Dassault Falcon 2000

Jet • twin engine • Low Wing • Retractable gear

Range Visualization

Origin: · click map to move · nm at current load

Payload vs. Range

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Default: 190 lbs (FAA standard)

Default: 30 lbs

Passengers
lbs @ lbs / pax
0 lbs
Fuel on board
gal
+ Weight
Range
Available Range / nm
Mission capable — Aircraft can handle the current load with full fuel tanks.
Fuel tradeoff required — You'll need to leave gallons of fuel behind ( gal usable for nm range).
Over max gross weight — Reduce payload by lbs to safely operate this aircraft.

Mission Profile

480
KTAS
Cruise Speed
12
Occupants
4000
nm
Max Range
-
lbs
Wet Payload

Estimated Ownership Costs

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About the Dassault Falcon 2000

The Dassault Falcon 2000 is a highly successful transcontinental, wide-body business jet. As a twin-engine member of the Falcon family, it was derived from the larger Falcon 900 trijet, offering a similarly spacious, stand-up cabin (over 6 ft tall) but with lower operating costs.

Over its production life, it has evolved through several popular variants:

  • Falcon 2000 (Original): Certified in 1994, it established the model’s reputation for comfort and performance.
  • Falcon 2000EX (EASy): A major upgrade in 2003, featuring more powerful Pratt & Whitney PW308C engines for a significant range increase (up to ~3,800 nm) and the advanced EASy (Honeywell Primus Epic) flight deck.
  • Falcon 2000LX / LXS: Introduced blended winglets to the “EX” airframe, boosting range to 4,000 nm. The “LXS” model (introduced in 2014) added high-performance inboard slats, giving it exceptional short-field takeoff and landing capabilities, allowing it to access smaller airports.
  • Falcon 2000S: A shorter-range (3,350 nm) variant introduced in 2011, also equipped with winglets and slats, designed to offer the wide-body cabin experience with best-in-class short-field performance and more accessible operating costs.

Overall, the Falcon 2000 series is prized by operators for its unique combination of a spacious, comfortable cabin, long-range capability, high cruise speeds (Mach 0.80+), and (especially in later models) the ability to use surprisingly short runways.

Technical Specifications

Dimensions

Wingspan
63.4 ft
Length
66.3 ft
Height
23.2 ft

Weights

Max Takeoff Weight
42,400 lbs
Max Landing Weight
39,300 lbs
Fuel Capacity
2500 gal

Performance

Cruise Speed
480 KTAS
Range
4000 NM
Service Ceiling
47,000 ft
Rate of Climb
3730 fpm

Engines

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