Dassault Falcon 2000S

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

Endorsements & ratings:
  • High-Altitude
  • Pressurization
  • Multi-Engine
  • Instrument
482
KTAS
Cruise Speed
10
Occupants
3350
nm
Max Range
1644
lbs
Wet Payload

Estimated Ownership Costs

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About the Dassault Falcon 2000S

Overview

The Dassault Falcon 2000S is the short-field member of the Falcon 2000 family, certified in 2013. It is the wide-body Falcon 2000 airframe with Pratt & Whitney Canada PW308C engines and the Honeywell Primus Epic EASy II flight deck, fitted with inboard wing slats and blended winglets for the best runway performance in the super-midsize class. The S trades the long-range LXS’s fuselage fuel tank for short-field access: a landing distance near 2,315 ft and roughly 3,350 nm of range. It shares the PW308C generation lineage with the 2000EX (2003), 2000EX EASy, 2000DX, and 2000LX that preceded it.

Key Features for GA Buyers

  • Class-leading short field. Inboard slats give the 2000S a landing distance near 2,315 ft and a takeoff field length around 4,325 ft, letting it work runways most super-mids cannot.
  • Wide-body cabin. The S keeps the full Falcon 2000 stand-up, flat-floor cabin, the same cross-section as the larger Falcon 900.
  • EASy II flight deck. The Honeywell Primus Epic EASy II deck is the modern Falcon cockpit, a generational step over the original 2000’s Pro Line 4.
  • Transcontinental range. At roughly 3,350 nm the S covers coast-to-coast US legs with reserves while keeping its short-field edge.

Trade-offs

  • Shorter range than the LXS. The removed fuselage tank that buys the short-field performance also caps range below the 4,000 nm LXS; buyers choosing the S are prioritising runway access over ultimate range.
  • Two-crew, program-maintained. Like every jet in the class it is a two-pilot airplane on an enrolled engine program; budget for crew and the PW308C program rate.
  • Avionics depth. The EASy II deck rewards thorough training, a consideration for crews moving from a conventional panel.

See Also

Technical Specifications

Dimensions & Weights

Wingspan 70.17 ft Height 23.33 ft
Length
66.33 ft
Parking area (ft2)
5718.53 ft2
Max Takeoff Weight
41,000 lbs
Max Landing Weight
39,300 lbs
Useful Load
16,250 lbs
Fuel Capacity
2180 gal

Performance

Cruise Speed
482 KTAS
Never-Exceed (Vne)
370 KIAS
Max Structural Cruise (Vno)
370 KIAS
Approach Speed
105 KIAS
Stall, Clean (Vs1)
98 KIAS
Range
3350 NM
Service Ceiling
47,000 ft
Rate of Climb
4350 fpm
Takeoff over 50 ft obstacle
4,325 ft
Landing ground roll
2,315 ft

Engines

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