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Dassault: Falcon 900LX

Program launch date May 2008
Certification date 1H/2010
First delivery date Mid 2010
Number of crew and passengers 2+12/19
Cabin dimensions (LxHxW) 33ft 2inx6ft 2inx7ft 8in / 10.11×1.88×2.34 m
Cabin volume 1,264 cu ft
Engine make/model Honeywell TFE731-60 (3)
Engine thrust rating (sea level,ISA) 5,000 lb
Avionics suite Honeywell EASy
MTOW 48,300 lb
MLW 42,000 lb
ZFW 30,864 lb
BOW 25,080 lb
Usable fuel weight 21,000 lb
Mmo Mach 0.87
Vmo 370 kcas
High-speed cruise Mach 0.84
Long-range cruise Mach 0.75
NBAA IFR range at long-distance cruise 4,800 nm
Certified maximum altitude 51,000 ft
Cabin altitude at maximum altitude 8,000 ft
Balanced field length for takeoff 5,060 ft
Landing distance 2,400 ft
Standard equipped price $39.45 million
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2 Comments to “Dassault: Falcon 900LX”

  1.  teasy the Ants work on December 20th, 2011

    teasy the Ants work…

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