 ft
- Wingspan
- 63.4 ft
- First flight
- 4 March 1993
Overview
Program history
Dassault developed the 2000 using experience from the Falcon 900, including its cabin cross-section and other established design elements. The prototype first flew in 1993. The program addressed customers who wanted a spacious cabin without the longest-range mission requirement, creating the foundation for later EX, DX, LX, S and LXS developments.