Dassault Aviation
Falcon 900
The Falcon 900 introduced a larger cabin to Dassault’s trijet range. It combines three rear-mounted engines with a wide fuselage that can support separate passenger areas, addressing owners who wanted more space and long-distance capability than the earlier Falcon 50 could provide.
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Aircraft profile
Development and lineage
- Manufacturer
- Dassault Aviation
- Family
- Falcon 900
- Aircraft category
- Business Jet
- Propulsion
- Jet
Aircraft data
Key specifications
- PAX
- 12
- Crew
- 2
- Range
- 4,080 nm
- Max operating speed
- 370 KIAS
- Max ceiling
- 51,000 ft
- Engines
- 3
- Engine model
- Honeywell TFE731-5AR
- Thrust per engine
- 4,500 lbf
- MTOW
- 45,500 lbs
- Cabin height
- 74 in
- Cabin width
- 91 in
- Cabin length
- 398 in
- Cabin volume
- 1,270 cu ft
- Baggage volume
- 127 cu ft
- Overall length
- 66.3 ft
- Wingspan
- 63.4 ft
Overview
Program history
Dassault developed the 900 in response to demand for greater cabin comfort from its established business-jet customers. The first flight took place in 1984, and digital design methods and composite components played a larger role in the program. Subsequent B, C, EX, DX and LX developments refined propulsion, cockpit systems and range while preserving its basic layout.