Aircraft Details

Manufacturer Dassault Falcon
Aircraft Type 2000LXS
Base Aircraft Price (USD) $ 35,100,000
Direct Operating Cost $ 3,073
DOC / nm $ 6.38
DOC / nm / Seat $ 0.80
Max Cruise Speed (ktas) 482
Max Range (nm) 4155
Useful Load (lbs) 18250
Total Seats 10
Cockpit 2
Standard Cabin Seats 8
Max Cabin Seats 10
Min Crew 2
Flight Deck (Base Spec) Honeywell Primus EASy II
Certification FAA / EASA
OEM Verification VERIFIED
Max Cruise Speed (Mach) 0.862
Max Cruise Speed (ktas) 482
Long Range Cruise (ktas) 441
Vref (kias) 106
Max Range (nm) 4155
Max Range Crew + 4 (nm) 4065
Take-off FL (ft) 5878
Landing Roll (ft) 4675
Max Climb Rate (fpm) 4350
Service Ceiling (ft) 47000
MRAMP (lbs) 43000
MTOW (lbs) 42800
MLW (lbs) 39300
MZFW (lbs) 29700
BOW (lbs) 24750
BEW (lbs) 24550
Useful Load (lbs) 18250
Max Payload (lbs) 4950
Fuel Capacity (lbs) 16660
Payload Max Fuel (lbs) 1590
Max Baggage Weight (lbs) 1600
Wingspan (ft) 70.2
Overall Height (ft) 23.2
Length (ft) 66.4
Cabin Height (ft) 6.2
Cabin Width (ft) 7.7
Cabin Width - Floor (ft) 6.3
Cabin Length (ft) 26.2
Cabin Length - Seating (ft) 17.1
Cabin Volume (cu. ft) 1024
Baggage Volume Int. (cu. ft) 131
No. of Engines 2
Manufacturer Pratt & Whitney
Model PW308C
Thrust (lbs) 7000
Flat Rating ISA + 15
FADEC Yes
TBO (hrs) 7000
Flight Deck Honeywell Primus EASy II
FMS 3
Autopilot 2
PFD 2
MFD 2
GPS 3
AHRS 1
Transponder 2
VHF Com 3
VHF Nav 3
Total Seats 10
Cockpit 2
Standard Cabin Seats 8
Max Cabin Seats 10
Min Crew 2
Lavatory 1 Enclosed Flushing
Lavatory Location AFT
Galley / Refreshment Galley
Galley Location FWD
Crew Rest No
Jump Seat No
SL Cabin Altitude 25300
Cabin Pressure 9.6
APU Manufacturer -
APU Model -
APU TBO (hrs) -
Airframe (Yrs) 3
Airframe (Hrs) 1000
Engine (Yrs) 2
Engine (Hrs) 1000
APU (Hrs) 2000
Standard Features
  • ADS-B Compliant
  • AHRS
  • FANS-1A Compliant
  • Lightning Detection
  • RVSM Compliant
  • TAWS B
  • TCAS II - 7.1

Disclaimer: The aircraft performance data provided has not been verified by air.one and should not be used for flight planning purposes. Click here for a comprehensive explanation of assumptions.

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